Date:
November 29th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 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
332/19:17:48
984 -0
2 1
6 1
7
N/A -1
1 0
1 189
5
000/00:05:37
969 1
2 -0
2 179
4
Coasting Arc #1 (Orbit 3168)
---------------------------------------
Vector Time (GMT): 2009/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6250682
37 A = 6723897
57 meter
Y = -1055483
17 meter E =
0015836
Z = 2233599
88 I = 51
61791
XDOT = 2755
169451 Wp = 79
70495
YDOT = 4677
275776 meter/sec RA = 186
62136 deg
ZDOT = -5464
571788 TA = 75
21130
MA = 75
03589
Ha = 188
734 n
mi
Hp = 179
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20507488
09 X = 6251169
72
Y = -3462871
31 feet Y = -985581
72 meter
Z = 7328083
58 Z = 2263967
55
XDOT = 9039
269852 XDOT = 2729
209087
YDOT = 15345
392965 feet/sec YDOT = 4707
940771 meter/sec
ZDOT = -17928
385132 ZDOT = -5451
249735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5242586
40 X = -1597940
34
Y = 20082140
78 feet Y = 6121036
51 meter
Z = 7447970
47 Z = 2270141
40
XDOT = -16281
625663 XDOT = -4962
639502
YDOT = 2421
639829 feet/sec YDOT = 738
115820 meter/sec
ZDOT = -17875
560702 ZDOT = -5448
470902
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 09331
53624735
00016717 00000-0 10270-3 0 9008
2 25544 51
6459 187
4857 0007554 17
1100 343
0318 15
76123500 31694
Satellite: ISS
Catalog Number: 25544
Epoch time: 09331
53624735 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 187
4857 deg
Eccentricity:
0007554
Arg of perigee: 17
1100 deg
Mean anomaly: 343
0318 deg
Mean motion: 15
76123500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3169
Checksum: 296
Coasting Arc #2 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2009/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1894820
99 A = 6715199
33 meter
Y = -4027939
85 meter E =
0008162
Z = 5020643
14 I = 51
61721
XDOT = 7394
748450 Wp = 62
34410
YDOT = -1234
061158 meter/sec RA = 181
50289 deg
ZDOT = 1802
270431 TA = 10
31580
MA = 10
29906
Ha = 188
883 n
mi
Hp = 179
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6216604
31 X = -1874029
07
Y = -13215025
75 feet Y = -4049012
87 meter
Z = 16471926
31 Z = 5011488
14
XDOT = 24260
985727 XDOT = 7399
242996
YDOT = -4048
757079 feet/sec YDOT = -1151
343681 meter/sec
ZDOT = 5912
960732 ZDOT = 1838
205943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14633449
38 X = 4460275
37
Y = -583974
42 feet Y = -177995
40 meter
Z = 16435588
35 Z = 5009567
33
XDOT = -5885
481640 XDOT = -1793
894804
YDOT = 22789
785429 feet/sec YDOT = 6946
326599 meter/sec
ZDOT = 6054
841561 ZDOT = 1845
515708
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 09332
55071384
00016717 00000-0 10270-3 0 9018
2 25544 51
6448 182
2594 0007509 21
0490 339
0982 15
76111411 31857
Satellite: ISS
Catalog Number: 25544
Epoch time: 09332
55071384 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 182
2594 deg
Eccentricity:
0007509
Arg of perigee: 21
0490 deg
Mean anomaly: 339
0982 deg
Mean motion: 15
76111411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 299
Coasting Arc #3 (Orbit 3189)
---------------------------------------
Vector Time (GMT): 2009/332/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6615104
59 A = 6726651
79 meter
Y = -708745
22 meter E =
0020945
Z = 908237
85 I = 51
66358
XDOT = 1331
435008 Wp = 41
75275
YDOT = -4712
660254 meter/sec RA = 179
91792 deg
ZDOT = 5957
051899 TA = 328
17718
MA = 328
30357
Ha = 189
504 n
mi
Hp = 179
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21703099
04 X = -6611099
80
Y = -2325279
59 feet Y = -782696
88 meter
Z = 2979782
97 Z = 876110
46
XDOT = 4368
225093 XDOT = 1355
094755
YDOT = -15461
483773 feet/sec YDOT = -4697
639422 meter/sec
ZDOT = 19544
133526 ZDOT = 5963
577386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21581262
71 X = -6577968
87
Y = -3379476
88 feet Y = -1030064
55 meter
Z = 2852853
98 Z = 869549
89
XDOT = 4754
786148 XDOT = 1449
258818
YDOT = -13661
971574 feet/sec YDOT = -4164
168936 meter/sec
ZDOT = 19569
700848 ZDOT = 5964
844819
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 09332
86774207
00016717 00000-0 10270-3 0 9027
2 25544 51
6460 180
6241 0008257 19
9019 340
2465 15
75831388 31903
Satellite: ISS
Catalog Number: 25544
Epoch time: 09332
86774207 = yrday
fracday
Element set: 902
Inclination: 51
6460 deg
RA of node: 180
6241 deg
Eccentricity:
0008257
Arg of perigee: 19
9019 deg
Mean anomaly: 340
2465 deg
Mean motion: 15
75831388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3190
Checksum: 314
Coasting Arc #4 (Orbit 3204)
---------------------------------------
Vector Time (GMT): 2009/333/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1576264
10 A = 6715655
45 meter
Y = 4154739
23 meter E =
0017090
Z = -5048203
46 I = 51
65684
XDOT = -7456
657827 Wp = 74
88840
YDOT = -708
290052 meter/sec RA = 174
74795 deg
ZDOT = 1754
640177 TA = 211
96598
MA = 212
06977
Ha = 189
466 n
mi
Hp = 179
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5171470
14 X = -1598081
98
Y = 13631034
21 feet Y = 4136990
95 meter
Z = -16562347
30 Z = -5055913
82
XDOT = -24464
100481 XDOT = -7456
707378
YDOT = -2323
786259 feet/sec YDOT = -791
675224 meter/sec
ZDOT = 5756
693494 ZDOT = 1718
414474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5501051
33 X = -1676720
45
Y = 13464163
78 feet Y = 4103877
12 meter
Z = -16592627
07 Z = -5057432
73
XDOT = -23430
248221 XDOT = -7141
539658
YDOT = -2692
468131 feet/sec YDOT = -820
664286 meter/sec
ZDOT = 5613
563638 ZDOT = 1711
014197
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 09333
81896110
00016717 00000-0 10270-3 0 9032
2 25544 51
6454 175
7272 0008267 23
2481 336
9056 15
75898675 32054
Satellite: ISS
Catalog Number: 25544
Epoch time: 09333
81896110 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 175
7272 deg
Eccentricity:
0008267
Arg of perigee: 23
2481 deg
Mean anomaly: 336
9056 deg
Mean motion: 15
75898675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3205
Checksum: 330
Coasting Arc #5 (Orbit 3220)
---------------------------------------
Vector Time (GMT): 2009/334/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6347607
40 A = 6724780
83 meter
Y = 570229
42 meter E =
0008306
Z = -2157591
61 I = 51
71641
XDOT = -2304
709442 Wp = 72
56414
YDOT = 4846
284143 meter/sec RA = 169
63514 deg
ZDOT = -5514
528116 TA = 131
54745
MA = 131
47618
Ha = 189
525 n
mi
Hp = 179
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20825483
59 X = 6351240
71
Y = 1870831
42 feet Y = 641232
67 meter
Z = -7078712
64 Z = -2126745
14
XDOT = -7561
382685 XDOT = -2331
940785
YDOT = 15899
882359 feet/sec YDOT = 4820
359896 meter/sec
ZDOT = -18092
283844 ZDOT = -5525
790314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20837691
68 X = 6351328
42
Y = 2168444
20 feet Y = 660941
79 meter
Z = -6956824
32 Z = -2120440
05
XDOT = -7523
582396 XDOT = -2293
187914
YDOT = 14271
864765 feet/sec YDOT = 4350
064381 meter/sec
ZDOT = -18136
576240 ZDOT = -5528
028438
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 09334
83357172
00016717 00000-0 10270-3 0 9046
2 25544 51
6444 170
5024 0008226 26
8262 333
3327 15
75910420 32215
Satellite: ISS
Catalog Number: 25544
Epoch time: 09334
83357172 = yrday
fracday
Element set: 904
Inclination: 51
6444 deg
RA of node: 170
5024 deg
Eccentricity:
0008226
Arg of perigee: 26
8262 deg
Mean anomaly: 333
3327 deg
Mean motion: 15
75910420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3221
Checksum: 285
Coasting Arc #6 (Orbit 3236)
---------------------------------------
Vector Time (GMT): 2009/335/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2414983
36 A = 6717651
10 meter
Y = -4358423
55 meter E =
0016253
Z = 4500508
21 I = 51
72290
XDOT = 7009
983400 Wp = 48
84642
YDOT = 622
115636 meter/sec RA = 164
44807 deg
ZDOT = -3141
282880 TA = 72
52225
MA = 72
34467
Ha = 189
471 n
mi
Hp = 178
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7923173
74 X = 2441677
30
Y = -14299289
87 feet Y = -4331269
17 meter
Z = 14765446
90 Z = 4512304
73
XDOT = 22998
633202 XDOT = 7017
765968
YDOT = 2041
061798 feet/sec YDOT = 700
549366 meter/sec
ZDOT = -10306
046194 ZDOT = -3107
208502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7794850
84 X = 2375870
54
Y = -14321774
36 feet Y = -4365276
83 meter
Z = 14811882
88 Z = 4514661
90
XDOT = 22020
030694 XDOT = 6711
705356
YDOT = 1405
023569 feet/sec YDOT = 428
251184 meter/sec
ZDOT = -10171
385432 ZDOT = -3100
238280
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 09335
84815639
00016717 00000-0 10270-3 0 9056
2 25544 51
6447 165
2771 0008378 29
6853 330
4785 15
75980786 32378
Satellite: ISS
Catalog Number: 25544
Epoch time: 09335
84815639 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 165
2771 deg
Eccentricity:
0008378
Arg of perigee: 29
6853 deg
Mean anomaly: 330
4785 deg
Mean motion: 15
75980786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3237
Checksum: 358
Coasting Arc #7 (Orbit 3252)
---------------------------------------
Vector Time (GMT): 2009/336/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5828568
86 A = 6721888
68 meter
Y = -563622
22 meter E =
0018969
Z = 3277756
39 I = 51
76534
XDOT = 3176
292990 Wp = 67
21303
YDOT = -5189
032463 meter/sec RA = 159
35384 deg
ZDOT = 4741
481304 TA = 331
23688
MA = 331
34134
Ha = 189
643 n
mi
Hp = 178
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19122601
25 X = -5837756
21
Y = -1849154
27 feet Y = -628852
61 meter
Z = 10753793
94 Z = 3249418
23
XDOT = 10420
908761 XDOT = 3211
047869
YDOT = -17024
384721 feet/sec YDOT = -5153
319715 meter/sec
ZDOT = 15556
041023 ZDOT = 4756
995639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19218505
97 X = -5857800
62
Y = -1462463
09 feet Y = -445758
75 meter
Z = 10641783
87 Z = 3243615
73
XDOT = 9878
417325 XDOT = 3010
941601
YDOT = -15826
989237 feet/sec YDOT = -4824
066320 meter/sec
ZDOT = 15617
149083 ZDOT = 4760
107041
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 09336
86271731
00016717 00000-0 10270-3 0 9069
2 25544 51
6442 160
0522 0008338 33
7695 326
3999 15
76003595 32530
Satellite: ISS
Catalog Number: 25544
Epoch time: 09336
86271731 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 160
0522 deg
Eccentricity:
0008338
Arg of perigee: 33
7695 deg
Mean anomaly: 326
3999 deg
Mean motion: 15
76003595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3253
Checksum: 323
Coasting Arc #8 (Orbit 3267)
---------------------------------------
Vector Time (GMT): 2009/337/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3077069
90 A = 6720387
20 meter
Y = 4709595
70 meter E =
0012163
Z = -3680771
15 I = 51
78813
XDOT = -6312
725787 Wp = 63
43922
YDOT = -742
511261 meter/sec RA = 154
16215 deg
ZDOT = 4343
598565 TA = 252
38937
MA = 252
52225
Ha = 189
555 n
mi
Hp = 178
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10095373
70 X = -3111623
98
Y = 15451429
45 feet Y = 4674993
48 meter
Z = -12076020
84 Z = -3695802
92
XDOT = -20711
042609 XDOT = -6325
054409
YDOT = -2436
060569 feet/sec YDOT = -813
173524 meter/sec
ZDOT = 14250
651461 ZDOT = 4312
900866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9440963
08 X = -2877605
55
Y = 15814466
41 feet Y = 4820249
36 meter
Z = -12135254
01 Z = -3698825
42
XDOT = -19717
267898 XDOT = -6009
823255
YDOT = -969
589120 feet/sec YDOT = -295
530764 meter/sec
ZDOT = 14129
290635 ZDOT = 4306
607786
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 09337
81384634
00016717 00000-0 10270-3 0 9073
2 25544 51
6436 155
1541 0008457 37
3697 322
8054 15
76048117 32681
Satellite: ISS
Catalog Number: 25544
Epoch time: 09337
81384634 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 155
1541 deg
Eccentricity:
0008457
Arg of perigee: 37
3697 deg
Mean anomaly: 322
8054 deg
Mean motion: 15
76048117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3268
Checksum: 328
Coasting Arc #9 (Orbit 3283)
---------------------------------------
Vector Time (GMT): 2009/338/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5147135
06 A = 6718586
86 meter
Y = 820078
66 meter E =
0016292
Z = -4256878
11 I = 51
80836
XDOT = -3858
719373 Wp = 55
33405
YDOT = 5601
568621 meter/sec RA = 149
07303 deg
ZDOT = -3587
179270 TA = 178
26144
MA = 178
25577
Ha = 189
655 n
mi
Hp = 178
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16886926
06 X = 5158261
54
Y = 2690546
77 feet Y = 877699
81 meter
Z = -13966135
54 Z = -4231846
00
XDOT = -12659
840461 XDOT = -3903
644315
YDOT = 18377
849806 feet/sec YDOT = 5558
167498 meter/sec
ZDOT = -11768
960859 ZDOT = -3606
033340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17089758
49 X = 5208958
39
Y = 1761411
14 feet Y = 536878
11 meter
Z = -13867149
71 Z = -4226707
23
XDOT = -11441
995610 XDOT = -3487
520262
YDOT = 17790
259375 feet/sec YDOT = 5422
471058 meter/sec
ZDOT = -11843
281517 ZDOT = -3609
832206
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 09338
82835998
00016717 00000-0 10270-3 0 9080
2 25544 51
6436 149
9282 0008514 40
7670 319
4130 15
76049653 32848
Satellite: ISS
Catalog Number: 25544
Epoch time: 09338
82835998 = yrday
fracday
Element set: 908
Inclination: 51
6436 deg
RA of node: 149
9282 deg
Eccentricity:
0008514
Arg of perigee: 40
7670 deg
Mean anomaly: 319
4130 deg
Mean motion: 15
76049653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3284
Checksum: 342
Coasting Arc #10 (Orbit 3299)
---------------------------------------
Vector Time (GMT): 2009/339/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3601341
47 A = 6723286
47 meter
Y = -5080135
33 meter E =
0019610
Z = 2522828
46 I = 51
85136
XDOT = 5444
251936 Wp = 81
32863
YDOT = 1199
433397 meter/sec RA = 143
88845 deg
ZDOT = -5318
596034 TA = 70
15099
MA = 69
93973
Ha = 189
603 n
mi
Hp = 178
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11815424
78 X = 3645625
30
Y = -16667110
66 feet Y = -5039615
73 meter
Z = 8276996
26 Z = 2540430
75
XDOT = 17861
718949 XDOT = 5456
271882
YDOT = 3935
148941 feet/sec YDOT = 1260
382123 meter/sec
ZDOT = -17449
462053 ZDOT = -5292
118426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10542022
70 X = 3213208
52
Y = -17467366
59 feet Y = -5324053
34 meter
Z = 8346398
60 Z = 2543982
29
XDOT = 16925
590307 XDOT = 5158
919926
YDOT = 1868
444215 feet/sec YDOT = 569
501797 meter/sec
ZDOT = -17344
733030 ZDOT = -5286
674628
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 09339
84284714
00016717 00000-0 10270-3 0 9098
2 25544 51
6445 144
7025 0008693 43
2019 316
9826 15
76136700 33002
Satellite: ISS
Catalog Number: 25544
Epoch time: 09339
84284714 = yrday
fracday
Element set: 909
Inclination: 51
6445 deg
RA of node: 144
7025 deg
Eccentricity:
0008693
Arg of perigee: 43
2019 deg
Mean anomaly: 316
9826 deg
Mean motion: 15
76136700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3300
Checksum: 314
Coasting Arc #11 (Orbit 3315)
---------------------------------------
Vector Time (GMT): 2009/340/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4348154
66 A = 6715529
15 meter
Y = -1338829
86 meter E =
0011994
Z = 4928774
85 I = 51
84865
XDOT = 4305
187147 Wp = 78
75752
YDOT = -6024
786146 meter/sec RA = 138
79157 deg
ZDOT = 2159
379299 TA = 350
37611
MA = 350
39906
Ha = 189
787 n
mi
Hp = 177
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14265599
29 X = -4356803
61
Y = -4392486
41 feet Y = -1387502
35 meter
Z = 16170521
15 Z = 4907630
33
XDOT = 14124
629747 XDOT = 4361
747496
YDOT = -19766
358748 feet/sec YDOT = -5976
326977 meter/sec
ZDOT = 7084
577752 ZDOT = 2180
430709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14693328
00 X = -4478526
38
Y = -3099351
13 feet Y = -944682
22 meter
Z = 16086862
63 Z = 4903275
73
XDOT = 12045
715329 XDOT = 3671
534032
YDOT = -19867
403804 feet/sec YDOT = -6055
584679 meter/sec
ZDOT = 7167
591168 ZDOT = 2184
681788
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 09340
85731098
00016717 00000-0 10270-3 0 9105
2 25544 51
6443 139
4771 0008691 47
6316 312
5583 15
76154603 33166
Satellite: ISS
Catalog Number: 25544
Epoch time: 09340
85731098 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 139
4771 deg
Eccentricity:
0008691
Arg of perigee: 47
6316 deg
Mean anomaly: 312
5583 deg
Mean motion: 15
76154603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3316
Checksum: 315
Coasting Arc #12 (Orbit 3330)
---------------------------------------
Vector Time (GMT): 2009/341/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3838091
19 A = 6725393
40 meter
Y = 5383747
42 meter E =
0017976
Z = -1194482
35 I = 51
90401
XDOT = -4547
024662 Wp = 44
06081
YDOT = -1944
889623 meter/sec RA = 133
62765 deg
ZDOT = 5909
825898 TA = 302
88314
MA = 303
05599
Ha = 189
733 n
mi
Hp = 177
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12592162
70 X = -3892205
34
Y = 17663213
31 feet Y = 5340525
14 meter
Z = -3918905
36 Z = -1213258
88
XDOT = -14918
059915 XDOT = -4553
647578
YDOT = -6380
871465 feet/sec YDOT = -1995
774634 meter/sec
ZDOT = 19389
192580 ZDOT = 5887
720137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10627125
68 X = -3239147
91
Y = 18895237
23 feet Y = 5759268
31 meter
Z = -3992955
66 Z = -1217052
89
XDOT = -14244
752572 XDOT = -4341
800584
YDOT = -3977
213843 feet/sec YDOT = -1212
254779 meter/sec
ZDOT = 19301
702863 ZDOT = 5883
159033
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 09341
80834862
00016717 00000-0 10270-3 0 9115
2 25544 51
6444 134
5780 0008869 50
2921 309
9023 15
76157665 33319
Satellite: ISS
Catalog Number: 25544
Epoch time: 09341
80834862 = yrday
fracday
Element set: 911
Inclination: 51
6444 deg
RA of node: 134
5780 deg
Eccentricity:
0008869
Arg of perigee: 50
2921 deg
Mean anomaly: 309
9023 deg
Mean motion: 15
76157665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3331
Checksum: 318
Coasting Arc #13 (Orbit 3346)
---------------------------------------
Vector Time (GMT): 2009/342/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3588832
23 A = 6713938
92 meter
Y = 2136918
53 meter E =
0022934
Z = -5275814
57 I = 51
88619
XDOT = -4461
412275 Wp = 74
50959
YDOT = 6240
591538 meter/sec RA = 128
50934 deg
ZDOT = -502
965876 TA = 190
69612
MA = 190
74498
Ha = 189
730 n
mi
Hp = 177
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11774383
96 X = 3590299
23
Y = 7010887
55 feet Y = 2177059
52 meter
Z = -17309102
91 Z = -5258376
20
XDOT = -14637
179381 XDOT = -4528
420745
YDOT = 20474
381687 feet/sec YDOT = 6190
326761 meter/sec
ZDOT = -1650
150513 ZDOT = -524
801918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12647740
98 X = 3855031
45
Y = 5496243
77 feet Y = 1675255
10 meter
Z = -17240059
69 Z = -5254770
19
XDOT = -11596
511674 XDOT = -3534
616758
YDOT = 21196
038456 feet/sec YDOT = 6460
552521 meter/sec
ZDOT = -1736
277295 ZDOT = -529
217320
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 09342
82276382
00016717 00000-0 10270-3 0 9126
2 25544 51
6451 129
3516 0008841 54
4098 305
7889 15
76199297 33475
Satellite: ISS
Catalog Number: 25544
Epoch time: 09342
82276382 = yrday
fracday
Element set: 912
Inclination: 51
6451 deg
RA of node: 129
3516 deg
Eccentricity:
0008841
Arg of perigee: 54
4098 deg
Mean anomaly: 305
7889 deg
Mean motion: 15
76199297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3347
Checksum: 345
Coasting Arc #14 (Orbit 3362)
---------------------------------------
Vector Time (GMT): 2009/343/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3914197
94 A = 6725689
01 meter
Y = -5456355
35 meter E =
0015936
Z = -341165
97 I = 51
94393
XDOT = 3689
887870 Wp = 103
89042
YDOT = 3010
495702 meter/sec RA = 123
37485 deg
ZDOT = -6051
510466 TA = 79
80425
MA = 79
62456
Ha = 189
736 n
mi
Hp = 177
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12841856
77 X = 3976578
29
Y = -17901428
31 feet Y = -5412235
67 meter
Z = -1119310
91 Z = -321999
41
XDOT = 12105
931331 XDOT = 3685
347202
YDOT = 9876
954404 feet/sec YDOT = 3051
733208 meter/sec
ZDOT = -19854
036963 ZDOT = -6033
595629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10213925
62 X = 3113204
53
Y = -19524694
27 feet Y = -5951126
81 meter
Z = -1043702
39 Z = -318120
49
XDOT = 12061
135758 XDOT = 3676
234179
YDOT = 7322
281219 feet/sec YDOT = 2231
831316 meter/sec
ZDOT = -19783
076238 ZDOT = -6029
881637
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 09343
83715321
00016717 00000-0 10270-3 0 9130
2 25544 51
6447 124
1250 0009008 58
0409 302
1630 15
76265311 33634
Satellite: ISS
Catalog Number: 25544
Epoch time: 09343
83715321 = yrday
fracday
Element set: 913
Inclination: 51
6447 deg
RA of node: 124
1250 deg
Eccentricity:
0009008
Arg of perigee: 58
0409 deg
Mean anomaly: 302
1630 deg
Mean motion: 15
76265311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3363
Checksum: 278
Coasting Arc #15 (Orbit 3378)
---------------------------------------
Vector Time (GMT): 2009/344/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2905438
25 A = 6714013
77 meter
Y = -3142998
65 meter E =
0013143
Z = 5164339
88 I = 51
91959
XDOT = 4436
922848 Wp = 59
62916
YDOT = -6181
984104 meter/sec RA = 118
22916 deg
ZDOT = -1257
272890 TA = 42
37384
MA = 42
27241
Ha = 189
806 n
mi
Hp = 177
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9532277
73 X = -2895164
55
Y = -10311675
36 feet Y = -3175431
92 meter
Z = 16943372
31 Z = 5150249
77
XDOT = 14556
833492 XDOT = 4511
828808
YDOT = -20282
100080 feet/sec YDOT = -6131
948899 meter/sec
ZDOT = -4124
911055 ZDOT = -1235
536506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11131489
83 X = -3392878
10
Y = -8670289
44 feet Y = -2642704
22 meter
Z = 16887535
29 Z = 5147320
76
XDOT = 10581
358799 XDOT = 3225
198162
YDOT = -21509
125034 feet/sec YDOT = -6555
981310 meter/sec
ZDOT = -4039
150906 ZDOT = -1231
133196
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 09344
85151738
00016717 00000-0 10270-3 0 9140
2 25544 51
6437 118
8986 0009067 61
5506 298
6571 15
76310226 33797
Satellite: ISS
Catalog Number: 25544
Epoch time: 09344
85151738 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 118
8986 deg
Eccentricity:
0009067
Arg of perigee: 61
5506 deg
Mean anomaly: 298
6571 deg
Mean motion: 15
76310226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3379
Checksum: 341
Coasting Arc #16 (Orbit 3394)
---------------------------------------
Vector Time (GMT): 2009/345/19:20:37
969
Vector Time (MET): N/A
Weight (LBS) : 759075
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3791039
40 A = 6724165
92 meter
Y = 5228531
02 meter E =
0023319
Z = 1831940
94 I = 51
96716
XDOT = -3042
476392 Wp = 65
40469
YDOT = -4217
613147 meter/sec RA = 113
12522 deg
ZDOT = 5694
697370 TA = 314
86618
MA = 315
05534
Ha = 189
798 n
mi
Hp = 177
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12437793
29 X = -3858123
38
Y = 17153973
15 feet Y = 5185762
12 meter
Z = 6010304
93 Z = 1813361
28
XDOT = -9981
877925 XDOT = -3022
752466
YDOT = -13837
313473 feet/sec YDOT = -4251
526155 meter/sec
ZDOT = 18683
390320 ZDOT = 5679
964283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9296658
31 X = -2833621
45
Y = 19063200
97 feet Y = 5810463
65 meter
Z = 5936983
68 Z = 1809592
63
XDOT = -10955
275317 XDOT = -3339
167917
YDOT = -11191
359488 feet/sec YDOT = -3411
126372 meter/sec
ZDOT = 18624
977446 ZDOT = 5676
893126
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 09345
86585772
00016717 00000-0 10270-3 0 9152
2 25544 51
6439 113
6722 0009174 64
4830 295
7282 15
76319363 33957
Satellite: ISS
Catalog Number: 25544
Epoch time: 09345
86585772 = yrday
fracday
Element set: 915
Inclination: 51
6439 deg
RA of node: 113
6722 deg
Eccentricity:
0009174
Arg of perigee: 64
4830 deg
Mean anomaly: 295
7282 deg
Mean motion: 15
76319363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3395
Checksum: 343
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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