Date:
July 25th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10387 17 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 2918)
---------------------------------------
Vector Time (GMT): 2010/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5051674
66 A = 6731415
42 meter
Y = -50264
26 meter E =
0013596
Z = 4435802
57 I = 51
87389
XDOT = -2837
795095 Wp = 100
34300
YDOT = -6358
898142 meter/sec RA = 44
13051 deg
ZDOT = -3297
747213 TA = 22
64964
MA = 22
58970
Ha = 196
702 n
mi
Hp = 185
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16573735
78 X = -5072285
11
Y = -164908
98 feet Y = -106871
01 meter
Z = 14553158
04 Z = 4411211
87
XDOT = -9310
351360 XDOT = -2750
458238
YDOT = -20862
526713 feet/sec YDOT = -6390
143233 meter/sec
ZDOT = -10819
380619 ZDOT = -3311
321822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8273573
14 X = 2521785
09
Y = 14460859
84 feet Y = 4407670
08 meter
Z = 14454820
71 Z = 4405829
35
XDOT = -12280
265708 XDOT = -3743
024988
YDOT = 17915
198097 feet/sec YDOT = 5460
552380 meter/sec
ZDOT = -10873
599199 ZDOT = -3314
273036
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10204
54185273
00016717 00000-0 10270-3 0 9009
2 25544 51
6449 44
5248 0007462 141
2594 218
9104 15
71306044 29190
Satellite: ISS
Catalog Number: 25544
Epoch time: 10204
54185273 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 44
5248 deg
Eccentricity:
0007462
Arg of perigee: 141
2594 deg
Mean anomaly: 218
9104 deg
Mean motion: 15
71306044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2919
Checksum: 293
Coasting Arc #2 (Orbit 2934)
---------------------------------------
Vector Time (GMT): 2010/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3770743
64 A = 6737879
31 meter
Y = 5173459
83 meter E =
0017588
Z = 2088943
22 I = 51
87211
XDOT = -5115
506066 Wp = 94
25892
YDOT = 1467
131688 meter/sec RA = 39
07357 deg
ZDOT = 5559
253285 TA = 288
96641
MA = 289
15693
Ha = 196
503 n
mi
Hp = 185
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12371206
16 X = 3702465
32
Y = 16973293
40 feet Y = 5215244
48 meter
Z = 6853488
25 Z = 2107096
00
XDOT = -16783
156385 XDOT = -5158
536899
YDOT = 4813
424173 feet/sec YDOT = 1409
685668 meter/sec
ZDOT = 18239
019963 ZDOT = 5534
298344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8088328
87 X = 2465322
64
Y = -19357654
91 feet Y = -5900213
22 meter
Z = 6926028
05 Z = 2111053
35
XDOT = 11482
423366 XDOT = 3499
842642
YDOT = 11335
752543 feet/sec YDOT = 3455
137375 meter/sec
ZDOT = 18139
206288 ZDOT = 5528
830077
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10205
55943429
00016717 00000-0 10270-3 0 9017
2 25544 51
6435 39
3195 0007584 145
4463 214
7193 15
71323332 29353
Satellite: ISS
Catalog Number: 25544
Epoch time: 10205
55943429 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 39
3195 deg
Eccentricity:
0007584
Arg of perigee: 145
4463 deg
Mean anomaly: 214
7193 deg
Mean motion: 15
71323332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2935
Checksum: 304
Coasting Arc #3 (Orbit 2949)
---------------------------------------
Vector Time (GMT): 2010/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3606099
04 A = 6728489
19 meter
Y = -2448567
73 meter E =
0019904
Z = -5142832
23 I = 51
81533
XDOT = 5548
138306 Wp = 117
16657
YDOT = 5110
810811 meter/sec RA = 33
94078 deg
ZDOT = 1452
380116 TA = 166
77763
MA = 166
72538
Ha = 196
491 n
mi
Hp = 186
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11831033
58 X = 3658193
73
Y = -8033358
71 feet Y = -2407950
27 meter
Z = -16872809
14 Z = -5125187
96
XDOT = 18202
553499 XDOT = 5483
520700
YDOT = 16767
752003 feet/sec YDOT = 5172
491933 meter/sec
ZDOT = 4765
026627 ZDOT = 1479
176038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13167180
91 X = -4013356
74
Y = -5788838
65 feet Y = -1764438
02 meter
Z = -16802219
80 Z = -5121316
59
XDOT = 4034
666007 XDOT = 1229
766199
YDOT = -23362
564699 feet/sec YDOT = -7120
909720 meter/sec
ZDOT = 4872
134206 ZDOT = 1485
026506
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 10206
51340896
00016717 00000-0 10270-3 0 9024
2 25544 51
6428 34
4389 0007639 148
0345 212
1282 15
71320767 29502
Satellite: ISS
Catalog Number: 25544
Epoch time: 10206
51340896 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 34
4389 deg
Eccentricity:
0007639
Arg of perigee: 148
0345 deg
Mean anomaly: 212
1282 deg
Mean motion: 15
71320767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2950
Checksum: 300
Coasting Arc #4 (Orbit 2965)
---------------------------------------
Vector Time (GMT): 2010/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5714205
85 A = 6739593
39 meter
Y = -3530278
66 meter E =
0018541
Z = -425239
47 I = 51
82799
XDOT = 2823
580087 Wp = 143
14837
YDOT = -3861
336081 meter/sec RA = 28
85529 deg
ZDOT = -6035
343478 TA = 41
46147
MA = 41
32094
Ha = 196
255 n
mi
Hp = 186
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18747394
52 X = -5672239
25
Y = -11582279
06 feet Y = -3593943
63 meter
Z = -1395142
62 Z = -452896
86
XDOT = 9263
714197 XDOT = 2895
866314
YDOT = -12668
425461 feet/sec YDOT = -3829
356328 meter/sec
ZDOT = -19800
995662 ZDOT = -6021
451664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 606567
08 X = 184881
64
Y = 22021019
85 feet Y = 6712006
85 meter
Z = -1505713
59 Z = -458941
50
XDOT = -14133
322696 XDOT = -4307
836758
YDOT = -929
755272 feet/sec YDOT = -283
389407 meter/sec
ZDOT = -19745
398379 ZDOT = -6018
397426
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 10207
53097022
00016717 00000-0 10270-3 0 9038
2 25544 51
6433 29
2344 0007408 151
3723 208
7847 15
71366676 29666
Satellite: ISS
Catalog Number: 25544
Epoch time: 10207
53097022 = yrday
fracday
Element set: 903
Inclination: 51
6433 deg
RA of node: 29
2344 deg
Eccentricity:
0007408
Arg of perigee: 151
3723 deg
Mean anomaly: 208
7847 deg
Mean motion: 15
71366676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2966
Checksum: 308
Coasting Arc #5 (Orbit 2981)
---------------------------------------
Vector Time (GMT): 2010/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1132726
84 A = 6727869
73 meter
Y = 4031436
18 meter E =
0009768
Z = 5261384
14 I = 51
76022
XDOT = -7188
471543 Wp = 143
29056
YDOT = -2712
856441 meter/sec RA = 23
75027 deg
ZDOT = 522
888832 TA = 301
70261
MA = 301
79780
Ha = 196
407 n
mi
Hp = 186
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3716295
42 X = -1203281
18
Y = 13226496
66 feet Y = 4018374
43 meter
Z = 17261758
98 Z = 5255710
44
XDOT = -23584
224222 XDOT = -7160
141667
YDOT = -8900
447641 feet/sec YDOT = -2793
083868 meter/sec
ZDOT = 1715
514540 ZDOT = 488
036617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13079874
16 X = 3986745
64
Y = -4295603
59 feet Y = -1309299
97 meter
Z = 17239027
54 Z = 5254455
59
XDOT = 5622
848889 XDOT = 1713
844341
YDOT = 23554
467450 feet/sec YDOT = 7179
401679 meter/sec
ZDOT = 1576
162048 ZDOT = 480
414192
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 10208
54852465
00016717 00000-0 10270-3 0 9041
2 25544 51
6426 24
0288 0007625 154
9149 205
2384 15
71302027 29826
Satellite: ISS
Catalog Number: 25544
Epoch time: 10208
54852465 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 24
0288 deg
Eccentricity:
0007625
Arg of perigee: 154
9149 deg
Mean anomaly: 205
2384 deg
Mean motion: 15
71302027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2982
Checksum: 301
Coasting Arc #6 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2010/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6518213
74 A = 6738968
27 meter
Y = 1106846
55 meter E =
0008243
Z = -1311392
10 I = 51
77054
XDOT = 326
320347 Wp = 89
83245
YDOT = 4975
761012 meter/sec RA = 18
62672 deg
ZDOT = 5853
215940 TA = 255
82752
MA = 255
91912
Ha = 196
226 n
mi
Hp = 186
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21385215
67 X = 6511722
70
Y = 3631386
32 feet Y = 1179700
90 meter
Z = -4302467
52 Z = -1279742
96
XDOT = 1070
604812 XDOT = 242
222948
YDOT = 16324
675235 feet/sec YDOT = 4978
939530 meter/sec
ZDOT = 19203
464369 ZDOT = 5854
597224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9397905
85 X = -2864481
70
Y = -19577200
34 feet Y = -5967130
66 meter
Z = -4175911
31 Z = -1272817
77
XDOT = 11348
673224 XDOT = 3459
075599
YDOT = -9522
435226 feet/sec YDOT = -2902
438257 meter/sec
ZDOT = 19208
938643 ZDOT = 5854
884498
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 10209
50246904
00016717 00000-0 10270-3 0 9054
2 25544 51
6432 19
1486 0007713 159
1281 201
0197 15
71367079 29970
Satellite: ISS
Catalog Number: 25544
Epoch time: 10209
50246904 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 19
1486 deg
Eccentricity:
0007713
Arg of perigee: 159
1281 deg
Mean anomaly: 201
0197 deg
Mean motion: 15
71367079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 308
Coasting Arc #7 (Orbit 3012)
---------------------------------------
Vector Time (GMT): 2010/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1701616
64 A = 6729368
66 meter
Y = -4351498
58 meter E =
0014499
Z = -4853562
31 I = 51
71021
XDOT = 7300
941565 Wp = 104
45011
YDOT = -189
112303 meter/sec RA = 13
54983 deg
ZDOT = -2399
597178 TA = 142
16695
MA = 142
06495
Ha = 196
094 n
mi
Hp = 186
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5582731
76 X = -1629253
60
Y = -14276570
16 feet Y = -4370122
23 meter
Z = -15923760
87 Z = -4861653
08
XDOT = 23953
220357 XDOT = 7314
170238
YDOT = -620
447189 feet/sec YDOT = -107
394723 meter/sec
ZDOT = -7872
694154 ZDOT = -2364
097697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8267326
67 X = -2519881
17
Y = 12868898
92 feet Y = 3922440
39 meter
Z = -15956072
83 Z = -4863411
00
XDOT = -13754
737687 XDOT = -4192
444047
YDOT = -18383
133758 feet/sec YDOT = -5603
179169 meter/sec
ZDOT = -7730
732664 ZDOT = -2356
327316
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 10210
52000145
00016717 00000-0 10270-3 0 9064
2 25544 51
6438 13
9442 0007671 161
7897 198
3541 15
71394010 30131
Satellite: ISS
Catalog Number: 25544
Epoch time: 10210
52000145 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 13
9442 deg
Eccentricity:
0007671
Arg of perigee: 161
7897 deg
Mean anomaly: 198
3541 deg
Mean motion: 15
71394010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 279
Coasting Arc #8 (Orbit 3028)
---------------------------------------
Vector Time (GMT): 2010/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5930962
41 A = 6736211
62 meter
Y = 1396682
44 meter E =
0017924
Z = 2846425
60 I = 51
70268
XDOT = -3528
660965 Wp = 122
37886
YDOT = -4583
582721 meter/sec RA = 8
39639 deg
ZDOT = -5089
674738 TA = 24
98530
MA = 24
89866
Ha = 196
086 n
mi
Hp = 186
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19458538
10 X = -5959966
80
Y = 4582291
47 feet Y = 1330196
58 meter
Z = 9338666
68 Z = 2817542
99
XDOT = -11576
971671 XDOT = -3452
419865
YDOT = -15038
001054 feet/sec YDOT = -4622
615817 meter/sec
ZDOT = -16698
407934 ZDOT = -5106
631747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15456956
54 X = 4711280
35
Y = 12761607
52 feet Y = 3889737
97 meter
Z = 9223159
08 Z = 2811218
89
XDOT = -4095
729320 XDOT = -1248
378297
YDOT = 17111
178159 feet/sec YDOT = 5215
487103 meter/sec
ZDOT = -16766
170221 ZDOT = -5110
328683
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 10211
53752327
00016717 00000-0 10270-3 0 9073
2 25544 51
6433 8
7385 0007662 166
8970 193
2392 15
71381329 30296
Satellite: ISS
Catalog Number: 25544
Epoch time: 10211
53752327 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 8
7385 deg
Eccentricity:
0007662
Arg of perigee: 166
8970 deg
Mean anomaly: 193
2392 deg
Mean motion: 15
71381329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3029
Checksum: 313
Coasting Arc #9 (Orbit 3044)
---------------------------------------
Vector Time (GMT): 2010/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4315912
00 A = 6732738
72 meter
Y = 3359313
73 meter E =
0015481
Z = 3923438
07 I = 51
66253
XDOT = -5903
086034 Wp = 128
10688
YDOT = 2850
700287 meter/sec RA = 3
33295 deg
ZDOT = 4032
641981 TA = 279
89262
MA = 280
06734
Ha = 195
790 n
mi
Hp = 186
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14159816
27 X = 4258967
60
Y = 11021370
51 feet Y = 3407258
29 meter
Z = 12872172
14 Z = 3944266
39
XDOT = -19367
080165 XDOT = -5954
114009
YDOT = 9352
691230 feet/sec YDOT = 2784
402969 meter/sec
ZDOT = 13230
452693 ZDOT = 4003
841240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -55774
47 X = -17000
06
Y = -17883448
70 feet Y = -5450875
16 meter
Z = 12955422
51 Z = 3948812
78
XDOT = 18075
392861 XDOT = 5509
379744
YDOT = 9492
340840 feet/sec YDOT = 2893
265488 meter/sec
ZDOT = 13115
263431 ZDOT = 3997
532294
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 10212
55503423
00016717 00000-0 10270-3 0 9088
2 25544 51
6442 3
5336 0007690 170
8398 189
2906 15
71432117 30451
Satellite: ISS
Catalog Number: 25544
Epoch time: 10212
55503423 = yrday
fracday
Element set: 908
Inclination: 51
6442 deg
RA of node: 3
5336 deg
Eccentricity:
0007690
Arg of perigee: 170
8398 deg
Mean anomaly: 189
2906 deg
Mean motion: 15
71432117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3045
Checksum: 293
Coasting Arc #10 (Orbit 3059)
---------------------------------------
Vector Time (GMT): 2010/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4143151
08 A = 6732333
45 meter
Y = -3382286
71 meter E =
0012776
Z = -4102685
92 I = 51
63161
XDOT = 6060
174809 Wp = 141
21920
YDOT = 2813
658124 meter/sec RA = 358
16745 deg
ZDOT = 3796
947835 TA = 167
85857
MA = 167
82775
Ha = 195
761 n
mi
Hp = 186
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13593015
35 X = 4200594
48
Y = -11096741
17 feet Y = -3335634
14 meter
Z = -13460255
65 Z = -4082419
25
XDOT = 19882
463284 XDOT = 6009
816795
YDOT = 9231
161825 feet/sec YDOT = 2881
144874 meter/sec
ZDOT = 12457
177936 ZDOT = 3826
265792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17241803
89 X = -5255301
83
Y = -3578232
32 feet Y = -1090645
21 meter
Z = -13379187
76 Z = -4077976
43
XDOT = -5630
662363 XDOT = -1716
225888
YDOT = -19926
641613 feet/sec YDOT = -6073
640364 meter/sec
ZDOT = 12574
374227 ZDOT = 3832
669264
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 10213
50894282
00016717 00000-0 10270-3 0 9091
2 25544 51
6453 358
6546 0007622 173
5463 186
5799 15
71421803 30605
Satellite: ISS
Catalog Number: 25544
Epoch time: 10213
50894282 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 358
6546 deg
Eccentricity:
0007622
Arg of perigee: 173
5463 deg
Mean anomaly: 186
5799 deg
Mean motion: 15
71421803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3060
Checksum: 320
Coasting Arc #11 (Orbit 3075)
---------------------------------------
Vector Time (GMT): 2010/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6030253
76 A = 6736319
68 meter
Y = -1386123
84 meter E =
0011167
Z = -2651905
94 I = 51
61520
XDOT = 3337
600407 Wp = 156
50062
YDOT = -4568
545929 meter/sec RA = 353
09814 deg
ZDOT = -5219
111720 TA = 53
66872
MA = 53
56568
Ha = 195
510 n
mi
Hp = 186
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19784297
10 X = -6001423
26
Y = -4547650
40 feet Y = -1453396
38 meter
Z = -8700478
82 Z = -2681130
85
XDOT = 10950
132569 XDOT = 3413
792058
YDOT = -14988
667745 feet/sec YDOT = -4530
796561 meter/sec
ZDOT = -17123
069948 ZDOT = -5202
712931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9261823
55 X = 2823003
82
Y = 18007539
53 feet Y = 5488698
05 meter
Z = -8817313
21 Z = -2687517
07
XDOT = -17268
797050 XDOT = -5263
529341
YDOT = 557
603808 feet/sec YDOT = 169
957641 meter/sec
ZDOT = -17057
455857 ZDOT = -5199
112545
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 10214
52643407
00016717 00000-0 10270-3 0 9107
2 25544 51
6451 353
4494 0007543 177
6233 182
4966 15
71445583 30769
Satellite: ISS
Catalog Number: 25544
Epoch time: 10214
52643407 = yrday
fracday
Element set: 910
Inclination: 51
6451 deg
RA of node: 353
4494 deg
Eccentricity:
0007543
Arg of perigee: 177
6233 deg
Mean anomaly: 182
4966 deg
Mean motion: 15
71445583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3076
Checksum: 310
Coasting Arc #12 (Orbit 3091)
---------------------------------------
Vector Time (GMT): 2010/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1546498
27 A = 6729061
70 meter
Y = 4320234
81 meter E =
0006728
Z = 4915846
57 I = 51
56084
XDOT = -7387
967414 Wp = 126
75017
YDOT = -180
564658 meter/sec RA = 347
93906 deg
ZDOT = -2167
443875 TA = 344
29696
MA = 344
31782
Ha = 195
566 n
mi
Hp = 187
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5073813
23 X = -1618573
20
Y = 14173998
72 feet Y = 4302537
57 meter
Z = 16128105
55 Z = 4908158
97
XDOT = -24238
738236 XDOT = -7374
870203
YDOT = -592
403732 feet/sec YDOT = -263
107931 meter/sec
ZDOT = -7111
036335 ZDOT = -2203
302695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14071678
46 X = 4289047
59
Y = -5442947
43 feet Y = -1659010
38 meter
Z = 16097322
69 Z = 4906463
96
XDOT = 15089
335250 XDOT = 4599
229384
YDOT = 17574
526314 feet/sec YDOT = 5356
715620 meter/sec
ZDOT = -7254
404772 ZDOT = -2211
142575
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 10215
54391660
00016717 00000-0 10270-3 0 9112
2 25544 51
6456 348
2447 0007544 180
5928 179
5226 15
71422124 30929
Satellite: ISS
Catalog Number: 25544
Epoch time: 10215
54391660 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 348
2447 deg
Eccentricity:
0007544
Arg of perigee: 180
5928 deg
Mean anomaly: 179
5226 deg
Mean motion: 15
71422124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3092
Checksum: 305
Coasting Arc #13 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2010/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6553441
98 A = 6738767
78 meter
Y = -1106404
93 meter E =
0011012
Z = 1103517
20 I = 51
56591
XDOT = -165
849792 Wp = 89
71124
YDOT = 4943
982521 meter/sec RA = 342
84587 deg
ZDOT = 5891
343652 TA = 282
35855
MA = 282
48179
Ha = 195
299 n
mi
Hp = 187
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21500793
90 X = 6559966
27
Y = -3629937
43 feet Y = -1033084
04 meter
Z = 3620463
25 Z = 1135369
41
XDOT = -544
126615 XDOT = -249
740924
YDOT = 16220
415095 feet/sec YDOT = 4941
658282 meter/sec
ZDOT = 19328
555289 ZDOT = 5890
334646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17109386
99 X = -5214941
15
Y = -13482989
66 feet Y = -4109615
25 meter
Z = 3747826
64 Z = 1142337
56
XDOT = 11481
566150 XDOT = 3499
581363
YDOT = -9153
599326 feet/sec YDOT = -2790
017075 meter/sec
ZDOT = 19324
466743 ZDOT = 5890
097463
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 10216
56138510
00016717 00000-0 10270-3 0 9129
2 25544 51
6465 343
0397 0007495 185
1589 174
9497 15
71488715 31080
Satellite: ISS
Catalog Number: 25544
Epoch time: 10216
56138510 = yrday
fracday
Element set: 912
Inclination: 51
6465 deg
RA of node: 343
0397 deg
Eccentricity:
0007495
Arg of perigee: 185
1589 deg
Mean anomaly: 174
9497 deg
Mean motion: 15
71488715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 333
Coasting Arc #14 (Orbit 3122)
---------------------------------------
Vector Time (GMT): 2010/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1216022
89 A = 6727258
66 meter
Y = -4026064
53 meter E =
0015978
Z = -5262851
01 I = 51
49878
XDOT = 7206
725024 Wp = 119
89370
YDOT = -2649
475893 meter/sec RA = 337
70896 deg
ZDOT = 354
652571 TA = 153
52713
MA = 153
44542
Ha = 195
092 n
mi
Hp = 187
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3989576
43 X = -1145346
55
Y = -13208873
13 feet Y = -4039267
09 meter
Z = -17266571
55 Z = -5268587
16
XDOT = 23644
110972 XDOT = 7234
093502
YDOT = -8692
506212 feet/sec YDOT = -2568
732999 meter/sec
ZDOT = 1163
558303 ZDOT = 389
728766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6977813
76 X = -2126837
63
Y = 11870558
51 feet Y = 3618146
23 meter
Z = -17289462
06 Z = -5269828
03
XDOT = -21642
334340 XDOT = -6596
583507
YDOT = -10789
389376 feet/sec YDOT = -3288
605882 meter/sec
ZDOT = 1303
831155 ZDOT = 397
407736
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 10217
51525455
00016717 00000-0 10270-3 0 9134
2 25544 51
6466 338
1608 0007339 188
9605 171
1427 15
71511266 31235
Satellite: ISS
Catalog Number: 25544
Epoch time: 10217
51525455 = yrday
fracday
Element set: 913
Inclination: 51
6466 deg
RA of node: 338
1608 deg
Eccentricity:
0007339
Arg of perigee: 188
9605 deg
Mean anomaly: 171
1427 deg
Mean motion: 15
71511266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 303
Coasting Arc #15 (Orbit 3138)
---------------------------------------
Vector Time (GMT): 2010/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5766055
94 A = 6739212
81 meter
Y = 3432149
99 meter E =
0017667
Z = 492251
71 I = 51
51160
XDOT = -2841
666616 Wp = 151
61571
YDOT = -3902
680609 meter/sec RA = 332
58130 deg
ZDOT = -6002
766251 TA = 23
02104
MA = 22
94196
Ha = 194
971 n
mi
Hp = 187
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18917506
36 X = -5806397
56
Y = 11260334
62 feet Y = 3367444
89 meter
Z = 1614999
06 Z = 464142
95
XDOT = -9323
053201 XDOT = -2768
654938
YDOT = -12804
070241 feet/sec YDOT = -3934
048918 meter/sec
ZDOT = -19694
114998 ZDOT = -6016
393996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21261697
15 X = 6480565
29
Y = 5740898
27 feet Y = 1749825
79 meter
Z = 1502573
11 Z = 457984
28
XDOT = -2359
321556 XDOT = -719
121210
YDOT = 13973
713086 feet/sec YDOT = 4259
187749 meter/sec
ZDOT = -19748
562764 ZDOT = -6019
361930
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 10218
53270511
00016717 00000-0 10270-3 0 9148
2 25544 51
6468 332
9551 0007375 193
1987 166
8983 15
71501333 31396
Satellite: ISS
Catalog Number: 25544
Epoch time: 10218
53270511 = yrday
fracday
Element set: 914
Inclination: 51
6468 deg
RA of node: 332
9551 deg
Eccentricity:
0007375
Arg of perigee: 193
1987 deg
Mean anomaly: 166
8983 deg
Mean motion: 15
71501333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 318
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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