Date:
July 11th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 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
197/08:06:48
755 1
5 6
2 6
2
N/A 6
0 0
0 196
3
000/00:18:37
509 -0
7 -0
3 186
7
Coasting Arc #1 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2010/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4727081
37 A = 6729471
32 meter
Y = 2279234
91 meter E =
0018487
Z = 4195168
01 I = 51
94543
XDOT = 25
689767 Wp = 81
64778
YDOT = -6766
005098 meter/sec RA = 115
51812 deg
ZDOT = 3693
807278 TA = 330
81699
MA = 330
92016
Ha = 196
318 n
mi
Hp = 183
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15508797
16 X = -4772596
14
Y = 7477804
81 feet Y = 2226118
55 meter
Z = 13763674
58 Z = 4172093
84
XDOT = 84
284012 XDOT = 83
402794
YDOT = -22198
179456 feet/sec YDOT = -6765
395854 meter/sec
ZDOT = 12118
790283 ZDOT = 3694
070935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11607550
78 X = 3537981
48
Y = 12815405
49 feet Y = 3906135
59 meter
Z = 13671475
38 Z = 4167065
69
XDOT = -20348
079757 XDOT = -6202
094710
YDOT = 5461
695492 feet/sec YDOT = 1664
724786 meter/sec
ZDOT = 12119
819636 ZDOT = 3694
121025
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 10190
55435216
00016717 00000-0 10270-3 0 9009
2 25544 51
6456 116
1064 0010028 57
0262 303
1863 15
72295968 26995
Satellite: ISS
Catalog Number: 25544
Epoch time: 10190
55435216 = yrday
fracday
Element set: 900
Inclination: 51
6456 deg
RA of node: 116
1064 deg
Eccentricity:
0010028
Arg of perigee: 57
0262 deg
Mean anomaly: 303
1863 deg
Mean motion: 15
72295968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 298
Coasting Arc #2 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2010/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 983988
43 A = 6731207
05 meter
Y = 5570248
66 meter E =
0014816
Z = -3657367
44 I = 51
96420
XDOT = -5064
251976 Wp = 74
51232
YDOT = 3766
851784 meter/sec RA = 110
36739 deg
ZDOT = 4393
019757 TA = 241
90728
MA = 242
05714
Ha = 196
227 n
mi
Hp = 183
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3228308
51 X = 939394
41
Y = 18275094
02 feet Y = 5581003
59 meter
Z = -11999237
02 Z = -3652694
49
XDOT = -16614
999920 XDOT = -5127
337479
YDOT = 12358
437613 feet/sec YDOT = 3709
866697 meter/sec
ZDOT = 14412
794478 ZDOT = 4368
265386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16432575
80 X = 5008649
10
Y = -8649836
31 feet Y = -2636470
11 meter
Z = -11980547
17 Z = -3651670
78
XDOT = 16183
874776 XDOT = 4932
845032
YDOT = 11004
142601 feet/sec YDOT = 3354
062665 meter/sec
ZDOT = 14313
869626 ZDOT = 4362
867462
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 10191
50772880
00016717 00000-0 10270-3 0 9017
2 25544 51
6463 111
2235 0010056 60
1868 300
0293 15
72309255 27143
Satellite: ISS
Catalog Number: 25544
Epoch time: 10191
50772880 = yrday
fracday
Element set: 901
Inclination: 51
6463 deg
RA of node: 111
2235 deg
Eccentricity:
0010056
Arg of perigee: 60
1868 deg
Mean anomaly: 300
0293 deg
Mean motion: 15
72309255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 274
Coasting Arc #3 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2010/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3964630
88 A = 6731790
25 meter
Y = -4204285
47 meter E =
0014798
Z = -3469566
70 I = 51
97668
XDOT = 2132
884786 Wp = 71
61356
YDOT = 5786
393562 meter/sec RA = 105
31931 deg
ZDOT = -4585
835976 TA = 149
18718
MA = 149
10024
Ha = 196
231 n
mi
Hp = 183
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13007319
15 X = 4028203
55
Y = -13793587
50 feet Y = -4159594
50 meter
Z = -11383092
85 Z = -3450153
20
XDOT = 6997
653499 XDOT = 2090
298555
YDOT = 18984
230848 feet/sec YDOT = 5810
007496 meter/sec
ZDOT = -15045
393623 ZDOT = -4575
576950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17231612
99 X = -5252195
64
Y = -8017813
93 feet Y = -2443829
69 meter
Z = -11305502
38 Z = -3445917
12
XDOT = 15166
453130 XDOT = 4622
734914
YDOT = -11491
113365 feet/sec YDOT = -3502
491354 meter/sec
ZDOT = -15004
376809 ZDOT = -4573
334051
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 10192
52465393
00016717 00000-0 10270-3 0 9029
2 25544 51
6473 106
0148 0010080 63
7397 296
4800 15
72329586 27301
Satellite: ISS
Catalog Number: 25544
Epoch time: 10192
52465393 = yrday
fracday
Element set: 902
Inclination: 51
6473 deg
RA of node: 106
0148 deg
Eccentricity:
0010080
Arg of perigee: 63
7397 deg
Mean anomaly: 296
4800 deg
Mean motion: 15
72329586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 304
Coasting Arc #4 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2010/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2657232
66 A = 6728791
50 meter
Y = -4394186
34 meter E =
0019711
Z = 4336633
02 I = 51
97306
XDOT = 3789
769689 Wp = 69
19968
YDOT = -5739
303171 meter/sec RA = 100
17108 deg
ZDOT = -3473
875909 TA = 55
80765
MA = 55
62098
Ha = 196
304 n
mi
Hp = 182
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8717954
91 X = -2628964
72
Y = -14416621
86 feet Y = -4423743
76 meter
Z = 14227798
63 Z = 4323792
40
XDOT = 12433
627588 XDOT = 3870
541068
YDOT = -18829
734814 feet/sec YDOT = -5696
471523 meter/sec
ZDOT = -11397
230674 ZDOT = -3455
270330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10651299
94 X = -3246516
22
Y = 13109146
49 feet Y = 3995667
85 meter
Z = 14176461
67 Z = 4320985
52
XDOT = -20966
889756 XDOT = -6390
707998
YDOT = -4721
790748 feet/sec YDOT = -1439
201820 meter/sec
ZDOT = -11322
862499 ZDOT = -3451
208490
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 10193
54156961
00016717 00000-0 10270-3 0 9031
2 25544 51
6468 100
8064 0010070 67
3483 292
8743 15
72337900 27461
Satellite: ISS
Catalog Number: 25544
Epoch time: 10193
54156961 = yrday
fracday
Element set: 903
Inclination: 51
6468 deg
RA of node: 100
8064 deg
Eccentricity:
0010070
Arg of perigee: 67
3483 deg
Mean anomaly: 292
8743 deg
Mean motion: 15
72337900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 306
Coasting Arc #5 (Orbit 2761)
---------------------------------------
Vector Time (GMT): 2010/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2516011
79 A = 6734111
50 meter
Y = 5685260
25 meter E =
0023848
Z = 2557908
99 I = 51
99556
XDOT = -3801
824528 Wp = 73
95242
YDOT = -4088
137593 meter/sec RA = 95
11837 deg
ZDOT = 5312
679464 TA = 314
92073
MA = 315
11399
Ha = 196
308 n
mi
Hp = 182
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8254631
87 X = -2591824
00
Y = 18652428
65 feet Y = 5656700
48 meter
Z = 8392089
85 Z = 2545503
08
XDOT = -12473
177585 XDOT = -3781
635134
YDOT = -13412
524911 feet/sec YDOT = -4130
539686 meter/sec
ZDOT = 17430
050736 ZDOT = 5294
259100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20379304
06 X = 6211611
88
Y = 1251348
20 feet Y = 381410
93 meter
Z = 8342500
09 Z = 2542794
03
XDOT = -8071
501712 XDOT = -2460
193722
YDOT = 14988
363894 feet/sec YDOT = 4568
453315 meter/sec
ZDOT = 17356
404085 ZDOT = 5290
231965
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 10194
55847559
00016717 00000-0 10270-3 0 9044
2 25544 51
6473 95
5975 0010077 70
9162 289
3091 15
72337423 27624
Satellite: ISS
Catalog Number: 25544
Epoch time: 10194
55847559 = yrday
fracday
Element set: 904
Inclination: 51
6473 deg
RA of node: 95
5975 deg
Eccentricity:
0010077
Arg of perigee: 70
9162 deg
Mean anomaly: 289
3091 deg
Mean motion: 15
72337423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2762
Checksum: 332
Coasting Arc #6 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2010/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3817186
51 A = 6726629
84 meter
Y = 2654036
39 meter E =
0021138
Z = -4879710
71 I = 51
97250
XDOT = -1865
384050 Wp = 92
31993
YDOT = 7059
672383 meter/sec RA = 89
97917 deg
ZDOT = 2388
502581 TA = 200
88275
MA = 200
96922
Ha = 196
203 n
mi
Hp = 182
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12523577
80 X = 3810929
16
Y = 8707468
46 feet Y = 2696687
98 meter
Z = -16009549
57 Z = -4861182
11
XDOT = -6120
026410 XDOT = -1955
790629
YDOT = 23161
654799 feet/sec YDOT = 7038
306802 meter/sec
ZDOT = 7836
294557 ZDOT = 2379
221883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3484277
29 X = 1062007
72
Y = -14929377
71 feet Y = -4550474
33 meter
Z = -15935469
19 Z = -4857131
01
XDOT = 22722
946934 XDOT = 6925
954225
YDOT = -2993
427993 feet/sec YDOT = -912
396852 meter/sec
ZDOT = 7799
196741 ZDOT = 2377
195167
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 10195
51181475
00016717 00000-0 10270-3 0 9050
2 25544 51
6475 90
7142 0009950 74
1805 286
0454 15
72366565 27779
Satellite: ISS
Catalog Number: 25544
Epoch time: 10195
51181475 = yrday
fracday
Element set: 905
Inclination: 51
6475 deg
RA of node: 90
7142 deg
Eccentricity:
0009950
Arg of perigee: 74
1805 deg
Mean anomaly: 286
0454 deg
Mean motion: 15
72366565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 323
Coasting Arc #7 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2010/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 694365
36 A = 6735735
78 meter
Y = -6500473
88 meter E =
0015125
Z = -1622996
42 I = 52
00182
XDOT = 4700
924066 Wp = 106
76330
YDOT = 1931
797322 meter/sec RA = 84
91368 deg
ZDOT = -5774
382443 TA = 91
04050
MA = 90
86720
Ha = 196
202 n
mi
Hp = 182
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2278101
59 X = 774887
33
Y = -21327014
03 feet Y = -6492258
70 meter
Z = -5324791
39 Z = -1619428
23
XDOT = 15422
979220 XDOT = 4707
023416
YDOT = 6337
917723 feet/sec YDOT = 1984
400472 meter/sec
ZDOT = -18944
824289 ZDOT = -5751
530744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20592205
51 X = -6276504
24
Y = 6011991
77 feet Y = 1832455
09 meter
Z = -5310527
75 Z = -1618648
86
XDOT = 361
287408 XDOT = 110
120402
YDOT = -15275
906606 feet/sec YDOT = -4656
096333 meter/sec
ZDOT = -18853
459517 ZDOT = -5746
534461
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 10196
52870157
00016717 00000-0 10270-3 0 9065
2 25544 51
6475 85
5047 0009827 78
6571 281
5695 15
72348678 27937
Satellite: ISS
Catalog Number: 25544
Epoch time: 10196
52870157 = yrday
fracday
Element set: 906
Inclination: 51
6475 deg
RA of node: 85
5047 deg
Eccentricity:
0009827
Arg of perigee: 78
6571 deg
Mean anomaly: 281
5695 deg
Mean motion: 15
72348678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2793
Checksum: 356
Coasting Arc #8 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2010/197/08:16:07
509
Vector Time (MET): N/A
Weight (LBS) : 828051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4075482
97 A = 6731739
62 meter
Y = 2866138
36 meter E =
0014056
Z = -4539904
30 I = 51
97048
XDOT = -1347
395847 Wp = 99
90777
YDOT = 6882
779227 meter/sec RA = 80
56864 deg
ZDOT = 3141
525065 TA = 201
32643
MA = 201
38506
Ha = 196
320 n
mi
Hp = 186
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13371007
14 X = 4065184
15
Y = 9403341
07 feet Y = 2911655
63 meter
Z = -14894699
15 Z = -4520130
63
XDOT = -4420
590048 XDOT = -1439
520965
YDOT = 22581
296676 feet/sec YDOT = 6867
196484 meter/sec
ZDOT = 10306
840763 ZDOT = 3134
756293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15181497
54 X = 4627320
45
Y = -6251207
85 feet Y = -1905368
15 meter
Z = -14815642
10 Z = -4515807
71
XDOT = 16131
241478 XDOT = 4916
802403
YDOT = 14857
982039 feet/sec YDOT = 4528
712925 meter/sec
ZDOT = 10279
775030 ZDOT = 3133
275429
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 10197
35491844
00016717 00000-0 10270-3 0 9070
2 25544 51
6452 81
2715 0004662 77
3154 282
8529 15
71060568 28065
Satellite: ISS
Catalog Number: 25544
Epoch time: 10197
35491844 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 81
2715 deg
Eccentricity:
0004662
Arg of perigee: 77
3154 deg
Mean anomaly: 282
8529 deg
Mean motion: 15
71060568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 319
Coasting Arc #9 (Orbit 2821)
---------------------------------------
Vector Time (GMT): 2010/198/08:16:07
509
Vector Time (MET): N/A
Weight (LBS) : 828051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -127370
17 A = 6738906
57 meter
Y = -6460736
78 meter E =
0010194
Z = -1909255
95 I = 51
98961
XDOT = 4970
834373 Wp = 117
38237
YDOT = 1565
626570 meter/sec RA = 75
51909 deg
ZDOT = -5657
043582 TA = 83
69497
MA = 83
57887
Ha = 196
290 n
mi
Hp = 186
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -417881
15 X = -45840
83
Y = -21196642
98 feet Y = -6461705
09 meter
Z = -6263963
10 Z = -1909677
24
XDOT = 16308
511722 XDOT = 4980
438478
YDOT = 5136
570112 feet/sec YDOT = 1621
267601 meter/sec
ZDOT = -18559
854273 ZDOT = -5632
871998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18235617
21 X = -5558216
13
Y = -10812659
39 feet Y = -3295698
58 meter
Z = -6265635
96 Z = -1909765
84
XDOT = 12207
437644 XDOT = 3720
826994
YDOT = -9941
269351 feet/sec YDOT = -3030
098898 meter/sec
ZDOT = -18463
214483 ZDOT = -5627
587774
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 10198
37264541
00016717 00000-0 10270-3 0 9086
2 25544 51
6460 76
0679 0004676 80
6814 279
4876 15
71082532 28220
Satellite: ISS
Catalog Number: 25544
Epoch time: 10198
37264541 = yrday
fracday
Element set: 908
Inclination: 51
6460 deg
RA of node: 76
0679 deg
Eccentricity:
0004676
Arg of perigee: 80
6814 deg
Mean anomaly: 279
4876 deg
Mean motion: 15
71082532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2822
Checksum: 330
Coasting Arc #10 (Orbit 2837)
---------------------------------------
Vector Time (GMT): 2010/199/08:16:07
509
Vector Time (MET): N/A
Weight (LBS) : 828051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4254415
29 A = 6728761
75 meter
Y = 193826
06 meter E =
0008220
Z = 5203270
77 I = 51
94707
XDOT = -1712
999691 Wp = 70
87730
YDOT = -7425
243880 meter/sec RA = 70
40293 deg
ZDOT = -1119
963560 TA = 29
78742
MA = 29
74066
Ha = 196
365 n
mi
Hp = 186
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13958055
42 X = -4281542
91
Y = 635912
26 feet Y = 146098
44 meter
Z = 17071098
34 Z = 5182537
05
XDOT = -5620
077727 XDOT = -1624
401394
YDOT = -24361
036351 feet/sec YDOT = -7443
904172 meter/sec
ZDOT = -3674
421128 ZDOT = -1128
070820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6632329
95 X = -2021534
17
Y = 12412387
79 feet Y = 3783295
80 meter
Z = 16988199
52 Z = 5178003
21
XDOT = -22898
800923 XDOT = -6979
554521
YDOT = -7143
903445 feet/sec YDOT = -2177
461770 meter/sec
ZDOT = -3706
810308 ZDOT = -1129
835782
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 10199
39036329
00016717 00000-0 10270-3 0 9091
2 25544 51
6461 70
8651 0004595 83
8326 276
3359 15
71110149 28381
Satellite: ISS
Catalog Number: 25544
Epoch time: 10199
39036329 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 70
8651 deg
Eccentricity:
0004595
Arg of perigee: 83
8326 deg
Mean anomaly: 276
3359 deg
Mean motion: 15
71110149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2838
Checksum: 326
Coasting Arc #11 (Orbit 2853)
---------------------------------------
Vector Time (GMT): 2010/200/08:16:07
509
Vector Time (MET): N/A
Weight (LBS) : 828051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2798456
73 A = 6740456
16 meter
Y = 6125407
47 meter E =
0016085
Z = 18742
62 I = 51
97525
XDOT = -4323
831032 Wp = 56
40828
YDOT = 1945
534298 meter/sec RA = 65
32152 deg
ZDOT = 6063
089876 TA = 303
79414
MA = 303
94722
Ha = 196
273 n
mi
Hp = 186
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9181288
50 X = 2729662
28
Y = 20096481
18 feet Y = 6156316
83 meter
Z = 61491
54 Z = 32171
11
XDOT = -14185
797350 XDOT = -4374
718272
YDOT = 6382
986542 feet/sec YDOT = 1896
897384 meter/sec
ZDOT = 19892
027153 ZDOT = 6041
961412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22004314
55 X = 6706915
07
Y = 1991300
36 feet Y = 606948
35 meter
Z = 115150
92 Z = 35098
00
XDOT = -1402
819342 XDOT = -427
579335
YDOT = 13981
860556 feet/sec YDOT = 4261
671097 meter/sec
ZDOT = 19807
538761 ZDOT = 6037
337814
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 10200
40807404
00016717 00000-0 10270-3 0 9108
2 25544 51
6463 65
6614 0004622 87
0418 273
1273 15
71096034 28547
Satellite: ISS
Catalog Number: 25544
Epoch time: 10200
40807404 = yrday
fracday
Element set: 910
Inclination: 51
6463 deg
RA of node: 65
6614 deg
Eccentricity:
0004622
Arg of perigee: 87
0418 deg
Mean anomaly: 273
1273 deg
Mean motion: 15
71096034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2854
Checksum: 279
Coasting Arc #12 (Orbit 2868)
---------------------------------------
Vector Time (GMT): 2010/201/08:16:07
509
Vector Time (MET): N/A
Weight (LBS) : 828051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2983777
03 A = 6728635
61 meter
Y = -3034151
96 meter E =
0019119
Z = -5228615
18 I = 51
92313
XDOT = 4460
909031 Wp = 84
03487
YDOT = 6167
923601 meter/sec RA = 60
23798 deg
ZDOT = -1034
838749 TA = 176
11919
MA = 176
10434
Ha = 196
216 n
mi
Hp = 186
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9789294
73 X = 3042883
25
Y = -9954566
79 feet Y = -3000454
38 meter
Z = -17154249
29 Z = -5213976
91
XDOT = 14635
528317 XDOT = 4396
633674
YDOT = 20235
969821 feet/sec YDOT = 6217
448910 meter/sec
ZDOT = -3395
140253 ZDOT = -1013
323026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3973498
54 X = -1211122
35
Y = -13458840
09 feet Y = -4102254
46 meter
Z = -17095698
07 Z = -5210768
77
XDOT = 23808
290618 XDOT = 7256
766980
YDOT = -2831
015637 feet/sec YDOT = -862
893566 meter/sec
ZDOT = -3309
153583 ZDOT = -1008
630012
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 10201
36216871
00016717 00000-0 10270-3 0 9117
2 25544 51
6473 60
7831 0004656 90
6309 269
5386 15
71129851 28695
Satellite: ISS
Catalog Number: 25544
Epoch time: 10201
36216871 = yrday
fracday
Element set: 911
Inclination: 51
6473 deg
RA of node: 60
7831 deg
Eccentricity:
0004656
Arg of perigee: 90
6309 deg
Mean anomaly: 269
5386 deg
Mean motion: 15
71129851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2869
Checksum: 316
Coasting Arc #13 (Orbit 2884)
---------------------------------------
Vector Time (GMT): 2010/202/08:16:07
509
Vector Time (MET): N/A
Weight (LBS) : 828051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4777825
77 A = 6739028
82 meter
Y = -4384932
84 meter E =
0018510
Z = 1803468
56 I = 51
94191
XDOT = 2155
434688 Wp = 109
47137
YDOT = -4708
969490 meter/sec RA = 55
12036 deg
ZDOT = -5697
988747 TA = 50
63479
MA = 50
47095
Ha = 196
253 n
mi
Hp = 186
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15675281
41 X = -4737198
41
Y = -14386262
58 feet Y = -4438134
45 meter
Z = 5916891
61 Z = 1780356
08
XDOT = 7071
636117 XDOT = 2235
610625
YDOT = -15449
374966 feet/sec YDOT = -4684
416980 meter/sec
ZDOT = -18694
188801 ZDOT = -5687
323694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20046591
85 X = -6110201
20
Y = 7204015
14 feet Y = 2195783
81 meter
Z = 5824510
78 Z = 1775310
89
XDOT = -9803
087285 XDOT = -2987
981004
YDOT = -12088
427484 feet/sec YDOT = -3684
552697 meter/sec
ZDOT = -18651
503830 ZDOT = -5684
978367
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 10202
37986233
00016717 00000-0 10270-3 0 9126
2 25544 51
6473 55
5798 0004623 94
7448 265
4242 15
71118494 28857
Satellite: ISS
Catalog Number: 25544
Epoch time: 10202
37986233 = yrday
fracday
Element set: 912
Inclination: 51
6473 deg
RA of node: 55
5798 deg
Eccentricity:
0004623
Arg of perigee: 94
7448 deg
Mean anomaly: 265
4242 deg
Mean motion: 15
71118494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2885
Checksum: 327
Coasting Arc #14 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2010/203/08:16:07
509
Vector Time (MET): N/A
Weight (LBS) : 828051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -572940
40 A = 6731255
50 meter
Y = 4899752
31 meter E =
0012968
Z = 4571227
13 I = 51
89814
XDOT = -6106
026050 Wp = 108
28623
YDOT = -3568
956945 meter/sec RA = 50
06528 deg
ZDOT = 3049
140130 TA = 311
45274
MA = 311
56405
Ha = 196
195 n
mi
Hp = 186
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1879725
71 X = -649893
66
Y = 16075302
85 feet Y = 4892914
36 meter
Z = 14997464
33 Z = 4568257
67
XDOT = -20032
893864 XDOT = -6080
475501
YDOT = -11709
176328 feet/sec YDOT = -3637
095792 meter/sec
ZDOT = 10003
740583 ZDOT = 3019
538905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13466743
19 X = 4104663
32
Y = 8997387
74 feet Y = 2742403
78 meter
Z = 14985543
31 Z = 4567593
60
XDOT = -18846
599781 XDOT = -5744
443613
YDOT = 11683
688699 feet/sec YDOT = 3561
188315 meter/sec
ZDOT = 9885
405632 ZDOT = 3013
071637
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 10203
39754652
00016717 00000-0 10270-3 0 9138
2 25544 51
6475 50
3765 0004591 97
5782 262
5902 15
71144703 29014
Satellite: ISS
Catalog Number: 25544
Epoch time: 10203
39754652 = yrday
fracday
Element set: 913
Inclination: 51
6475 deg
RA of node: 50
3765 deg
Eccentricity:
0004591
Arg of perigee: 97
5782 deg
Mean anomaly: 262
5902 deg
Mean motion: 15
71144703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 306
Coasting Arc #15 (Orbit 2915)
---------------------------------------
Vector Time (GMT): 2010/204/08:16:07
509
Vector Time (MET): N/A
Weight (LBS) : 828051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5538663
80 A = 6735243
87 meter
Y = 1720724
81 meter E =
0009372
Z = -3433092
15 I = 51
89177
XDOT = 966
287172 Wp = 94
84320
YDOT = 6073
585205 meter/sec RA = 44
92183 deg
ZDOT = 4613
088159 TA = 224
81306
MA = 224
88879
Ha = 196
115 n
mi
Hp = 186
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18171469
15 X = 5535687
76
Y = 5645422
59 feet Y = 1782645
34 meter
Z = -11263425
68 Z = -3406192
72
XDOT = 3170
233505 XDOT = 875
890238
YDOT = 19926
460645 feet/sec YDOT = 6083
884660 meter/sec
ZDOT = 15134
803670 ZDOT = 4617
563669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13015388
60 X = 3967090
44
Y = -13967247
01 feet Y = -4257216
89 meter
Z = -11155873
62 Z = -3400310
28
XDOT = 18264
838745 XDOT = 5567
122849
YDOT = 4943
830358 feet/sec YDOT = 1506
879493 meter/sec
ZDOT = 15152
638407 ZDOT = 4618
524186
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 10204
35161765
00016717 00000-0 10270-3 0 9143
2 25544 51
6480 45
4981 0004504 100
2232 259
9438 15
71166605 29166
Satellite: ISS
Catalog Number: 25544
Epoch time: 10204
35161765 = yrday
fracday
Element set: 914
Inclination: 51
6480 deg
RA of node: 45
4981 deg
Eccentricity:
0004504
Arg of perigee: 100
2232 deg
Mean anomaly: 259
9438 deg
Mean motion: 15
71166605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2916
Checksum: 293
Coasting Arc #16 (Orbit 2931)
---------------------------------------
Vector Time (GMT): 2010/205/08:16:07
509
Vector Time (MET): N/A
Weight (LBS) : 828051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2262165
85 A = 6735232
30 meter
Y = -5362994
50 meter E =
0009175
Z = -3395694
20 I = 51
86982
XDOT = 6115
390211 Wp = 95
85167
YDOT = 355
580339 meter/sec RA = 39
87545 deg
ZDOT = -4647
191155 TA = 123
98570
MA = 123
89849
Ha = 196
015 n
mi
Hp = 186
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7421803
98 X = -2185532
40
Y = -17595126
31 feet Y = -5387862
42 meter
Z = -11140729
00 Z = -3406498
21
XDOT = 20063
616177 XDOT = 6133
534301
YDOT = 1166
602162 feet/sec YDOT = 424
068394 meter/sec
ZDOT = -15246
690142 ZDOT = -4617
439054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19058230
42 X = -5808948
63
Y = -701577
72 feet Y = -213840
89 meter
Z = -11183878
07 Z = -3408846
04
XDOT = 9459
410931 XDOT = 2883
228452
YDOT = -16416
783990 feet/sec YDOT = -5003
835760 meter/sec
ZDOT = -15127
712088 ZDOT = -4610
926644
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 10205
36928514
00016717 00000-0 10270-3 0 9159
2 25544 51
6481 40
2943 0004335 104
3595 255
8049 15
71161745 29328
Satellite: ISS
Catalog Number: 25544
Epoch time: 10205
36928514 = yrday
fracday
Element set: 915
Inclination: 51
6481 deg
RA of node: 40
2943 deg
Eccentricity:
0004335
Arg of perigee: 104
3595 deg
Mean anomaly: 255
8049 deg
Mean motion: 15
71161745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2932
Checksum: 301
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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