Date:
September 16th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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
There are no maneuvers
Coasting Arc #1 (Orbit 1997)
---------------------------------------
Vector Time (GMT): 2009/257/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5067846
55 A = 6723751
24 meter
Y = -1090927
73 meter E =
0018456
Z = 4268539
40 I = 51
46978
XDOT = 4146
549863 Wp = 79
27383
YDOT = 5470
776397 meter/sec RA = 208
82321 deg
ZDOT = -3508
642674 TA = 46
37858
MA = 46
22563
Ha = 193
019 n
mi
Hp = 180
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16626793
15 X = 5058933
17
Y = -3579159
21 feet Y = -1034305
90 meter
Z = 14004394
34 Z = 4293137
21
XDOT = 13604
166216 XDOT = 4102
110770
YDOT = 17948
741459 feet/sec YDOT = 5516
897062 meter/sec
ZDOT = -11511
294863 ZDOT = -3488
606829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3012615
89 X = 918245
32
Y = -16657284
82 feet Y = -5077140
41 meter
Z = 14101159
52 Z = 4298033
42
XDOT = 20595
052750 XDOT = 6277
372078
YDOT = -5997
613605 feet/sec YDOT = -1828
072627 meter/sec
ZDOT = -11432
066936 ZDOT = -3484
494002
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 09257
24978686
00020000 00000-0 20000-3 0 9002
2 25544 51
6390 209
6314 0008886 87
1107 273
1074 15
74131203 19983
Satellite: ISS
Catalog Number: 25544
Epoch time: 09257
24978686 = yrday
fracday
Element set: 900
Inclination: 51
6390 deg
RA of node: 209
6314 deg
Eccentricity:
0008886
Arg of perigee: 87
1107 deg
Mean anomaly: 273
1074 deg
Mean motion: 15
74131203 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1998
Checksum: 307
Coasting Arc #2 (Orbit 2013)
---------------------------------------
Vector Time (GMT): 2009/258/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3990777
98 A = 6727790
19 meter
Y = -4435914
31 meter E =
0022262
Z = 3087747
54 I = 51
50925
XDOT = 5713
790788 Wp = 87
57019
YDOT = -1725
103742 meter/sec RA = 203
72555 deg
ZDOT = 4877
283475 TA = 308
38697
MA = 308
58672
Ha = 193
300 n
mi
Hp = 180
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13093103
62 X = -3955877
81
Y = -14553524
63 feet Y = -4480346
29 meter
Z = 10130405
32 Z = 3068445
43
XDOT = 18746
032768 XDOT = 5708
963771
YDOT = -5659
789179 feet/sec YDOT = -1661
235599 meter/sec
ZDOT = 16001
586204 ZDOT = 4905
029167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18357536
15 X = -5595377
02
Y = 6911955
03 feet Y = 2106763
89 meter
Z = 10054118
44 Z = 3064495
30
XDOT = 2064
932479 XDOT = 629
391420
YDOT = -18090
866754 feet/sec YDOT = -5514
096187 meter/sec
ZDOT = 16110
712904 ZDOT = 4910
545293
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 09258
26555382
00020000 00000-0 20000-3 0 9010
2 25544 51
6386 204
4140 0009142 91
1635 269
0576 15
74108382 20148
Satellite: ISS
Catalog Number: 25544
Epoch time: 09258
26555382 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 204
4140 deg
Eccentricity:
0009142
Arg of perigee: 91
1635 deg
Mean anomaly: 269
0576 deg
Mean motion: 15
74108382 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2014
Checksum: 280
Coasting Arc #3 (Orbit 2028)
---------------------------------------
Vector Time (GMT): 2009/259/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4883881
22 A = 6723931
41 meter
Y = 1906116
85 meter E =
0017443
Z = -4227227
91 I = 51
52530
XDOT = -4931
328057 Wp = 102
36509
YDOT = -4670
494188 meter/sec RA = 198
53058 deg
ZDOT = 3600
180982 TA = 204
33611
MA = 204
41857
Ha = 193
204 n
mi
Hp = 180
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16023232
35 X = -4884297
83
Y = 6253664
22 feet Y = 1851499
82 meter
Z = -13868857
98 Z = -4250954
74
XDOT = -16178
897826 XDOT = -4896
224163
YDOT = -15323
143663 feet/sec YDOT = -4725
442697 meter/sec
ZDOT = 11811
617395 ZDOT = 3576
310353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 278461
65 X = 84875
11
Y = 17122446
44 feet Y = 5218921
67 meter
Z = -13962155
98 Z = -4255665
14
XDOT = -18791
653744 XDOT = -5727
696061
YDOT = 9836
825150 feet/sec YDOT = 2998
264306 meter/sec
ZDOT = 11717
313387 ZDOT = 3571
437120
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 09259
21782415
00020000 00000-0 20000-3 0 9026
2 25544 51
6391 199
5224 0009176 94
1662 266
0550 15
74137299 20295
Satellite: ISS
Catalog Number: 25544
Epoch time: 09259
21782415 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 199
5224 deg
Eccentricity:
0009176
Arg of perigee: 94
1662 deg
Mean anomaly: 266
0550 deg
Mean motion: 15
74137299 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2029
Checksum: 303
Coasting Arc #4 (Orbit 2044)
---------------------------------------
Vector Time (GMT): 2009/260/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4586582
69 A = 6727288
17 meter
Y = 3726287
25 meter E =
0013791
Z = -3224101
99 I = 51
56631
XDOT = -5447
389500 Wp = 98
70340
YDOT = 2592
413585 meter/sec RA = 193
43691 deg
ZDOT = -4772
595799 TA = 118
98843
MA = 118
85012
Ha = 193
219 n
mi
Hp = 180
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15047843
48 X = 4560235
85
Y = 12225351
87 feet Y = 3777429
52 meter
Z = -10577762
45 Z = -3201884
82
XDOT = -17872
012795 XDOT = -5452
789162
YDOT = 8505
293913 feet/sec YDOT = 2531
467058 meter/sec
ZDOT = -15658
122700 ZDOT = -4799
072421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16567685
38 X = 5049830
50
Y = -10161551
00 feet Y = -3097240
75 meter
Z = -10490022
05 Z = -3197358
72
XDOT = 1340
738255 XDOT = 408
657020
YDOT = 18391
480284 feet/sec YDOT = 5605
723191 meter/sec
ZDOT = -15762
206831 ZDOT = -4804
320642
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 09260
23356850
00020000 00000-0 20000-3 0 9031
2 25544 51
6401 194
3043 0009208 97
8985 262
3223 15
74156009 20457
Satellite: ISS
Catalog Number: 25544
Epoch time: 09260
23356850 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 194
3043 deg
Eccentricity:
0009208
Arg of perigee: 97
8985 deg
Mean anomaly: 262
3223 deg
Mean motion: 15
74156009 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2045
Checksum: 280
Coasting Arc #5 (Orbit 2060)
---------------------------------------
Vector Time (GMT): 2009/261/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4599731
15 A = 6724132
28 meter
Y = -2635454
19 meter E =
0018952
Z = 4120822
48 I = 51
58490
XDOT = 5556
298041 Wp = 87
56293
YDOT = 3809
950383 meter/sec RA = 188
24566 deg
ZDOT = -3749
836430 TA = 40
87542
MA = 40
73345
Ha = 193
012 n
mi
Hp = 180
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15090981
45 X = 4608841
17
Y = -8646503
26 feet Y = -2583965
94 meter
Z = 13519758
80 Z = 4143190
37
XDOT = 18229
324280 XDOT = 5531
497594
YDOT = 12499
837213 feet/sec YDOT = 3871
945131 meter/sec
ZDOT = -12302
612958 ZDOT = -3722
904558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3431652
15 X = -1045967
58
Y = -16980543
75 feet Y = -5175669
73 meter
Z = 13607663
84 Z = 4147615
94
XDOT = 16425
928925 XDOT = 5006
623136
YDOT = -13133
930558 feet/sec YDOT = -4003
222034 meter/sec
ZDOT = -12196
293095 ZDOT = -3717
430135
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 09261
24930072
00020000 00000-0 20000-3 0 9048
2 25544 51
6394 189
0871 0009124 101
2183 259
0006 15
74191421 20612
Satellite: ISS
Catalog Number: 25544
Epoch time: 09261
24930072 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 189
0871 deg
Eccentricity:
0009124
Arg of perigee: 101
2183 deg
Mean anomaly: 259
0006 deg
Mean motion: 15
74191421 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2061
Checksum: 262
Coasting Arc #6 (Orbit 2076)
---------------------------------------
Vector Time (GMT): 2009/262/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5070991
87 A = 6727025
31 meter
Y = -2907319
13 meter E =
0021839
Z = 3313024
22 I = 51
62380
XDOT = 5055
591365 Wp = 95
49254
YDOT = -3440
993351 meter/sec RA = 183
15706 deg
ZDOT = 4690
152690 TA = 303
48243
MA = 303
69097
Ha = 193
259 n
mi
Hp = 180
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16637112
43 X = -5054199
01
Y = -9538448
58 feet Y = -2963931
71 meter
Z = 10869502
03 Z = 3288430
28
XDOT = 16586
585843 XDOT = 5070
909340
YDOT = -11289
348263 feet/sec YDOT = -3384
372625 meter/sec
ZDOT = 15387
640059 ZDOT = 4714
750465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14125405
10 X = -4305423
47
Y = 13051778
50 feet Y = 3978182
09 meter
Z = 10772446
09 Z = 3283441
57
XDOT = -4844
385809 XDOT = -1476
568795
YDOT = -18100
711585 feet/sec YDOT = -5517
096891 meter/sec
ZDOT = 15484
275737 ZDOT = 4719
607245
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 09262
26502420
00020000 00000-0 20000-3 0 9054
2 25544 51
6393 183
8694 0009292 104
5886 255
6308 15
74164320 20770
Satellite: ISS
Catalog Number: 25544
Epoch time: 09262
26502420 = yrday
fracday
Element set: 905
Inclination: 51
6393 deg
RA of node: 183
8694 deg
Eccentricity:
0009292
Arg of perigee: 104
5886 deg
Mean anomaly: 255
6308 deg
Mean motion: 15
74164320 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2077
Checksum: 296
Coasting Arc #7 (Orbit 2091)
---------------------------------------
Vector Time (GMT): 2009/263/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4210492
78 A = 6724442
36 meter
Y = 3353876
61 meter E =
0016607
Z = -4047431
50 I = 51
64678
XDOT = -5993
047018 Wp = 109
00222
YDOT = -2855
984212 meter/sec RA = 177
96938 deg
ZDOT = 3875
514979 TA = 200
97113
MA = 201
03932
Ha = 193
064 n
mi
Hp = 180
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13813952
70 X = -4228021
55
Y = 11003532
19 feet Y = 3306694
02 meter
Z = -13278974
73 Z = -4067929
19
XDOT = -19662
227749 XDOT = -5979
492262
YDOT = -9370
026942 feet/sec YDOT = -2922
925848 meter/sec
ZDOT = 12714
944158 ZDOT = 3846
433610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6636392
88 X = 2022772
55
Y = 16300824
81 feet Y = 4968491
40 meter
Z = -13359475
27 Z = -4071968
06
XDOT = -13413
107045 XDOT = -4088
315027
YDOT = 15767
004051 feet/sec YDOT = 4805
782835 meter/sec
ZDOT = 12600
214486 ZDOT = 3840
545375
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 09263
21725220
00020000 00000-0 20000-3 0 9066
2 25544 51
6405 178
9783 0009136 108
1813 252
0345 15
74190469 20927
Satellite: ISS
Catalog Number: 25544
Epoch time: 09263
21725220 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 178
9783 deg
Eccentricity:
0009136
Arg of perigee: 108
1813 deg
Mean anomaly: 252
0345 deg
Mean motion: 15
74190469 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2092
Checksum: 285
Coasting Arc #8 (Orbit 2107)
---------------------------------------
Vector Time (GMT): 2009/264/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5366535
66 A = 6726410
51 meter
Y = 2099653
60 meter E =
0013826
Z = -3477585
64 I = 51
68209
XDOT = -4575
043985 Wp = 103
89335
YDOT = 4192
410898 meter/sec RA = 172
88493 deg
ZDOT = -4547
173642 TA = 117
29516
MA = 117
15430
Ha = 193
043 n
mi
Hp = 180
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17606744
28 X = 5359551
85
Y = 6888627
29 feet Y = 2159626
05 meter
Z = -11409401
70 Z = -3451531
74
XDOT = -15009
986829 XDOT = -4599
494540
YDOT = 13754
628932 feet/sec YDOT = 4141
113016 meter/sec
ZDOT = -14918
548693 ZDOT = -4569
459235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11376272
38 X = 3467487
82
Y = -15177791
21 feet Y = -4626190
76 meter
Z = -11306642
21 Z = -3446264
55
XDOT = 8141
058901 XDOT = 2481
394753
YDOT = 17235
553738 feet/sec YDOT = 5253
396779 meter/sec
ZDOT = -15006
043040 ZDOT = -4573
841918
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 09264
23295172
00020000 00000-0 20000-3 0 9078
2 25544 51
6394 173
7600 0009117 112
4163 247
7967 15
74211886 21086
Satellite: ISS
Catalog Number: 25544
Epoch time: 09264
23295172 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 173
7600 deg
Eccentricity:
0009117
Arg of perigee: 112
4163 deg
Mean anomaly: 247
7967 deg
Mean motion: 15
74211886 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2108
Checksum: 296
Coasting Arc #9 (Orbit 2123)
---------------------------------------
Vector Time (GMT): 2009/265/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3745510
36 A = 6724714
57 meter
Y = -3973807
35 meter E =
0019165
Z = 3906649
05 I = 51
70540
XDOT = 6273
294117 Wp = 95
95498
YDOT = 1910
356665 meter/sec RA = 167
70006 deg
ZDOT = -4056
363654 TA = 36
19822
MA = 36
06867
Ha = 192
825 n
mi
Hp = 180
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12288419
81 X = 3770689
69
Y = -13037425
70 feet Y = -3931781
86 meter
Z = 12817090
04 Z = 3924906
40
XDOT = 20581
673611 XDOT = 6271
171323
YDOT = 6267
574361 feet/sec YDOT = 1980
496245 meter/sec
ZDOT = -13308
279706 ZDOT = -4025
892772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9544790
31 X = -2909252
09
Y = -15100821
24 feet Y = -4602730
31 meter
Z = 12888743
28 Z = 3928488
95
XDOT = 10162
527682 XDOT = 3097
538438
YDOT = -17721
379468 feet/sec YDOT = -5401
476462 meter/sec
ZDOT = -13188
128006 ZDOT = -4019
741416
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 09265
24863919
00020000 00000-0 20000-3 0 9081
2 25544 51
6382 168
5420 0009042 115
5239 244
6860 15
74258102 21248
Satellite: ISS
Catalog Number: 25544
Epoch time: 09265
24863919 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 168
5420 deg
Eccentricity:
0009042
Arg of perigee: 115
5239 deg
Mean anomaly: 244
6860 deg
Mean motion: 15
74258102 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2124
Checksum: 291
Coasting Arc #10 (Orbit 2139)
---------------------------------------
Vector Time (GMT): 2009/266/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5541081
48 A = 6725937
91 meter
Y = -1236086
34 meter E =
0020590
Z = 3594248
29 I = 51
73740
XDOT = 3978
019857 Wp = 104
79737
YDOT = -4899
251779 meter/sec RA = 162
62067 deg
ZDOT = 4421
709215 TA = 298
14434
MA = 298
35223
Ha = 192
918 n
mi
Hp = 180
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18179401
18 X = -5544307
99
Y = -4055401
37 feet Y = -1298067
89 meter
Z = 11792153
19 Z = 3567321
53
XDOT = 13051
246250 XDOT = 4011
028298
YDOT = -16073
660691 feet/sec YDOT = -4854
582506 meter/sec
ZDOT = 14506
919998 ZDOT = 4441
115068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8228568
08 X = -2508067
55
Y = 16784514
02 feet Y = 5115919
87 meter
Z = 11685997
63 Z = 3561892
08
XDOT = -11353
532519 XDOT = -3460
556712
YDOT = -15779
525163 feet/sec YDOT = -4809
599270 meter/sec
ZDOT = 14583
048751 ZDOT = 4444
913259
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 09266
26431605
00020000 00000-0 20000-3 0 9098
2 25544 51
6374 163
3243 0008982 119
6458 240
5600 15
74254519 21408
Satellite: ISS
Catalog Number: 25544
Epoch time: 09266
26431605 = yrday
fracday
Element set: 909
Inclination: 51
6374 deg
RA of node: 163
3243 deg
Eccentricity:
0008982
Arg of perigee: 119
6458 deg
Mean anomaly: 240
5600 deg
Mean motion: 15
74254519 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2140
Checksum: 288
Coasting Arc #11 (Orbit 2154)
---------------------------------------
Vector Time (GMT): 2009/267/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3188757
87 A = 6725172
63 meter
Y = 4561040
26 meter E =
0015011
Z = -3792820
46 I = 51
76321
XDOT = -6361
032455 Wp = 115
64577
YDOT = -950
621227 meter/sec RA = 157
43938 deg
ZDOT = 4211
306057 TA = 198
54711
MA = 198
60188
Ha = 192
791 n
mi
Hp = 180
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10461804
04 X = -3221098
15
Y = 14964042
85 feet Y = 4525200
79 meter
Z = -12443636
69 Z = -3808390
29
XDOT = -20869
529052 XDOT = -6370
387690
YDOT = -3118
836048 feet/sec YDOT = -1021
806256 meter/sec
ZDOT = 13816
620923 ZDOT = 4180
381080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12336811
08 X = 3760260
02
Y = 13403429
11 feet Y = 4085365
19 meter
Z = -12504686
99 Z = -3811428
59
XDOT = -6636
670197 XDOT = -2022
857076
YDOT = 18865
102561 feet/sec YDOT = 5750
083261 meter/sec
ZDOT = 13694
721240 ZDOT = 4174
151034
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 09267
21650217
00020000 00000-0 20000-3 0 9108
2 25544 51
6374 158
4324 0008934 122
6441 237
5585 15
74245961 21551
Satellite: ISS
Catalog Number: 25544
Epoch time: 09267
21650217 = yrday
fracday
Element set: 910
Inclination: 51
6374 deg
RA of node: 158
4324 deg
Eccentricity:
0008934
Arg of perigee: 122
6441 deg
Mean anomaly: 237
5585 deg
Mean motion: 15
74245961 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2155
Checksum: 291
Coasting Arc #12 (Orbit 2170)
---------------------------------------
Vector Time (GMT): 2009/268/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5549274
24 A = 6725302
51 meter
Y = 453144
95 meter E =
0013606
Z = -3779983
56 I = 51
78991
XDOT = -3320
981854 Wp = 107
26403
YDOT = 5499
944110 meter/sec RA = 152
36231 deg
ZDOT = -4232
503891 TA = 118
36686
MA = 118
22960
Ha = 192
763 n
mi
Hp = 180
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18206280
31 X = 5562157
30
Y = 1486696
04 feet Y = 515272
18 meter
Z = -12401520
88 Z = -3752993
66
XDOT = -10895
609757 XDOT = -3361
675428
YDOT = 18044
436058 feet/sec YDOT = 5462
579347 meter/sec
ZDOT = -13886
167622 ZDOT = -4248
736291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5136370
99 X = 1565565
88
Y = -17604650
79 feet Y = -5365897
56 meter
Z = -12295145
05 Z = -3747560
21
XDOT = 14213
421639 XDOT = 4332
250916
YDOT = 13851
584544 feet/sec YDOT = 4221
962969 meter/sec
ZDOT = -13949
779816 ZDOT = -4251
892888
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 09268
23215642
00020000 00000-0 20000-3 0 9111
2 25544 51
6365 153
2131 0008934 126
7008 233
4977 15
74270327 21716
Satellite: ISS
Catalog Number: 25544
Epoch time: 09268
23215642 = yrday
fracday
Element set: 911
Inclination: 51
6365 deg
RA of node: 153
2131 deg
Eccentricity:
0008934
Arg of perigee: 126
7008 deg
Mean anomaly: 233
4977 deg
Mean motion: 15
74270327 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2171
Checksum: 279
Coasting Arc #13 (Orbit 2186)
---------------------------------------
Vector Time (GMT): 2009/269/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2576525
48 A = 6725552
73 meter
Y = -5040625
60 meter E =
0019152
Z = 3611145
50 I = 51
81717
XDOT = 6320
832780 Wp = 104
44945
YDOT = 56
602434 meter/sec RA = 147
18459 deg
ZDOT = -4416
177236 TA = 32
37888
MA = 32
26149
Ha = 192
495 n
mi
Hp = 180
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8453167
58 X = 2615156
73
Y = -16537485
57 feet Y = -5011597
32 meter
Z = 11847590
22 Z = 3623756
25
XDOT = 20737
640353 XDOT = 6341
183180
YDOT = 185
703523 feet/sec YDOT = 127
399422 meter/sec
ZDOT = -14488
770459 ZDOT = -4385
421018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14706891
43 X = -4482660
51
Y = -11290673
97 feet Y = -3441397
42 meter
Z = 11896969
82 Z = 3626196
40
XDOT = 3199
959285 XDOT = 975
347590
YDOT = -19357
800818 feet/sec YDOT = -5900
257689 meter/sec
ZDOT = -14367
566017 ZDOT = -4379
234122
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 09269
24779796
00020000 00000-0 20000-3 0 9129
2 25544 51
6364 147
9948 0008701 130
3405 229
8520 15
74314222 21878
Satellite: ISS
Catalog Number: 25544
Epoch time: 09269
24779796 = yrday
fracday
Element set: 912
Inclination: 51
6364 deg
RA of node: 147
9948 deg
Eccentricity:
0008701
Arg of perigee: 130
3405 deg
Mean anomaly: 229
8520 deg
Mean motion: 15
74314222 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2187
Checksum: 309
Coasting Arc #14 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2009/270/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5448192
04 A = 6724608
63 meter
Y = 337361
82 meter E =
0018990
Z = 3918865
84 I = 51
83874
XDOT = 2560
220013 Wp = 115
28279
YDOT = -6030
062971 meter/sec RA = 142
11249 deg
ZDOT = 4055
300271 TA = 292
59496
MA = 292
79576
Ha = 192
481 n
mi
Hp = 180
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17874645
79 X = -5470596
76
Y = 1106830
13 feet Y = 276311
76 meter
Z = 12857171
38 Z = 3892344
00
XDOT = 8399
671958 XDOT = 2607
758953
YDOT = -19783
671166 feet/sec YDOT = -6001
167182 meter/sec
ZDOT = 13304
790916 ZDOT = 4067
853481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1915784
69 X = -583931
18
Y = 17881111
34 feet Y = 5450162
74 meter
Z = 12752667
07 Z = 3887012
92
XDOT = -16805
686014 XDOT = -5122
373097
YDOT = -11379
053894 feet/sec YDOT = -3468
335627 meter/sec
ZDOT = 13353
889446 ZDOT = 4070
265503
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 09270
26342779
00020000 00000-0 20000-3 0 9131
2 25544 51
6366 142
7770 0008674 135
1860 225
0005 15
74350703 22032
Satellite: ISS
Catalog Number: 25544
Epoch time: 09270
26342779 = yrday
fracday
Element set: 913
Inclination: 51
6366 deg
RA of node: 142
7770 deg
Eccentricity:
0008674
Arg of perigee: 135
1860 deg
Mean anomaly: 225
0005 deg
Mean motion: 15
74350703 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2203
Checksum: 275
Coasting Arc #15 (Orbit 2217)
---------------------------------------
Vector Time (GMT): 2009/271/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1885671
58 A = 6726076
19 meter
Y = 5468067
07 meter E =
0012775
Z = -3448865
35 I = 51
86653
XDOT = -6117
218807 Wp = 121
53857
YDOT = 782
940030 meter/sec RA = 136
93771 deg
ZDOT = 4591
805970 TA = 197
83694
MA = 197
88182
Ha = 192
397 n
mi
Hp = 180
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6186586
55 X = -1929922
30
Y = 17939852
60 feet Y = 5446732
84 meter
Z = -11315175
02 Z = -3458133
65
XDOT = -20069
615509 XDOT = -6147
825342
YDOT = 2568
700885 feet/sec YDOT = 714
362731 meter/sec
ZDOT = 15064
980217 ZDOT = 4562
014089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16813723
73 X = 5124822
99
Y = 8751600
09 feet Y = 2667487
71 meter
Z = -11351367
35 Z = -3459896
77
XDOT = 143
101473 XDOT = 43
617329
YDOT = 19088
089590 feet/sec YDOT = 5818
049707 meter/sec
ZDOT = 14947
604920 ZDOT = 4556
029980
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 09271
21557202
00020000 00000-0 20000-3 0 9147
2 25544 51
6366 137
8843 0008649 137
1581 223
0258 15
74316831 22180
Satellite: ISS
Catalog Number: 25544
Epoch time: 09271
21557202 = yrday
fracday
Element set: 914
Inclination: 51
6366 deg
RA of node: 137
8843 deg
Eccentricity:
0008649
Arg of perigee: 137
1581 deg
Mean anomaly: 223
0258 deg
Mean motion: 15
74316831 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2218
Checksum: 289
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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