Date:
February 19th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 30138 95 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
049/06:58:00
000 0
0 0
0 0
0
N/A 0
0 0
0 188
7
000/00:00:00
000 0
0 0
0 180
1
049/07:11:30
000 0
0 0
7 0
7
N/A 0
7 -0
2 188
8
000/00:05:00
000 -0
2 -0
1 180
6
049/07:47:30
000 -0
5 1
7 1
7
N/A -1
3 0
2 190
3
000/00:33:00
000 1
0 0
1 180
7
049/08:11:30
000 0
2 0
4 0
5
N/A -0
5 0
0 190
4
000/00:05:00
000 -0
0 -0
3 180
8
Coasting Arc #1 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2010/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4823079
59 A = 6724106
20 meter
Y = 4163548
18 meter E =
0017784
Z = 2111130
88 I = 51
93738
XDOT = -1875
956397 Wp = 30
47605
YDOT = -4998
315291 meter/sec RA = 124
15996 deg
ZDOT = 5566
565941 TA = 353
06917
MA = 353
09373
Ha = 188
711 n
mi
Hp = 180
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15823751
93 X = -4879533
98
Y = 13659934
96 feet Y = 4109298
13 meter
Z = 6926282
40 Z = 2087563
33
XDOT = -6154
712587 XDOT = -1846
965842
YDOT = -16398
672215 feet/sec YDOT = -5019
130865 meter/sec
ZDOT = 18263
011616 ZDOT = 5557
523465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20764470
96 X = -6329010
75
Y = 2665879
03 feet Y = 812559
93 meter
Z = 6832874
28 Z = 2082660
08
XDOT = 3997
949528 XDOT = 1218
575016
YDOT = -15621
967169 feet/sec YDOT = -4761
575593 meter/sec
ZDOT = 18226
913248 ZDOT = 5555
563158
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 10048
55930847
00016717 00000-0 10270-3 0 9001
2 25544 51
6457 124
7558 0011285 338
0399 22
0280 15
76175425 4634
Satellite: ISS
Catalog Number: 25544
Epoch time: 10048
55930847 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 124
7558 deg
Eccentricity:
0011285
Arg of perigee: 338
0399 deg
Mean anomaly: 22
0280 deg
Mean motion: 15
76175425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 309
Coasting Arc #2 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2010/049/06:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010367
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3988899
09 A = 6725380
00 meter
Y = -5324669
13 meter E =
0003916
Z = -998767
65 I = 51
95220
XDOT = 3303
890017 Wp = 42
32282
YDOT = 3589
539942 meter/sec RA = 120
09096 deg
ZDOT = -5952
147430 TA = 148
54351
MA = 148
52009
Ha = 188
678 n
mi
Hp = 180
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13086939
27 X = 4052995
79
Y = -17469386
92 feet Y = -5279704
58 meter
Z = -3276796
76 Z = -979233
81
XDOT = 10839
534176 XDOT = 3292
419656
YDOT = 11776
705846 feet/sec YDOT = 3626
421477 meter/sec
ZDOT = -19528
042750 ZDOT = -5936
125449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12522132
97 X = 3816746
13
Y = 17892585
34 feet Y = 5453660
01 meter
Z = -3199442
40 Z = -975190
04
XDOT = -13296
150491 XDOT = -4052
666670
YDOT = 5831
198215 feet/sec YDOT = 1777
349216 meter/sec
ZDOT = -19464
289865 ZDOT = -5932
715551
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 10049
32012087
00016717 00000-0 10270-3 0 9015
2 25544 51
6427 120
8321 0011254 341
8518 18
2243 15
76242531 4759
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
32012087 = yrday
fracday
Element set: 901
Inclination: 51
6427 deg
RA of node: 120
8321 deg
Eccentricity:
0011254
Arg of perigee: 341
8518 deg
Mean anomaly: 18
2243 deg
Mean motion: 15
76242531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 268
Coasting Arc #3 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2010/049/07:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010288
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4385792
67 A = 6715065
61 meter
Y = 371799
81 meter E =
0016259
Z = -5082613
07 I = 51
91712
XDOT = -2559
527386 Wp = 35
02435
YDOT = 7058
979036 meter/sec RA = 120
03925 deg
ZDOT = -1681
863129 TA = 218
79498
MA = 218
91182
Ha = 188
768 n
mi
Hp = 180
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14389083
56 X = 4405999
26
Y = 1219815
66 feet Y = 420957
00 meter
Z = -16675239
74 Z = -5061258
13
XDOT = -8397
399559 XDOT = -2630
101836
YDOT = 23159
380038 feet/sec YDOT = 7029
962169 meter/sec
ZDOT = -5517
923653 ZDOT = -1694
469027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4717840
27 X = -1437997
71
Y = 13751244
05 feet Y = 4191379
19 meter
Z = -16590435
99 Z = -5056764
89
XDOT = -19415
008012 XDOT = -5917
694442
YDOT = -13419
553649 feet/sec YDOT = -4090
279952 meter/sec
ZDOT = -5567
704239 ZDOT = -1697
036252
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 10049
32012214
00016717 00000-0 10270-3 0 9028
2 25544 51
6436 120
8330 0011061 339
2342 20
8371 15
76106210 4755
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
32012214 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 120
8330 deg
Eccentricity:
0011061
Arg of perigee: 339
2342 deg
Mean anomaly: 20
8371 deg
Mean motion: 15
76106210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 247
Coasting Arc #4 (Orbit 475)
---------------------------------------
Vector Time (GMT): 2010/049/08:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 1009763
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3523678
22 A = 6715666
85 meter
Y = -2181563
49 meter E =
0012240
Z = 5285293
08 I = 51
91465
XDOT = 3912
953601 Wp = 356
08896
YDOT = -6634
459005 meter/sec RA = 119
84525 deg
ZDOT = -117
764109 TA = 95
09381
MA = 94
95409
Ha = 190
303 n
mi
Hp = 180
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11560624
09 X = -3524696
36
Y = -7157360
54 feet Y = -2220972
70 meter
Z = 17340200
40 Z = 5268172
95
XDOT = 12837
774281 XDOT = 3987
422549
YDOT = -21766
597784 feet/sec YDOT = -6590
285665 meter/sec
ZDOT = -386
365188 ZDOT = -98
573925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7477908
50 X = 2279266
51
Y = -11459162
37 feet Y = -3492752
69 meter
Z = 17272141
48 Z = 5264548
72
XDOT = 20566
214078 XDOT = 6268
582051
YDOT = 12893
743955 feet/sec YDOT = 3930
013157 meter/sec
ZDOT = -310
425081 ZDOT = -94
617565
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 10049
38354930
00016717 00000-0 10270-3 0 9039
2 25544 51
6438 120
5055 0012440 345
0056 15
0738 15
75555283 4768
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
38354930 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 120
5055 deg
Eccentricity:
0012440
Arg of perigee: 345
0056 deg
Mean anomaly: 15
0738 deg
Mean motion: 15
75555283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 476
Checksum: 291
Coasting Arc #5 (Orbit 475)
---------------------------------------
Vector Time (GMT): 2010/049/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 1009683
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -556936
07 A = 6721062
56 meter
Y = -5361710
80 meter E =
0016059
Z = 4017867
97 I = 51
93186
XDOT = 5583
937523 Wp = 29
11840
YDOT = -3546
476989 meter/sec RA = 119
78539 deg
ZDOT = -3938
359176 TA = 101
49781
MA = 101
31743
Ha = 190
364 n
mi
Hp = 180
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1827218
09 X = -516456
89
Y = -17590914
69 feet Y = -5367712
20 meter
Z = 13181981
53 Z = 4015261
08
XDOT = 18320
004997 XDOT = 5642
311429
YDOT = -11635
423191 feet/sec YDOT = -3483
707955 meter/sec
ZDOT = -12921
125907 ZDOT = -3911
090757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17557901
42 X = 5351648
35
Y = -2185701
91 feet Y = -666201
94 meter
Z = 13171425
42 Z = 4014650
47
XDOT = 11769
028683 XDOT = 3587
199943
YDOT = 16926
835874 feet/sec YDOT = 5159
299574 meter/sec
ZDOT = -12812
992764 ZDOT = -3905
400194
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 10049
38355316
00016717 00000-0 10270-3 0 9049
2 25544 51
6437 120
5059 0012105 346
6235 13
4606 15
75443026 4762
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
38355316 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 120
5059 deg
Eccentricity:
0012105
Arg of perigee: 346
6235 deg
Mean anomaly: 13
4606 deg
Mean motion: 15
75443026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 476
Checksum: 285
Coasting Arc #6 (Orbit 491)
---------------------------------------
Vector Time (GMT): 2010/050/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4653267
69 A = 6721541
90 meter
Y = 2985747
48 meter E =
0014038
Z = 3805931
20 I = 51
94910
XDOT = -675
404535 Wp = 41
93051
YDOT = -6422
779621 meter/sec RA = 114
71130 deg
ZDOT = 4214
260234 TA = 4
12912
MA = 4
11755
Ha = 190
482 n
mi
Hp = 180
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15266626
28 X = -4704797
34
Y = 9795759
45 feet Y = 2933423
96 meter
Z = 12486650
93 Z = 3783200
54
XDOT = -2215
894145 XDOT = -624
005579
YDOT = -21072
111619 feet/sec YDOT = -6430
044786 meter/sec
ZDOT = 13826
313104 ZDOT = 4211
104339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10299756
48 X = -3139365
77
Y = -15006162
13 feet Y = -4573878
22 meter
Z = 12396505
44 Z = 3778454
86
XDOT = 19889
677633 XDOT = 6062
373743
YDOT = -2244
103894 feet/sec YDOT = -684
002867 meter/sec
ZDOT = 13813
544992 ZDOT = 4210
368513
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 10050
39842192
00016717 00000-0 10270-3 0 9056
2 25544 51
6445 115
2827 0012177 350
2367 9
8559 15
75546767 4921
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
39842192 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 115
2827 deg
Eccentricity:
0012177
Arg of perigee: 350
2367 deg
Mean anomaly: 9
8559 deg
Mean motion: 15
75546767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 492
Checksum: 321
Coasting Arc #7 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2010/051/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 661077
70 A = 6723102
89 meter
Y = 5822223
61 meter E =
0013141
Z = -3285388
05 I = 51
96591
XDOT = -5108
304857 Wp = 14
94267
YDOT = 3257
643524 meter/sec RA = 109
53610 deg
ZDOT = 4761
769600 TA = 306
67475
MA = 306
79546
Ha = 190
621 n
mi
Hp = 180
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2168890
09 X = 611883
11
Y = 19101783
51 feet Y = 5829340
99 meter
Z = -10778832
19 Z = -3282296
27
XDOT = -16759
530372 XDOT = -5167
484355
YDOT = 10687
806838 feet/sec YDOT = 3200
188712 meter/sec
ZDOT = 15622
603674 ZDOT = 4736
809815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18964831
02 X = -5780480
49
Y = 3191604
70 feet Y = 972801
11 meter
Z = -10766349
65 Z = -3281583
37
XDOT = -11290
746018 XDOT = -3441
419386
YDOT = -14908
282021 feet/sec YDOT = -4544
044360 meter/sec
ZDOT = 15523
606712 ZDOT = 4731
595326
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 10051
34983636
00016717 00000-0 10270-3 0 9062
2 25544 51
6445 110
3867 0012395 353
8504 6
2506 15
75536865 5073
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051
34983636 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 110
3867 deg
Eccentricity:
0012395
Arg of perigee: 353
8504 deg
Mean anomaly: 6
2506 deg
Mean motion: 15
75536865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 309
Coasting Arc #8 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2010/052/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4290436
05 A = 6719044
44 meter
Y = -2618728
36 meter E =
0017796
Z = -4474438
60 I = 51
96201
XDOT = 834
121883 Wp = 28
62061
YDOT = 6923
313561 meter/sec RA = 104
46036 deg
ZDOT = -3242
163092 TA = 208
96640
MA = 209
06528
Ha = 190
603 n
mi
Hp = 179
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14076233
75 X = 4341136
06
Y = -8591628
48 feet Y = -2570466
77 meter
Z = -14679916
65 Z = -4453472
66
XDOT = 2736
620350 XDOT = 772
391860
YDOT = 22714
283336 feet/sec YDOT = 6932
295995 meter/sec
ZDOT = -10637
018017 ZDOT = -3238
261038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9528976
07 X = 2904431
91
Y = 13549538
53 feet Y = 4129899
34 meter
Z = -14596746
56 Z = -4449088
35
XDOT = -21485
035897 XDOT = -6548
638941
YDOT = 3632
100155 feet/sec YDOT = 1107
064127 meter/sec
ZDOT = -10621
289707 ZDOT = -3237
369103
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 10052
36464737
00016717 00000-0 10270-3 0 9072
2 25544 51
6449 105
1634 0012267 357
8805 2
2305 15
75595725 5238
Satellite: ISS
Catalog Number: 25544
Epoch time: 10052
36464737 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 105
1634 deg
Eccentricity:
0012267
Arg of perigee: 357
8805 deg
Mean anomaly: 2
2305 deg
Mean motion: 15
75595725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 523
Checksum: 304
Coasting Arc #9 (Orbit 538)
---------------------------------------
Vector Time (GMT): 2010/053/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -822431
37 A = 6725146
56 meter
Y = -6255345
18 meter E =
0016125
Z = 2330814
80 I = 51
98939
XDOT = 4746
547945 Wp = 59
55376
YDOT = -2665
354326 meter/sec RA = 99
29259 deg
ZDOT = -5442
623206 TA = 94
35322
MA = 94
16896
Ha = 190
678 n
mi
Hp = 179
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2698265
63 X = -763744
40
Y = -20522786
01 feet Y = -6264213
95 meter
Z = 7647030
20 Z = 2326962
05
XDOT = 15572
663861 XDOT = 4802
438598
YDOT = -8744
600806 feet/sec YDOT = -2611
963126 meter/sec
ZDOT = -17856
375347 ZDOT = -5419
428989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20216512
88 X = 6161993
13
Y = -4471557
62 feet Y = -1362930
76 meter
Z = 7631528
89 Z = 2326090
01
XDOT = 9715
391106 XDOT = 2961
251209
YDOT = 13406
079649 feet/sec YDOT = 4086
173077 meter/sec
ZDOT = -17764
346823 ZDOT = -5414
572912
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 10053
37942757
00016717 00000-0 10270-3 0 9088
2 25544 51
6448 99
9402 0012283 2
5263 357
5961 15
75644840 5394
Satellite: ISS
Catalog Number: 25544
Epoch time: 10053
37942757 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 99
9402 deg
Eccentricity:
0012283
Arg of perigee: 2
5263 deg
Mean anomaly: 357
5961 deg
Mean motion: 15
75644840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 539
Checksum: 326
Coasting Arc #10 (Orbit 554)
---------------------------------------
Vector Time (GMT): 2010/054/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4044290
27 A = 6716548
56 meter
Y = 1995750
09 meter E =
0010907
Z = 4969082
77 I = 51
96572
XDOT = -1086
021132 Wp = 35
40928
YDOT = -7346
757295 meter/sec RA = 94
20502 deg
ZDOT = 2073
255402 TA = 34
66526
MA = 34
59421
Ha = 190
796 n
mi
Hp = 179
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13268668
86 X = -4090445
04
Y = 6547736
51 feet Y = 1950266
34 meter
Z = 16302764
98 Z = 4949323
83
XDOT = -3563
061457 XDOT = -1013
859009
YDOT = -24103
534434 feet/sec YDOT = -7358
498363 meter/sec
ZDOT = 6802
019037 ZDOT = 2068
154823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7874923
51 X = -2400276
69
Y = -12628010
95 feet Y = -3849017
74 meter
Z = 16224348
74 Z = 4945181
50
XDOT = 22690
359457 XDOT = 6916
021563
YDOT = -5464
365110 feet/sec YDOT = -1665
538486 meter/sec
ZDOT = 6781
535108 ZDOT = 2067
011901
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 10054
39417450
00016717 00000-0 10270-3 0 9099
2 25544 51
6456 94
7160 0012343 6
1084 354
0229 15
75735803 5552
Satellite: ISS
Catalog Number: 25544
Epoch time: 10054
39417450 = yrday
fracday
Element set: 909
Inclination: 51
6456 deg
RA of node: 94
7160 deg
Eccentricity:
0012343
Arg of perigee: 6
1084 deg
Mean anomaly: 354
0229 deg
Mean motion: 15
75735803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 555
Checksum: 295
Coasting Arc #11 (Orbit 569)
---------------------------------------
Vector Time (GMT): 2010/055/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1089562
48 A = 6726617
17 meter
Y = 6505717
43 meter E =
0021087
Z = -1256793
50 I = 52
00048
XDOT = -4582
193819 Wp = 21
24540
YDOT = 1898
437781 meter/sec RA = 89
05306 deg
ZDOT = 5904
399883 TA = 325
01491
MA = 325
15328
Ha = 190
921 n
mi
Hp = 178
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3574680
06 X = 1022838
56
Y = 21344217
30 feet Y = 6517528
50 meter
Z = -4123338
26 Z = -1251662
54
XDOT = -15033
444289 XDOT = -4631
763829
YDOT = 6228
470410 feet/sec YDOT = 1846
919769 meter/sec
ZDOT = 19371
390692 ZDOT = 5882
019669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20764661
29 X = -6329068
76
Y = 6111631
39 feet Y = 1862825
25 meter
Z = -4102763
86 Z = -1250522
43
XDOT = -7540
396042 XDOT = -2298
312714
YDOT = -12784
596387 feet/sec YDOT = -3896
744979 meter/sec
ZDOT = 19282
550916 ZDOT = 5877
321519
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 10055
34547363
00016717 00000-0 10270-3 0 9104
2 25544 51
6457 89
8197 0012591 9
6324 350
5079 15
75715904 5709
Satellite: ISS
Catalog Number: 25544
Epoch time: 10055
34547363 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 89
8197 deg
Eccentricity:
0012591
Arg of perigee: 9
6324 deg
Mean anomaly: 350
5079 deg
Mean motion: 15
75715904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 570
Checksum: 317
Coasting Arc #12 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2010/056/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4003046
11 A = 6715211
45 meter
Y = -1263023
20 meter E =
0022217
Z = -5258036
52 I = 51
96021
XDOT = 1383
433562 Wp = 52
26315
YDOT = 7527
572689 meter/sec RA = 83
94698 deg
ZDOT = -743
794102 TA = 210
61737
MA = 210
74722
Ha = 190
869 n
mi
Hp = 178
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13133353
38 X = 4042413
87
Y = -4143776
91 feet Y = -1218038
68 meter
Z = -17250775
99 Z = -5238494
60
XDOT = 4538
824021 XDOT = 1302
769210
YDOT = 24696
760790 feet/sec YDOT = 7542
592041 meter/sec
ZDOT = -2440
269362 ZDOT = -737
269533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5905385
16 X = 1799961
40
Y = 12548039
03 feet Y = 3824642
30 meter
Z = -17173184
71 Z = -5234386
70
XDOT = -22933
122787 XDOT = -6990
015825
YDOT = 7438
553594 feet/sec YDOT = 2267
271135 meter/sec
ZDOT = -2414
130844 ZDOT = -735
827081
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 10056
36016088
00016717 00000-0 10270-3 0 9113
2 25544 51
6450 84
5960 0012442 13
4084 346
7409 15
75782630 5864
Satellite: ISS
Catalog Number: 25544
Epoch time: 10056
36016088 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 84
5960 deg
Eccentricity:
0012442
Arg of perigee: 13
4084 deg
Mean anomaly: 346
7409 deg
Mean motion: 15
75782630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 586
Checksum: 301
Coasting Arc #13 (Orbit 601)
---------------------------------------
Vector Time (GMT): 2010/057/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1310864
23 A = 6726906
53 meter
Y = -6600170
92 meter E =
0013003
Z = 7281
20 I = 51
99522
XDOT = 4644
206798 Wp = 75
38333
YDOT = -938
956516 meter/sec RA = 78
81508 deg
ZDOT = -6063
488510 TA = 104
53799
MA = 104
39372
Ha = 190
888 n
mi
Hp = 178
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4300735
68 X = -1236997
89
Y = -21654104
08 feet Y = -6614416
78 meter
Z = 23888
46 Z = 1092
84
XDOT = 15236
898942 XDOT = 4683
815679
YDOT = -3080
565996 feet/sec YDOT = -886
800970 meter/sec
ZDOT = -19893
335008 ZDOT = -6040
831380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20741079
38 X = 6321881
00
Y = -7563381
97 feet Y = -2305318
82 meter
Z = -887
60 Z = -270
54
XDOT = 4842
417000 XDOT = 1475
968702
YDOT = 13188
905763 feet/sec YDOT = 4019
978477 meter/sec
ZDOT = -19803
353986 ZDOT = -6036
062295
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 10057
37481627
00016717 00000-0 10270-3 0 9121
2 25544 51
6442 79
3715 0012507 18
0929 342
0678 15
75850600 6025
Satellite: ISS
Catalog Number: 25544
Epoch time: 10057
37481627 = yrday
fracday
Element set: 912
Inclination: 51
6442 deg
RA of node: 79
3715 deg
Eccentricity:
0012507
Arg of perigee: 18
0929 deg
Mean anomaly: 342
0678 deg
Mean motion: 15
75850600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 602
Checksum: 300
Coasting Arc #14 (Orbit 617)
---------------------------------------
Vector Time (GMT): 2010/058/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4167297
48 A = 6714755
56 meter
Y = 381599
57 meter E =
0014941
Z = 5246512
86 I = 51
94837
XDOT = -1610
222025 Wp = 28
62411
YDOT = -7504
490768 meter/sec RA = 73
68197 deg
ZDOT = -719
488091 TA = 68
26222
MA = 68
10325
Ha = 190
939 n
mi
Hp = 178
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13672235
83 X = -4196740
73
Y = 1251967
10 feet Y = 334834
09 meter
Z = 17212968
70 Z = 5226197
19
XDOT = -5282
880661 XDOT = -1522
690760
YDOT = -24621
032705 feet/sec YDOT = -7522
007860 meter/sec
ZDOT = -2360
525233 ZDOT = -727
097228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3575340
53 X = -1089763
79
Y = -13359864
51 feet Y = -4072086
70 meter
Z = 17132270
90 Z = 5221916
17
XDOT = 22392
936744 XDOT = 6825
367120
YDOT = -9116
677757 feet/sec YDOT = -2778
763380 meter/sec
ZDOT = -2390
972280 ZDOT = -728
768351
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 10058
38943687
00016717 00000-0 10270-3 0 9133
2 25544 51
6446 74
1461 0012465 21
1547 339
0130 15
75935905 6182
Satellite: ISS
Catalog Number: 25544
Epoch time: 10058
38943687 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 74
1461 deg
Eccentricity:
0012465
Arg of perigee: 21
1547 deg
Mean anomaly: 339
0130 deg
Mean motion: 15
75935905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 618
Checksum: 309
Coasting Arc #15 (Orbit 633)
---------------------------------------
Vector Time (GMT): 2010/059/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1467575
45 A = 6726021
45 meter
Y = 6427092
57 meter E =
0025544
Z = 1255526
27 I = 51
97589
XDOT = -4969
056439 Wp = 42
90890
YDOT = -28
341184 meter/sec RA = 68
57299 deg
ZDOT = 5902
142138 TA = 330
82965
MA = 330
97208
Ha = 191
042 n
mi
Hp = 177
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4814880
10 X = 1389498
53
Y = 21086261
71 feet Y = 6443067
43 meter
Z = 4119180
67 Z = 1262465
32
XDOT = -16302
678605 XDOT = -4997
041001
YDOT = -92
982888 feet/sec YDOT = -84
064048 meter/sec
ZDOT = 19363
983394 ZDOT = 5877
935131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19819356
74 X = -6040939
93
Y = 8647380
91 feet Y = 2635721
70 meter
Z = 4146933
14 Z = 1263985
22
XDOT = -2346
845508 XDOT = -715
318511
YDOT = -14698
978267 feet/sec YDOT = -4480
248576 meter/sec
ZDOT = 19267
814284 ZDOT = 5872
829794
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 10059
40402865
00016717 00000-0 10270-3 0 9146
2 25544 51
6440 68
9212 0012699 25
8374 334
3421 15
75924916 6348
Satellite: ISS
Catalog Number: 25544
Epoch time: 10059
40402865 = yrday
fracday
Element set: 914
Inclination: 51
6440 deg
RA of node: 68
9212 deg
Eccentricity:
0012699
Arg of perigee: 25
8374 deg
Mean anomaly: 334
3421 deg
Mean motion: 15
75924916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 634
Checksum: 308
Coasting Arc #16 (Orbit 648)
---------------------------------------
Vector Time (GMT): 2010/060/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4541480
03 A = 6715995
10 meter
Y = 424782
33 meter E =
0019795
Z = -4942473
80 I = 51
93008
XDOT = 1685
074059 Wp = 67
28122
YDOT = 7182
596509 meter/sec RA = 63
41479 deg
ZDOT = 2180
017208 TA = 223
73772
MA = 223
89471
Ha = 191
041 n
mi
Hp = 177
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14899868
88 X = 4560401
66
Y = 1393642
83 feet Y = 475673
12 meter
Z = -16215465
24 Z = -4920365
84
XDOT = 5528
458200 XDOT = 1594
041836
YDOT = 23564
949178 feet/sec YDOT = 7200
931257 meter/sec
ZDOT = 7152
287427 ZDOT = 2187
981236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1691614
05 X = 515603
96
Y = 14964216
36 feet Y = 4561093
15 meter
Z = -16127625
88 Z = -4915700
37
XDOT = -20861
437563 XDOT = -6358
566169
YDOT = 10049
921569 feet/sec YDOT = 3063
216094 meter/sec
ZDOT = 7184
128906 ZDOT = 2189
722491
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 10060
35517473
00016717 00000-0 10270-3 0 9155
2 25544 51
6435 64
0223 0012680 29
3002 330
8871 15
75994519 6490
Satellite: ISS
Catalog Number: 25544
Epoch time: 10060
35517473 = yrday
fracday
Element set: 915
Inclination: 51
6435 deg
RA of node: 64
0223 deg
Eccentricity:
0012680
Arg of perigee: 29
3002 deg
Mean anomaly: 330
8871 deg
Mean motion: 15
75994519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 649
Checksum: 299
Coasting Arc #17 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2010/061/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1397176
37 A = 6723444
46 meter
Y = -6069931
95 meter E =
0013306
Z = -2552526
89 I = 51
94208
XDOT = 5479
881878 Wp = 56
15618
YDOT = 965
870836 meter/sec RA = 58
32363 deg
ZDOT = -5308
791747 TA = 152
63309
MA = 152
56294
Ha = 190
994 n
mi
Hp = 177
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4583911
99 X = -1316797
94
Y = -19914474
91 feet Y = -6085106
87 meter
Z = -8374432
04 Z = -2559118
38
XDOT = 17978
615086 XDOT = 5494
462844
YDOT = 3168
867573 feet/sec YDOT = 1027
231081 meter/sec
ZDOT = -17417
295759 ZDOT = -5282
135558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18423817
51 X = 5615579
58
Y = -8815864
94 feet Y = -2687075
63 meter
Z = -8400782
46 Z = -2560558
49
XDOT = 255
122008 XDOT = 77
761188
YDOT = 16990
754332 feet/sec YDOT = 5178
781920 meter/sec
ZDOT = -17311
376851 ZDOT = -5276
507664
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 10061
36969913
00016717 00000-0 10270-3 0 9168
2 25544 51
6442 58
7961 0012731 33
7692 326
4281 15
76065778 6659
Satellite: ISS
Catalog Number: 25544
Epoch time: 10061
36969913 = yrday
fracday
Element set: 916
Inclination: 51
6442 deg
RA of node: 58
7961 deg
Eccentricity:
0012731
Arg of perigee: 33
7692 deg
Mean anomaly: 326
4281 deg
Mean motion: 15
76065778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 331
Coasting Arc #18 (Orbit 680)
---------------------------------------
Vector Time (GMT): 2010/062/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5062355
47 A = 6718352
56 meter
Y = -1210626
80 meter E =
0021641
Z = 4241306
45 I = 51
90852
XDOT = -1452
940138 Wp = 52
71037
YDOT = -6653
761987 meter/sec RA = 53
14558 deg
ZDOT = -3608
083053 TA = 73
90864
MA = 73
67048
Ha = 191
013 n
mi
Hp = 177
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16608777
79 X = -5069045
08
Y = -3971872
70 feet Y = -1267274
07 meter
Z = 13915047
42 Z = 4216697
64
XDOT = -4766
863970 XDOT = -1360
901353
YDOT = -21829
927778 feet/sec YDOT = -6669
495354 meter/sec
ZDOT = -11837
542825 ZDOT = -3614
917174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -103098
45 X = -31424
41
Y = -17156005
36 feet Y = -5229150
43 meter
Z = 13817259
78 Z = 4211500
78
XDOT = 18840
625651 XDOT = 5742
622698
YDOT = -9736
522946 feet/sec YDOT = -2967
692194 meter/sec
ZDOT = -11864
862810 ZDOT = -3616
410185
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 10062
38418755
00016717 00000-0 10270-3 0 9175
2 25544 51
6442 53
5704 0012683 36
9292 323
2743 15
76141072 6812
Satellite: ISS
Catalog Number: 25544
Epoch time: 10062
38418755 = yrday
fracday
Element set: 917
Inclination: 51
6442 deg
RA of node: 53
5704 deg
Eccentricity:
0012683
Arg of perigee: 36
9292 deg
Mean anomaly: 323
2743 deg
Mean motion: 15
76141072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 681
Checksum: 301
Coasting Arc #19 (Orbit 696)
---------------------------------------
Vector Time (GMT): 2010/063/08:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1064910
91 A = 6720104
71 meter
Y = 5504273
55 meter E =
0021938
Z = 3680563
10 I = 51
89565
XDOT = -6136
792118 Wp = 67
27481
YDOT = -1728
339763 meter/sec RA = 48
06336 deg
ZDOT = 4348
253262 TA = 336
94668
MA = 337
04497
Ha = 191
048 n
mi
Hp = 176
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3493802
20 X = 985402
61
Y = 18058640
27 feet Y = 5515737
74 meter
Z = 12075338
27 Z = 3685542
87
XDOT = -20133
832407 XDOT = -6138
132293
YDOT = -5670
406046 feet/sec YDOT = -1796
972187 meter/sec
ZDOT = 14265
922776 ZDOT = 4318
437817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16597208
69 X = -5058829
21
Y = 7897623
31 feet Y = 2407195
59 meter
Z = 12095253
05 Z = 3686633
13
XDOT = 924
624004 XDOT = 281
825397
YDOT = -19784
223396 feet/sec YDOT = -6030
231291 meter/sec
ZDOT = 14147
443880 ZDOT = 4312
140895
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 10063
39864412
00016717 00000-0 10270-3 0 9183
2 25544 51
6442 48
3445 0012820 41
9118 318
3025 15
76155710 6971
Satellite: ISS
Catalog Number: 25544
Epoch time: 10063
39864412 = yrday
fracday
Element set: 918
Inclination: 51
6442 deg
RA of node: 48
3445 deg
Eccentricity:
0012820
Arg of perigee: 41
9118 deg
Mean anomaly: 318
3025 deg
Mean motion: 15
76155710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 697
Checksum: 298
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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