ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 10494.81
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 72.1
Monthly MSFC 50% earth geomagnetic index (Kp) : 2.19
ET - UTC (sec) : 66.18
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
------------------------------------------------------------------------
There are no maneuvers.
Coasting Arc #1 (Orbit 820)
---------------------------------------
Vector Time (GMT): 2009/182/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2065539.19 A = 6720761.87 meter
Y = 3939609.98 meter E = .0014826
Z = -5048877.50 I = 51.35731
XDOT = -5557.731516 Wp = 109.03118
YDOT = -5047.406667 meter/sec RA = 232.51093 deg
ZDOT = -1673.508725 TA = 144.84375
MA = 144.74584
Ha = 191.647 n.mi
Hp = 182.666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6776703.39 X = -2084912.46
Y = 12925229.59 feet Y = 3916404.36 meter
Z = -16564558.73 Z = -5058958.38
XDOT = -18234.027282 XDOT = -5492.747866
YDOT = -16559.733158 feet/sec YDOT = -5109.192873 meter/sec
ZDOT = -5490.514191 ZDOT = -1700.351193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13803555.36 X = 4207323.67
Y = 4598150.29 feet Y = 1401516.21 meter
Z = -16603877.51 Z = -5060861.86
XDOT = -13205.929689 XDOT = -4025.167369
YDOT = 19540.191309 feet/sec YDOT = 5955.850311 meter/sec
ZDOT = -5596.056185 ZDOT = -1705.677925
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 09182.51880199 .00010596 00000-0 82463-4 0 9001
2 25544 51.6396 233.3229 0007827 173.9476 186.1783 15.74103705 8215
Satellite: ISS
Catalog Number: 25544
Epoch time: 09182.51880199 = yrday.fracday
Element set: 900
Inclination: 51.6396 deg
RA of node: 233.3229 deg
Eccentricity: .0007827
Arg of perigee: 173.9476 deg
Mean anomaly: 186.1783 deg
Mean motion: 15.74103705 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 821
Checksum: 326
Coasting Arc #2 (Orbit 836)
---------------------------------------
Vector Time (GMT): 2009/183/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5210667.55 A = 6730882.05 meter
Y = 4004725.39 meter E = .0019213
Z = 1399580.74 I = 51.41116
XDOT = -2010.116650 Wp = 139.05537
YDOT = 4655.298045 meter/sec RA = 227.32895 deg
ZDOT = -5806.302317 TA = 25.48944
MA = 25.39482
Ha = 191.418 n.mi
Hp = 182.829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17095365.97 X = 5158699.83
Y = 13138862.81 feet Y = 4062703.31 meter
Z = 4591800.34 Z = 1424768.70
XDOT = -6594.870898 XDOT = -2033.817547
YDOT = 15273.287548 feet/sec YDOT = 4632.688219 meter/sec
ZDOT = -19049.548284 ZDOT = -5816.124266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10010557.16 X = 3051217.82
Y = -19072256.48 feet Y = -5813223.77 meter
Z = 4690806.16 Z = 1429757.72
XDOT = 14769.194673 XDOT = 4501.650536
YDOT = 3033.225115 feet/sec YDOT = 924.527015 meter/sec
ZDOT = -19087.815856 ZDOT = -5817.966273
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 09183.53455379 .00010596 00000-0 82463-4 0 9013
2 25544 51.6397 228.1057 0007643 177.1499 182.9709 15.74144713 8377
Satellite: ISS
Catalog Number: 25544
Epoch time: 09183.53455379 = yrday.fracday
Element set: 901
Inclination: 51.6397 deg
RA of node: 228.1057 deg
Eccentricity: .0007643
Arg of perigee: 177.1499 deg
Mean anomaly: 182.9709 deg
Mean motion: 15.74144713 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 837
Checksum: 340
Coasting Arc #3 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2009/184/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1436047.93 A = 6720558.48 meter
Y = -4165821.87 meter E = .0011262
Z = 5073454.29 I = 51.39643
XDOT = 6343.649874 Wp = 159.65439
YDOT = 4085.040393 meter/sec RA = 222.20264 deg
ZDOT = 1547.218122 TA = 275.38620
MA = 275.51467
Ha = 191.401 n.mi
Hp = 182.989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4711443.35 X = 1457878.19
Y = -13667394.59 feet Y = -4149642.03 meter
Z = 16645191.23 Z = 5080482.86
XDOT = 20812.499587 XDOT = 6289.982672
YDOT = 13402.363493 feet/sec YDOT = 4155.678435 meter/sec
ZDOT = 5076.174940 ZDOT = 1577.906010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14292454.87 X = -4356340.25
Y = -1951961.36 feet Y = -594957.82 meter
Z = 16672532.65 Z = 5081787.95
XDOT = 9096.356352 XDOT = 2772.569416
YDOT = -21896.634099 feet/sec YDOT = -6674.094073 meter/sec
ZDOT = 5196.769200 ZDOT = 1583.975252
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 09184.55030636 .00010596 00000-0 82463-4 0 9022
2 25544 51.6389 222.8886 0007677 180.3851 179.7308 15.74131210 8539
Satellite: ISS
Catalog Number: 25544
Epoch time: 09184.55030636 = yrday.fracday
Element set: 902
Inclination: 51.6389 deg
RA of node: 222.8886 deg
Eccentricity: .0007677
Arg of perigee: 180.3851 deg
Mean anomaly: 179.7308 deg
Mean motion: 15.74131210 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 853
Checksum: 321
Coasting Arc #4 (Orbit 867)
---------------------------------------
Vector Time (GMT): 2009/185/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5830485.37 A = 6731014.23 meter
Y = -3107458.63 meter E = .0004880
Z = -1292841.83 I = 51.45519
XDOT = 1293.409790 Wp = 96.67092
YDOT = -4846.458788 meter/sec RA = 217.02526 deg
ZDOT = 5834.112056 TA = 249.11556
MA = 249.16781
Ha = 191.286 n.mi
Hp = 183.146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19128889.00 X = -5789023.53
Y = -10195074.23 feet Y = -3172426.44 meter
Z = -4241607.06 Z = -1321066.17
XDOT = 4243.470439 XDOT = 1319.166602
YDOT = -15900.455342 feet/sec YDOT = -4831.852265 meter/sec
ZDOT = 19140.787586 ZDOT = 5840.457030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6049160.67 X = -1843784.17
Y = 20792031.43 feet Y = 6337411.18 meter
Z = -4352499.00 Z = -1326641.70
XDOT = -14893.829566 XDOT = -4539.639252
YDOT = -333.396091 feet/sec YDOT = -101.619129 meter/sec
ZDOT = 19165.412375 ZDOT = 5841.617692
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 09185.50257442 .00010596 00000-0 82463-4 0 9035
2 25544 51.6393 217.9973 0007621 184.0064 176.1039 15.74136452 8683
Satellite: ISS
Catalog Number: 25544
Epoch time: 09185.50257442 = yrday.fracday
Element set: 903
Inclination: 51.6393 deg
RA of node: 217.9973 deg
Eccentricity: .0007621
Arg of perigee: 184.0064 deg
Mean anomaly: 176.1039 deg
Mean motion: 15.74136452 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 868
Checksum: 318
Coasting Arc #5 (Orbit 883)
---------------------------------------
Vector Time (GMT): 2009/186/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -836277.55 A = 6720458.26 meter
Y = 4285196.81 meter E = .0013574
Z = -5118887.64 I = 51.44383
XDOT = -6940.455480 Wp = 111.40931
YDOT = -3010.830525 meter/sec RA = 211.89943 deg
ZDOT = -1394.436033 TA = 145.23220
MA = 145.14342
Ha = 191.168 n.mi
Hp = 183.371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2743692.77 X = -859266.73
Y = 14059044.65 feet Y = 4275717.56 meter
Z = -16794250.79 Z = -5123005.23
XDOT = -22770.523227 XDOT = -6899.498157
YDOT = -9878.052905 feet/sec YDOT = -3088.213471 meter/sec
ZDOT = -4574.921368 ZDOT = -1428.053678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14295111.74 X = 4357150.06
Y = -547216.54 feet Y = -166791.60 meter
Z = -16810168.96 Z = -5123739.50
XDOT = -4611.906731 XDOT = -1405.709172
YDOT = 23328.543189 feet/sec YDOT = 7110.539964 meter/sec
ZDOT = -4706.984011 ZDOT = -1434.688727
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 09186.51832632 .00010596 00000-0 82463-4 0 9048
2 25544 51.6393 212.7795 0007598 188.1265 171.9777 15.74111609 8846
Satellite: ISS
Catalog Number: 25544
Epoch time: 09186.51832632 = yrday.fracday
Element set: 904
Inclination: 51.6393 deg
RA of node: 212.7795 deg
Eccentricity: .0007598
Arg of perigee: 188.1265 deg
Mean anomaly: 171.9777 deg
Mean motion: 15.74111609 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 884
Checksum: 344
Coasting Arc #6 (Orbit 899)
---------------------------------------
Vector Time (GMT): 2009/187/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6268711.38 A = 6731211.77 meter
Y = 2127101.88 meter E = .0017997
Z = 1156236.83 I = 51.50483
XDOT = -586.739821 Wp = 145.20668
YDOT = 4944.187588 meter/sec RA = 206.72792 deg
ZDOT = -5884.334564 TA = 22.09373
MA = 22.01626
Ha = 191.005 n.mi
Hp = 183.514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20566638.39 X = 6238843.13
Y = 6978680.69 feet Y = 2197035.04 meter
Z = 3793427.93 Z = 1186617.80
XDOT = -1924.999412 XDOT = -613.398228
YDOT = 16221.087888 feet/sec YDOT = 4937.478427 meter/sec
ZDOT = -19305.559593 ZDOT = -5887.248694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1862854.84 X = 567798.16
Y = -21617094.46 feet Y = -6588890.39 meter
Z = 3912760.29 Z = 1192609.34
XDOT = 14607.208787 XDOT = 4452.277238
YDOT = -2255.037306 feet/sec YDOT = -687.335371 meter/sec
ZDOT = -19316.717977 ZDOT = -5887.735640
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 09187.53407813 .00010596 00000-0 82463-4 0 9051
2 25544 51.6379 207.5619 0007490 191.0279 169.0721 15.74123877 9002
Satellite: ISS
Catalog Number: 25544
Epoch time: 09187.53407813 = yrday.fracday
Element set: 905
Inclination: 51.6379 deg
RA of node: 207.5619 deg
Eccentricity: .0007490
Arg of perigee: 191.0279 deg
Mean anomaly: 169.0721 deg
Mean motion: 15.74123877 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 900
Checksum: 323
Coasting Arc #7 (Orbit 915)
---------------------------------------
Vector Time (GMT): 2009/188/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 187483.00 A = 6720320.16 meter
Y = -4324803.38 meter E = .0009754
Z = 5140868.97 I = 51.49453
XDOT = 7371.150935 Wp = 171.06673
YDOT = 1835.822450 meter/sec RA = 201.60339 deg
ZDOT = 1265.778161 TA = 266.75295
MA = 266.86455
Ha = 190.917 n.mi
Hp = 183.728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 615101.72 X = 210856.69
Y = -14188987.46 feet Y = -4322577.11 meter
Z = 16866368.00 Z = 5141835.71
XDOT = 24183.566061 XDOT = 7343.925781
YDOT = 6023.039534 feet/sec YDOT = 1918.098509 meter/sec
ZDOT = 4152.815490 ZDOT = 1301.520942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13848795.11 X = -4221112.75
Y = 3129995.87 feet Y = 954022.74 meter
Z = 16869916.56 Z = 5141950.57
XDOT = -129.612819 XDOT = -39.505987
YDOT = -23886.077334 feet/sec YDOT = -7280.476372 meter/sec
ZDOT = 4293.191179 ZDOT = 1308.564671
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 09188.54982962 .00010596 00000-0 82463-4 0 9067
2 25544 51.6372 202.3439 0007412 195.1590 164.9352 15.74122066 9163
Satellite: ISS
Catalog Number: 25544
Epoch time: 09188.54982962 = yrday.fracday
Element set: 906
Inclination: 51.6372 deg
RA of node: 202.3439 deg
Eccentricity: .0007412
Arg of perigee: 195.1590 deg
Mean anomaly: 164.9352 deg
Mean motion: 15.74122066 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 916
Checksum: 320
Coasting Arc #8 (Orbit 930)
---------------------------------------
Vector Time (GMT): 2009/189/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6562815.06 A = 6731169.51 meter
Y = -1070763.73 meter E = .0003535
Z = -1045943.87 I = 51.56054
XDOT = -134.631578 Wp = 82.93198
YDOT = -4928.740707 meter/sec RA = 196.43840 deg
ZDOT = 5907.906198 TA = 265.62579
MA = 265.66619
Ha = 190.736 n.mi
Hp = 183.810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21531545.48 X = -6545272.91
Y = -3513004.37 feet Y = -1144054.70 meter
Z = -3431574.37 Z = -1077783.09
XDOT = -441.704652 XDOT = -108.206627
YDOT = -16170.409144 feet/sec YDOT = -4930.099510 meter/sec
ZDOT = 19382.894352 ZDOT = 5907.315500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2479856.93 X = 755860.39
Y = 21654681.50 feet Y = 6600346.92 meter
Z = -3556603.96 Z = -1084052.89
XDOT = -13828.387552 XDOT = -4214.892526
YDOT = 4757.581051 feet/sec YDOT = 1450.110704 meter/sec
ZDOT = 19380.291425 ZDOT = 5907.112826
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 09189.50209644 .00010596 00000-0 82463-4 0 9074
2 25544 51.6378 197.4531 0007507 198.6194 161.4696 15.74171424 9311
Satellite: ISS
Catalog Number: 25544
Epoch time: 09189.50209644 = yrday.fracday
Element set: 907
Inclination: 51.6378 deg
RA of node: 197.4531 deg
Eccentricity: .0007507
Arg of perigee: 198.6194 deg
Mean anomaly: 161.4696 deg
Mean motion: 15.74171424 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 931
Checksum: 335
Coasting Arc #9 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2009/190/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 409758.41 A = 6720222.22 meter
Y = 4274739.17 meter E = .0012104
Z = -5178020.45 I = 51.55107
XDOT = -7587.570959 Wp = 112.27098
YDOT = -615.370047 meter/sec RA = 191.31518 deg
ZDOT = -1115.035849 TA = 147.10239
MA = 147.02699
Ha = 190.595 n.mi
Hp = 184.184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1344351.74 X = 387080.55
Y = 14024734.79 feet Y = 4279195.33 meter
Z = -16988256.08 Z = -5176084.30
XDOT = -24893.605510 XDOT = -7574.709314
YDOT = -2018.930601 feet/sec YDOT = -700.146619 meter/sec
ZDOT = -3658.254097 ZDOT = -1151.864500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13009350.45 X = 3965250.02
Y = -5433595.45 feet Y = -1656159.89 meter
Z = -16980404.99 Z = -5175627.44
XDOT = 4857.102958 XDOT = 1480.444982
YDOT = 23445.836952 feet/sec YDOT = 7146.291103 meter/sec
ZDOT = -3802.857930 ZDOT = -1159.111097
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 09190.51784799 .00010596 00000-0 82463-4 0 9087
2 25544 51.6370 192.2347 0007342 203.7648 156.3177 15.74111910 9478
Satellite: ISS
Catalog Number: 25544
Epoch time: 09190.51784799 = yrday.fracday
Element set: 908
Inclination: 51.6370 deg
RA of node: 192.2347 deg
Eccentricity: .0007342
Arg of perigee: 203.7648 deg
Mean anomaly: 156.3177 deg
Mean motion: 15.74111910 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 947
Checksum: 325
Coasting Arc #10 (Orbit 962)
---------------------------------------
Vector Time (GMT): 2009/191/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6658745.52 A = 6731414.91 meter
Y = -9307.17 meter E = .0016217
Z = 913175.88 I = 51.61828
XDOT = 826.700021 Wp = 151.26652
YDOT = 4828.867975 meter/sec RA = 186.15591 deg
ZDOT = -5949.433398 TA = 18.75232
MA = 18.69265
Ha = 190.356 n.mi
Hp = 184.329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21846277.97 X = 6653918.74
Y = -30535.35 feet Y = 65127.70 meter
Z = 2995983.84 Z = 945511.81
XDOT = 2712.270409 XDOT = 801.542149
YDOT = 15842.742700 feet/sec YDOT = 4837.972752 meter/sec
ZDOT = -19519.138446 ZDOT = -5945.477814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6694438.75 X = -2040464.93
Y = -20776634.04 feet Y = -6332718.05 meter
Z = 3122928.21 Z = 951868.52
XDOT = 12707.857222 XDOT = 3873.354881
YDOT = -7040.104332 feet/sec YDOT = -2145.823800 meter/sec
ZDOT = -19503.321590 ZDOT = -5944.612421
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 09191.53359957 .00010596 00000-0 82463-4 0 9095
2 25544 51.6367 187.0167 0007172 207.8234 152.2546 15.74131149 9632
Satellite: ISS
Catalog Number: 25544
Epoch time: 09191.53359957 = yrday.fracday
Element set: 909
Inclination: 51.6367 deg
RA of node: 187.0167 deg
Eccentricity: .0007172
Arg of perigee: 207.8234 deg
Mean anomaly: 152.2546 deg
Mean motion: 15.74131149 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 963
Checksum: 327
Coasting Arc #11 (Orbit 978)
---------------------------------------
Vector Time (GMT): 2009/192/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1027712.97 A = 6720133.86 meter
Y = -4136960.50 meter E = .0008106
Z = 5197020.78 I = 51.60941
XDOT = 7609.525550 Wp = 186.02112
YDOT = -643.118224 meter/sec RA = 181.03519 deg
ZDOT = 985.066591 TA = 254.54019
MA = 254.62973
Ha = 190.286 n.mi
Hp = 184.609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3371761.72 X = -1006622.22
Y = -13572705.05 feet Y = -4148335.66 meter
Z = 17050593.11 Z = 5192078.97
XDOT = 24965.635008 XDOT = 7611.366245
YDOT = -2109.967927 feet/sec YDOT = -558.013877 meter/sec
ZDOT = 3231.845770 ZDOT = 1022.037539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11734449.55 X = -3576660.22
Y = 7652422.15 feet Y = 2332458.27 meter
Z = 17030941.07 Z = 5191030.84
XDOT = -9464.711320 XDOT = -2884.844010
YDOT = -22085.989630 feet/sec YDOT = -6731.809639 meter/sec
ZDOT = 3376.961131 ZDOT = 1029.297753
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 09192.54935142 .00010596 00000-0 82463-4 0 9105
2 25544 51.6364 181.7989 0007190 212.7050 147.3669 15.74111287 9792
Satellite: ISS
Catalog Number: 25544
Epoch time: 09192.54935142 = yrday.fracday
Element set: 910
Inclination: 51.6364 deg
RA of node: 181.7989 deg
Eccentricity: .0007190
Arg of perigee: 212.7050 deg
Mean anomaly: 147.3669 deg
Mean motion: 15.74111287 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 979
Checksum: 327
Coasting Arc #12 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2009/193/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6589881.67 A = 6731424.64 meter
Y = 1108738.28 meter E = .0003142
Z = -800595.21 I = 51.67792
XDOT = -1500.608415 Wp = 48.82684
YDOT = -4621.614708 meter/sec RA = 175.88305 deg
ZDOT = 5968.561876 TA = 302.45215
MA = 302.48253
Ha = 190.093 n.mi
Hp = 184.665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21620346.70 X = -6597900.89
Y = 3637592.78 feet Y = 1035001.61 meter
Z = -2626624.71 Z = -832627.88
XDOT = -4923.255956 XDOT = -1477.811080
YDOT = -15162.777913 feet/sec YDOT = -4638.268530 meter/sec
ZDOT = 19581.895917 ZDOT = 5961.326903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10724389.40 X = 3268793.89
Y = 19104522.11 feet Y = 5823058.34 meter
Z = -2752332.99 Z = -838911.10
XDOT = -11175.192522 XDOT = -3406.198681
YDOT = 9082.470073 feet/sec YDOT = 2768.336878 meter/sec
ZDOT = 19553.206903 ZDOT = 5959.817464
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 09193.50161815 .00010596 00000-0 82463-4 0 9111
2 25544 51.6365 176.9079 0007207 214.9860 145.0830 15.74154175 9946
Satellite: ISS
Catalog Number: 25544
Epoch time: 09193.50161815 = yrday.fracday
Element set: 911
Inclination: 51.6365 deg
RA of node: 176.9079 deg
Eccentricity: .0007207
Arg of perigee: 214.9860 deg
Mean anomaly: 145.0830 deg
Mean motion: 15.74154175 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 994
Checksum: 317
Coasting Arc #13 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2009/194/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1581524.73 A = 6720036.03 meter
Y = 3928665.76 meter E = .0010595
Z = -5225641.49 I = 51.66886
XDOT = -7414.828566 Wp = 110.58845
YDOT = 1876.996095 meter/sec RA = 170.76360 deg
ZDOT = -837.957795 TA = 151.46043
MA = 151.40238
Ha = 189.919 n.mi
Hp = 185.040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5188729.44 X = 1562861.23
Y = 12889323.34 feet Y = 3946247.44 meter
Z = -17144493.09 Z = -5218003.45
XDOT = -24326.865374 XDOT = -7431.195750
YDOT = 6158.123670 feet/sec YDOT = 1793.987707 meter/sec
ZDOT = -2749.205364 ZDOT = -874.018365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10181656.65 X = 3103368.95
Y = -9509318.84 feet Y = -2898440.38 meter
Z = -17114261.18 Z = -5216426.81
XDOT = 13673.265110 XDOT = 4167.611205
YDOT = 19812.807606 feet/sec YDOT = 6038.943758 meter/sec
ZDOT = -2890.692771 ZDOT = -881.083157
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 09194.51736999 .00010596 00000-0 82463-4 0 9125
2 25544 51.6367 171.6895 0007086 220.5975 139.4661 15.74111658 10109
Satellite: ISS
Catalog Number: 25544
Epoch time: 09194.51736999 = yrday.fracday
Element set: 912
Inclination: 51.6367 deg
RA of node: 171.6895 deg
Eccentricity: .0007086
Arg of perigee: 220.5975 deg
Mean anomaly: 139.4661 deg
Mean motion: 15.74111658 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1010
Checksum: 334
Coasting Arc #14 (Orbit 1025)
---------------------------------------
Vector Time (GMT): 2009/195/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6327110.85 A = 6731590.53 meter
Y = -2169439.55 meter E = .0014222
Z = 671851.30 I = 51.73758
XDOT = 2128.435609 Wp = 157.18579
YDOT = 4340.085296 meter/sec RA = 165.61793 deg
ZDOT = -6000.783035 TA = 15.50142
MA = 15.45791
Ha = 189.643 n.mi
Hp = 185.188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20758237.71 X = 6347635.93
Y = -7117583.83 feet Y = -2098571.40 meter
Z = 2204236.54 Z = 702637.96
XDOT = 6983.056459 XDOT = 2108.896482
YDOT = 14239.124988 feet/sec YDOT = 4363.778060 meter/sec
ZDOT = -19687.608382 ZDOT = -5990.490149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14289925.77 X = -4355569.37
Y = -16637772.02 feet Y = -5071192.91 meter
Z = 2325006.40 Z = 708661.95
XDOT = 9387.698514 XDOT = 2861.370507
YDOT = -10821.182993 feet/sec YDOT = -3298.296576 meter/sec
ZDOT = -19646.924933 ZDOT = -5988.382720
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 09195.53312128 .00010596 00000-0 82463-4 0 9133
2 25544 51.6369 166.4721 0007015 225.8534 134.2053 15.74130746 10266
Satellite: ISS
Catalog Number: 25544
Epoch time: 09195.53312128 = yrday.fracday
Element set: 913
Inclination: 51.6369 deg
RA of node: 166.4721 deg
Eccentricity: .0007015
Arg of perigee: 225.8534 deg
Mean anomaly: 134.2053 deg
Mean motion: 15.74130746 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1026
Checksum: 289
Coasting Arc #15 (Orbit 1041)
---------------------------------------
Vector Time (GMT): 2009/196/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 672678.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2124545.35 A = 6719932.26 meter
Y = -3634288.70 meter E = .0006583
Z = 5240837.64 I = 51.72673
XDOT = 7021.694281 Wp = 204.30026
YDOT = -3077.730742 meter/sec RA = 160.50167 deg
ZDOT = 706.632900 TA = 238.95365
MA = 239.01829
Ha = 189.548 n.mi
Hp = 185.424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6970293.14 X = -2109207.26
Y = -11923519.34 feet Y = -3657961.43 meter
Z = 17194349.20 Z = 5230553.44
XDOT = 23037.054729 XDOT = 7052.155426
YDOT = -10097.541803 feet/sec YDOT = -2999.039807 meter/sec
ZDOT = 2318.349408 ZDOT = 740.817954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8269754.32 X = -2520621.12
Y = 11124802.88 feet Y = 3390839.92 meter
Z = 17153742.12 Z = 5228460.60
XDOT = -17391.155308 XDOT = -5300.824138
YDOT = -16737.653461 feet/sec YDOT = -5101.636775 meter/sec
ZDOT = 2452.423110 ZDOT = 747.498564
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 09196.54887292 .00010596 00000-0 82463-4 0 9145
2 25544 51.6369 161.2551 0007056 230.2861 129.7681 15.74123426 10429
Satellite: ISS
Catalog Number: 25544
Epoch time: 09196.54887292 = yrday.fracday
Element set: 914
Inclination: 51.6369 deg
RA of node: 161.2551 deg
Eccentricity: .0007056
Arg of perigee: 230.2861 deg
Mean anomaly: 129.7681 deg
Mean motion: 15.74123426 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 1042
Checksum: 314
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