Date:
February 17th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 29062 56 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
049/07:10:30
000 0
1 0
6 0
7
N/A 0
6 -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
049/08:18:31
000 0
3 0
4 0
4
N/A -0
1 -0
0 190
3
000/00:04:58
000 -0
2 -0
1 180
9
049/08:26:00
000 0
0 0
0 0
0
N/A 0
0 0
0 190
3
000/00:00:00
000 0
0 0
0 180
9
Coasting Arc #1 (Orbit 430)
---------------------------------------
Vector Time (GMT): 2010/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5070338
43 A = 6726125
89 meter
Y = -4360953
49 meter E =
0001797
Z = -727094
33 I = 51
90490
XDOT = 2620
781142 Wp = 37
45751
YDOT = 4046
426967 meter/sec RA = 134
41208 deg
ZDOT = -6000
080113 TA = 150
43631
MA = 150
42615
Ha = 188
430 n
mi
Hp = 181
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16634968
60 X = 5122258
55
Y = -14307590
18 feet Y = -4303963
70 meter
Z = -2385480
08 Z = -702336
88
XDOT = 8598
363326 XDOT = 2604
485066
YDOT = 13275
679026 feet/sec YDOT = 4075
642628 meter/sec
ZDOT = -19685
302208 ZDOT = -5987
388502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21858464
88 X = 6662460
10
Y = -2023681
77 feet Y = -616818
20 meter
Z = -2287369
11 Z = -697190
11
XDOT = -730
813865 XDOT = -222
752066
YDOT = 14274
986670 feet/sec YDOT = 4351
015937 meter/sec
ZDOT = -19634
751844 ZDOT = -5984
672362
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 10046
53037800
00016717 00000-0 10270-3 0 9004
2 25544 51
6460 135
2057 0011216 329
2536 30
7970 15
76051528 4312
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
53037800 = yrday
fracday
Element set: 900
Inclination: 51
6460 deg
RA of node: 135
2057 deg
Eccentricity:
0011216
Arg of perigee: 329
2536 deg
Mean anomaly: 30
7970 deg
Mean motion: 15
76051528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 431
Checksum: 270
Coasting Arc #2 (Orbit 446)
---------------------------------------
Vector Time (GMT): 2010/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1939706
21 A = 6714855
12 meter
Y = -3934021
58 meter E =
0013090
Z = 5088372
06 I = 51
88858
XDOT = 5684
981981 Wp = 355
19418
YDOT = -4931
575698 meter/sec RA = 129
25822 deg
ZDOT = -1633
189383 TA = 110
51263
MA = 110
37209
Ha = 188
536 n
mi
Hp = 180
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6363865
52 X = -1920288
99
Y = -12906894
96 feet Y = -3955603
62 meter
Z = 16694134
04 Z = 5078996
59
XDOT = 18651
515685 XDOT = 5747
638788
YDOT = -16179
710294 feet/sec YDOT = -4867
652634 meter/sec
ZDOT = -5358
232883 ZDOT = -1605
419801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1960056
99 X = 597425
37
Y = -14300054
74 feet Y = -4358656
69 meter
Z = 16656753
71 Z = 5076978
53
XDOT = 23513
633932 XDOT = 7166
955622
YDOT = -2937
932657 feet/sec YDOT = -895
481874 meter/sec
ZDOT = -5248
179584 ZDOT = -1599
645137
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 10047
54486709
00016717 00000-0 10270-3 0 9013
2 25544 51
6465 129
9798 0011401 333
1040 26
9532 15
76141307 4472
Satellite: ISS
Catalog Number: 25544
Epoch time: 10047
54486709 = yrday
fracday
Element set: 901
Inclination: 51
6465 deg
RA of node: 129
9798 deg
Eccentricity:
0011401
Arg of perigee: 333
1040 deg
Mean anomaly: 26
9532 deg
Mean motion: 15
76141307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 447
Checksum: 299
Coasting Arc #3 (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 = -4820047
13 A = 6724191
12 meter
Y = 4171584
06 meter E =
0017827
Z = 2102332
90 I = 51
93754
XDOT = -1886
162022 Wp = 30
12015
YDOT = -4989
517936 meter/sec RA = 124
15882 deg
ZDOT = 5570
996008 TA = 353
32082
MA = 353
34455
Ha = 188
766 n
mi
Hp = 180
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15813802
94 X = -4876548
87
Y = 13686299
39 feet Y = 4117367
66 meter
Z = 6897417
65 Z = 2078779
98
XDOT = -6188
195610 XDOT = -1857
290603
YDOT = -16369
809502 feet/sec YDOT = -5010
448301 meter/sec
ZDOT = 18277
545958 ZDOT = 5561
903664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20770543
40 X = -6330861
63
Y = 2693457
21 feet Y = 820965
76 meter
Z = 6804067
88 Z = 2073879
89
XDOT = 3956
046538 XDOT = 1205
802985
YDOT = -15615
917764 feet/sec YDOT = -4759
731734 meter/sec
ZDOT = 18241
249942 ZDOT = 5559
932982
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
55932774
00016717 00000-0 10270-3 0 9024
2 25544 51
6459 124
7546 0011369 337
8535 22
2137 15
76151158 4635
Satellite: ISS
Catalog Number: 25544
Epoch time: 10048
55932774 = yrday
fracday
Element set: 902
Inclination: 51
6459 deg
RA of node: 124
7546 deg
Eccentricity:
0011369
Arg of perigee: 337
8535 deg
Mean anomaly: 22
2137 deg
Mean motion: 15
76151158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 313
Coasting Arc #4 (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 = 3979961
44 A = 6725465
71 meter
Y = -5334454
93 meter E =
0003928
Z = -982780
14 I = 51
95235
XDOT = 3317
917067 Wp = 41
65523
YDOT = 3570
701163 meter/sec RA = 120
08989 deg
ZDOT = -5955
584003 TA = 149
03491
MA = 149
01175
Ha = 188
735 n
mi
Hp = 180
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13057616
27 X = 4044090
57
Y = -17501492
56 feet Y = -5289590
14 meter
Z = -3224344
29 Z = -963289
64
XDOT = 10885
554682 XDOT = 3306
673017
YDOT = 11714
898829 feet/sec YDOT = 3607
740822 meter/sec
ZDOT = -19539
317595 ZDOT = -5939
493328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12561865
61 X = 3828856
64
Y = 17874419
76 feet Y = 5448123
14 meter
Z = -3147162
39 Z = -959255
10
XDOT = -13253
083462 XDOT = -4039
539839
YDOT = 5891
336036 feet/sec YDOT = 1795
679224 meter/sec
ZDOT = -19475
292687 ZDOT = -5936
069211
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
32015218
00016717 00000-0 10270-3 0 9036
2 25544 51
6428 120
8310 0011337 341
6511 18
4243 15
76217059 4750
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
32015218 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 120
8310 deg
Eccentricity:
0011337
Arg of perigee: 341
6511 deg
Mean anomaly: 18
4243 deg
Mean motion: 15
76217059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 270
Coasting Arc #5 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2010/049/07:13:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010288
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4534903
17 A = 6715657
12 meter
Y = -71485
35 meter E =
0016095
Z = -4964189
94 I = 51
91891
XDOT = -2193
475256 Wp = 31
19747
YDOT = 7071
328435 meter/sec RA = 120
04477 deg
ZDOT = -2095
162092 TA = 218
50647
MA = 218
62141
Ha = 188
811 n
mi
Hp = 180
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14878291
25 X = 4559480
30
Y = -234531
99 feet Y = -20636
28 meter
Z = -16286712
40 Z = -4942099
98
XDOT = -7196
441130 XDOT = -2262
207301
YDOT = 23199
896441 feet/sec YDOT = 7046
415255 meter/sec
ZDOT = -6873
891377 ZDOT = -2105
985258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3490046
67 X = -1063766
22
Y = 14563217
12 feet Y = 4438868
58 meter
Z = -16199007
31 Z = -4937457
43
XDOT = -19634
741451 XDOT = -5984
669194
YDOT = -12437
284902 feet/sec YDOT = -3790
884438 meter/sec
ZDOT = -6916
593171 ZDOT = -2108
177599
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
32015354
00016717 00000-0 10270-3 0 9048
2 25544 51
6437 120
8318 0011112 339
1008 20
9701 15
76081146 4755
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
32015354 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 120
8318 deg
Eccentricity:
0011112
Arg of perigee: 339
1008 deg
Mean anomaly: 20
9701 deg
Mean motion: 15
76081146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 267
Coasting Arc #6 (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 = -3534439
20 A = 6715730
45 meter
Y = -2163376
22 meter E =
0012243
Z = 5285663
73 I = 51
91471
XDOT = 3900
127128 Wp = 355
91376
YDOT = -6642
275754 meter/sec RA = 119
84449 deg
ZDOT = -98
734453 TA = 95
08918
MA = 94
94942
Ha = 190
349 n
mi
Hp = 180
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11595929
14 X = -3535661
71
Y = -7097691
02 feet Y = -2202906
91 meter
Z = 17341416
44 Z = 5268490
83
XDOT = 12795
692676 XDOT = 3974
591996
YDOT = -21792
243286 feet/sec YDOT = -6598
245869 meter/sec
ZDOT = -323
931932 ZDOT = -79
606588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7419242
08 X = 2261384
98
Y = -11496116
57 feet Y = -3504016
33 meter
Z = 17273148
69 Z = 5264855
72
XDOT = 20590
331719 XDOT = 6275
933108
YDOT = 12856
302413 feet/sec YDOT = 3918
600976 meter/sec
ZDOT = -248
239562 ZDOT = -75
663419
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
38358163
00016717 00000-0 10270-3 0 9053
2 25544 51
6439 120
5043 0012487 344
8964 15
1825 15
75532506 4763
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
38358163 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 120
5043 deg
Eccentricity:
0012487
Arg of perigee: 344
8964 deg
Mean anomaly: 15
1825 deg
Mean motion: 15
75532506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 476
Checksum: 310
Coasting Arc #7 (Orbit 475)
---------------------------------------
Vector Time (GMT): 2010/049/08:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 1009683
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1747553
21 A = 6726348
32 meter
Y = -6185967
26 meter E =
0011923
Z = 1985727
32 I = 51
94968
XDOT = 5252
093836 Wp = 57
51700
YDOT = -328
905736 meter/sec RA = 119
76722 deg
ZDOT = -5616
173847 TA = 100
47034
MA = 100
33597
Ha = 190
297 n
mi
Hp = 180
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5733442
29 X = 1806949
74
Y = -20295168
17 feet Y = -6166092
85 meter
Z = 6514853
40 Z = 1994361
49
XDOT = 17231
278989 XDOT = 5282
663365
YDOT = -1079
087059 feet/sec YDOT = -270
003147 meter/sec
ZDOT = -18425
767215 ZDOT = -5590
585247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20538370
85 X = 6260095
43
Y = 4743077
13 feet Y = 1445689
91 meter
Z = 6548898
27 Z = 1996104
19
XDOT = 2232
262614 XDOT = 680
393645
YDOT = 15772
415024 feet/sec YDOT = 4807
432099 meter/sec
ZDOT = -18324
180421 ZDOT = -5585
210192
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
38358407
00016717 00000-0 10270-3 0 9065
2 25544 51
6437 120
5049 0012053 345
2825 14
7986 15
75439573 4760
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
38358407 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 120
5049 deg
Eccentricity:
0012053
Arg of perigee: 345
2825 deg
Mean anomaly: 14
7986 deg
Mean motion: 15
75439573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 476
Checksum: 319
Coasting Arc #8 (Orbit 491)
---------------------------------------
Vector Time (GMT): 2010/050/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4282492
34 A = 6716327
93 meter
Y = -356416
82 meter E =
0009501
Z = 5158799
50 I = 51
93144
XDOT = 2193
326786 Wp = 7
19067
YDOT = -7267
254514 meter/sec RA = 114
66745 deg
ZDOT = 1327
630243 TA = 70
22017
MA = 70
11774
Ha = 190
452 n
mi
Hp = 180
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14050171
72 X = -4303248
80
Y = -1169346
51 feet Y = -404421
97 meter
Z = 16925195
22 Z = 5137944
98
XDOT = 7195
954023 XDOT = 2267
978182
YDOT = -23842
698536 feet/sec YDOT = -7242
309964 meter/sec
ZDOT = 4355
742267 ZDOT = 1338
467022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 202041
30 X = 61582
19
Y = -14196143
33 feet Y = -4326984
49 meter
Z = 16842375
84 Z = 5133556
15
XDOT = 23240
583777 XDOT = 7083
729935
YDOT = 5514
105186 feet/sec YDOT = 1680
699261 meter/sec
ZDOT = 4398
503233 ZDOT = 1340
663785
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
39846761
00016717 00000-0 10270-3 0 9074
2 25544 51
6446 115
2818 0012169 348
9887 11
1009 15
75527368 4926
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
39846761 = yrday
fracday
Element set: 907
Inclination: 51
6446 deg
RA of node: 115
2818 deg
Eccentricity:
0012169
Arg of perigee: 348
9887 deg
Mean anomaly: 11
1009 deg
Mean motion: 15
75527368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 492
Checksum: 324
Coasting Arc #9 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2010/051/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1741796
51 A = 6727662
08 meter
Y = 6451149
39 meter E =
0021166
Z = -658135
87 I = 51
98137
XDOT = -4761
322214 Wp = 15
18523
YDOT = -676
892980 meter/sec RA = 109
52570 deg
ZDOT = 6029
275888 TA = 337
66766
MA = 337
75968
Ha = 190
570 n
mi
Hp = 180
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5714555
48 X = -1810607
88
Y = 21165188
29 feet Y = 6431286
82 meter
Z = -2159238
42 Z = -666764
82
XDOT = -15621
135874 XDOT = -4782
688076
YDOT = -2220
777492 feet/sec YDOT = -730
256153 meter/sec
ZDOT = 19781
088871 ZDOT = 6006
093721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21574339
33 X = -6575858
63
Y = -3875703
35 feet Y = -1181314
38 meter
Z = -2193275
14 Z = -668510
26
XDOT = 587
303048 XDOT = 179
009969
YDOT = -14295
903728 feet/sec YDOT = -4357
391456 meter/sec
ZDOT = 19689
011667 ZDOT = 6001
210756
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
34989634
00016717 00000-0 10270-3 0 9088
2 25544 51
6448 110
3857 0012293 353
3613 6
7386 15
75521057 5076
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051
34989634 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 110
3857 deg
Eccentricity:
0012293
Arg of perigee: 353
3613 deg
Mean anomaly: 6
7386 deg
Mean motion: 15
75521057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 308
Coasting Arc #10 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2010/052/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4053771
31 A = 6715584
00 meter
Y = 875087
90 meter E =
0019137
Z = -5294635
06 I = 51
95038
XDOT = -1809
437870 Wp = 49
00892
YDOT = 7475
756918 meter/sec RA = 104
40998 deg
ZDOT = -137
851561 TA = 219
61715
MA = 219
75714
Ha = 190
627 n
mi
Hp = 180
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13299774
64 X = 4069404
77
Y = 2871023
29 feet Y = 920506
89 meter
Z = -17370849
93 Z = -5274904
07
XDOT = -5936
475951 XDOT = -1892
228978
YDOT = 24526
761542 feet/sec YDOT = 7455
059798 meter/sec
ZDOT = -452
268901 ZDOT = -146
842964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1482907
05 X = -451990
07
Y = 13625153
12 feet Y = 4152946
67 meter
Z = -17292466
48 Z = -5270743
78
XDOT = -24011
943776 XDOT = -7318
840463
YDOT = -3282
312989 feet/sec YDOT = -1000
448999 meter/sec
ZDOT = -487
723537 ZDOT = -148
658134
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
36472346
00016717 00000-0 10270-3 0 9099
2 25544 51
6450 105
1632 0012282 357
0937 3
0154 15
75588751 5235
Satellite: ISS
Catalog Number: 25544
Epoch time: 10052
36472346 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 105
1632 deg
Eccentricity:
0012282
Arg of perigee: 357
0937 deg
Mean anomaly: 3
0154 deg
Mean motion: 15
75588751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 523
Checksum: 288
Coasting Arc #11 (Orbit 538)
---------------------------------------
Vector Time (GMT): 2010/053/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1426968
49 A = 6727451
55 meter
Y = -6562203
08 meter E =
0008626
Z = -446693
84 I = 51
99701
XDOT = 4555
103510 Wp = 64
25136
YDOT = 1395
910052 meter/sec RA = 99
28891 deg
ZDOT = -6041
558315 TA = 120
58025
MA = 120
49513
Ha = 190
635 n
mi
Hp = 179
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4681655
15 X = 1502412
09
Y = -21529537
67 feet Y = -6545824
05 meter
Z = -1465530
99 Z = -439578
45
XDOT = 14944
565323 XDOT = 4568
504096
YDOT = 4579
757390 feet/sec YDOT = 1446
922831 meter/sec
ZDOT = -19821
385547 ZDOT = -6019
397344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21935808
31 X = 6686034
37
Y = 2083416
68 feet Y = 635025
40 meter
Z = -1437482
97 Z = -438144
81
XDOT = -2594
519088 XDOT = -790
809418
YDOT = 13900
552836 feet/sec YDOT = 4236
888504 meter/sec
ZDOT = -19733
330312 ZDOT = -6014
719079
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
37952104
00016717 00000-0 10270-3 0 9108
2 25544 51
6448 99
9397 0012216 1
2486 358
8706 15
75628886 5399
Satellite: ISS
Catalog Number: 25544
Epoch time: 10053
37952104 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 99
9397 deg
Eccentricity:
0012216
Arg of perigee: 1
2486 deg
Mean anomaly: 358
8706 deg
Mean motion: 15
75628886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 539
Checksum: 331
Coasting Arc #12 (Orbit 554)
---------------------------------------
Vector Time (GMT): 2010/054/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3956937
81 A = 6715659
65 meter
Y = -1577545
04 meter E =
0015121
Z = 5190490
21 I = 51
96244
XDOT = 1448
139312 Wp = 16
38771
YDOT = -7479
406497 meter/sec RA = 94
15054 deg
ZDOT = -1154
229929 TA = 84
66263
MA = 84
49013
Ha = 190
758 n
mi
Hp = 179
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12982079
43 X = -3964217
39
Y = -5175672
69 feet Y = -1621834
60 meter
Z = 17029167
36 Z = 5171250
03
XDOT = 4751
113229 XDOT = 1537
274685
YDOT = -24538
735228 feet/sec YDOT = -7462
714154 meter/sec
ZDOT = -3786
843599 ZDOT = -1146
978530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3340077
24 X = 1018055
54
Y = -13666173
74 feet Y = -4165449
76 meter
Z = 16952701
69 Z = 5167183
47
XDOT = 23964
251111 XDOT = 7304
303739
YDOT = 1133
546057 feet/sec YDOT = 345
504838 meter/sec
ZDOT = -3758
272536 ZDOT = -1145
521469
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
39428716
00016717 00000-0 10270-3 0 9119
2 25544 51
6456 94
7157 0012346 4
9246 355
2038 15
75711388 5550
Satellite: ISS
Catalog Number: 25544
Epoch time: 10054
39428716 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 94
7157 deg
Eccentricity:
0012346
Arg of perigee: 4
9246 deg
Mean anomaly: 355
2038 deg
Mean motion: 15
75711388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 555
Checksum: 313
Coasting Arc #13 (Orbit 570)
---------------------------------------
Vector Time (GMT): 2010/055/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1109685
63 A = 6726256
91 meter
Y = 6433374
85 meter E =
0023672
Z = 1556415
23 I = 51
99914
XDOT = -4575
566634 Wp = 37
67538
YDOT = -2201
230877 meter/sec RA = 89
05139 deg
ZDOT = 5808
831245 TA = 339
44013
MA = 339
53523
Ha = 190
836 n
mi
Hp = 179
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3640700
88 X = -1189102
92
Y = 21106872
85 feet Y = 6420521
63 meter
Z = 5106349
17 Z = 1550831
64
XDOT = -15011
701554 XDOT = -4578
829667
YDOT = -7221
886081 feet/sec YDOT = -2252
415864 meter/sec
ZDOT = 19057
845292 ZDOT = 5786
595673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21420329
94 X = -6528916
56
Y = -385113
94 feet Y = -117382
73 meter
Z = 5084362
21 Z = 1549713
60
XDOT = 4784
737565 XDOT = 1458
388010
YDOT = -14491
188802 feet/sec YDOT = -4416
914347 meter/sec
ZDOT = 18969
457921 ZDOT = 5781
890774
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
40902535
00016717 00000-0 10270-3 0 9129
2 25544 51
6456 89
4927 0012377 9
3892 350
7501 15
75717889 5711
Satellite: ISS
Catalog Number: 25544
Epoch time: 10055
40902535 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 89
4927 deg
Eccentricity:
0012377
Arg of perigee: 9
3892 deg
Mean anomaly: 350
7501 deg
Mean motion: 15
75717889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 571
Checksum: 324
Coasting Arc #14 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2010/056/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4062444
93 A = 6716920
89 meter
Y = 2262243
18 meter E =
0016622
Z = -4856263
22 I = 51
96597
XDOT = -1136
031700 Wp = 59
23769
YDOT = 7214
999956 meter/sec RA = 83
89417 deg
ZDOT = 2425
095441 TA = 234
26744
MA = 234
42217
Ha = 190
878 n
mi
Hp = 178
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13328231
40 X = 4060436
43
Y = 7422057
69 feet Y = 2307660
59 meter
Z = -15932622
12 Z = -4836533
28
XDOT = -3727
138123 XDOT = -1228
407047
YDOT = 23671
259698 feet/sec YDOT = 7201
779693 meter/sec
ZDOT = 7956
349873 ZDOT = 2419
352323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5023565
45 X = -1531182
75
Y = 14490889
72 feet Y = 4416823
19 meter
Z = -15854180
71 Z = -4832354
28
XDOT = -22911
565817 XDOT = -6983
445261
YDOT = 685
471299 feet/sec YDOT = 208
931652 meter/sec
ZDOT = 7933
747064 ZDOT = 2418
206105
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
36031308
00016717 00000-0 10270-3 0 9137
2 25544 51
6449 84
5961 0012412 13
1252 347
0232 15
75789771 5865
Satellite: ISS
Catalog Number: 25544
Epoch time: 10056
36031308 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 84
5961 deg
Eccentricity:
0012412
Arg of perigee: 13
1252 deg
Mean anomaly: 347
0232 deg
Mean motion: 15
75789771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 586
Checksum: 296
Coasting Arc #15 (Orbit 601)
---------------------------------------
Vector Time (GMT): 2010/057/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 928976
51 A = 6723912
72 meter
Y = -6104490
61 meter E =
0011849
Z = -2681205
65 I = 51
98448
XDOT = 4763
522974 Wp = 40
06595
YDOT = 3019
534238 meter/sec RA = 78
81015 deg
ZDOT = -5228
193875 TA = 170
30167
MA = 170
27878
Ha = 190
878 n
mi
Hp = 178
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3047823
19 X = 1010193
40
Y = -20027856
32 feet Y = -6093648
22 meter
Z = -8796606
48 Z = -2676495
35
XDOT = 15628
356213 XDOT = 4754
800848
YDOT = 9906
608392 feet/sec YDOT = 3072
753841 meter/sec
ZDOT = -17152
867045 ZDOT = -5205
074645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20254010
64 X = 6173422
44
Y = -710667
70 feet Y = -216611
51 meter
Z = -8778071
81 Z = -2675556
29
XDOT = -6833
244366 XDOT = -2082
772883
YDOT = 15830
395711 feet/sec YDOT = 4825
104613 meter/sec
ZDOT = -17060
935100 ZDOT = -5200
173019
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
37499087
00016717 00000-0 10270-3 0 9142
2 25544 51
6440 79
3714 0012383 16
9995 343
1582 15
75809738 6026
Satellite: ISS
Catalog Number: 25544
Epoch time: 10057
37499087 = yrday
fracday
Element set: 914
Inclination: 51
6440 deg
RA of node: 79
3714 deg
Eccentricity:
0012383
Arg of perigee: 16
9995 deg
Mean anomaly: 343
1582 deg
Mean motion: 15
75809738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 602
Checksum: 332
Coasting Arc #16 (Orbit 617)
---------------------------------------
Vector Time (GMT): 2010/058/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4305206
38 A = 6719161
25 meter
Y = -2984098
74 meter E =
0020261
Z = 4205444
97 I = 51
96268
XDOT = 1028
572928 Wp = 44
05989
YDOT = -6693
939984 meter/sec RA = 73
63593 deg
ZDOT = -3672
154995 TA = 83
29812
MA = 83
06758
Ha = 190
924 n
mi
Hp = 178
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14124692
84 X = -4291946
37
Y = -9790350
19 feet Y = -3032167
70 meter
Z = 13797391
64 Z = 4184563
30
XDOT = 3374
583098 XDOT = 1121
187450
YDOT = -21961
745355 feet/sec YDOT = -6681
920272 meter/sec
ZDOT = -12047
752609 ZDOT = -3666
932951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6680304
68 X = 2036156
87
Y = -15906480
52 feet Y = -4848295
26 meter
Z = 13714347
51 Z = 4180133
12
XDOT = 21042
698813 XDOT = 6413
814598
YDOT = -1602
758272 feet/sec YDOT = -488
520721 meter/sec
ZDOT = -12027
201116 ZDOT = -3665
890900
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
38963530
00016717 00000-0 10270-3 0 9154
2 25544 51
6446 74
1463 0012500 20
1630 340
0025 15
75899834 6181
Satellite: ISS
Catalog Number: 25544
Epoch time: 10058
38963530 = yrday
fracday
Element set: 915
Inclination: 51
6446 deg
RA of node: 74
1463 deg
Eccentricity:
0012500
Arg of perigee: 20
1630 deg
Mean anomaly: 340
0025 deg
Mean motion: 15
75899834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 618
Checksum: 289
Coasting Arc #17 (Orbit 633)
---------------------------------------
Vector Time (GMT): 2010/059/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -917971
29 A = 6720807
90 meter
Y = 5534455
78 meter E =
0019782
Z = 3677462
25 I = 51
95827
XDOT = -5140
235748 Wp = 58
89313
YDOT = -3754
800015 meter/sec RA = 68
55971 deg
ZDOT = 4360
648032 TA = 345
22205
MA = 345
27979
Ha = 190
966 n
mi
Hp = 177
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3011716
83 X = -997654
31
Y = 18157663
31 feet Y = 5523745
29 meter
Z = 12065164
88 Z = 3672808
81
XDOT = -16864
290513 XDOT = -5119
049560
YDOT = -12318
897686 feet/sec YDOT = -3812
162321 meter/sec
ZDOT = 14306
588033 ZDOT = 4335
729235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18390035
76 X = -5605282
90
Y = 1009785
94 feet Y = 307782
76 meter
Z = 12046837
57 Z = 3671876
09
XDOT = 8338
682319 XDOT = 2541
630371
YDOT = -17911
883463 feet/sec YDOT = -5459
542079 meter/sec
ZDOT = 14207
483710 ZDOT = 4330
441035
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
40424988
00016717 00000-0 10270-3 0 9168
2 25544 51
6439 68
9214 0012441 24
7715 335
4044 15
75925410 6343
Satellite: ISS
Catalog Number: 25544
Epoch time: 10059
40424988 = yrday
fracday
Element set: 916
Inclination: 51
6439 deg
RA of node: 68
9214 deg
Eccentricity:
0012441
Arg of perigee: 24
7715 deg
Mean anomaly: 335
4044 deg
Mean motion: 15
75925410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 634
Checksum: 305
Coasting Arc #18 (Orbit 648)
---------------------------------------
Vector Time (GMT): 2010/060/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4668345
24 A = 6721802
96 meter
Y = 3512695
15 meter E =
0015599
Z = -3321258
91 I = 51
94940
XDOT = -1146
593490 Wp = 43
30463
YDOT = 5971
337574 meter/sec RA = 63
38027 deg
ZDOT = 4727
957452 TA = 277
82262
MA = 277
99969
Ha = 191
020 n
mi
Hp = 177
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15316093
32 X = 4644852
45
Y = 11524590
39 feet Y = 3564767
65 meter
Z = -10896518
74 Z = -3298638
00
XDOT = -3761
789666 XDOT = -1236
247926
YDOT = 19591
002538 feet/sec YDOT = 5958
014912 meter/sec
ZDOT = 15511
671430 ZDOT = 4722
169002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7534328
49 X = -2296463
32
Y = 17680081
93 feet Y = 5388888
97 meter
Z = -10806554
32 Z = -3293837
76
XDOT = -18656
220999 XDOT = -5686
416161
YDOT = 1468
210630 feet/sec YDOT = 447
510600 meter/sec
ZDOT = 15488
844726 ZDOT = 4720
999872
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
35542206
00016717 00000-0 10270-3 0 9179
2 25544 51
6435 64
0229 0012524 28
7903 331
3950 15
75982010 6493
Satellite: ISS
Catalog Number: 25544
Epoch time: 10060
35542206 = yrday
fracday
Element set: 917
Inclination: 51
6435 deg
RA of node: 64
0229 deg
Eccentricity:
0012524
Arg of perigee: 28
7903 deg
Mean anomaly: 331
3950 deg
Mean motion: 15
75982010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 649
Checksum: 286
Coasting Arc #19 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2010/061/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1177130
76 A = 6717631
24 meter
Y = -4842200
20 meter E =
0021394
Z = -4525969
32 I = 51
92157
XDOT = 5547
337201 Wp = 48
71205
YDOT = 4292
163331 meter/sec RA = 58
29824 deg
ZDOT = -3145
051131 TA = 189
94960
MA = 189
99203
Ha = 191
009 n
mi
Hp = 177
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3861977
57 X = 1253175
65
Y = -15886483
61 feet Y = -4828612
13 meter
Z = -14848980
71 Z = -4520065
67
XDOT = 18199
925200 XDOT = 5514
207049
YDOT = 14081
900691 feet/sec YDOT = 4354
011369 meter/sec
ZDOT = -10318
409221 ZDOT = -3118
183496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16368763
06 X = 4989198
98
Y = -225506
42 feet Y = -68734
36 meter
Z = -14825660
30 Z = -4518861
26
XDOT = -8985
287342 XDOT = -2738
715582
YDOT = 20049
974080 feet/sec YDOT = 6111
232100 meter/sec
ZDOT = -10211
559711 ZDOT = -3112
483400
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
36997389
00016717 00000-0 10270-3 0 9188
2 25544 51
6441 58
7968 0012545 32
7164 327
4775 15
75999423 6652
Satellite: ISS
Catalog Number: 25544
Epoch time: 10061
36997389 = yrday
fracday
Element set: 918
Inclination: 51
6441 deg
RA of node: 58
7968 deg
Eccentricity:
0012545
Arg of perigee: 32
7164 deg
Mean anomaly: 327
4775 deg
Mean motion: 15
75999423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 354
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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