Date:
August 30th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18567 75 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
There are no maneuvers
Coasting Arc #1 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2010/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2116659
73 A = 6728217
75 meter
Y = 3736165
50 meter E =
0009670
Z = -5186996
88 I = 51
38172
XDOT = -5948
813946 Wp = 49
55588
YDOT = -4769
716509 meter/sec RA = 224
75478 deg
ZDOT = -1003
117774 TA = 210
80570
MA = 210
86248
Ha = 193
710 n
mi
Hp = 190
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6944421
69 X = -2133083
56
Y = 12257760
83 feet Y = 3712403
62 meter
Z = -17017706
31 Z = -5197319
66
XDOT = -19517
106121 XDOT = -5890
163033
YDOT = -15648
676209 feet/sec YDOT = -4835
911834 meter/sec
ZDOT = -3291
068811 ZDOT = -1031
874207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11405669
68 X = 3476448
12
Y = -8184315
72 feet Y = -2494579
43 meter
Z = -17058947
69 Z = -5199567
26
XDOT = 10396
539229 XDOT = 3168
865157
YDOT = 21622
097260 feet/sec YDOT = 6590
415245 meter/sec
ZDOT = -3406
206913 ZDOT = -1038
211867
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 10239
51765441
00016717 00000-0 10270-3 0 9005
2 25544 51
6417 225
6233 0008214 301
6070 58
4290 15
71281760 34699
Satellite: ISS
Catalog Number: 25544
Epoch time: 10239
51765441 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 225
6233 deg
Eccentricity:
0008214
Arg of perigee: 301
6070 deg
Mean anomaly: 58
4290 deg
Mean motion: 15
71281760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 288
Coasting Arc #2 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2010/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5779175
60 A = 6738424
72 meter
Y = 3006768
58 meter E =
0006070
Z = 1714688
33 I = 51
43933
XDOT = -957
107024 Wp = 99
93045
YDOT = 5092
007356 meter/sec RA = 219
59875 deg
ZDOT = -5687
140858 TA = 61
07253
MA = 61
01167
Ha = 193
898 n
mi
Hp = 189
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18960549
87 X = 5736794
21
Y = 9864726
32 feet Y = 3071157
91 meter
Z = 5625617
90 Z = 1742660
41
XDOT = -3140
114907 XDOT = -986
348599
YDOT = 16706
060879 feet/sec YDOT = 5081
140613 meter/sec
ZDOT = -18658
598617 ZDOT = -5691
861771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13226437
74 X = -4031418
22
Y = -16751244
55 feet Y = -5105779
34 meter
Z = 5737595
67 Z = 1748819
16
XDOT = 8384
074597 XDOT = 2555
465937
YDOT = -13034
917180 feet/sec YDOT = -3973
042757 meter/sec
ZDOT = -18677
401489 ZDOT = -5692
871974
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 10240
53522830
00016717 00000-0 10270-3 0 9013
2 25544 51
6419 220
4184 0008399 306
1829 53
8555 15
71342293 34855
Satellite: ISS
Catalog Number: 25544
Epoch time: 10240
53522830 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 220
4184 deg
Eccentricity:
0008399
Arg of perigee: 306
1829 deg
Mean anomaly: 53
8555 deg
Mean motion: 15
71342293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 302
Coasting Arc #3 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2010/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -543031
09 A = 6730379
69 meter
Y = -4852898
67 meter E =
0001869
Z = 4630200
17 I = 51
43656
XDOT = 6872
470086 Wp = 25
93865
YDOT = 1958
131649 meter/sec RA = 214
50752 deg
ZDOT = 2859
536562 TA = 35
69931
MA = 35
68682
Ha = 193
965 n
mi
Hp = 189
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1781598
05 X = -511217
42
Y = -15921583
55 feet Y = -4858793
09 meter
Z = 15190945
45 Z = 4627639
60
XDOT = 22547
474037 XDOT = 6836
171992
YDOT = 6424
316433 feet/sec YDOT = 2034
780894 meter/sec
ZDOT = 9381
681633 ZDOT = 2892
834804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4549437
35 X = -1386668
50
Y = 15371639
30 feet Y = 4685275
66 meter
Z = 15180614
71 Z = 4627051
36
XDOT = -17023
066876 XDOT = -5188
630784
YDOT = -14430
963079 feet/sec YDOT = -4398
557546 meter/sec
ZDOT = 9514
961884 ZDOT = 2900
160382
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 10241
55278286
00016717 00000-0 10270-3 0 9020
2 25544 51
6420 215
2140 0008435 308
9481 51
0928 15
71371570 35019
Satellite: ISS
Catalog Number: 25544
Epoch time: 10241
55278286 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 215
2140 deg
Eccentricity:
0008435
Arg of perigee: 308
9481 deg
Mean anomaly: 51
0928 deg
Mean motion: 15
71371570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 283
Coasting Arc #4 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2010/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5899372
44 A = 6735093
00 meter
Y = -375171
82 meter E =
0006465
Z = -3219488
00 I = 51
47824
XDOT = -2242
090080 Wp = 347
58919
YDOT = -5612
641873 meter/sec RA = 209
33248 deg
ZDOT = 4766
883074 TA = 334
72422
MA = 334
75584
Ha = 194
091 n
mi
Hp = 189
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19354896
46 X = -5879099
01
Y = -1230878
68 feet Y = -441028
87 meter
Z = -10562624
67 Z = -3248097
97
XDOT = -7355
938583 XDOT = -2202
318568
YDOT = -18414
179373 feet/sec YDOT = -5637
491770 meter/sec
ZDOT = 15639
380164 ZDOT = 4756
087724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17395785
30 X = 5302235
36
Y = 8431000
15 feet Y = 2569768
85 meter
Z = -10677125
54 Z = -3254387
86
XDOT = 551
688945 XDOT = 168
154790
YDOT = 18594
518950 feet/sec YDOT = 5667
609376 meter/sec
ZDOT = 15596
080265 ZDOT = 4753
685265
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 10242
50672292
00016717 00000-0 10270-3 0 9032
2 25544 51
6420 210
3344 0008379 313
7396 46
3072 15
71363552 35161
Satellite: ISS
Catalog Number: 25544
Epoch time: 10242
50672292 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 210
3344 deg
Eccentricity:
0008379
Arg of perigee: 313
7396 deg
Mean anomaly: 46
3072 deg
Mean motion: 15
71363552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 287
Coasting Arc #5 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2010/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3298286
97 A = 6733941
14 meter
Y = 4635086
75 meter E =
0007001
Z = -3609396
54 I = 51
50225
XDOT = -6234
732579 Wp = 357
71870
YDOT = 1016
169959 meter/sec RA = 204
25718 deg
ZDOT = -4385
228164 TA = 225
48019
MA = 225
53741
Ha = 194
302 n
mi
Hp = 189
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10821151
47 X = 3263745
28
Y = 15206977
52 feet Y = 4671777
00 meter
Z = -11841852
17 Z = -3593457
37
XDOT = -20455
159380 XDOT = -6224
329498
YDOT = 3333
890941 feet/sec YDOT = 946
507568 meter/sec
ZDOT = -14387
231510 ZDOT = -4415
491308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4648606
91 X = -1416895
39
Y = -18117632
86 feet Y = -5522254
50 meter
Z = -11777978
62 Z = -3589927
88
XDOT = 18873
774486 XDOT = 5752
726463
YDOT = 4604
387844 feet/sec YDOT = 1403
417415 meter/sec
ZDOT = -14508
335233 ZDOT = -4422
140579
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 10243
52423831
00016717 00000-0 10270-3 0 9049
2 25544 51
6426 205
1293 0008429 317
6357 42
4153 15
71423042 35324
Satellite: ISS
Catalog Number: 25544
Epoch time: 10243
52423831 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 205
1293 deg
Eccentricity:
0008429
Arg of perigee: 317
6357 deg
Mean anomaly: 42
4153 deg
Mean motion: 15
71423042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 277
Coasting Arc #6 (Orbit 3547)
---------------------------------------
Vector Time (GMT): 2010/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4717754
48 A = 6731120
51 meter
Y = -2029589
86 meter E =
0010421
Z = 4353736
50 I = 51
52136
XDOT = 5128
891745 Wp = 19
85399
YDOT = 4625
147920 meter/sec RA = 199
08304 deg
ZDOT = -3389
598053 TA = 104
45424
MA = 104
33858
Ha = 194
362 n
mi
Hp = 188
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15478197
12 X = 4718949
42
Y = -6658759
40 feet Y = -1976826
45 meter
Z = 14283912
39 Z = 4376658
25
XDOT = 16827
072653 XDOT = 5093
257361
YDOT = 15174
369817 feet/sec YDOT = 4682
303035 meter/sec
ZDOT = -11120
728520 ZDOT = -3364
768420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16746119
51 X = -5104217
23
Y = 923395
42 feet Y = 281450
92 meter
Z = 14375626
54 Z = 4381690
97
XDOT = -10534
656446 XDOT = -3210
963285
YDOT = -18858
993925 feet/sec YDOT = -5748
221348 meter/sec
ZDOT = -11021
262190 ZDOT = -3359
280716
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 10244
54173268
00016717 00000-0 10270-3 0 9059
2 25544 51
6425 199
9245 0008509 320
9442 39
1105 15
71452402 35480
Satellite: ISS
Catalog Number: 25544
Epoch time: 10244
54173268 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 199
9245 deg
Eccentricity:
0008509
Arg of perigee: 320
9442 deg
Mean anomaly: 39
1105 deg
Mean motion: 15
71452402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3548
Checksum: 303
Coasting Arc #7 (Orbit 3563)
---------------------------------------
Vector Time (GMT): 2010/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5469853
71 A = 6737189
98 meter
Y = -3205505
01 meter E =
0014049
Z = 2251734
38 I = 51
57111
XDOT = 4242
149635 Wp = 36
88594
YDOT = -3402
450297 meter/sec RA = 194
00431 deg
ZDOT = 5454
797220 TA = 348
40610
MA = 348
43842
Ha = 194
519 n
mi
Hp = 188
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17945714
27 X = -5444541
12
Y = -10516748
73 feet Y = -3266530
69 meter
Z = 7387580
00 Z = 2225223
35
XDOT = 13917
813762 XDOT = 4253
382831
YDOT = -11162
894674 feet/sec YDOT = -3354
949302 meter/sec
ZDOT = 17896
316339 ZDOT = 5475
432762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13516481
35 X = 4119823
52
Y = 15859162
25 feet Y = 4833872
66 meter
Z = 7281394
58 Z = 2219369
07
XDOT = -15562
801293 XDOT = -4743
541834
YDOT = 4999
369833 feet/sec YDOT = 1523
807925 meter/sec
ZDOT = 17978
865548 ZDOT = 5479
958219
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 10245
55920542
00016717 00000-0 10270-3 0 9067
2 25544 51
6427 194
7193 0008442 324
4604 35
5995 15
71492367 35641
Satellite: ISS
Catalog Number: 25544
Epoch time: 10245
55920542 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 194
7193 deg
Eccentricity:
0008442
Arg of perigee: 324
4604 deg
Mean anomaly: 35
5995 deg
Mean motion: 15
71492367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3564
Checksum: 322
Coasting Arc #8 (Orbit 3578)
---------------------------------------
Vector Time (GMT): 2010/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2499048
65 A = 6728123
53 meter
Y = 3673283
60 meter E =
0009763
Z = -5059131
11 I = 51
57087
XDOT = -7079
744665 Wp = 64
18699
YDOT = -2473
634587 meter/sec RA = 188
84948 deg
ZDOT = 1707
857818 TA = 222
24143
MA = 222
31668
Ha = 194
603 n
mi
Hp = 188
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8198978
52 X = -2515362
08
Y = 12051455
38 feet Y = 3645246
59 meter
Z = -16598199
18 Z = -5071310
98
XDOT = -23227
508743 XDOT = -7059
854250
YDOT = -8115
599040 feet/sec YDOT = -2552
693343 meter/sec
ZDOT = 5603
208063 ZDOT = 1673
512945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11468964
04 X = 3495740
24
Y = -8905316
13 feet Y = -2714340
36 meter
Z = -16646899
11 Z = -5073974
85
XDOT = 18895
959695 XDOT = 5759
488515
YDOT = 14159
740264 feet/sec YDOT = 4315
888833 meter/sec
ZDOT = 5465
655570 ZDOT = 1665
931818
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 10246
51306725
00016717 00000-0 10270-3 0 9076
2 25544 51
6429 189
8392 0008557 328
2353 31
8292 15
71507932 35799
Satellite: ISS
Catalog Number: 25544
Epoch time: 10246
51306725 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 189
8392 deg
Eccentricity:
0008557
Arg of perigee: 328
2353 deg
Mean anomaly: 31
8292 deg
Mean motion: 15
71507932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3579
Checksum: 329
Coasting Arc #9 (Orbit 3594)
---------------------------------------
Vector Time (GMT): 2010/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6623373
04 A = 6738965
66 meter
Y = 1008768
83 meter E =
0002915
Z = -724284
12 I = 51
63853
XDOT = -1359
114795 Wp = 103
03143
YDOT = 4649
380223 meter/sec RA = 183
75130 deg
ZDOT = -5973
928001 TA = 84
84704
MA = 84
81377
Ha = 194
728 n
mi
Hp = 188
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21730226
51 X = 6615118
94
Y = 3309609
03 feet Y = 1082789
21 meter
Z = -2376260
24 Z = -692128
19
XDOT = -4459
038042 XDOT = -1381
984069
YDOT = 15253
872124 feet/sec YDOT = 4634
053923 meter/sec
ZDOT = -19599
501315 ZDOT = -5980
586052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19779814
80 X = -6028887
55
Y = -9618244
59 feet Y = -2931640
95 meter
Z = -2247480
01 Z = -685031
91
XDOT = 7975
699411 XDOT = 2430
993180
YDOT = -11832
783388 feet/sec YDOT = -3606
632377 meter/sec
ZDOT = -19626
076496 ZDOT = -5982
028116
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 10247
53049846
00016717 00000-0 10270-3 0 9088
2 25544 51
6437 184
6337 0008549 332
0700 28
0002 15
71543973 35950
Satellite: ISS
Catalog Number: 25544
Epoch time: 10247
53049846 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 184
6337 deg
Eccentricity:
0008549
Arg of perigee: 332
0700 deg
Mean anomaly: 28
0002 deg
Mean motion: 15
71543973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3595
Checksum: 312
Coasting Arc #10 (Orbit 3610)
---------------------------------------
Vector Time (GMT): 2010/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -173995
12 A = 6726922
66 meter
Y = -4172960
54 meter E =
0007672
Z = 5274243
83 I = 51
62927
XDOT = 7692
759661 Wp = 351
01709
YDOT = -240
413694 meter/sec RA = 178
62858 deg
ZDOT = 71
019424 TA = 98
35206
MA = 98
26508
Ha = 194
742 n
mi
Hp = 188
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -570850
12 X = -152940
33
Y = -13690815
43 feet Y = -4174788
42 meter
Z = 17303949
58 Z = 5273449
81
XDOT = 25238
712798 XDOT = 7694
531273
YDOT = -788
758838 feet/sec YDOT = -154
378736 meter/sec
ZDOT = 233
003360 ZDOT = 108
394627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3194204
54 X = -973593
54
Y = 13329447
40 feet Y = 4062815
57 meter
Z = 17300689
51 Z = 5273250
16
XDOT = -23472
739736 XDOT = -7154
491071
YDOT = -6089
841507 feet/sec YDOT = -1856
183691 meter/sec
ZDOT = 382
678271 ZDOT = 116
640337
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 10248
54790639
00016717 00000-0 10270-3 0 9094
2 25544 51
6440 179
4285 0008608 335
1721 24
9026 15
71608896 36117
Satellite: ISS
Catalog Number: 25544
Epoch time: 10248
54790639 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 179
4285 deg
Eccentricity:
0008608
Arg of perigee: 335
1721 deg
Mean anomaly: 24
9026 deg
Mean motion: 15
71608896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3611
Checksum: 325
Coasting Arc #11 (Orbit 3625)
---------------------------------------
Vector Time (GMT): 2010/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6522874
36 A = 6738678
86 meter
Y = 1416282
97 meter E =
0016329
Z = -847354
40 I = 51
69923
XDOT = -1756
840713 Wp = 12
12698
YDOT = -4543
033023 meter/sec RA = 173
50388 deg
ZDOT = 5967
054102 TA = 338
63850
MA = 338
70657
Ha = 194
901 n
mi
Hp = 187
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21400506
43 X = -6534110
47
Y = 4646597
68 feet Y = 1343277
41 meter
Z = -2780034
12 Z = -879069
42
XDOT = -5763
913102 XDOT = -1734
895554
YDOT = -14904
963986 feet/sec YDOT = -4562
556053 meter/sec
ZDOT = 19576
949155 ZDOT = 5958
573041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21851708
76 X = 6660400
83
Y = 1163242
33 feet Y = 354556
26 meter
Z = -2907030
57 Z = -886062
92
XDOT = 1821
646854 XDOT = 555
237961
YDOT = 14334
401360 feet/sec YDOT = 4369
125535 meter/sec
ZDOT = 19542
889461 ZDOT = 5956
672708
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 10249
50170814
00016717 00000-0 10270-3 0 9100
2 25544 51
6442 174
5478 0008645 339
3199 20
7612 15
71599304 36269
Satellite: ISS
Catalog Number: 25544
Epoch time: 10249
50170814 = yrday
fracday
Element set: 910
Inclination: 51
6442 deg
RA of node: 174
5478 deg
Eccentricity:
0008645
Arg of perigee: 339
3199 deg
Mean anomaly: 20
7612 deg
Mean motion: 15
71599304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3626
Checksum: 313
Coasting Arc #12 (Orbit 3641)
---------------------------------------
Vector Time (GMT): 2010/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2790159
38 A = 6727917
62 meter
Y = 3492229
23 meter E =
0015435
Z = -5040399
10 I = 51
69458
XDOT = -6893
336683 Wp = 42
74507
YDOT = 2876
662060 meter/sec RA = 168
41408 deg
ZDOT = -1814
913631 TA = 209
70048
MA = 209
78820
Ha = 194
999 n
mi
Hp = 187
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9154066
22 X = 2775386
31
Y = 11457444
99 feet Y = 3523347
46 meter
Z = -16536742
46 Z = -5026880
84
XDOT = -22615
933999 XDOT = -6916
175304
YDOT = 9437
867650 feet/sec YDOT = 2799
448790 meter/sec
ZDOT = -5954
441048 ZDOT = -1848
456751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6130557
59 X = -1868593
95
Y = -13389419
26 feet Y = -4081094
99 meter
Z = -16482522
28 Z = -5023872
79
XDOT = 23236
622903 XDOT = 7082
522661
YDOT = -3112
071409 feet/sec YDOT = -948
559365 meter/sec
ZDOT = -6088
739000 ZDOT = -1855
847647
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 10250
51907415
00016717 00000-0 10270-3 0 9119
2 25544 51
6453 169
3419 0008585 343
5347 16
5543 15
71663760 36425
Satellite: ISS
Catalog Number: 25544
Epoch time: 10250
51907415 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 169
3419 deg
Eccentricity:
0008585
Arg of perigee: 343
5347 deg
Mean anomaly: 16
5543 deg
Mean motion: 15
71663760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3642
Checksum: 308
Coasting Arc #13 (Orbit 3657)
---------------------------------------
Vector Time (GMT): 2010/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5301230
31 A = 6736475
77 meter
Y = -3472309
03 meter E =
0012129
Z = 2282350
27 I = 51
75319
XDOT = 4422
977870 Wp = 70
11110
YDOT = 3154
045771 meter/sec RA = 163
26758 deg
ZDOT = -5447
395781 TA = 84
32879
MA = 84
19049
Ha = 195
052 n
mi
Hp = 187
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17392487
91 X = 5328577
14
Y = -11392089
99 feet Y = -3412874
36 meter
Z = 7488025
83 Z = 2308170
23
XDOT = 14511
082250 XDOT = 4413
842302
YDOT = 10347
919196 feet/sec YDOT = 3203
454553 meter/sec
ZDOT = -17872
033401 ZDOT = -5425
931607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19507555
67 X = -5945902
97
Y = 7083436
71 feet Y = 2159031
51 meter
Z = 7591381
76 Z = 2313853
16
XDOT = -11319
542471 XDOT = -3450
196545
YDOT = -12017
223516 feet/sec YDOT = -3662
849728 meter/sec
ZDOT = -17785
986654 ZDOT = -5421
168732
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 10251
53641747
00016717 00000-0 10270-3 0 9126
2 25544 51
6453 164
1361 0008564 346
8732 13
2206 15
71677512 36582
Satellite: ISS
Catalog Number: 25544
Epoch time: 10251
53641747 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 164
1361 deg
Eccentricity:
0008564
Arg of perigee: 346
8732 deg
Mean anomaly: 13
2206 deg
Mean motion: 15
71677512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 302
Coasting Arc #14 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2010/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4752647
22 A = 6730408
82 meter
Y = -1826806
05 meter E =
0009158
Z = 4392107
19 I = 51
76168
XDOT = 4964
331219 Wp = 55
36840
YDOT = -4837
080425 meter/sec RA = 158
20210 deg
ZDOT = 3360
129172 TA =
89508
MA =
89344
Ha = 195
248 n
mi
Hp = 187
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15592674
60 X = -4753202
35
Y = -5993458
16 feet Y = -1879955
67 meter
Z = 14409800
50 Z = 4369017
69
XDOT = 16287
175915 XDOT = 5001
728492
YDOT = -15869
686435 feet/sec YDOT = -4781
356865 meter/sec
ZDOT = 11024
045841 ZDOT = 3384
337182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14033296
04 X = 4277348
63
Y = 9207489
60 feet Y = 2806442
83 meter
Z = 14317266
84 Z = 4363902
93
XDOT = -18568
840534 XDOT = -5659
782595
YDOT = 11009
383534 feet/sec YDOT = 3355
660101 meter/sec
ZDOT = 11120
922910 ZDOT = 3389
657303
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 10252
55373780
00016717 00000-0 10270-3 0 9139
2 25544 51
6454 158
9299 0008588 350
7226 9
3776 15
71715490 36746
Satellite: ISS
Catalog Number: 25544
Epoch time: 10252
55373780 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 158
9299 deg
Eccentricity:
0008588
Arg of perigee: 350
7226 deg
Mean anomaly: 9
3776 deg
Mean motion: 15
71715490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 339
Coasting Arc #15 (Orbit 3688)
---------------------------------------
Vector Time (GMT): 2010/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3211663
47 A = 6733091
73 meter
Y = 4748126
21 meter E =
0009069
Z = -3528161
68 I = 51
79940
XDOT = -6180
155037 Wp = 28
95622
YDOT = -838
582048 meter/sec RA = 153
04458 deg
ZDOT = 4509
781199 TA = 289
20805
MA = 289
30617
Ha = 195
155 n
mi
Hp = 186
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10536953
64 X = -3247379
94
Y = 15577841
91 feet Y = 4712011
47 meter
Z = -11575333
61 Z = -3543851
17
XDOT = -20276
099203 XDOT = -6192
226333
YDOT = -2751
253437 feet/sec YDOT = -907
759362 meter/sec
ZDOT = 14795
870077 ZDOT = 4479
728628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13332332
21 X = 4063694
86
Y = -13209411
37 feet Y = -4026228
59 meter
Z = -11638095
54 Z = -3547291
52
XDOT = 18458
981391 XDOT = 5626
297528
YDOT = 5737
144906 feet/sec YDOT = 1748
681767 meter/sec
ZDOT = 14675
457019 ZDOT = 4473
079300
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 10253
50745442
00016717 00000-0 10270-3 0 9144
2 25544 51
6457 154
0491 0008640 353
8654 6
2401 15
71760945 36890
Satellite: ISS
Catalog Number: 25544
Epoch time: 10253
50745442 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 154
0491 deg
Eccentricity:
0008640
Arg of perigee: 353
8654 deg
Mean anomaly: 6
2401 deg
Mean motion: 15
71760945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3689
Checksum: 308
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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