ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 14248.1882 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 71.9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2.118 ET - UTC (sec) : 68.18 UT1 - UTC (sec) : 0.00 Maneuvers contained within the current ephemeris are as follows: IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP ------------------------------------------------------------------------ 265/17:52:27.000 0.0 0.0 0.0 N/A 0.0 0.0 221.7 000/00:00:00.000 0.0 0.0 215.4 267/01:30:00.000 0.0 0.0 0.0 N/A 0.0 0.0 221.7 000/00:00:00.000 0.0 0.0 215.7 270/11:54:38.000 0.0 0.0 0.0 N/A 0.0 0.0 221.3 000/00:00:00.000 0.0 0.0 216.0 271/01:02:30.000 0.0 0.0 0.0 N/A 0.0 0.0 221.3 000/00:00:00.000 0.0 0.0 216.1 274/09:07:30.000 0.0 0.0 0.0 N/A 0.0 0.0 220.8 000/00:00:00.000 0.0 0.0 216.3 277/07:57:30.000 0.0 0.0 0.0 N/A 0.0 0.0 220.6 000/00:00:00.000 0.0 0.0 216.4 Coasting Arc #1 (Orbit 1348) --------------------------------------- Vector Time (GMT): 2018/264/12:03:24.619 Vector Time (MET): N/A Weight (LBS) : 909660.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2611787.56 A = 6789418.99 meter Y = 6053002.01 meter E = .0015531 Z = 1585388.86 I = 51.27943 XDOT = -3985.690604 Wp = 131.38446 YDOT = 3222.079650 meter/sec RA = 257.77713 deg ZDOT = -5709.455164 TA = 31.17658 MA = 31.08453 Ha = 221.866 n.mi Hp = 215.426 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 8568856.82 X = 2536206.15 Y = 19858930.48 feet Y = 6081786.37 meter Z = 5201407.01 Z = 1597891.86 XDOT = -13076.412742 XDOT = -3993.691162 YDOT = 10571.127462 feet/sec YDOT = 3177.463659 meter/sec ZDOT = -18731.808280 ZDOT = -5728.835897 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8635066.37 X = -2631968.23 Y = -19815612.68 feet Y = -6039798.75 meter Z = 5256822.70 Z = 1602279.56 XDOT = 11452.645850 XDOT = 3490.766455 YDOT = -10005.877893 feet/sec YDOT = -3049.791582 meter/sec ZDOT = -18819.091228 ZDOT = -5736.059006 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18264.53769407 .00016717 00000-0 10270-3 0 9009 2 25544 51.6363 258.5570 0004017 190.7069 169.3998 15.53724827 13498 Satellite: ISS Catalog Number: 25544 Epoch time: 18264.53769407 = yrday.fracday Element set: 900 Inclination: 51.6363 deg RA of node: 258.5570 deg Eccentricity: .0004017 Arg of perigee: 190.7069 deg Mean anomaly: 169.3998 deg Mean motion: 15.53724827 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1349 Checksum: 341 Coasting Arc #2 (Orbit 1363) --------------------------------------- Vector Time (GMT): 2018/265/12:03:24.619 Vector Time (MET): N/A Weight (LBS) : 909660.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2043523.60 A = 6790383.79 meter Y = -6472449.76 meter E = .0008689 Z = -45284.96 I = 51.29136 XDOT = 4560.729810 Wp = 60.69593 YDOT = -1475.672249 meter/sec RA = 252.78407 deg ZDOT = 5980.981892 TA = 298.81420 MA = 298.90141 Ha = 221.871 n.mi Hp = 215.422 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6704473.77 X = -1970775.02 Y = -21235071.40 feet Y = -6494895.10 meter Z = -148572.69 Z = -55034.28 XDOT = 14963.024310 XDOT = 4547.839854 YDOT = -4841.444386 feet/sec YDOT = -1424.742452 meter/sec ZDOT = 19622.644004 ZDOT = 6003.105112 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 7175015.08 X = 2186944.60 Y = 21080387.65 feet Y = 6425302.16 meter Z = -191610.75 Z = -58402.96 XDOT = -13183.460285 XDOT = -4018.318695 YDOT = 4646.228827 feet/sec YDOT = 1416.170547 meter/sec ZDOT = 19722.036314 ZDOT = 6011.276669 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18265.50248361 .00016717 00000-0 10270-3 0 9019 2 25544 51.6365 253.7509 0004301 192.3770 167.7277 15.53763701 13645 Satellite: ISS Catalog Number: 25544 Epoch time: 18265.50248361 = yrday.fracday Element set: 901 Inclination: 51.6365 deg RA of node: 253.7509 deg Eccentricity: .0004301 Arg of perigee: 192.3770 deg Mean anomaly: 167.7277 deg Mean motion: 15.53763701 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1364 Checksum: 308 Coasting Arc #3 (Orbit 1367) --------------------------------------- Vector Time (GMT): 2018/265/17:52:27.000 Vector Time (MET): N/A Weight (LBS) : 909660.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4241523.68 A = 6778654.20 meter Y = 627631.02 meter E = .0014322 Z = -5262428.74 I = 51.25795 XDOT = -1909.028233 Wp = 110.90184 YDOT = -7386.971378 meter/sec RA = 251.56571 deg ZDOT = 654.091967 TA = 165.40609 MA = 165.36470 Ha = 221.722 n.mi Hp = 215.449 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -13915760.11 X = -4222664.74 Y = 2059156.87 feet Y = 580304.23 meter Z = -17265186.17 Z = -5282986.80 XDOT = -6263.215988 XDOT = -1829.460411 YDOT = -24235.470401 feet/sec YDOT = -7407.874494 meter/sec ZDOT = 2145.971019 ZDOT = 645.012649 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -1762658.05 X = -537258.17 Y = -13841477.85 feet Y = -4218882.45 meter Z = -17357467.76 Z = -5290556.17 XDOT = 23354.535348 XDOT = 7118.462374 YDOT = -5629.717593 feet/sec YDOT = -1715.937922 meter/sec ZDOT = 2106.030997 ZDOT = 641.918248 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18265.75976082 .00016717 00000-0 10270-3 0 9025 2 25544 51.6403 252.4695 0003990 197.6950 162.4064 15.53730364 13680 Satellite: ISS Catalog Number: 25544 Epoch time: 18265.75976082 = yrday.fracday Element set: 902 Inclination: 51.6403 deg RA of node: 252.4695 deg Eccentricity: .0003990 Arg of perigee: 197.6950 deg Mean anomaly: 162.4064 deg Mean motion: 15.53730364 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1368 Checksum: 329 Coasting Arc #4 (Orbit 1383) --------------------------------------- Vector Time (GMT): 2018/266/17:52:27.000 Vector Time (MET): N/A Weight (LBS) : 909660.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4641142.07 A = 6780281.76 meter Y = 921211.45 meter E = .0004350 Z = 4852455.04 I = 51.27492 XDOT = 1053.885512 Wp = 91.37056 YDOT = 7216.533103 meter/sec RA = 246.54604 deg ZDOT = -2376.261908 TA = 22.03536 MA = 22.01666 Ha = 221.406 n.mi Hp = 215.701 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 15226844.08 X = 4606925.22 Y = 3022347.28 feet Y = 972921.19 meter Z = 15920128.09 Z = 4874916.89 XDOT = 3457.629632 XDOT = 984.652539 YDOT = 23676.289709 feet/sec YDOT = 7227.930989 meter/sec ZDOT = -7796.134868 ZDOT = -2371.311526 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -3086362.40 X = -940723.26 Y = 15107960.45 feet Y = 4604906.35 meter Z = 16020790.87 Z = 4883137.06 XDOT = -22588.432095 XDOT = -6884.954103 YDOT = 3635.943690 feet/sec YDOT = 1108.235637 meter/sec ZDOT = -7774.677938 ZDOT = -2369.721836 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18266.78886499 .00016717 00000-0 10270-3 0 9032 2 25544 51.6400 247.3426 0003904 202.7723 157.3257 15.53758719 13842 Satellite: ISS Catalog Number: 25544 Epoch time: 18266.78886499 = yrday.fracday Element set: 903 Inclination: 51.6400 deg RA of node: 247.3426 deg Eccentricity: .0003904 Arg of perigee: 202.7723 deg Mean anomaly: 157.3257 deg Mean motion: 15.53758719 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1384 Checksum: 338 Coasting Arc #5 (Orbit 1388) --------------------------------------- Vector Time (GMT): 2018/267/01:30:00.000 Vector Time (MET): N/A Weight (LBS) : 909660.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3930788.96 A = 6778592.38 meter Y = -1599581.99 meter E = .0003906 Z = 5284816.99 I = 51.27058 XDOT = 3104.625626 Wp = 165.22205 YDOT = 7010.048129 meter/sec RA = 244.96685 deg ZDOT = -191.101846 TA = 286.58695 MA = 286.62985 Ha = 221.685 n.mi Hp = 215.717 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12896289.24 X = 3922712.89 Y = -5247972.39 feet Y = -1555669.68 meter Z = 17338638.41 Z = 5303892.00 XDOT = 10185.779614 XDOT = 3026.934852 YDOT = 22998.845567 feet/sec YDOT = 7044.331787 meter/sec ZDOT = -626.974562 ZDOT = -176.210201 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9460806.77 X = 2883653.90 Y = -10068183.83 feet Y = -3068782.43 meter Z = 17424370.34 Z = 5310948.08 XDOT = 18064.544706 XDOT = 5506.073226 YDOT = 16024.870380 feet/sec YDOT = 4884.380492 meter/sec ZDOT = -560.895898 ZDOT = -170.961070 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18267.11046221 .00016717 00000-0 10270-3 0 9042 2 25544 51.6376 245.7349 0004351 199.1875 160.9114 15.53704150 13891 Satellite: ISS Catalog Number: 25544 Epoch time: 18267.11046221 = yrday.fracday Element set: 904 Inclination: 51.6376 deg RA of node: 245.7349 deg Eccentricity: .0004351 Arg of perigee: 199.1875 deg Mean anomaly: 160.9114 deg Mean motion: 15.53704150 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1389 Checksum: 307 Coasting Arc #6 (Orbit 1403) --------------------------------------- Vector Time (GMT): 2018/268/01:30:00.000 Vector Time (MET): N/A Weight (LBS) : 909660.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4581836.91 A = 6779749.15 meter Y = 94841.55 meter E = .0013011 Z = -5007812.60 I = 51.29042 XDOT = -2276.387671 Wp = 124.35773 YDOT = -7048.250068 meter/sec RA = 239.94769 deg ZDOT = 1945.691549 TA = 164.66377 MA = 164.62430 Ha = 221.660 n.mi Hp = 215.629 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -15032273.34 X = -4558231.48 Y = 311159.93 feet Y = 43735.61 meter Z = -16429831.35 Z = -5030012.37 XDOT = -7468.463488 XDOT = -2206.854191 YDOT = -23124.180012 feet/sec YDOT = -7073.317178 meter/sec ZDOT = 6383.502458 ZDOT = 1934.803383 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13341653.71 X = -4066536.05 Y = 6692059.93 feet Y = 2039739.87 meter Z = -16529429.23 Z = -5038170.03 XDOT = -16230.088783 XDOT = -4946.931061 YDOT = -16679.975099 feet/sec YDOT = -5084.056410 meter/sec ZDOT = 6335.369020 ZDOT = 1931.020477 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18268.07524550 .00016717 00000-0 10270-3 0 9055 2 25544 51.6383 240.9290 0004445 203.2275 156.8677 15.53732375 14042 Satellite: ISS Catalog Number: 25544 Epoch time: 18268.07524550 = yrday.fracday Element set: 905 Inclination: 51.6383 deg RA of node: 240.9290 deg Eccentricity: .0004445 Arg of perigee: 203.2275 deg Mean anomaly: 156.8677 deg Mean motion: 15.53732375 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1404 Checksum: 311 Coasting Arc #7 (Orbit 1419) --------------------------------------- Vector Time (GMT): 2018/269/01:30:00.000 Vector Time (MET): N/A Weight (LBS) : 909660.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5097450.12 A = 6782703.45 meter Y = 1309641.07 meter E = .0007456 Z = 4271466.65 I = 51.31879 XDOT = 1243.754618 Wp = 98.02542 YDOT = 6694.661835 meter/sec RA = 234.93384 deg ZDOT = -3532.581904 TA = 28.14583 MA = 28.10555 Ha = 221.484 n.mi Hp = 215.922 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 16723917.73 X = 5061677.76 Y = 4296722.67 feet Y = 1366444.82 meter Z = 14013998.20 Z = 4296141.48 XDOT = 4080.559771 XDOT = 1185.960200 YDOT = 21964.113632 feet/sec YDOT = 6708.246768 meter/sec ZDOT = -11589.835643 ZDOT = -3526.681336 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 16804869.77 X = 5122124.31 Y = -3554772.10 feet Y = -1083494.54 meter Z = 14124565.22 Z = 4305167.48 XDOT = 13240.820104 XDOT = 4035.801968 YDOT = 16590.848270 feet/sec YDOT = 5056.890553 meter/sec ZDOT = -11564.027306 ZDOT = -3524.715523 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18269.10434642 .00016717 00000-0 10270-3 0 9063 2 25544 51.6396 235.8012 0004407 206.1875 153.9055 15.53701778 14206 Satellite: ISS Catalog Number: 25544 Epoch time: 18269.10434642 = yrday.fracday Element set: 906 Inclination: 51.6396 deg RA of node: 235.8012 deg Eccentricity: .0004407 Arg of perigee: 206.1875 deg Mean anomaly: 153.9055 deg Mean motion: 15.53701778 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1420 Checksum: 303 Coasting Arc #8 (Orbit 1434) --------------------------------------- Vector Time (GMT): 2018/270/01:30:00.000 Vector Time (MET): N/A Weight (LBS) : 909660.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5442755.13 A = 6786196.99 meter Y = -2534128.95 meter E = .0003595 Z = -3168624.50 I = 51.35084 XDOT = -11.533151 Wp = 141.97722 YDOT = -5973.393265 meter/sec RA = 229.93101 deg ZDOT = 4797.208412 TA = 181.32114 MA = 181.32209 Ha = 221.444 n.mi Hp = 215.969 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -17856808.16 X = -5398621.56 Y = -8314071.37 feet Y = -2594747.22 meter Z = -10395749.68 Z = -3194956.39 XDOT = -37.838423 XDOT = 31.961218 YDOT = -19597.746933 feet/sec YDOT = -5973.278484 meter/sec ZDOT = 15738.872744 ZDOT = 4797.258727 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -19618049.13 X = -5979581.37 Y = 810256.42 feet Y = 246966.16 meter Z = -10513639.94 Z = -3204557.46 XDOT = -9091.573993 XDOT = -2771.111753 YDOT = -15898.973708 feet/sec YDOT = -4846.007186 meter/sec ZDOT = 15739.681205 ZDOT = 4797.454831 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18270.06912444 .00016717 00000-0 10270-3 0 9072 2 25544 51.6399 230.9951 0004274 212.0098 148.0796 15.53709750 14353 Satellite: ISS Catalog Number: 25544 Epoch time: 18270.06912444 = yrday.fracday Element set: 907 Inclination: 51.6399 deg RA of node: 230.9951 deg Eccentricity: .0004274 Arg of perigee: 212.0098 deg Mean anomaly: 148.0796 deg Mean motion: 15.53709750 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1435 Checksum: 319 Coasting Arc #9 (Orbit 1441) --------------------------------------- Vector Time (GMT): 2018/270/11:54:38.000 Vector Time (MET): N/A Weight (LBS) : 943739.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 399521.86 A = 6783242.58 meter Y = 5365315.99 meter E = .0004946 Z = -4134933.71 I = 51.34820 XDOT = -6233.260003 Wp = 97.43171 YDOT = -2418.183460 meter/sec RA = 227.81385 deg ZDOT = -3744.484351 TA = 133.85539 MA = 133.81451 Ha = 221.251 n.mi Hp = 216.043 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 1310767.27 X = 359581.35 Y = 17602742.75 feet Y = 5369559.94 meter Z = -13566055.47 Z = -4133090.54 XDOT = -20450.328095 XDOT = -6187.566925 YDOT = -7933.672770 feet/sec YDOT = -2487.633029 meter/sec ZDOT = -12285.053646 ZDOT = -3774.652571 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -2626899.90 X = -800679.09 Y = -17460934.74 feet Y = -5322092.91 meter Z = -13558306.65 Z = -4132571.87 XDOT = 19599.375869 XDOT = 5973.889765 YDOT = 6684.132719 feet/sec YDOT = 2037.323653 meter/sec ZDOT = -12420.172060 ZDOT = -3785.668444 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18270.51935405 .00016717 00000-0 10270-3 0 9085 2 25544 51.6378 228.7550 0003823 215.8494 144.2402 15.53733689 14428 Satellite: ISS Catalog Number: 25544 Epoch time: 18270.51935405 = yrday.fracday Element set: 908 Inclination: 51.6378 deg RA of node: 228.7550 deg Eccentricity: .0003823 Arg of perigee: 215.8494 deg Mean anomaly: 144.2402 deg Mean motion: 15.53733689 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1442 Checksum: 317 Coasting Arc #10 (Orbit 1450) --------------------------------------- Vector Time (GMT): 2018/271/01:02:30.000 Vector Time (MET): N/A Weight (LBS) : 943739.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -436902.57 A = 6782721.60 meter Y = -5259159.87 meter E = .0009562 Z = 4259007.05 I = 51.36109 XDOT = 6369.470199 Wp = 132.74452 YDOT = 2360.170503 meter/sec RA = 225.07382 deg ZDOT = 3556.349800 TA = 280.77312 MA = 280.88075 Ha = 221.309 n.mi Hp = 216.080 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -1433407.37 X = -398749.06 Y = -17254461.52 feet Y = -5263831.85 meter Z = 13973120.24 Z = 4256977.90 XDOT = 20897.211939 XDOT = 6325.329561 YDOT = 7743.341546 feet/sec YDOT = 2431.151896 meter/sec ZDOT = 11667.814305 ZDOT = 3587.183537 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7746458.47 X = -2361120.54 Y = -15492051.49 feet Y = -4721977.30 meter Z = 13964523.26 Z = 4256386.69 XDOT = 21079.004522 XDOT = 6424.880578 YDOT = 135.695764 feet/sec YDOT = 41.360069 meter/sec ZDOT = 11805.931476 ZDOT = 3598.447914 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18271.09821932 .00016717 00000-0 10270-3 0 9099 2 25544 51.6399 225.8678 0004404 214.9521 145.1342 15.53760303 14513 Satellite: ISS Catalog Number: 25544 Epoch time: 18271.09821932 = yrday.fracday Element set: 909 Inclination: 51.6399 deg RA of node: 225.8678 deg Eccentricity: .0004404 Arg of perigee: 214.9521 deg Mean anomaly: 145.1342 deg Mean motion: 15.53760303 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1451 Checksum: 306 Coasting Arc #11 (Orbit 1465) --------------------------------------- Vector Time (GMT): 2018/272/01:02:30.000 Vector Time (MET): N/A Weight (LBS) : 943739.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -871412.36 A = 6779838.44 meter Y = 4495456.96 meter E = .0009618 Z = -5008073.91 I = 51.37626 XDOT = -6548.419710 Wp = 90.90100 YDOT = -3455.433130 meter/sec RA = 220.06596 deg ZDOT = -1965.733758 TA = 159.94357 MA = 159.90574 Ha = 221.184 n.mi Hp = 216.181 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -2858964.44 X = -897290.02 Y = 14748874.55 feet Y = 4485567.12 meter Z = -16430688.69 Z = -5012370.23 XDOT = -21484.316635 XDOT = -6499.744731 YDOT = -11336.722866 feet/sec YDOT = -3528.390106 meter/sec ZDOT = -6449.257736 ZDOT = -1997.425771 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 3102470.84 X = 945633.11 Y = 14677520.83 feet Y = 4473708.35 meter Z = -16450397.13 Z = -5014081.05 XDOT = -23076.989492 XDOT = -7033.866397 YDOT = -2496.769183 feet/sec YDOT = -761.015247 meter/sec ZDOT = -6591.136247 ZDOT = -2008.978328 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18272.06299481 .00016717 00000-0 10270-3 0 9107 2 25544 51.6407 221.0621 0004340 219.0970 140.9869 15.53733140 14664 Satellite: ISS Catalog Number: 25544 Epoch time: 18272.06299481 = yrday.fracday Element set: 910 Inclination: 51.6407 deg RA of node: 221.0621 deg Eccentricity: .0004340 Arg of perigee: 219.0970 deg Mean anomaly: 140.9869 deg Mean motion: 15.53733140 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1466 Checksum: 295 Coasting Arc #12 (Orbit 1481) --------------------------------------- Vector Time (GMT): 2018/273/01:02:30.000 Vector Time (MET): N/A Weight (LBS) : 943739.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2229978.93 A = 6778385.27 meter Y = -3598617.49 meter E = .0003627 Z = 5294265.18 I = 51.39803 XDOT = 6370.055903 Wp = 187.63633 YDOT = 4263.248687 meter/sec RA = 215.05340 deg ZDOT = 211.195379 TA = 260.32347 MA = 260.36444 Ha = 220.951 n.mi Hp = 216.240 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 7316203.83 X = 2244336.73 Y = -11806487.84 feet Y = -3573599.71 meter Z = 17369636.42 Z = 5305132.93 XDOT = 20899.133541 XDOT = 6320.883740 YDOT = 13987.036374 feet/sec YDOT = 4334.208146 meter/sec ZDOT = 692.898225 ZDOT = 242.019742 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 1900268.79 X = 579201.93 Y = -13696729.86 feet Y = -4174763.26 meter Z = 17418749.45 Z = 5309234.83 XDOT = 23738.276686 XDOT = 7235.426734 YDOT = 4364.625636 feet/sec YDOT = 1330.337894 meter/sec ZDOT = 830.824760 ZDOT = 253.235387 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18273.09208285 .00016717 00000-0 10270-3 0 9114 2 25544 51.6408 215.9348 0004240 223.4724 136.6094 15.53779625 14826 Satellite: ISS Catalog Number: 25544 Epoch time: 18273.09208285 = yrday.fracday Element set: 911 Inclination: 51.6408 deg RA of node: 215.9348 deg Eccentricity: .0004240 Arg of perigee: 223.4724 deg Mean anomaly: 136.6094 deg Mean motion: 15.53779625 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1482 Checksum: 314 Coasting Arc #13 (Orbit 1496) --------------------------------------- Vector Time (GMT): 2018/274/01:02:30.000 Vector Time (MET): N/A Weight (LBS) : 943739.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3588162.37 A = 6779179.67 meter Y = 2641350.21 meter E = .0011817 Z = -5119687.70 I = 51.42789 XDOT = -5769.860654 Wp = 118.96344 YDOT = -4785.410259 meter/sec RA = 210.04356 deg ZDOT = 1572.099722 TA = 166.27325 MA = 166.24109 Ha = 220.933 n.mi Hp = 216.159 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -11772186.26 X = -3592562.89 Y = 8665847.15 feet Y = 2601200.06 meter Z = -16796875.67 Z = -5137128.82 XDOT = -18929.989022 XDOT = -5723.556582 YDOT = -15700.164891 feet/sec YDOT = -4849.673871 meter/sec ZDOT = 5157.807486 ZDOT = 1544.184006 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7024348.06 X = -2141021.29 Y = 12715955.62 feet Y = 3875823.27 meter Z = -16875405.63 Z = -5143623.64 XDOT = -22836.112555 XDOT = -6960.447107 YDOT = -5923.142646 feet/sec YDOT = -1805.373878 meter/sec ZDOT = 5032.963912 ZDOT = 1534.047400 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18274.05685279 .00016717 00000-0 10270-3 0 9124 2 25544 51.6403 211.1297 0004158 225.9421 134.1389 15.53770459 14973 Satellite: ISS Catalog Number: 25544 Epoch time: 18274.05685279 = yrday.fracday Element set: 912 Inclination: 51.6403 deg RA of node: 211.1297 deg Eccentricity: .0004158 Arg of perigee: 225.9421 deg Mean anomaly: 134.1389 deg Mean motion: 15.53770459 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1497 Checksum: 321 Coasting Arc #14 (Orbit 1502) --------------------------------------- Vector Time (GMT): 2018/274/09:07:30.000 Vector Time (MET): N/A Weight (LBS) : 943739.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5513248.50 A = 6789943.84 meter Y = -3839826.67 meter E = .0009514 Z = 950860.35 I = 51.46988 XDOT = 3446.325605 Wp = 58.05470 YDOT = -3477.744816 meter/sec RA = 208.38540 deg ZDOT = 5899.823403 TA = 312.26434 MA = 312.34498 Ha = 220.845 n.mi Hp = 216.286 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -18088085.63 X = -5474519.57 Y = -12597856.53 feet Y = -3901263.05 meter Z = 3119620.56 Z = 924172.76 XDOT = 11306.842535 XDOT = 3456.299955 YDOT = -11409.923937 feet/sec YDOT = -3439.149604 meter/sec ZDOT = 19356.375994 ZDOT = 5916.589050 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 7985930.34 X = 2434111.57 Y = 20563088.75 feet Y = 6267629.45 meter Z = 3000193.49 Z = 914458.98 XDOT = -14144.173849 XDOT = -4311.144189 YDOT = 2638.745494 feet/sec YDOT = 804.289627 meter/sec ZDOT = 19431.955565 ZDOT = 5922.860056 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18274.44275797 .00016717 00000-0 10270-3 0 9138 2 25544 51.6366 209.2095 0003988 228.4583 131.6228 15.53795519 15038 Satellite: ISS Catalog Number: 25544 Epoch time: 18274.44275797 = yrday.fracday Element set: 913 Inclination: 51.6366 deg RA of node: 209.2095 deg Eccentricity: .0003988 Arg of perigee: 228.4583 deg Mean anomaly: 131.6228 deg Mean motion: 15.53795519 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1503 Checksum: 340 Coasting Arc #15 (Orbit 1517) --------------------------------------- Vector Time (GMT): 2018/275/09:07:30.000 Vector Time (MET): N/A Weight (LBS) : 943739.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4734170.32 A = 6787901.01 meter Y = 4187441.83 meter E = .0005915 Z = -2466703.00 I = 51.49310 XDOT = -4945.988901 Wp = 171.39555 YDOT = 2466.020444 meter/sec RA = 203.40276 deg ZDOT = -5313.586305 TA = 36.28924 MA = 36.24914 Ha = 220.777 n.mi Hp = 216.427 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 15532054.84 X = 4698975.38 Y = 13738326.20 feet Y = 4240185.73 meter Z = -8092857.60 Z = -2443791.46 XDOT = -16226.997708 XDOT = -4947.386188 YDOT = 8090.618254 feet/sec YDOT = 2410.702963 meter/sec ZDOT = -17433.025935 ZDOT = -5337.615909 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -5601371.32 X = -1707297.98 Y = -20006472.30 feet Y = -6097972.76 meter Z = -7990393.24 Z = -2435471.86 XDOT = 16459.690379 XDOT = 5016.913628 YDOT = 2387.614658 feet/sec YDOT = 727.744948 meter/sec ZDOT = -17541.128539 ZDOT = -5346.535979 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18275.40752481 .00016717 00000-0 10270-3 0 9146 2 25544 51.6374 204.4021 0003783 235.5576 124.5219 15.53754296 15181 Satellite: ISS Catalog Number: 25544 Epoch time: 18275.40752481 = yrday.fracday Element set: 914 Inclination: 51.6374 deg RA of node: 204.4021 deg Eccentricity: .0003783 Arg of perigee: 235.5576 deg Mean anomaly: 124.5219 deg Mean motion: 15.53754296 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1518 Checksum: 311 Coasting Arc #16 (Orbit 1533) --------------------------------------- Vector Time (GMT): 2018/276/09:07:30.000 Vector Time (MET): N/A Weight (LBS) : 943739.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3625087.22 A = 6784463.22 meter Y = -4342362.19 meter E = .0008836 Z = 3741507.59 I = 51.51296 XDOT = 6200.167797 Wp = 111.15555 YDOT = -1500.628258 meter/sec RA = 198.41620 deg ZDOT = 4254.382222 TA = 293.65745 MA = 293.75017 Ha = 220.612 n.mi Hp = 216.460 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -11893330.78 X = -3594434.66 Y = -14246595.12 feet Y = -4382728.88 meter Z = 12275287.37 Z = 3723972.72 XDOT = 20341.757863 XDOT = 6195.821773 YDOT = -4923.321056 feet/sec YDOT = -1431.317798 meter/sec ZDOT = 13957.946922 ZDOT = 4284.490155 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 2612800.62 X = 796381.63 Y = 18425714.72 feet Y = 5616157.85 meter Z = 12196957.80 Z = 3717632.74 XDOT = -18438.893939 XDOT = -5620.174873 YDOT = -6738.989027 feet/sec YDOT = -2054.043855 meter/sec ZDOT = 14093.265060 ZDOT = 4295.627190 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18276.43660152 .00016717 00000-0 10270-3 0 9154 2 25544 51.6377 199.2755 0003917 239.7645 120.3120 15.53787714 15345 Satellite: ISS Catalog Number: 25544 Epoch time: 18276.43660152 = yrday.fracday Element set: 915 Inclination: 51.6377 deg RA of node: 199.2755 deg Eccentricity: .0003917 Arg of perigee: 239.7645 deg Mean anomaly: 120.3120 deg Mean motion: 15.53787714 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1534 Checksum: 323 Coasting Arc #17 (Orbit 1547) --------------------------------------- Vector Time (GMT): 2018/277/07:57:30.000 Vector Time (MET): N/A Weight (LBS) : 928631.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6210762.08 A = 6787324.35 meter Y = 663922.01 meter E = .0001300 Z = -2654887.91 I = 51.55161 XDOT = -2747.149315 Wp = 35.44628 YDOT = -4913.850353 meter/sec RA = 193.62118 deg ZDOT = 5200.078072 TA = 294.58829 MA = 294.60183 Ha = 220.553 n.mi Hp = 216.397 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20376516.02 X = -6204828.57 Y = 2178221.81 feet Y = 594501.98 meter Z = -8710262.16 Z = -2685043.34 XDOT = -9012.957071 XDOT = -2717.256408 YDOT = -16121.556275 feet/sec YDOT = -4944.403432 meter/sec ZDOT = 17060.623597 ZDOT = 5186.806234 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15084191.63 X = 4597661.61 Y = 13785349.64 feet Y = 4201774.57 meter Z = -8845734.59 Z = -2696179.90 XDOT = -5033.575596 XDOT = -1534.233842 YDOT = 16412.479737 feet/sec YDOT = 5002.523824 meter/sec ZDOT = 17001.473032 ZDOT = 5182.048980 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18277.33704292 .00016717 00000-0 10270-3 0 9169 2 25544 51.6366 194.7893 0003707 243.0096 117.0679 15.53757861 15488 Satellite: ISS Catalog Number: 25544 Epoch time: 18277.33704292 = yrday.fracday Element set: 916 Inclination: 51.6366 deg RA of node: 194.7893 deg Eccentricity: .0003707 Arg of perigee: 243.0096 deg Mean anomaly: 117.0679 deg Mean motion: 15.53757861 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1548 Checksum: 341 Coasting Arc #18 (Orbit 1563) --------------------------------------- Vector Time (GMT): 2018/278/07:57:30.000 Vector Time (MET): N/A Weight (LBS) : 928631.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6682531.59 A = 6789728.98 meter Y = 86744.74 meter E = .0011820 Z = 1158709.64 I = 51.59304 XDOT = 958.633972 Wp = 137.08783 YDOT = 4848.767899 meter/sec RA = 188.64419 deg ZDOT = -5864.882500 TA = 30.32044 MA = 30.25211 Ha = 220.358 n.mi Hp = 216.478 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21924316.24 X = 6675436.52 Y = 284595.61 feet Y = 161433.87 meter Z = 3801540.81 Z = 1191153.88 XDOT = 3145.124580 XDOT = 932.831018 YDOT = 15908.031165 feet/sec YDOT = 4859.343258 meter/sec ZDOT = -19241.740487 ZDOT = -5860.288846 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14568528.84 X = -4440487.59 Y = -16351929.40 feet Y = -4984068.08 meter Z = 3947242.35 Z = 1203119.47 XDOT = 8336.769281 XDOT = 2541.047277 YDOT = -12087.892101 feet/sec YDOT = -3684.389512 meter/sec ZDOT = -19221.544556 ZDOT = -5858.726781 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18278.36611453 .00016717 00000-0 10270-3 0 9170 2 25544 51.6374 189.6615 0003786 249.0913 110.9834 15.53780819 15645 Satellite: ISS Catalog Number: 25544 Epoch time: 18278.36611453 = yrday.fracday Element set: 917 Inclination: 51.6374 deg RA of node: 189.6615 deg Eccentricity: .0003786 Arg of perigee: 249.0913 deg Mean anomaly: 110.9834 deg Mean motion: 15.53780819 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1564 Checksum: 339 Coasting Arc #19 (Orbit 1579) --------------------------------------- Vector Time (GMT): 2018/279/07:57:30.000 Vector Time (MET): N/A Weight (LBS) : 928631.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6727764.54 A = 6790208.12 meter Y = -770264.42 meter E = .0009319 Z = 426319.29 I = 51.62839 XDOT = 921.466526 Wp = 41.12594 YDOT = -4694.740118 meter/sec RA = 183.67415 deg ZDOT = 5991.711309 TA = 323.47080 MA = 323.53432 Ha = 220.304 n.mi Hp = 216.529 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -22072718.30 X = -6720722.05 Y = -2527114.25 feet Y = -845459.54 meter Z = 1398685.33 Z = 393655.22 XDOT = 3023.184141 XDOT = 944.791253 YDOT = -15402.690677 feet/sec YDOT = -4684.304608 meter/sec ZDOT = 19657.845501 ZDOT = 5996.244622 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13345162.92 X = 4067605.66 Y = 17773197.34 feet Y = 5417270.55 meter Z = 1252039.72 Z = 381621.71 XDOT = -11877.021184 XDOT = -3620.116057 YDOT = 7514.234479 feet/sec YDOT = 2290.338669 meter/sec ZDOT = 19678.623268 ZDOT = 5998.044372 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 18279.39518044 .00016717 00000-0 10270-3 0 9187 2 25544 51.6381 184.5346 0003818 250.6963 109.3777 15.53805301 15807 Satellite: ISS Catalog Number: 25544 Epoch time: 18279.39518044 = yrday.fracday Element set: 918 Inclination: 51.6381 deg RA of node: 184.5346 deg Eccentricity: .0003818 Arg of perigee: 250.6963 deg Mean anomaly: 109.3777 deg Mean motion: 15.53805301 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1580 Checksum: 328