Date:
March 15th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 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
There are no maneuvers
Coasting Arc #1 (Orbit 828)
---------------------------------------
Vector Time (GMT): 2010/071/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4426536
32 A = 6726348
51 meter
Y = 3384497
11 meter E =
0016731
Z = 3749800
32 I = 51
67738
XDOT = -5775
477932 Wp = 73
29757
YDOT = 2837
617272 meter/sec RA = 5
26755 deg
ZDOT = 4245
809799 TA = 332
07103
MA = 332
16073
Ha = 192
595 n
mi
Hp = 182
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14522756
95 X = 4370145
81
Y = 11103993
15 feet Y = 3433682
30 meter
Z = 12302494
47 Z = 3771166
71
XDOT = -18948
418411 XDOT = -5827
404372
YDOT = 9309
767952 feet/sec YDOT = 2772
742475 meter/sec
ZDOT = 13929
822174 ZDOT = 4217
626752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14071399
54 X = 4288962
58
Y = -11580485
02 feet Y = -3529731
84 meter
Z = 12387436
58 Z = 3775690
67
XDOT = 3944
143639 XDOT = 1202
174981
YDOT = 19610
961216 feet/sec YDOT = 5977
420979 meter/sec
ZDOT = 13817
927964 ZDOT = 4211
704443
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 10071
79849211
00016717 00000-0 10270-3 0 9007
2 25544 51
6465 5
4628 0007707 36
8111 323
3580 15
73865164 8294
Satellite: ISS
Catalog Number: 25544
Epoch time: 10071
79849211 = yrday
fracday
Element set: 900
Inclination: 51
6465 deg
RA of node: 5
4628 deg
Eccentricity:
0007707
Arg of perigee: 36
8111 deg
Mean anomaly: 323
3580 deg
Mean motion: 15
73865164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 829
Checksum: 305
Coasting Arc #2 (Orbit 843)
---------------------------------------
Vector Time (GMT): 2010/072/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4772598
01 A = 6726482
92 meter
Y = -2939515
38 meter E =
0011627
Z = -3723660
71 I = 51
64716
XDOT = 5418
717652 Wp = 66
65292
YDOT = 3394
643044 meter/sec RA =
08209 deg
ZDOT = 4280
407083 TA = 248
46781
MA = 248
59179
Ha = 192
675 n
mi
Hp = 181
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15658129
95 X = 4823202
02
Y = -9644079
35 feet Y = -2885862
79 meter
Z = -12216734
61 Z = -3700352
65
XDOT = 17777
945053 XDOT = 5359
562355
YDOT = 11137
280329 feet/sec YDOT = 3454
908043 meter/sec
ZDOT = 14043
330326 ZDOT = 4306
586696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6157126
01 X = -1876692
01
Y = -17393307
98 feet Y = -5301480
27 meter
Z = -12124213
00 Z = -3695460
12
XDOT = 13310
134775 XDOT = 4056
929080
YDOT = -14538
640797 feet/sec YDOT = -4431
377715 meter/sec
ZDOT = 14147
389277 ZDOT = 4312
124252
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 10072
75090078
00016717 00000-0 10270-3 0 9014
2 25544 51
6457
5723 0007606 41
3402 318
8336 15
73913726 8442
Satellite: ISS
Catalog Number: 25544
Epoch time: 10072
75090078 = yrday
fracday
Element set: 901
Inclination: 51
6457 deg
RA of node:
5723 deg
Eccentricity:
0007606
Arg of perigee: 41
3402 deg
Mean anomaly: 318
8336 deg
Mean motion: 15
73913726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 844
Checksum: 290
Coasting Arc #3 (Orbit 859)
---------------------------------------
Vector Time (GMT): 2010/073/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4978948
56 A = 6726101
72 meter
Y = -2547726
25 meter E =
0013309
Z = -3751924
97 I = 51
61588
XDOT = 5148
733044 Wp = 58
42994
YDOT = -3822
765380 meter/sec RA = 354
99914 deg
ZDOT = -4240
916591 TA = 166
86200
MA = 166
82730
Ha = 192
641 n
mi
Hp = 181
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16335133
08 X = -4931863
48
Y = -8358681
93 feet Y = -2603140
97 meter
Z = -12309465
11 Z = -3775997
69
XDOT = 16892
168780 XDOT = 5211
698533
YDOT = -12541
881169 feet/sec YDOT = -3764
837604 meter/sec
ZDOT = -13913
768342 ZDOT = -4215
751044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11317045
42 X = -3449435
44
Y = 14361901
34 feet Y = 4377507
53 meter
Z = -12405133
64 Z = -3781084
73
XDOT = -8014
281190 XDOT = -2442
752907
YDOT = -18235
215652 feet/sec YDOT = -5558
093731 meter/sec
ZDOT = -13813
893928 ZDOT = -4210
474869
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 10073
76678028
00016717 00000-0 10270-3 0 9024
2 25544 51
6452 355
3567 0007665 45
3233 314
8554 15
73955233 8600
Satellite: ISS
Catalog Number: 25544
Epoch time: 10073
76678028 = yrday
fracday
Element set: 902
Inclination: 51
6452 deg
RA of node: 355
3567 deg
Eccentricity:
0007665
Arg of perigee: 45
3233 deg
Mean anomaly: 314
8554 deg
Mean motion: 15
73955233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 860
Checksum: 318
Coasting Arc #4 (Orbit 875)
---------------------------------------
Vector Time (GMT): 2010/074/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4201365
30 A = 6726337
07 meter
Y = 3728558
85 meter E =
0018419
Z = 3690487
07 I = 51
58721
XDOT = -5925
753855 Wp = 70
37212
YDOT = -2398
562682 meter/sec RA = 349
80899 deg
ZDOT = -4299
326110 TA = 65
13935
MA = 64
94795
Ha = 192
609 n
mi
Hp = 181
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13784006
88 X = -4260674
00
Y = 12232804
61 feet Y = 3681245
50 meter
Z = 12107897
21 Z = 3669932
54
XDOT = -19441
449657 XDOT = -5877
607139
YDOT = -7869
300138 feet/sec YDOT = -2464
559290 meter/sec
ZDOT = -14105
400622 ZDOT = -4327
995900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9627895
70 X = 2934582
61
Y = 15776953
63 feet Y = 4808815
47 meter
Z = 12026341
41 Z = 3665628
86
XDOT = -9976
180283 XDOT = -3040
739750
YDOT = 16985
961696 feet/sec YDOT = 5177
321125 meter/sec
ZDOT = -14219
318813 ZDOT = -4334
048374
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 10074
78263419
00016717 00000-0 10270-3 0 9032
2 25544 51
6456 350
1400 0007464 48
3919 311
7883 15
73998303 8767
Satellite: ISS
Catalog Number: 25544
Epoch time: 10074
78263419 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 350
1400 deg
Eccentricity:
0007464
Arg of perigee: 48
3919 deg
Mean anomaly: 311
7883 deg
Mean motion: 15
73998303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 876
Checksum: 323
Coasting Arc #5 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2010/075/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5326346
48 A = 6725827
24 meter
Y = 1632001
23 meter E =
0017619
Z = 3751281
72 I = 51
55577
XDOT = -4424
336633 Wp = 80
07001
YDOT = 4688
443643 meter/sec RA = 344
72059 deg
ZDOT = 4228
502898 TA = 325
42228
MA = 325
53674
Ha = 192
425 n
mi
Hp = 181
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17474890
03 X = 5289478
33
Y = 5354334
74 feet Y = 1691357
90 meter
Z = 12307354
73 Z = 3777067
23
XDOT = -14515
540136 XDOT = -4496
976019
YDOT = 15382
032948 feet/sec YDOT = 4638
562426 meter/sec
ZDOT = 13873
041005 ZDOT = 4206
832597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8029033
90 X = 2447249
53
Y = -16341458
46 feet Y = -4980876
54 meter
Z = 12409795
01 Z = 3782505
52
XDOT = 11699
301249 XDOT = 3565
947021
YDOT = 16252
245759 feet/sec YDOT = 4953
684507 meter/sec
ZDOT = 13787
079884 ZDOT = 4202
301949
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 10075
79846469
00016717 00000-0 10270-3 0 9047
2 25544 51
6447 344
9234 0007409 53
4305 306
7539 15
74040359 8928
Satellite: ISS
Catalog Number: 25544
Epoch time: 10075
79846469 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node: 344
9234 deg
Eccentricity:
0007409
Arg of perigee: 53
4305 deg
Mean anomaly: 306
7539 deg
Mean motion: 15
74040359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 329
Coasting Arc #6 (Orbit 906)
---------------------------------------
Vector Time (GMT): 2010/076/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3501276
84 A = 6726213
52 meter
Y = -4422018
99 meter E =
0012304
Z = -3672102
39 I = 51
52822
XDOT = 6219
153868 Wp = 75
82058
YDOT = 1345
803098 meter/sec RA = 339
52565 deg
ZDOT = 4324
231987 TA = 240
00154
MA = 240
12371
Ha = 192
610 n
mi
Hp = 181
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11487128
74 X = 3568302
82
Y = -14507936
30 feet Y = -4382491
26 meter
Z = -12047580
03 Z = -3654929
93
XDOT = 20404
048123 XDOT = 6182
636314
YDOT = 4415
364495 feet/sec YDOT = 1415
145659 meter/sec
ZDOT = 14187
112818 ZDOT = 4354
355758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12740235
93 X = -3883223
91
Y = -13481728
06 feet Y = -4109230
71 meter
Z = -11979479
29 Z = -3651345
29
XDOT = 6244
066261 XDOT = 1903
191396
YDOT = -18569
151138 feet/sec YDOT = -5659
877267 meter/sec
ZDOT = 14306
769170 ZDOT = 4360
703243
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 10076
75078415
00016717 00000-0 10270-3 0 9053
2 25544 51
6447 340
0326 0007518 58
3280 301
8615 15
74058262 9074
Satellite: ISS
Catalog Number: 25544
Epoch time: 10076
75078415 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 340
0326 deg
Eccentricity:
0007518
Arg of perigee: 58
3280 deg
Mean anomaly: 301
8615 deg
Mean motion: 15
74058262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 907
Checksum: 301
Coasting Arc #7 (Orbit 922)
---------------------------------------
Vector Time (GMT): 2010/077/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5490227
14 A = 6725389
48 meter
Y = -748305
85 meter E =
0014016
Z = -3827154
25 I = 51
49849
XDOT = 3613
457041 Wp = 67
09332
YDOT = -5378
342738 meter/sec RA = 334
43311 deg
ZDOT = -4138
723302 TA = 159
47508
MA = 159
41871
Ha = 192
567 n
mi
Hp = 180
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18012556
23 X = -5462859
73
Y = -2455071
68 feet Y = -809548
16 meter
Z = -12556280
35 Z = -3853759
28
XDOT = 11855
174019 XDOT = 3693
435284
YDOT = -17645
481424 feet/sec YDOT = -5337
488109 meter/sec
ZDOT = -13578
488522 ZDOT = -4120
974333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4651304
24 X = -1417717
53
Y = 17498006
69 feet Y = 5333392
44 meter
Z = -12661945
58 Z = -3859361
01
XDOT = -14761
306764 XDOT = -4499
246302
YDOT = -13682
939797 feet/sec YDOT = -4170
560050 meter/sec
ZDOT = -13508
120372 ZDOT = -4117
275089
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 10077
76656622
00016717 00000-0 10270-3 0 9068
2 25544 51
6448 334
8162 0007633 61
8812 298
3122 15
74113781 9231
Satellite: ISS
Catalog Number: 25544
Epoch time: 10077
76656622 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 334
8162 deg
Eccentricity:
0007633
Arg of perigee: 61
8812 deg
Mean anomaly: 298
3122 deg
Mean motion: 15
74113781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 923
Checksum: 313
Coasting Arc #8 (Orbit 938)
---------------------------------------
Vector Time (GMT): 2010/078/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2793276
62 A = 6726363
10 meter
Y = 4964957
24 meter E =
0019313
Z = 3563650
10 I = 51
47402
XDOT = -6298
797526 Wp = 78
68688
YDOT = -350
355661 meter/sec RA = 329
23331 deg
ZDOT = -4425
092648 TA = 58
63343
MA = 58
44460
Ha = 192
572 n
mi
Hp = 181
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9164293
37 X = -2865899
69
Y = 16289229
78 feet Y = 4933315
35 meter
Z = 11691765
41 Z = 3549903
56
XDOT = -20665
346214 XDOT = -6272
915264
YDOT = -1149
460829 feet/sec YDOT = -420
648156 meter/sec
ZDOT = -14518
020499 ZDOT = -4455
629420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15214928
41 X = 4637510
18
Y = 10913307
22 feet Y = 3326376
04 meter
Z = 11637282
22 Z = 3547043
62
XDOT = -2536
619726 XDOT = -773
161693
YDOT = 19231
033389 feet/sec YDOT = 5861
618977 meter/sec
ZDOT = -14639
286995 ZDOT = -4462
054676
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 10078
78232359
00016717 00000-0 10270-3 0 9079
2 25544 51
6439 329
5985 0007444 66
2075 293
9868 15
74119106 9397
Satellite: ISS
Catalog Number: 25544
Epoch time: 10078
78232359 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 329
5985 deg
Eccentricity:
0007444
Arg of perigee: 66
2075 deg
Mean anomaly: 293
9868 deg
Mean motion: 15
74119106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 350
Coasting Arc #9 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2010/079/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5470627
09 A = 6724909
90 meter
Y = -126055
97 meter E =
0017895
Z = 3893236
50 I = 51
44519
XDOT = -2749
461287 Wp = 88
14873
YDOT = 5961
911271 meter/sec RA = 324
13570 deg
ZDOT = 4041
101190 TA = 319
69506
MA = 319
82757
Ha = 192
319 n
mi
Hp = 180
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17948251
61 X = 5452717
38
Y = -413569
45 feet Y = -64980
11 meter
Z = 12773085
63 Z = 3919769
39
XDOT = -9020
542281 XDOT = -2835
555096
YDOT = 19560
076348 feet/sec YDOT = 5930
683986 meter/sec
ZDOT = 13258
206005 ZDOT = 4027
534848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1183628
35 X = 360769
92
Y = -17838364
17 feet Y = -5437133
40 meter
Z = 12878442
45 Z = 3925349
26
XDOT = 17369
445828 XDOT = 5294
207089
YDOT = 10721
612764 feet/sec YDOT = 3267
947570 meter/sec
ZDOT = 13204
458002 ZDOT = 4024
718799
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 10079
79805509
00016717 00000-0 10270-3 0 9085
2 25544 51
6443 324
3813 0007393 70
5786 289
6176 15
74193653 9556
Satellite: ISS
Catalog Number: 25544
Epoch time: 10079
79805509 = yrday
fracday
Element set: 908
Inclination: 51
6443 deg
RA of node: 324
3813 deg
Eccentricity:
0007393
Arg of perigee: 70
5786 deg
Mean anomaly: 289
6176 deg
Mean motion: 15
74193653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 345
Coasting Arc #10 (Orbit 969)
---------------------------------------
Vector Time (GMT): 2010/080/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1998013
19 A = 6726376
70 meter
Y = -5410763
70 meter E =
0012387
Z = -3469343
60 I = 51
42747
XDOT = 6190
671724 Wp = 81
54387
YDOT = -606
296240 meter/sec RA = 318
93293 deg
ZDOT = 4526
367941 TA = 237
21127
MA = 237
33065
Ha = 192
470 n
mi
Hp = 180
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6555161
39 X = 2075222
27
Y = -17751849
41 feet Y = -5387989
15 meter
Z = -11382360
90 Z = -3459449
53
XDOT = 20310
602768 XDOT = 6175
003042
YDOT = -1989
160894 feet/sec YDOT = -537
155930 meter/sec
ZDOT = 14850
288519 ZDOT = 4556
404196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17228396
60 X = -5251215
28
Y = -7884857
68 feet Y = -2403304
62 meter
Z = -11343183
32 Z = -3457402
28
XDOT = -1100
337298 XDOT = -335
382808
YDOT = -19057
351534 feet/sec YDOT = -5808
680747 meter/sec
ZDOT = 14969
548381 ZDOT = 4562
718347
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 10080
75028216
00016717 00000-0 10270-3 0 9096
2 25544 51
6454 319
4905 0007502 74
2874 285
9117 15
74211161 9702
Satellite: ISS
Catalog Number: 25544
Epoch time: 10080
75028216 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 319
4905 deg
Eccentricity:
0007502
Arg of perigee: 74
2874 deg
Mean anomaly: 285
9117 deg
Mean motion: 15
74211161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 970
Checksum: 302
Coasting Arc #11 (Orbit 985)
---------------------------------------
Vector Time (GMT): 2010/081/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5316874
42 A = 6724279
62 meter
Y = 886677
97 meter E =
0014883
Z = -4035320
57 I = 51
39916
XDOT = 1858
546381 Wp = 73
84013
YDOT = -6384
908652 meter/sec RA = 313
83115 deg
ZDOT = -3859
449034 TA = 156
23103
MA = 156
16222
Ha = 192
381 n
mi
Hp = 180
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17443813
71 X = -5306791
46
Y = 2909048
45 feet Y = 827277
80 meter
Z = -13239240
72 Z = -4061125
38
XDOT = 6097
593114 XDOT = 1948
553877
YDOT = -20947
863030 feet/sec YDOT = -6363
622113 meter/sec
ZDOT = -12662
234363 ZDOT = -3850
201473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1950228
78 X = 594429
73
Y = 17499213
93 feet Y = 5333760
41 meter
Z = -13341694
56 Z = -4066548
50
XDOT = -19301
358395 XDOT = -5883
054039
YDOT = -7455
803262 feet/sec YDOT = -2272
528834 meter/sec
ZDOT = -12625
645273 ZDOT = -3848
296679
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
76596552
00016717 00000-0 10270-3 0 9103
2 25544 51
6455 314
2732 0007457 77
4382 282
7615 15
74253283 9868
Satellite: ISS
Catalog Number: 25544
Epoch time: 10081
76596552 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 314
2732 deg
Eccentricity:
0007457
Arg of perigee: 77
4382 deg
Mean anomaly: 282
7615 deg
Mean motion: 15
74253283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 986
Checksum: 325
Coasting Arc #12 (Orbit 1001)
---------------------------------------
Vector Time (GMT): 2010/082/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1231072
26 A = 6726750
53 meter
Y = 5734316
08 meter E =
0020125
Z = 3277600
89 I = 51
38721
XDOT = -5941
048739 Wp = 87
89938
YDOT = 1424
517736 meter/sec RA = 308
62465 deg
ZDOT = -4698
211307 TA = 53
46809
MA = 53
28295
Ha = 192
374 n
mi
Hp = 180
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4038950
99 X = -1311024
77
Y = 18813372
98 feet Y = 5720102
54 meter
Z = 10753283
76 Z = 3271426
05
XDOT = -19491
629721 XDOT = -5933
713522
YDOT = 4673
614618 feet/sec YDOT = 1358
122299 meter/sec
ZDOT = -15414
079092 ZDOT = -4727
054902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18645321
46 X = 5683093
98
Y = 4809596
28 feet Y = 1465964
95 meter
Z = 10728886
75 Z = 3270164
68
XDOT = 4288
088256 XDOT = 1307
009300
YDOT = 18203
595427 feet/sec YDOT = 5548
455886 meter/sec
ZDOT = -15528
591830 ZDOT = -4733
114790
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
78162440
00016717 00000-0 10270-3 0 9112
2 25544 51
6453 309
0552 0007418 81
8225 278
3780 15
74271569 10021
Satellite: ISS
Catalog Number: 25544
Epoch time: 10082
78162440 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 309
0552 deg
Eccentricity:
0007418
Arg of perigee: 81
8225 deg
Mean anomaly: 278
3780 deg
Mean motion: 15
74271569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1002
Checksum: 297
Coasting Arc #13 (Orbit 1017)
---------------------------------------
Vector Time (GMT): 2010/083/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5031562
33 A = 6723511
96 meter
Y = -1576055
52 meter E =
0017188
Z = 4158653
23 I = 51
36052
XDOT = -936
416590 Wp = 97
08533
YDOT = 6717
811988 meter/sec RA = 303
51907 deg
ZDOT = 3663
889654 TA = 315
36670
MA = 315
50494
Ha = 192
082 n
mi
Hp = 180
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16507750
42 X = 5028610
36
Y = -5170785
83 feet Y = -1519805
95 meter
Z = 13643875
43 Z = 4183089
15
XDOT = -3072
232906 XDOT = -1029
265066
YDOT = 22040
065577 feet/sec YDOT = 6706
821410 meter/sec
ZDOT = 12020
635349 ZDOT = 3659
114829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4831553
88 X = -1472657
62
Y = -16530045
85 feet Y = -5038357
98 meter
Z = 13740882
71 Z = 4188221
05
XDOT = 20765
669930 XDOT = 6329
376195
YDOT = 3947
799433 feet/sec YDOT = 1203
289267 meter/sec
ZDOT = 12001
827020 ZDOT = 3658
156876
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
79725580
00016717 00000-0 10270-3 0 9125
2 25544 51
6464 303
8381 0007284 85
3304 274
8691 15
74357265 10180
Satellite: ISS
Catalog Number: 25544
Epoch time: 10083
79725580 = yrday
fracday
Element set: 912
Inclination: 51
6464 deg
RA of node: 303
8381 deg
Eccentricity:
0007284
Arg of perigee: 85
3304 deg
Mean anomaly: 274
8691 deg
Mean motion: 15
74357265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1018
Checksum: 319
Coasting Arc #14 (Orbit 1032)
---------------------------------------
Vector Time (GMT): 2010/084/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 402177
82 A = 6727017
07 meter
Y = -5963633
96 meter E =
0011774
Z = -3094691
57 I = 51
35668
XDOT = 5566
459506 Wp = 82
60181
YDOT = -2138
158423 meter/sec RA = 298
31172 deg
ZDOT = 4861
042892 TA = 241
33549
MA = 241
45393
Ha = 192
213 n
mi
Hp = 180
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1319481
04 X = 483867
59
Y = -19565728
20 feet Y = -5958679
99 meter
Z = -10153187
57 Z = -3092539
05
XDOT = 18262
662421 XDOT = 5566
341334
YDOT = -7014
955455 feet/sec YDOT = -2075
911342 meter/sec
ZDOT = 15948
303450 ZDOT = 4888
084198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19561218
95 X = -5962259
54
Y = -1444996
10 feet Y = -440434
81 meter
Z = -10144785
23 Z = -3092130
54
XDOT = -7058
798465 XDOT = -2151
521772
YDOT = -16765
575909 feet/sec YDOT = -5110
147537 meter/sec
ZDOT = 16055
644161 ZDOT = 4893
760340
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
74938943
00016717 00000-0 10270-3 0 9131
2 25544 51
6465 298
9473 0007312 87
5273 272
6728 15
74350596 10332
Satellite: ISS
Catalog Number: 25544
Epoch time: 10084
74938943 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 298
9473 deg
Eccentricity:
0007312
Arg of perigee: 87
5273 deg
Mean anomaly: 272
6728 deg
Mean motion: 15
74350596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1033
Checksum: 337
Coasting Arc #15 (Orbit 1048)
---------------------------------------
Vector Time (GMT): 2010/085/17:50:00
074
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4688873
43 A = 6722749
26 meter
Y = 2105348
49 meter E =
0016050
Z = -4348650
67 I = 51
32954
XDOT = 21
825009 Wp = 78
99488
YDOT = -6908
104323 meter/sec RA = 293
20117 deg
ZDOT = -3375
540272 TA = 156
82574
MA = 156
75329
Ha = 192
102 n
mi
Hp = 180
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15383443
01 X = -4690942
66
Y = 6907311
33 feet Y = 2052902
79 meter
Z = -14267226
62 Z = -4371434
10
XDOT = 71
604360 XDOT = 115
468580
YDOT = -22664
384262 feet/sec YDOT = -6907
336957 meter/sec
ZDOT = -11074
607193 ZDOT = -3375
206212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7118028
49 X = 2169575
08
Y = 15202184
65 feet Y = 4633625
88 meter
Z = -14357655
67 Z = -4376213
45
XDOT = -21555
805974 XDOT = -6570
209661
YDOT = -342
165184 feet/sec YDOT = -104
291948 meter/sec
ZDOT = -11073
461699 ZDOT = -3375
191126
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
76497264
00016717 00000-0 10270-3 0 9141
2 25544 51
6465 293
7293 0007221 91
8351 268
3640 15
74392762 10492
Satellite: ISS
Catalog Number: 25544
Epoch time: 10085
76497264 = yrday
fracday
Element set: 914
Inclination: 51
6465 deg
RA of node: 293
7293 deg
Eccentricity:
0007221
Arg of perigee: 91
8351 deg
Mean anomaly: 268
3640 deg
Mean motion: 15
74392762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1049
Checksum: 327
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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