Date:
March 24th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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
083/09:18:32
836 -0
9 3
4 3
4
N/A -1
9 0
2 192
7
000/00:07:05
671 -2
6 -0
1 181
9
Coasting Arc #1 (Orbit 981)
---------------------------------------
Vector Time (GMT): 2010/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782863
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -815348
87 A = 6721117
93 meter
Y = -4626774
50 meter E =
0018105
Z = -4822459
56 I = 51
39556
XDOT = 6342
354326 Wp = 94
32006
YDOT = -3618
217948 meter/sec RA = 315
04612 deg
ZDOT = 2405
492917 TA = 199
24833
MA = 199
31681
Ha = 192
073 n
mi
Hp = 180
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2675029
09 X = -740124
27
Y = -15179706
35 feet Y = -4635471
73 meter
Z = -15821717
72 Z = -4826237
68
XDOT = 20808
249102 XDOT = 6370
657085
YDOT = -11870
793792 feet/sec YDOT = -3547
135664 meter/sec
ZDOT = 7892
037130 ZDOT = 2436
372832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2345968
00 X = -715051
05
Y = -15218333
70 feet Y = -4638548
11 meter
Z = -15836816
94 Z = -4827061
80
XDOT = 19833
487326 XDOT = 6045
246937
YDOT = -11375
830170 feet/sec YDOT = -3467
353036 meter/sec
ZDOT = 8014
586831 ZDOT = 2442
846066
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 10081
51167848
00016717 00000-0 10270-3 0 9007
2 25544 51
6469 315
5868 0006999 72
2002 287
9924 15
74335183 9825
Satellite: ISS
Catalog Number: 25544
Epoch time: 10081
51167848 = yrday
fracday
Element set: 900
Inclination: 51
6469 deg
RA of node: 315
5868 deg
Eccentricity:
0006999
Arg of perigee: 72
2002 deg
Mean anomaly: 287
9924 deg
Mean motion: 15
74335183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 982
Checksum: 336
Coasting Arc #2 (Orbit 997)
---------------------------------------
Vector Time (GMT): 2010/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782863
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5281241
65 A = 6728963
46 meter
Y = 3516063
43 meter E =
0011089
Z = -2246123
47 I = 51
40141
XDOT = -1226
202911 Wp = 103
53260
YDOT = -5301
422612 meter/sec RA = 309
93051 deg
ZDOT = -5440
708291 TA = 101
74542
MA = 101
62099
Ha = 192
024 n
mi
Hp = 180
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17326908
31 X = -5309255
20
Y = 11535641
17 feet Y = 3456848
76 meter
Z = -7369171
50 Z = -2271847
69
XDOT = -4022
975430 XDOT = -1140
400531
YDOT = -17393
118806 feet/sec YDOT = -5314
655119 meter/sec
ZDOT = -17850
092819 ZDOT = -5446
456609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17263864
74 X = -5262025
97
Y = 11564464
48 feet Y = 3524848
77 meter
Z = -7471251
10 Z = -2277237
33
XDOT = -3103
800909 XDOT = -946
038517
YDOT = -16128
043024 feet/sec YDOT = -4915
827514 meter/sec
ZDOT = -17873
034134 ZDOT = -5447
700804
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 10082
52729111
00016717 00000-0 10270-3 0 9017
2 25544 51
6466 310
3692 0006859 76
5313 283
6614 15
74334563 9984
Satellite: ISS
Catalog Number: 25544
Epoch time: 10082
52729111 = yrday
fracday
Element set: 901
Inclination: 51
6466 deg
RA of node: 310
3692 deg
Eccentricity:
0006859
Arg of perigee: 76
5313 deg
Mean anomaly: 283
6614 deg
Mean motion: 15
74334563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 998
Checksum: 315
Coasting Arc #3 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2010/083/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5154804
46 A = 6728891
63 meter
Y = 3109723
89 meter E =
0010605
Z = -3011603
55 I = 51
37984
XDOT = -668
532810 Wp = 104
04120
YDOT = -5867
460235 meter/sec RA = 305
34346 deg
ZDOT = -4931
378367 TA = 110
89245
MA = 110
77888
Ha = 192
658 n
mi
Hp = 181
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16912088
12 X = -5174565
16
Y = 10202506
19 feet Y = 3051969
22 meter
Z = -9880589
06 Z = -3036693
41
XDOT = -2193
349115 XDOT = -578
916649
YDOT = -19250
197621 feet/sec YDOT = -5874
435246 meter/sec
ZDOT = -16179
062884 ZDOT = -4934
408209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19540762
24 X = -5956024
33
Y = -2508175
74 feet Y = -764491
96 meter
Z = -9980158
47 Z = -3041952
30
XDOT = 10159
614129 XDOT = 3096
650386
YDOT = -14946
367809 feet/sec YDOT = -4555
652908 meter/sec
ZDOT = -16191
227059 ZDOT = -4935
086007
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 10083
41594378
00016717 00000-0 10270-3 0 9022
2 25544 51
6475 305
8035 0006097 102
0627 258
1220 15
73740197 10122
Satellite: ISS
Catalog Number: 25544
Epoch time: 10083
41594378 = yrday
fracday
Element set: 902
Inclination: 51
6475 deg
RA of node: 305
8035 deg
Eccentricity:
0006097
Arg of perigee: 102
0627 deg
Mean anomaly: 258
1220 deg
Mean motion: 15
73740197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1012
Checksum: 288
Coasting Arc #4 (Orbit 1027)
---------------------------------------
Vector Time (GMT): 2010/084/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1097183
07 A = 6724530
31 meter
Y = 5013021
94 meter E =
0014993
Z = 4333887
08 I = 51
34857
XDOT = -5541
966845 Wp = 83
39816
YDOT = 4150
754854 meter/sec RA = 300
14173 deg
ZDOT = -3386
455327 TA = 40
89256
MA = 40
78018
Ha = 192
542 n
mi
Hp = 181
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3599681
98 X = 1019992
07
Y = 16446922
37 feet Y = 5024859
91 meter
Z = 14218789
63 Z = 4339029
38
XDOT = -18182
305922 XDOT = -5571
518875
YDOT = 13617
962120 feet/sec YDOT = 4088
615885 meter/sec
ZDOT = -11110
417738 ZDOT = -3413
449813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7227569
97 X = -2202963
33
Y = 15186724
60 feet Y = 4628913
66 meter
Z = 14239331
89 Z = 4340148
36
XDOT = -21555
309871 XDOT = -6570
058449
YDOT = 295
251407 feet/sec YDOT = 89
992629 meter/sec
ZDOT = -11217
524746 ZDOT = -3419
101543
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 10084
43192853
00016717 00000-0 10270-3 0 9038
2 25544 51
6469 300
5886 0006068 104
5426 255
6410 15
73801971 10281
Satellite: ISS
Catalog Number: 25544
Epoch time: 10084
43192853 = yrday
fracday
Element set: 903
Inclination: 51
6469 deg
RA of node: 300
5886 deg
Eccentricity:
0006068
Arg of perigee: 104
5426 deg
Mean anomaly: 255
6410 deg
Mean motion: 15
73801971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1028
Checksum: 303
Coasting Arc #5 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2010/085/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4473378
44 A = 6729015
56 meter
Y = -4092459
47 meter E =
0018995
Z = 2902582
00 I = 51
34980
XDOT = 1822
051977 Wp = 89
98390
YDOT = 5563
883442 meter/sec RA = 295
03522 deg
ZDOT = 5008
426614 TA = 303
58297
MA = 303
76417
Ha = 192
505 n
mi
Hp = 181
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14676438
47 X = 4504708
57
Y = -13426704
28 feet Y = -4042260
10 meter
Z = 9522906
82 Z = 2924389
76
XDOT = 5977
860818 XDOT = 1735
370538
YDOT = 18254
210768 feet/sec YDOT = 5583
774423 meter/sec
ZDOT = 16431
845847 ZDOT = 5017
067052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19740032
44 X = 6016761
89
Y = -2085743
07 feet Y = -635734
49 meter
Z = 9609411
18 Z = 2928948
53
XDOT = -6292
765286 XDOT = -1918
034859
YDOT = 16729
452445 feet/sec YDOT = 5099
137105 meter/sec
ZDOT = 16466
303799 ZDOT = 5018
929398
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 10085
44789193
00016717 00000-0 10270-3 0 9040
2 25544 51
6470 295
3731 0006042 107
9796 252
2026 15
73801569 10449
Satellite: ISS
Catalog Number: 25544
Epoch time: 10085
44789193 = yrday
fracday
Element set: 904
Inclination: 51
6470 deg
RA of node: 295
3731 deg
Eccentricity:
0006042
Arg of perigee: 107
9796 deg
Mean anomaly: 252
2026 deg
Mean motion: 15
73801569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1044
Checksum: 313
Coasting Arc #6 (Orbit 1058)
---------------------------------------
Vector Time (GMT): 2010/086/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2052974
55 A = 6724179
93 meter
Y = -4672983
17 meter E =
0015127
Z = -4392820
68 I = 51
32205
XDOT = 4662
904579 Wp = 111
04024
YDOT = -5145
864842 meter/sec RA = 289
83123 deg
ZDOT = 3298
654997 TA = 192
28214
MA = 192
31906
Ha = 192
373 n
mi
Hp = 181
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6735480
82 X = -1979228
57
Y = -15331309
60 feet Y = -4695528
85 meter
Z = -14412141
34 Z = -4402614
32
XDOT = 15298
243370 XDOT = 4704
075927
YDOT = -16882
758668 feet/sec YDOT = -5093
490942 meter/sec
ZDOT = 10822
358914 ZDOT = 3321
407619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3501869
44 X = 1067369
81
Y = -16340940
51 feet Y = -4980718
67 meter
Z = -14451164
24 Z = -4404714
86
XDOT = 21018
508054 XDOT = 6406
441255
YDOT = -5135
311936 feet/sec YDOT = -1565
243078 meter/sec
ZDOT = 10912
580212 ZDOT = 3326
154449
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 10086
40033528
00016717 00000-0 10270-3 0 9052
2 25544 51
6468 290
4835 0005831 111
9797 248
1987 15
73853884 10591
Satellite: ISS
Catalog Number: 25544
Epoch time: 10086
40033528 = yrday
fracday
Element set: 905
Inclination: 51
6468 deg
RA of node: 290
4835 deg
Eccentricity:
0005831
Arg of perigee: 111
9797 deg
Mean anomaly: 248
1987 deg
Mean motion: 15
73853884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1059
Checksum: 337
Coasting Arc #7 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2010/087/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3662179
90 A = 6728902
25 meter
Y = 4853771
42 meter E =
0010295
Z = -2884391
63 I = 51
32860
XDOT = -2817
967578 Wp = 115
68895
YDOT = -5101
603765 meter/sec RA = 284
72195 deg
ZDOT = -5025
313364 TA = 97
60698
MA = 97
49003
Ha = 192
255 n
mi
Hp = 182
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12015025
93 X = -3702171
71
Y = 15924446
90 feet Y = 4812594
80 meter
Z = -9463227
15 Z = -2902280
07
XDOT = -9245
300453 XDOT = -2736
299210
YDOT = -16737
545160 feet/sec YDOT = -5132
659900 meter/sec
ZDOT = -16487
248568 ZDOT = -5038
803988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18882077
90 X = -5755257
34
Y = 6330008
81 feet Y = 1929386
69 meter
Z = -9534130
68 Z = -2906003
03
XDOT = 2422
779525 XDOT = 738
463199
YDOT = -17596
772291 feet/sec YDOT = -5363
496194 meter/sec
ZDOT = -16540
972057 ZDOT = -5041
688283
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 10087
41625399
00016717 00000-0 10270-3 0 9068
2 25544 51
6464 285
2675 0005716 117
0695 243
1052 15
73859201 10752
Satellite: ISS
Catalog Number: 25544
Epoch time: 10087
41625399 = yrday
fracday
Element set: 906
Inclination: 51
6464 deg
RA of node: 285
2675 deg
Eccentricity:
0005716
Arg of perigee: 117
0695 deg
Mean anomaly: 243
1052 deg
Mean motion: 15
73859201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 314
Coasting Arc #8 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2010/088/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2860823
52 A = 6723807
47 meter
Y = 4201901
56 meter E =
0013575
Z = 4389750
72 I = 51
30584
XDOT = -3662
099837 Wp = 87
19706
YDOT = 5934
223395 meter/sec RA = 279
51585 deg
ZDOT = -3284
286800 TA = 35
93639
MA = 35
84517
Ha = 191
982 n
mi
Hp = 181
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9385903
93 X = 2792299
89
Y = 13785766
26 feet Y = 4233510
37 meter
Z = 14402069
28 Z = 4403481
64
XDOT = -12014
763244 XDOT = -3712
230754
YDOT = 19469
236861 feet/sec YDOT = 5892
990933 meter/sec
ZDOT = -10775
219161 ZDOT = -3302
199722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 125265
91 X = 38181
05
Y = 16629779
63 feet Y = 5068756
83 meter
Z = 14456724
43 Z = 4406409
61
XDOT = -19511
415631 XDOT = -5947
079484
YDOT = 9602
524178 feet/sec YDOT = 2926
849369 meter/sec
ZDOT = -10846
181941 ZDOT = -3305
916256
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 10088
43214814
00016717 00000-0 10270-3 0 9078
2 25544 51
6463 280
0511 0005578 118
6857 241
4868 15
73966253 10916
Satellite: ISS
Catalog Number: 25544
Epoch time: 10088
43214814 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 280
0511 deg
Eccentricity:
0005578
Arg of perigee: 118
6857 deg
Mean anomaly: 241
4868 deg
Mean motion: 15
73966253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 318
Coasting Arc #9 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2010/089/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2711104
74 A = 6728745
64 meter
Y = -5449963
41 meter E =
0018006
Z = 2853430
37 I = 51
31768
XDOT = 3702
405440 Wp = 92
91583
YDOT = 4496
351146 meter/sec RA = 274
40422 deg
ZDOT = 5041
886485 TA = 300
02216
MA = 300
20069
Ha = 192
020 n
mi
Hp = 182
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8894700
59 X = 2757984
20
Y = -17880457
37 feet Y = -5419383
80 meter
Z = 9361648
20 Z = 2866715
43
XDOT = 12146
999474 XDOT = 3627
358577
YDOT = 14751
808222 feet/sec YDOT = 4537
334575 meter/sec
ZDOT = 16541
622325 ZDOT = 5059
690079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17078191
07 X = 5205432
64
Y = -10304092
74 feet Y = -3140687
47 meter
Z = 9414243
15 Z = 2869461
31
XDOT = 1455
298883 XDOT = 443
575099
YDOT = 17674
135619 feet/sec YDOT = 5387
076537 meter/sec
ZDOT = 16612
461762 ZDOT = 5063
478345
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 10089
44802193
00016717 00000-0 10270-3 0 9084
2 25544 51
6454 274
8342 0005540 122
3926 237
7774 15
73949174 11072
Satellite: ISS
Catalog Number: 25544
Epoch time: 10089
44802193 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 274
8342 deg
Eccentricity:
0005540
Arg of perigee: 122
3926 deg
Mean anomaly: 237
7774 deg
Mean motion: 15
73949174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 320
Coasting Arc #10 (Orbit 1121)
---------------------------------------
Vector Time (GMT): 2010/090/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3573540
77 A = 6723716
13 meter
Y = -3639081
41 meter E =
0014718
Z = -4396309
30 I = 51
29963
XDOT = 2543
695931 Wp = 116
59227
YDOT = -6467
530616 meter/sec RA = 269
19644 deg
ZDOT = 3287
911145 TA = 186
62601
MA = 186
64549
Ha = 191
906 n
mi
Hp = 181
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11724215
12 X = -3511225
66
Y = -11939243
47 feet Y = -3678694
82 meter
Z = -14423586
93 Z = -4413518
02
XDOT = 8345
459092 XDOT = 2599
855748
YDOT = -21218
932467 feet/sec YDOT = -6438
771207 meter/sec
ZDOT = 10787
110056 ZDOT = 3300
405489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3656243
50 X = -1114423
02
Y = -16268229
67 feet Y = -4958556
40 meter
Z = -14492039
25 Z = -4417173
56
XDOT = 16986
660287 XDOT = 5177
534055
YDOT = -13465
267104 feet/sec YDOT = -4104
213413 meter/sec
ZDOT = 10836
533447 ZDOT = 3302
975395
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 10090
40038052
00016717 00000-0 10270-3 0 9098
2 25544 51
6449 269
9429 0005481 126
7314 233
4353 15
73999640 11226
Satellite: ISS
Catalog Number: 25544
Epoch time: 10090
40038052 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 269
9429 deg
Eccentricity:
0005481
Arg of perigee: 126
7314 deg
Mean anomaly: 233
4353 deg
Mean motion: 15
73999640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1122
Checksum: 308
Coasting Arc #11 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2010/091/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1742853
53 A = 6728414
53 meter
Y = 5809512
01 meter E =
0009855
Z = -2912841
99 I = 51
31677
XDOT = -4423
537129 Wp = 122
94803
YDOT = -3826
681539 meter/sec RA = 264
08536 deg
ZDOT = -5002
883095 TA = 90
73367
MA = 90
62075
Ha = 191
784 n
mi
Hp = 182
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5718023
38 X = -1793536
80
Y = 19060078
78 feet Y = 5789738
83 meter
Z = -9556568
19 Z = -2921432
31
XDOT = -14512
917089 XDOT = -4356
114388
YDOT = -12554
729459 feet/sec YDOT = -3875
771482 meter/sec
ZDOT = -16413
658448 ZDOT = -5024
208839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14579694
01 X = -4443890
73
Y = 13519062
92 feet Y = 4120610
38 meter
Z = -9590508
35 Z = -2923186
94
XDOT = -5026
005525 XDOT = -1531
926484
YDOT = -17083
803579 feet/sec YDOT = -5207
143331 meter/sec
ZDOT = -16498
469133 ZDOT = -5028
733392
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 10091
41620771
00016717 00000-0 10270-3 0 9107
2 25544 51
6444 264
7266 0005401 130
9749 229
1882 15
74014891 11387
Satellite: ISS
Catalog Number: 25544
Epoch time: 10091
41620771 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 264
7266 deg
Eccentricity:
0005401
Arg of perigee: 130
9749 deg
Mean anomaly: 229
1882 deg
Mean motion: 15
74014891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 298
Coasting Arc #12 (Orbit 1153)
---------------------------------------
Vector Time (GMT): 2010/092/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4139606
28 A = 6723602
18 meter
Y = 3016196
15 meter E =
0012617
Z = 4344671
21 I = 51
30607
XDOT = -1410
057761 Wp = 92
16469
YDOT = 6790
715831 meter/sec RA = 258
87715 deg
ZDOT = -3362
879619 TA = 31
85964
MA = 31
78339
Ha = 191
491 n
mi
Hp = 182
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13581385
43 X = 4084465
17
Y = 9895656
67 feet Y = 3062179
53 meter
Z = 14254170
64 Z = 4364647
53
XDOT = -4626
173757 XDOT = -1469
551566
YDOT = 22279
251415 feet/sec YDOT = 6774
614960 meter/sec
ZDOT = -11033
069617 ZDOT = -3369
874488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6839193
08 X = 2084586
05
Y = 15275232
30 feet Y = 4655890
81 meter
Z = 14333602
05 Z = 4368881
91
XDOT = -13866
144738 XDOT = -4226
400916
YDOT = 16611
389865 feet/sec YDOT = 5063
151631 meter/sec
ZDOT = -11060
644797 ZDOT = -3371
284534
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 10092
43200992
00016717 00000-0 10270-3 0 9110
2 25544 51
6448 259
5093 0005260 134
7985 225
3607 15
74088594 11540
Satellite: ISS
Catalog Number: 25544
Epoch time: 10092
43200992 = yrday
fracday
Element set: 911
Inclination: 51
6448 deg
RA of node: 259
5093 deg
Eccentricity:
0005260
Arg of perigee: 134
7985 deg
Mean anomaly: 225
3607 deg
Mean motion: 15
74088594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1154
Checksum: 314
Coasting Arc #13 (Orbit 1169)
---------------------------------------
Vector Time (GMT): 2010/093/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 725457
30 A = 6728009
06 meter
Y = -5991140
98 meter E =
0016818
Z = 2962889
60 I = 51
32695
XDOT = 5028
995126 Wp = 98
19678
YDOT = 3074
383458 meter/sec RA = 253
76585 deg
ZDOT = 4958
887033 TA = 296
16993
MA = 296
34280
Ha = 191
498 n
mi
Hp = 182
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2380109
26 X = 778004
14
Y = -19655974
34 feet Y = -5982734
63 meter
Z = 9720766
39 Z = 2966541
62
XDOT = 16499
327842 XDOT = 4970
153551
YDOT = 10086
559900 feet/sec YDOT = 3130
291756 meter/sec
ZDOT = 16269
314412 ZDOT = 4983
175035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11461578
28 X = 3493489
06
Y = -16136164
93 feet Y = -4918303
07 meter
Z = 9735088
67 Z = 2967255
03
XDOT = 8383
035603 XDOT = 2555
149252
YDOT = 15880
283029 feet/sec YDOT = 4840
310267 meter/sec
ZDOT = 16365
879945 ZDOT = 4988
320207
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 10093
44778926
00016717 00000-0 10270-3 0 9120
2 25544 51
6436 254
2919 0005280 139
5058 220
6499 15
74120542 11707
Satellite: ISS
Catalog Number: 25544
Epoch time: 10093
44778926 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 254
2919 deg
Eccentricity:
0005280
Arg of perigee: 139
5058 deg
Mean anomaly: 220
6499 deg
Mean motion: 15
74120542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1170
Checksum: 311
Coasting Arc #14 (Orbit 1184)
---------------------------------------
Vector Time (GMT): 2010/094/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4619247
13 A = 6723674
79 meter
Y = -2352766
05 meter E =
0013701
Z = -4296355
60 I = 51
32136
XDOT = 279
250493 Wp = 122
46107
YDOT = -6861
783140 meter/sec RA = 248
55705 deg
ZDOT = 3458
188052 TA = 182
71336
MA = 182
72080
Ha = 191
469 n
mi
Hp = 182
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15155010
27 X = -4571723
82
Y = -7719048
71 feet Y = -2404155
53 meter
Z = -14095654
87 Z = -4318680
48
XDOT = 916
176159 XDOT = 339
160151
YDOT = -22512
411876 feet/sec YDOT = -6858
325393 meter/sec
ZDOT = 11345
761327 ZDOT = 3459
690231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9765609
12 X = -2976557
66
Y = -13834049
96 feet Y = -4216618
43 meter
Z = -14184409
59 Z = -4323408
04
XDOT = 10194
498896 XDOT = 3107
283263
YDOT = -18832
795343 feet/sec YDOT = -5740
236021 meter/sec
ZDOT = 11351
514513 ZDOT = 3459
941624
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 10094
40006121
00016717 00000-0 10270-3 0 9139
2 25544 51
6427 249
4000 0005354 141
7714 218
3830 15
74138091 11857
Satellite: ISS
Catalog Number: 25544
Epoch time: 10094
40006121 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 249
4000 deg
Eccentricity:
0005354
Arg of perigee: 141
7714 deg
Mean anomaly: 218
3830 deg
Mean motion: 15
74138091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1185
Checksum: 270
Coasting Arc #15 (Orbit 1200)
---------------------------------------
Vector Time (GMT): 2010/095/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 211180
40 A = 6727480
52 meter
Y = 5967502
84 meter E =
0009200
Z = -3098901
38 I = 51
34634
XDOT = -5502
252292 Wp = 126
17413
YDOT = -2319
708839 meter/sec RA = 243
44852 deg
ZDOT = -4857
359396 TA = 89
97213
MA = 89
86671
Ha = 191
320 n
mi
Hp = 182
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 692849
10 X = 159488
89
Y = 19578421
39 feet Y = 5969575
33 meter
Z = -10166999
27 Z = -3098001
08
XDOT = -18052
008831 XDOT = -5452
307834
YDOT = -7610
593305 feet/sec YDOT = -2380
959089 meter/sec
ZDOT = -15936
218491 ZDOT = -4883
967935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8116735
07 X = -2473980
85
Y = 17832269
35 feet Y = 5435275
70 meter
Z = -10163231
75 Z = -3097753
04
XDOT = -11329
374412 XDOT = -3453
193321
YDOT = -14270
942347 feet/sec YDOT = -4349
783227 meter/sec
ZDOT = -16041
999452 ZDOT = -4889
601433
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 10095
41579318
00016717 00000-0 10270-3 0 9145
2 25544 51
6423 244
1833 0005260 144
5252 215
6262 15
74182292 12013
Satellite: ISS
Catalog Number: 25544
Epoch time: 10095
41579318 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 244
1833 deg
Eccentricity:
0005260
Arg of perigee: 144
5252 deg
Mean anomaly: 215
6262 deg
Mean motion: 15
74182292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1201
Checksum: 282
Coasting Arc #16 (Orbit 1216)
---------------------------------------
Vector Time (GMT): 2010/096/09:22:05
671
Vector Time (MET): N/A
Weight (LBS) : 782571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4976460
83 A = 6723845
13 meter
Y = 1675492
39 meter E =
0012409
Z = 4188038
11 I = 51
34881
XDOT = 778
158165 Wp = 97
89660
YDOT = 6759
448020 meter/sec RA = 238
24036 deg
ZDOT = -3621
420384 TA = 29
12350
MA = 29
05436
Ha = 191
089 n
mi
Hp = 182
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16326971
24 X = 4937010
69
Y = 5497022
28 feet Y = 1730921
64 meter
Z = 13740282
51 Z = 4212117
77
XDOT = 2553
012353 XDOT = 720
107086
YDOT = 22176
666733 feet/sec YDOT = 6767
825196 meter/sec
ZDOT = -11881
300474 ZDOT = -3617
781250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12256908
85 X = 3735905
82
Y = 11996487
46 feet Y = 3656529
38 meter
Z = 13836006
70 Z = 4217214
84
XDOT = -6374
947848 XDOT = -1943
084104
YDOT = 20227
582120 feet/sec YDOT = 6165
367030 meter/sec
ZDOT = -11866
618659 ZDOT = -3616
945367
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 10096
43150034
00016717 00000-0 10270-3 0 9159
2 25544 51
6421 238
9653 0005255 149
9110 210
2356 15
74202859 12172
Satellite: ISS
Catalog Number: 25544
Epoch time: 10096
43150034 = yrday
fracday
Element set: 915
Inclination: 51
6421 deg
RA of node: 238
9653 deg
Eccentricity:
0005255
Arg of perigee: 149
9110 deg
Mean anomaly: 210
2356 deg
Mean motion: 15
74202859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1217
Checksum: 285
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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