Date:
April 18th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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
113/20:49:49
979 -7
0 7
9 7
9
N/A 3
3 -0
4 189
4
000/00:19:35
957 1
8 0
2 188
3
Coasting Arc #1 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2010/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3116559
22 A = 6721154
27 meter
Y = 3919369
14 meter E =
0008955
Z = -4490265
06 I = 51
59887
XDOT = -6786
287739 Wp = 97
31504
YDOT = 1781
830247 meter/sec RA = 186
21260 deg
ZDOT = -3161
359449 TA = 141
10337
MA = 141
03890
Ha = 189
432 n
mi
Hp = 182
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10224931
82 X = 3094313
78
Y = 12858822
64 feet Y = 3954095
94 meter
Z = -14731840
75 Z = -4475178
61
XDOT = -22264
723554 XDOT = -6790
350519
YDOT = 5845
899762 feet/sec YDOT = 1705
919200 meter/sec
ZDOT = -10371
914204 ZDOT = -3194
337707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14617034
66 X = 4455272
16
Y = 7616339
49 feet Y = 2321460
28 meter
Z = -14671719
48 Z = -4471940
10
XDOT = -17412
990384 XDOT = -5307
479469
YDOT = 13227
257864 feet/sec YDOT = 4031
668197 meter/sec
ZDOT = -10502
960748 ZDOT = -3201
302436
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 10106
52154136
00016717 00000-0 10270-3 0 9002
2 25544 51
6466 187
1164 0004502 182
9065 177
2073 15
74817099 13765
Satellite: ISS
Catalog Number: 25544
Epoch time: 10106
52154136 = yrday
fracday
Element set: 900
Inclination: 51
6466 deg
RA of node: 187
1164 deg
Eccentricity:
0004502
Arg of perigee: 182
9065 deg
Mean anomaly: 177
2073 deg
Mean motion: 15
74817099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 301
Coasting Arc #2 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2010/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5950251
25 A = 6726853
58 meter
Y = -1869323
37 meter E =
0015058
Z = 2496799
97 I = 51
64905
XDOT = 3582
094187 Wp = 120
62584
YDOT = 4274
291272 meter/sec RA = 181
02495 deg
ZDOT = -5320
457991 TA = 31
08605
MA = 30
99704
Ha = 189
115 n
mi
Hp = 182
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19521821
70 X = 5958582
93
Y = -6132950
67 feet Y = -1802737
57 meter
Z = 8191600
94 Z = 2525726
96
XDOT = 11752
277517 XDOT = 3559
878302
YDOT = 14023
265328 feet/sec YDOT = 4314
224244 meter/sec
ZDOT = -17455
570836 ZDOT = -5303
109798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15120205
99 X = 4608638
79
Y = -13718508
85 feet Y = -4181401
50 meter
Z = 8306552
72 Z = 2531837
27
XDOT = 15634
482515 XDOT = 4765
390271
YDOT = 6672
912388 feet/sec YDOT = 2033
903696 meter/sec
ZDOT = -17386
440817 ZDOT = -5299
387161
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 10107
53682076
00016717 00000-0 10270-3 0 9014
2 25544 51
6464 181
8968 0004273 185
5575 174
5542 15
74890643 13921
Satellite: ISS
Catalog Number: 25544
Epoch time: 10107
53682076 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 181
8968 deg
Eccentricity:
0004273
Arg of perigee: 185
5575 deg
Mean anomaly: 174
5542 deg
Mean motion: 15
74890643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 329
Coasting Arc #3 (Orbit 1407)
---------------------------------------
Vector Time (GMT): 2010/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3098557
44 A = 6719643
94 meter
Y = -3567035
25 meter E =
0009699
Z = 4776268
47 I = 51
65486
XDOT = 6824
936783 Wp = 144
49735
YDOT = -2505
388978 meter/sec RA = 175
92551 deg
ZDOT = 2546
193753 TA = 280
52205
MA = 280
63131
Ha = 189
070 n
mi
Hp = 182
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10165870
87 X = -3081642
46
Y = -11702871
55 feet Y = -3601590
73 meter
Z = 15670172
15 Z = 4761256
47
XDOT = 22391
524880 XDOT = 6840
076141
YDOT = -8219
780110 feet/sec YDOT = -2428
983907 meter/sec
ZDOT = 8353
654046 ZDOT = 2579
386403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14320442
70 X = -4364870
94
Y = -6090835
53 feet Y = -1856486
67 meter
Z = 15610351
42 Z = 4758035
11
XDOT = 16116
581632 XDOT = 4912
334082
YDOT = -16057
376148 feet/sec YDOT = -4894
288250 meter/sec
ZDOT = 8485
563228 ZDOT = 2586
399672
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 10108
55207020
00016717 00000-0 10270-3 0 9020
2 25544 51
6460 176
6765 0004286 190
6484 169
4590 15
74938339 14083
Satellite: ISS
Catalog Number: 25544
Epoch time: 10108
55207020 = yrday
fracday
Element set: 902
Inclination: 51
6460 deg
RA of node: 176
6765 deg
Eccentricity:
0004286
Arg of perigee: 190
6484 deg
Mean anomaly: 169
4590 deg
Mean motion: 15
74938339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1408
Checksum: 317
Coasting Arc #4 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2010/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5942013
15 A = 6727816
82 meter
Y = 2503683
11 meter E =
0003658
Z = -1920205
39 I = 51
71199
XDOT = -3474
292455 Wp = 68
03856
YDOT = -3936
103667 meter/sec RA = 170
74856 deg
ZDOT = 5628
812775 TA = 270
63825
MA = 270
68016
Ha = 188
849 n
mi
Hp = 182
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19494793
80 X = -5960240
08
Y = 8214183
43 feet Y = 2437134
15 meter
Z = -6299886
45 Z = -1949116
09
XDOT = -11398
597293 XDOT = -3457
363984
YDOT = -12913
725943 feet/sec YDOT = -3974
860835 meter/sec
ZDOT = 18467
233514 ZDOT = 5611
975501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13689766
13 X = -4172640
72
Y = 16082574
43 feet Y = 4901968
69 meter
Z = -6414785
06 Z = -1955226
49
XDOT = -14910
414086 XDOT = -4544
694213
YDOT = -5365
500275 feet/sec YDOT = -1635
404484 meter/sec
ZDOT = 18400
134541 ZDOT = 5608
361008
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 10109
50384159
00016717 00000-0 10270-3 0 9036
2 25544 51
6452 171
7826 0004067 194
1169 165
9882 15
74945624 14231
Satellite: ISS
Catalog Number: 25544
Epoch time: 10109
50384159 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 171
7826 deg
Eccentricity:
0004067
Arg of perigee: 194
1169 deg
Mean anomaly: 165
9882 deg
Mean motion: 15
74945624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 321
Coasting Arc #5 (Orbit 1438)
---------------------------------------
Vector Time (GMT): 2010/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2937083
96 A = 6718404
19 meter
Y = 3352736
25 meter E =
0011747
Z = -5036714
05 I = 51
71017
XDOT = -6756
393365 Wp = 93
87297
YDOT = 3204
986499 meter/sec RA = 165
64332 deg
ZDOT = -1810
847864 TA = 158
70248
MA = 158
65355
Ha = 188
740 n
mi
Hp = 182
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9636102
24 X = 2923842
29
Y = 10999790
84 feet Y = 3385506
60 meter
Z = -16524652
39 Z = -5022477
70
XDOT = -22166
644897 XDOT = -6782
933147
YDOT = 10515
047568 feet/sec YDOT = 3129
284158 meter/sec
ZDOT = -5941
101917 ZDOT = -1843
734883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13730110
62 X = 4184937
72
Y = 5215934
42 feet Y = 1589816
81 meter
Z = -16467910
97 Z = -5019419
26
XDOT = -14329
052734 XDOT = -4367
495273
YDOT = 18594
437133 feet/sec YDOT = 5667
584438 meter/sec
ZDOT = -6071
809962 ZDOT = -1850
687676
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 10110
51903612
00016717 00000-0 10270-3 0 9041
2 25544 51
6452 166
5616 0004060 196
7684 163
3346 15
74991470 14397
Satellite: ISS
Catalog Number: 25544
Epoch time: 10110
51903612 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 166
5616 deg
Eccentricity:
0004060
Arg of perigee: 196
7684 deg
Mean anomaly: 163
3346 deg
Mean motion: 15
74991470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1439
Checksum: 302
Coasting Arc #6 (Orbit 1454)
---------------------------------------
Vector Time (GMT): 2010/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5835470
70 A = 6728416
54 meter
Y = -3096490
34 meter E =
0015135
Z = 1229940
89 I = 51
77451
XDOT = 3247
106306 Wp = 135
86974
YDOT = 3768
212374 meter/sec RA = 160
48066 deg
ZDOT = -5886
661681 TA = 30
65682
MA = 30
56847
Ha = 188
450 n
mi
Hp = 182
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19145245
09 X = 5863687
68
Y = -10159089
05 feet Y = -3031076
89 meter
Z = 4035239
14 Z = 1258358
09
XDOT = 10653
235913 XDOT = 3233
324476
YDOT = 12362
901488 feet/sec YDOT = 3804
446491 meter/sec
ZDOT = -19313
194490 ZDOT = -5870
920654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11900106
46 X = 3627152
45
Y = -18088965
67 feet Y = -5513516
74 meter
Z = 4148185
39 Z = 1264366
91
XDOT = 14059
607770 XDOT = 4285
368448
YDOT = 4811
041960 feet/sec YDOT = 1466
405589 meter/sec
ZDOT = -19250
446126 ZDOT = -5867
535979
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 10111
53420071
00016717 00000-0 10270-3 0 9058
2 25544 51
6458 161
3408 0003820 200
4515 159
6497 15
75078976 14555
Satellite: ISS
Catalog Number: 25544
Epoch time: 10111
53420071 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 161
3408 deg
Eccentricity:
0003820
Arg of perigee: 200
4515 deg
Mean anomaly: 159
6497 deg
Mean motion: 15
75078976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 297
Coasting Arc #7 (Orbit 1470)
---------------------------------------
Vector Time (GMT): 2010/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2718447
03 A = 6717294
35 meter
Y = -3263739
13 meter E =
0005764
Z = 5203330
90 I = 51
76491
XDOT = 6579
396032 Wp = 164
50675
YDOT = -3881
202005 meter/sec RA = 155
36734 deg
ZDOT = 997
216797 TA = 275
97479
MA = 276
04047
Ha = 188
447 n
mi
Hp = 182
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8918789
48 X = -2707026
08
Y = -10707805
55 feet Y = -3294074
54 meter
Z = 17071295
60 Z = 5190152
46
XDOT = 21585
944988 XDOT = 6617
463040
YDOT = -12733
602377 feet/sec YDOT = -3807
414433 meter/sec
ZDOT = 3271
708650 ZDOT = 1029
271945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13136403
42 X = -4003975
76
Y = -4840246
30 feet Y = -1475307
07 meter
Z = 17018753
17 Z = 5187315
97
XDOT = 12084
729324 XDOT = 3683
425498
YDOT = -20780
333165 feet/sec YDOT = -6333
845549 meter/sec
ZDOT = 3399
114666 ZDOT = 1036
050150
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 10112
54933752
00016717 00000-0 10270-3 0 9066
2 25544 51
6454 156
1201 0003832 203
1913 156
9079 15
75107636 14719
Satellite: ISS
Catalog Number: 25544
Epoch time: 10112
54933752 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 156
1201 deg
Eccentricity:
0003832
Arg of perigee: 203
1913 deg
Mean anomaly: 156
9079 deg
Mean motion: 15
75107636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1471
Checksum: 289
Coasting Arc #8 (Orbit 1485)
---------------------------------------
Vector Time (GMT): 2010/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5622334
22 A = 6728862
66 meter
Y = 3658903
12 meter E =
0007629
Z = -487747
35 I = 51
83151
XDOT = -2965
789443 Wp = 47
82913
YDOT = -3762
314146 meter/sec RA = 150
22112 deg
ZDOT = 6028
336360 TA = 306
87836
MA = 306
94826
Ha = 188
202 n
mi
Hp = 182
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18445978
41 X = -5660461
48
Y = 12004275
33 feet Y = 3595817
64 meter
Z = -1600220
97 Z = -515153
37
XDOT = -9730
280326 XDOT = -2952
782724
YDOT = -12343
550347 feet/sec YDOT = -3795
406478 meter/sec
ZDOT = 19778
006429 ZDOT = 6013
960248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9740918
34 X = -2969031
91
Y = 19725891
11 feet Y = 6012451
61 meter
Z = -1709146
77 Z = -520947
94
XDOT = -13324
970905 XDOT = -4061
451132
YDOT = -4888
597294 feet/sec YDOT = -1490
044455 meter/sec
ZDOT = 19720
677483 ZDOT = 6010
862497
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 10113
50100271
00016717 00000-0 10270-3 0 9076
2 25544 51
6458 151
2253 0003638 207
5409 152
5562 15
75121682 14860
Satellite: ISS
Catalog Number: 25544
Epoch time: 10113
50100271 = yrday
fracday
Element set: 907
Inclination: 51
6458 deg
RA of node: 151
2253 deg
Eccentricity:
0003638
Arg of perigee: 207
5409 deg
Mean anomaly: 152
5562 deg
Mean motion: 15
75121682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1486
Checksum: 280
Coasting Arc #9 (Orbit 1491)
---------------------------------------
Vector Time (GMT): 2010/113/20:59:37
957
Vector Time (MET): N/A
Weight (LBS) : 796736
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3089290
15 A = 6728984
51 meter
Y = 4973456
10 meter E =
0003967
Z = -3314877
07 I = 51
82685
XDOT = -6054
039110 Wp = 250
41885
YDOT = -614
585502 meter/sec RA = 148
27704 deg
ZDOT = 4714
102844 TA = 70
77286
MA = 70
72994
Ha = 189
444 n
mi
Hp = 188
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10135466
38 X = -3128571
53
Y = 16317113
20 feet Y = 4938690
08 meter
Z = -10875580
94 Z = -3329980
45
XDOT = -19862
333038 XDOT = -6069
617049
YDOT = -2016
356635 feet/sec YDOT = -682
372312 meter/sec
ZDOT = 15466
216679 ZDOT = 4684
654460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13736371
65 X = 4186846
08
Y = -13378369
96 feet Y = -4077727
16 meter
Z = -10935512
53 Z = -3333144
22
XDOT = 17888
541975 XDOT = 5452
427594
YDOT = 5805
302672 feet/sec YDOT = 1769
456254 meter/sec
ZDOT = 15349
017767 ZDOT = 4678
380615
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 10113
88166336
00016717 00000-0 10270-3 0 9082
2 25544 51
6472 149
2666 0008645 259
6844 100
3345 15
73425090 14920
Satellite: ISS
Catalog Number: 25544
Epoch time: 10113
88166336 = yrday
fracday
Element set: 908
Inclination: 51
6472 deg
RA of node: 149
2666 deg
Eccentricity:
0008645
Arg of perigee: 259
6844 deg
Mean anomaly: 100
3345 deg
Mean motion: 15
73425090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1492
Checksum: 316
Coasting Arc #10 (Orbit 1507)
---------------------------------------
Vector Time (GMT): 2010/114/20:59:37
957
Vector Time (MET): N/A
Weight (LBS) : 796736
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5398168
90 A = 6726830
55 meter
Y = -101117
57 meter E =
0002361
Z = -4011696
75 I = 51
84486
XDOT = -2821
251721 Wp = 302
79544
YDOT = 5978
970458 meter/sec RA = 143
21113 deg
ZDOT = -3944
079485 TA = 286
53369
MA = 286
55963
Ha = 189
289 n
mi
Hp = 188
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17710527
88 X = 5418386
63
Y = -331750
57 feet Y = -40639
17 meter
Z = -13161734
74 Z = -3985423
17
XDOT = -9256
075199 XDOT = -2868
740213
YDOT = 19616
044809 feet/sec YDOT = 5947
155847 meter/sec
ZDOT = -12939
893323 ZDOT = -3957
900821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17400960
89 X = -5303812
88
Y = -3704127
06 feet Y = -1129017
93 meter
Z = -13057186
54 Z = -3979830
46
XDOT = 13112
672707 XDOT = 3996
742641
YDOT = -15758
843676 feet/sec YDOT = -4803
295552 meter/sec
ZDOT = -12994
696581 ZDOT = -3960
783518
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 10114
89786120
00016717 00000-0 10270-3 0 9094
2 25544 51
6473 144
0533 0008739 264
1343 95
8824 15
73459497 15082
Satellite: ISS
Catalog Number: 25544
Epoch time: 10114
89786120 = yrday
fracday
Element set: 909
Inclination: 51
6473 deg
RA of node: 144
0533 deg
Eccentricity:
0008739
Arg of perigee: 264
1343 deg
Mean anomaly: 95
8824 deg
Mean motion: 15
73459497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1508
Checksum: 330
Coasting Arc #11 (Orbit 1523)
---------------------------------------
Vector Time (GMT): 2010/115/20:59:37
957
Vector Time (MET): N/A
Weight (LBS) : 796736
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1825622
09 A = 6728040
22 meter
Y = -5404115
71 meter E =
0003501
Z = 3565239
35 I = 51
87241
XDOT = 6206
249263 Wp = 82
74517
YDOT = -857
669665 meter/sec RA = 138
04399 deg
ZDOT = -4473
860534 TA = 54
89599
MA = 54
86318
Ha = 188
813 n
mi
Hp = 188
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5989573
80 X = 1868596
71
Y = -17730038
41 feet Y = -5383460
09 meter
Z = 11696979
49 Z = 3574212
93
XDOT = 20361
710182 XDOT = 6237
112079
YDOT = -2813
876854 feet/sec YDOT = -788
095305 meter/sec
ZDOT = -14678
020126 ZDOT = -4443
635219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9505827
02 X = -2897376
08
Y = 16094590
63 feet Y = 4905631
22 meter
Z = 11732518
52 Z = 3576071
65
XDOT = -19409
779575 XDOT = -5916
100814
YDOT = -841
720938 feet/sec YDOT = -256
556542 meter/sec
ZDOT = -14557
764632 ZDOT = -4437
206660
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 10115
91403415
00016717 00000-0 10270-3 0 9103
2 25544 51
6467 138
8395 0008620 268
2765 91
7411 15
73500778 15248
Satellite: ISS
Catalog Number: 25544
Epoch time: 10115
91403415 = yrday
fracday
Element set: 910
Inclination: 51
6467 deg
RA of node: 138
8395 deg
Eccentricity:
0008620
Arg of perigee: 268
2765 deg
Mean anomaly: 91
7411 deg
Mean motion: 15
73500778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1524
Checksum: 305
Coasting Arc #12 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2010/116/20:59:37
957
Vector Time (MET): N/A
Weight (LBS) : 796736
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5368859
13 A = 6727342
54 meter
Y = 1376467
83 meter E =
0003060
Z = 3811368
60 I = 51
89155
XDOT = 1369
418689 Wp = 112
01468
YDOT = -6303
610926 meter/sec RA = 132
98016 deg
ZDOT = 4201
761963 TA = 294
04945
MA = 294
08147
Ha = 188
875 n
mi
Hp = 188
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17614367
21 X = -5402367
26
Y = 4515970
58 feet Y = 1316242
79 meter
Z = 12504490
17 Z = 3785204
82
XDOT = 4492
843467 XDOT = 1419
393273
YDOT = -20681
138208 feet/sec YDOT = -6288
017747 meter/sec
ZDOT = 13785
308278 ZDOT = 4208
536253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18226585
25 X = 5555463
18
Y = -1021614
10 feet Y = -311387
98 meter
Z = 12400406
92 Z = 3779644
03
XDOT = -8390
294823 XDOT = -2557
361862
YDOT = 18113
217672 feet/sec YDOT = 5520
908747 meter/sec
ZDOT = 13812
078035 ZDOT = 4209
921385
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 10116
93018100
00016717 00000-0 10270-3 0 9110
2 25544 51
6466 133
6245 0008635 272
6094 87
4080 15
73517691 15408
Satellite: ISS
Catalog Number: 25544
Epoch time: 10116
93018100 = yrday
fracday
Element set: 911
Inclination: 51
6466 deg
RA of node: 133
6245 deg
Eccentricity:
0008635
Arg of perigee: 272
6094 deg
Mean anomaly: 87
4080 deg
Mean motion: 15
73517691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1540
Checksum: 292
Coasting Arc #13 (Orbit 1554)
---------------------------------------
Vector Time (GMT): 2010/117/20:59:37
957
Vector Time (MET): N/A
Weight (LBS) : 796736
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -567065
58 A = 6727211
23 meter
Y = 5544356
51 meter E =
0002908
Z = -3765449
07 I = 51
91110
XDOT = -5994
828995 Wp = 260
21569
YDOT = 2280
951557 meter/sec RA = 127
81461 deg
ZDOT = 4258
089468 TA = 54
44386
MA = 54
41675
Ha = 189
039 n
mi
Hp = 188
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1860451
39 X = -610729
19
Y = 18190146
03 feet Y = 5537771
11 meter
Z = -12353835
54 Z = -3768310
00
XDOT = -19668
074132 XDOT = -6040
574898
YDOT = 7483
436867 feet/sec YDOT = 2213
658034 meter/sec
ZDOT = 13970
109803 ZDOT = 4228
854883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4959009
78 X = 1511506
18
Y = -17591853
57 feet Y = -5361996
97 meter
Z = -12365065
89 Z = -3768872
08
XDOT = 19475
579869 XDOT = 5936
156744
YDOT = -4255
133775 feet/sec YDOT = -1296
964775 meter/sec
ZDOT = 13853
821457 ZDOT = 4222
644780
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 10117
88279365
00016717 00000-0 10270-3 0 9128
2 25544 51
6462 128
7358 0008843 276
1794 83
8361 15
73574434 15557
Satellite: ISS
Catalog Number: 25544
Epoch time: 10117
88279365 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 128
7358 deg
Eccentricity:
0008843
Arg of perigee: 276
1794 deg
Mean anomaly: 83
8361 deg
Mean motion: 15
73574434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1555
Checksum: 339
Coasting Arc #14 (Orbit 1570)
---------------------------------------
Vector Time (GMT): 2010/118/20:59:37
957
Vector Time (MET): N/A
Weight (LBS) : 796736
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5041462
24 A = 6727673
88 meter
Y = -2573034
10 meter E =
0004102
Z = -3635827
43 I = 51
92979
XDOT = 41
140741 Wp = 304
84614
YDOT = 6312
844443 meter/sec RA = 122
75374 deg
ZDOT = -4404
705163 TA = 278
50859
MA = 278
55508
Ha = 189
182 n
mi
Hp = 188
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16540230
46 X = 5087522
24
Y = -8441712
92 feet Y = -2516399
84 meter
Z = -11928567
68 Z = -3611223
68
XDOT = 134
976184 XDOT = -8
055970
YDOT = 20711
431901 feet/sec YDOT = 6313
029544 meter/sec
ZDOT = -14451
132426 ZDOT = -4404
624636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17740726
29 X = -5407373
37
Y = 5695042
38 feet Y = 1735848
92 meter
Z = -11830705
41 Z = -3605999
01
XDOT = 3489
402800 XDOT = 1063
569974
YDOT = -19189
134525 feet/sec YDOT = -5848
848203 meter/sec
ZDOT = -14450
648089 ZDOT = -4404
557537
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 10118
89888965
00016717 00000-0 10270-3 0 9133
2 25544 51
6457 123
5213 0008924 279
5954 80
4200 15
73596600 15711
Satellite: ISS
Catalog Number: 25544
Epoch time: 10118
89888965 = yrday
fracday
Element set: 913
Inclination: 51
6457 deg
RA of node: 123
5213 deg
Eccentricity:
0008924
Arg of perigee: 279
5954 deg
Mean anomaly: 80
4200 deg
Mean motion: 15
73596600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1571
Checksum: 328
Coasting Arc #15 (Orbit 1586)
---------------------------------------
Vector Time (GMT): 2010/119/20:59:37
957
Vector Time (MET): N/A
Weight (LBS) : 796736
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -623711
16 A = 6726374
02 meter
Y = -5431734
45 meter E =
0004790
Z = 3919303
60 I = 51
94231
XDOT = 5466
341283 Wp = 29
46768
YDOT = -3572
354766 meter/sec RA = 117
59012 deg
ZDOT = -4074
825319 TA = 102
80670
MA = 102
75317
Ha = 189
292 n
mi
Hp = 187
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2046296
44 X = -581965
80
Y = -17820651
07 feet Y = -5438475
94 meter
Z = 12858607
62 Z = 3916374
68
XDOT = 17934
190560 XDOT = 5525
676863
YDOT = -11720
324034 feet/sec YDOT = -3510
894916 meter/sec
ZDOT = -13368
849472 ZDOT = -4048
125377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -428428
01 X = -130584
86
Y = 17941081
23 feet Y = 5468441
56 meter
Z = 12846819
74 Z = 3915710
66
XDOT = -18185
372965 XDOT = -5542
901680
YDOT = 9077
052192 feet/sec YDOT = 2766
685508 meter/sec
ZDOT = -13262
652726 ZDOT = -4042
456551
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 10119
91495828
00016717 00000-0 10270-3 0 9140
2 25544 51
6462 118
3062 0008924 284
5437 75
4736 15
73698244 15875
Satellite: ISS
Catalog Number: 25544
Epoch time: 10119
91495828 = yrday
fracday
Element set: 914
Inclination: 51
6462 deg
RA of node: 118
3062 deg
Eccentricity:
0008924
Arg of perigee: 284
5437 deg
Mean anomaly: 75
4736 deg
Mean motion: 15
73698244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1587
Checksum: 339
Coasting Arc #16 (Orbit 1602)
---------------------------------------
Vector Time (GMT): 2010/120/20:59:37
957
Vector Time (MET): N/A
Weight (LBS) : 796736
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4461322
08 A = 6727862
16 meter
Y = 3622250
77 meter E =
0004599
Z = 3492881
30 I = 51
95914
XDOT = -1348
318494 Wp = 58
22041
YDOT = -6058
166125 meter/sec RA = 112
52945 deg
ZDOT = 4558
405750 TA = 343
04053
MA = 343
05590
Ha = 189
620 n
mi
Hp = 187
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14636883
47 X = -4518463
21
Y = 11884024
84 feet Y = 3572041
87 meter
Z = 11459584
33 Z = 3471069
32
XDOT = -4423
617107 XDOT = -1302
619037
YDOT = -19875
873114 feet/sec YDOT = -6072
988625 meter/sec
ZDOT = 14955
399442 ZDOT = 4551
966097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16073009
21 X = 4899053
21
Y = -9955279
21 feet Y = -3034369
10 meter
Z = 11372830
25 Z = 3466438
66
XDOT = 1268
609784 XDOT = 386
672262
YDOT = 19111
194954 feet/sec YDOT = 5825
092222 meter/sec
ZDOT = 14929
631475 ZDOT = 4550
551674
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 10120
93100318
00016717 00000-0 10270-3 0 9152
2 25544 51
6454 113
0904 0008902 288
2922 71
7272 15
73680371 16034
Satellite: ISS
Catalog Number: 25544
Epoch time: 10120
93100318 = yrday
fracday
Element set: 915
Inclination: 51
6454 deg
RA of node: 113
0904 deg
Eccentricity:
0008902
Arg of perigee: 288
2922 deg
Mean anomaly: 71
7272 deg
Mean motion: 15
73680371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1603
Checksum: 280
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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