Date:
December 7th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7104 18 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 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
330/17:15:59
000 2
4 -1
0 6
0
N/A 4
4 -0
3 195
6
000/01:41:00
000 3
4 5
9 186
1
330/18:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 195
7
000/00:00:00
000 0
0 0
0 186
2
Coasting Arc #1 (Orbit 1368)
---------------------------------------
Vector Time (GMT): 2008/329/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3752661
26 A = 6731498
17 meter
Y = 3759096
05 meter E =
0012849
Z = -4149239
72 I = 51
30960
XDOT = -2278
760499 Wp = 49
38569
YDOT = -6345
982612 meter/sec RA = 276
22359 deg
ZDOT = -3687
574004 TA = 182
67772
MA = 182
68461
Ha = 195
353 n
mi
Hp = 186
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12311880
77 X = -3774260
38
Y = 12332992
30 feet Y = 3717011
08 meter
Z = -13612991
22 Z = -4167522
90
XDOT = -7476
248355 XDOT = -2189
715277
YDOT = -20820
152926 feet/sec YDOT = -6370
966954 meter/sec
ZDOT = -12098
339909 ZDOT = -3698
428563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10418453
63 X = 3175544
67
Y = 13900132
88 feet Y = 4236760
50 meter
Z = -13683594
81 Z = -4170759
70
XDOT = -20663
736148 XDOT = -6298
306778
YDOT = 3533
740233 feet/sec YDOT = 1077
084023 meter/sec
ZDOT = -12140
903610 ZDOT = -3700
547420
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 08329
07539891
00020000 00000-0 20000-3 0 9003
2 25544 51
6419 276
8084 0006082 22
1144 338
0279 15
71598832 13693
Satellite: ISS
Catalog Number: 25544
Epoch time: 08329
07539891 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 276
8084 deg
Eccentricity:
0006082
Arg of perigee: 22
1144 deg
Mean anomaly: 338
0279 deg
Mean motion: 15
71598832 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1369
Checksum: 308
Coasting Arc #2 (Orbit 1384)
---------------------------------------
Vector Time (GMT): 2008/330/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2947029
53 A = 6732708
17 meter
Y = 4718563
72 meter E =
0015887
Z = 3785602
84 I = 51
31203
XDOT = -3430
239081 Wp = 63
58633
YDOT = 5495
630845 meter/sec RA = 271
03198 deg
ZDOT = -4159
185936 TA = 70
29901
MA = 70
12769
Ha = 195
426 n
mi
Hp = 186
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9668732
06 X = 2875656
46
Y = 15480852
10 feet Y = 4751119
76 meter
Z = 12419956
82 Z = 3799746
89
XDOT = -11254
065225 XDOT = -3471
232032
YDOT = 18030
284924 feet/sec YDOT = 5457
043030 meter/sec
ZDOT = -13645
623151 ZDOT = -4175
949681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16587296
49 X = 5055807
97
Y = -7525200
02 feet Y = -2293680
97 meter
Z = 12475153
26 Z = 3802426
71
XDOT = 15893
333653 XDOT = 4844
288097
YDOT = 12193
286205 feet/sec YDOT = 3716
513635 meter/sec
ZDOT = -13710
207299 ZDOT = -4178
871185
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 08330
09277122
00020000 00000-0 20000-3 0 9014
2 25544 51
6420 271
6026 0006195 27
4846 332
6643 15
71614422 13853
Satellite: ISS
Catalog Number: 25544
Epoch time: 08330
09277122 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 271
6026 deg
Eccentricity:
0006195
Arg of perigee: 27
4846 deg
Mean anomaly: 332
6643 deg
Mean motion: 15
71614422 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1385
Checksum: 269
Coasting Arc #3 (Orbit 1395)
---------------------------------------
Vector Time (GMT): 2008/330/18:06:29
000
Vector Time (MET): N/A
Weight (LBS) : 611749
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2549968
82 A = 6735479
26 meter
Y = 5528447
63 meter E =
0016597
Z = 2872409
41 I = 51
32203
XDOT = -3830
786353 Wp = 76
12351
YDOT = 4393
339918 meter/sec RA = 267
42910 deg
ZDOT = -5026
728875 TA = 70
74422
MA = 70
56475
Ha = 195
608 n
mi
Hp = 186
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8366039
43 X = 2474005
25
Y = 18137951
53 feet Y = 5556537
86 meter
Z = 9423915
38 Z = 2884613
48
XDOT = -12568
196696 XDOT = -3855
209049
YDOT = 14413
844874 feet/sec YDOT = 4350
365739 meter/sec
ZDOT = -16491
892636 ZDOT = -5045
398302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 186917
41 X = 56972
43
Y = 19950913
56 feet Y = 6081038
45 meter
Z = 9471652
04 Z = 2886959
54
XDOT = -15814
302905 XDOT = -4820
199525
YDOT = 8055
638424 feet/sec YDOT = 2455
358592 meter/sec
ZDOT = -16563
951753 ZDOT = -5048
692494
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 08330
79220596
00020000 00000-0 20000-3 0 9025
2 25544 51
6428 268
0257 0006600 25
7277 334
4212 15
71575369 13967
Satellite: ISS
Catalog Number: 25544
Epoch time: 08330
79220596 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 268
0257 deg
Eccentricity:
0006600
Arg of perigee: 25
7277 deg
Mean anomaly: 334
4212 deg
Mean motion: 15
71575369 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1396
Checksum: 294
Coasting Arc #4 (Orbit 1395)
---------------------------------------
Vector Time (GMT): 2008/330/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 279083
06 A = 6739230
86 meter
Y = 6731504
23 meter E =
0011931
Z = -29817
41 I = 51
33360
XDOT = -4802
999343 Wp = 103
76450
YDOT = 181
454948 meter/sec RA = 267
42301 deg
ZDOT = -6006
459231 TA = 76
56027
MA = 76
42732
Ha = 195
696 n
mi
Hp = 186
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 915626
84 X = 203934
39
Y = 22084987
62 feet Y = 6734204
92 meter
Z = -97826
14 Z = -28643
53
XDOT = -15757
871860 XDOT = -4775
492309
YDOT = 595
324633 feet/sec YDOT = 127
899363 meter/sec
ZDOT = -19706
231074 ZDOT = -6029
726034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7404772
70 X = -2256974
72
Y = 20826794
19 feet Y = 6348006
87 meter
Z = -92767
97 Z = -28275
68
XDOT = -13214
297759 XDOT = -4027
717957
YDOT = -4755
324038 feet/sec YDOT = -1449
422767 meter/sec
ZDOT = -19796
433236 ZDOT = -6033
952850
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 08330
79220742
00020000 00000-0 20000-3 0 9039
2 25544 51
6422 268
0259 0006481 27
2582 332
8919 15
71523634 13960
Satellite: ISS
Catalog Number: 25544
Epoch time: 08330
79220742 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 268
0259 deg
Eccentricity:
0006481
Arg of perigee: 27
2582 deg
Mean anomaly: 332
8919 deg
Mean motion: 15
71523634 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1396
Checksum: 291
Coasting Arc #5 (Orbit 1411)
---------------------------------------
Vector Time (GMT): 2008/331/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3989970
61 A = 6727430
55 meter
Y = -1528542
60 meter E =
0007320
Z = 5190470
71 I = 51
29577
XDOT = 1719
052126 Wp = 58
73674
YDOT = 7456
884396 meter/sec RA = 262
28928 deg
ZDOT = 877
363534 TA = 22
88669
MA = 22
85408
Ha = 195
651 n
mi
Hp = 186
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13090454
76 X = 3981551
42
Y = -5014903
56 feet Y = -1483972
08 meter
Z = 17029103
37 Z = 5209833
90
XDOT = 5639
934798 XDOT = 1631
278075
YDOT = 24464
843820 feet/sec YDOT = 7475
616966 meter/sec
ZDOT = 2878
489285 ZDOT = 885
502515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13926560
62 X = 4244815
68
Y = -34776
20 feet Y = -10599
79 meter
Z = 17104073
34 Z = 5213321
56
XDOT = -3503
778863 XDOT = -1067
951798
YDOT = 23841
908638 feet/sec YDOT = 7267
013753 meter/sec
ZDOT = 2910
610196 ZDOT = 887
153988
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 08331
80963282
00020000 00000-0 20000-3 0 9046
2 25544 51
6416 262
8191 0006488 31
4487 328
7061 15
71519793 14120
Satellite: ISS
Catalog Number: 25544
Epoch time: 08331
80963282 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 262
8191 deg
Eccentricity:
0006488
Arg of perigee: 31
4487 deg
Mean anomaly: 328
7061 deg
Mean motion: 15
71519793 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1412
Checksum: 298
Coasting Arc #6 (Orbit 1426)
---------------------------------------
Vector Time (GMT): 2008/332/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2638964
67 A = 6738059
22 meter
Y = -5997545
74 meter E =
0014525
Z = -1545254
41 I = 51
33629
XDOT = 3980
623841 Wp = 36
18716
YDOT = -3222
231088 meter/sec RA = 257
12643 deg
ZDOT = 5747
299203 TA = 306
71764
MA = 306
85097
Ha = 195
683 n
mi
Hp = 185
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8658020
57 X = -2564196
25
Y = -19676987
33 feet Y = -6026637
92 meter
Z = -5069732
30 Z = -1557893
94
XDOT = 13059
789506 XDOT = 3988
439479
YDOT = -10571
624304 feet/sec YDOT = -3177
674466 meter/sec
ZDOT = 18855
968515 ZDOT = 5766
656136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1387171
35 X = -422809
83
Y = -21441009
44 feet Y = -6535219
68 meter
Z = -5119199
73 Z = -1560332
08
XDOT = 14220
081924 XDOT = 4334
280971
YDOT = -5409
599760 feet/sec YDOT = -1648
846007 meter/sec
ZDOT = 18930
793074 ZDOT = 5770
105729
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 08332
76345467
00020000 00000-0 20000-3 0 9052
2 25544 51
6407 257
9378 0006381 34
4770 325
6805 15
71563620 14278
Satellite: ISS
Catalog Number: 25544
Epoch time: 08332
76345467 = yrday
fracday
Element set: 905
Inclination: 51
6407 deg
RA of node: 257
9378 deg
Eccentricity:
0006381
Arg of perigee: 34
4770 deg
Mean anomaly: 325
6805 deg
Mean motion: 15
71563620 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1427
Checksum: 302
Coasting Arc #7 (Orbit 1442)
---------------------------------------
Vector Time (GMT): 2008/333/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2727541
56 A = 6729201
73 meter
Y = 3925377
10 meter E =
0017300
Z = -4752943
23 I = 51
31373
XDOT = -4101
382072 Wp = 60
35875
YDOT = -5965
985482 meter/sec RA = 252
02177 deg
ZDOT = -2572
179246 TA = 184
23679
MA = 184
25146
Ha = 195
775 n
mi
Hp = 185
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8948627
16 X = -2748143
62
Y = 12878533
78 feet Y = 3894761
60 meter
Z = -15593645
76 Z = -4766243
42
XDOT = -13455
977927 XDOT = -4021
869180
YDOT = -19573
443184 feet/sec YDOT = -6011
404580 meter/sec
ZDOT = -8438
908289 ZDOT = -2591
911849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12567571
94 X = -3830595
93
Y = 9294543
87 feet Y = 2832976
97 meter
Z = -15644933
31 Z = -4768575
67
XDOT = -5630
115534 XDOT = -1716
059215
YDOT = -21954
684418 feet/sec YDOT = -6691
787811 meter/sec
ZDOT = -8515
889420 ZDOT = -2595
643095
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 08333
78085264
00020000 00000-0 20000-3 0 9062
2 25544 51
6399 252
7319 0006438 39
7024 320
4608 15
71596930 14431
Satellite: ISS
Catalog Number: 25544
Epoch time: 08333
78085264 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 252
7319 deg
Eccentricity:
0006438
Arg of perigee: 39
7024 deg
Mean anomaly: 320
4608 deg
Mean motion: 15
71596930 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1443
Checksum: 305
Coasting Arc #8 (Orbit 1458)
---------------------------------------
Vector Time (GMT): 2008/334/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4344584
70 A = 6735180
09 meter
Y = 4236926
55 meter E =
0017652
Z = 2910319
20 I = 51
34482
XDOT = -1996
715156 Wp = 80
52552
YDOT = 5502
120767 meter/sec RA = 246
83794 deg
ZDOT = -5000
752562 TA = 65
85101
MA = 65
66653
Ha = 195
659 n
mi
Hp = 185
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14253886
80 X = 4282745
75
Y = 13900677
66 feet Y = 4285164
04 meter
Z = 9548291
33 Z = 2931275
94
XDOT = -6550
902743 XDOT = -2033
799205
YDOT = 18051
577319 feet/sec YDOT = 5479
585699 meter/sec
ZDOT = -16406
668509 ZDOT = -5010
542075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9206606
16 X = 2806173
56
Y = 17608958
33 feet Y = 5367210
50 meter
Z = 9629900
57 Z = 2935193
69
XDOT = -10436
074882 XDOT = -3180
915624
YDOT = 14500
275058 feet/sec YDOT = 4419
683838 meter/sec
ZDOT = -16444
222459 ZDOT = -5012
199006
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 08334
79823497
00020000 00000-0 20000-3 0 9073
2 25544 51
6401 247
5252 0006316 41
6244 318
5398 15
71637224 14597
Satellite: ISS
Catalog Number: 25544
Epoch time: 08334
79823497 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 247
5252 deg
Eccentricity:
0006316
Arg of perigee: 41
6244 deg
Mean anomaly: 318
5398 deg
Mean motion: 15
71637224 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1459
Checksum: 302
Coasting Arc #9 (Orbit 1474)
---------------------------------------
Vector Time (GMT): 2008/335/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 604573
98 A = 6732276
71 meter
Y = -5449678
82 meter E =
0015811
Z = 3891015
88 I = 51
34676
XDOT = 5548
334310 Wp = 81
66302
YDOT = 3505
600230 meter/sec RA = 241
74901 deg
ZDOT = 4036
083084 TA = 326
15890
MA = 326
25970
Ha = 195
692 n
mi
Hp = 185
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1983510
44 X = 646566
15
Y = -17879523
68 feet Y = -5442683
87 meter
Z = 12765800
12 Z = 3894054
18
XDOT = 18203
196554 XDOT = 5489
114931
YDOT = 11501
313092 feet/sec YDOT = 3567
313238 meter/sec
ZDOT = 13241
742400 ZDOT = 4062
893892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7059798
47 X = 2151826
57
Y = -16537247
21 feet Y = -5040552
95 meter
Z = 12777168
46 Z = 3894480
95
XDOT = 12760
496521 XDOT = 3889
399340
YDOT = 15788
672142 feet/sec YDOT = 4812
387269 meter/sec
ZDOT = 13346
017016 ZDOT = 4067
865987
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 08335
81560564
00020000 00000-0 20000-3 0 9081
2 25544 51
6391 242
3186 0006250 47
4927 312
6762 15
71653704 14752
Satellite: ISS
Catalog Number: 25544
Epoch time: 08335
81560564 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node: 242
3186 deg
Eccentricity:
0006250
Arg of perigee: 47
4927 deg
Mean anomaly: 312
6762 deg
Mean motion: 15
71653704 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1475
Checksum: 295
Coasting Arc #10 (Orbit 1489)
---------------------------------------
Vector Time (GMT): 2008/336/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5070890
96 A = 6731625
79 meter
Y = -1791213
52 meter E =
0012269
Z = -4058323
10 I = 51
35995
XDOT = -711
964193 Wp = 83
81086
YDOT = -6630
086721 meter/sec RA = 236
55951 deg
ZDOT = 3827
132310 TA = 225
72892
MA = 225
82966
Ha = 195
788 n
mi
Hp = 185
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16636781
35 X = -5030769
64
Y = -5876684
79 feet Y = -1847694
30 meter
Z = -13314708
33 Z = -4082860
52
XDOT = -2335
840529 XDOT = -656
364267
YDOT = -21752
253022 feet/sec YDOT = -6637
737942 meter/sec
ZDOT = 12556
208365 ZDOT = 3823
807739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14292509
72 X = -4356356
96
Y = -10222242
89 feet Y = -3115739
63 meter
Z = -13410044
44 Z = -4087381
55
XDOT = 2948
469899 XDOT = 898
693625
YDOT = -20528
784785 feet/sec YDOT = -6257
173603 meter/sec
ZDOT = 12542
795042 ZDOT = 3823
043929
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 08336
76937899
00020000 00000-0 20000-3 0 9096
2 25544 51
6393 237
4373 0006373 52
8301 307
3442 15
71653887 14904
Satellite: ISS
Catalog Number: 25544
Epoch time: 08336
76937899 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 237
4373 deg
Eccentricity:
0006373
Arg of perigee: 52
8301 deg
Mean anomaly: 307
3442 deg
Mean motion: 15
71653887 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1490
Checksum: 322
Coasting Arc #11 (Orbit 1505)
---------------------------------------
Vector Time (GMT): 2008/337/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1851471
24 A = 6735463
65 meter
Y = 5863130
88 meter E =
0009507
Z = -2759644
19 I = 51
39031
XDOT = -5704
560077 Wp = 83
31300
YDOT = -601
486463 meter/sec RA = 231
47155 deg
ZDOT = -5119
177958 TA = 128
28933
MA = 128
20379
Ha = 195
845 n
mi
Hp = 185
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6074380
71 X = 1799177
11
Y = 19235993
69 feet Y = 5883543
03 meter
Z = -9053950
74 Z = -2750776
01
XDOT = -18715
748285 XDOT = -5672
541943
YDOT = -1973
380784 feet/sec YDOT = -665
098533 meter/sec
ZDOT = -16795
203275 ZDOT = -5146
813233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 921852
76 X = 280980
72
Y = 20166853
21 feet Y = 6146856
86 meter
Z = -9019079
62 Z = -2749015
47
XDOT = -15997
392224 XDOT = -4876
005150
YDOT = -6807
265491 feet/sec YDOT = -2074
854522 meter/sec
ZDOT = -16902
477082 ZDOT = -5151
875015
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 08337
78672258
00020000 00000-0 20000-3 0 9106
2 25544 51
6392 232
2308 0006500 55
8045 304
3733 15
71696510 15062
Satellite: ISS
Catalog Number: 25544
Epoch time: 08337
78672258 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 232
2308 deg
Eccentricity:
0006500
Arg of perigee: 55
8045 deg
Mean anomaly: 304
3733 deg
Mean motion: 15
71696510 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1506
Checksum: 280
Coasting Arc #12 (Orbit 1521)
---------------------------------------
Vector Time (GMT): 2008/338/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4634317
97 A = 6728641
78 meter
Y = -720101
96 meter E =
0013269
Z = 4817410
64 I = 51
38574
XDOT = 3500
345548 Wp = 60
11620
YDOT = 6430
111559 meter/sec RA = 226
29331 deg
ZDOT = -2394
701887 TA = 53
39026
MA = 53
26828
Ha = 195
792 n
mi
Hp = 185
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15204455
29 X = 4618623
55
Y = -2362539
25 feet Y = -668366
57 meter
Z = 15805153
03 Z = 4839886
14
XDOT = 11484
073319 XDOT = 3439
815950
YDOT = 21096
166531 feet/sec YDOT = 6468
916247 meter/sec
ZDOT = -7856
633486 ZDOT = -2377
843467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15234429
39 X = 4643454
08
Y = 1380785
45 feet Y = 420863
40 meter
Z = 15892309
69 Z = 4843975
99
XDOT = 6158
099101 XDOT = 1876
988606
YDOT = 22154
332691 feet/sec YDOT = 6752
640604 meter/sec
ZDOT = -7790
701617 ZDOT = -2374
605853
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 08338
80405469
00020000 00000-0 20000-3 0 9119
2 25544 51
6385 227
0235 0006404 61
1562 299
0242 15
71662384 15227
Satellite: ISS
Catalog Number: 25544
Epoch time: 08338
80405469 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 227
0235 deg
Eccentricity:
0006404
Arg of perigee: 61
1562 deg
Mean anomaly: 299
0242 deg
Mean motion: 15
71662384 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1522
Checksum: 278
Coasting Arc #13 (Orbit 1537)
---------------------------------------
Vector Time (GMT): 2008/339/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4161081
29 A = 6737851
26 meter
Y = -5104087
34 meter E =
0020295
Z = 1380570
55 I = 51
43960
XDOT = 4578
955769 Wp = 61
96617
YDOT = -2146
650977 meter/sec RA = 221
19115 deg
ZDOT = 5809
343896 TA = 313
24631
MA = 313
41553
Ha = 195
809 n
mi
Hp = 185
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13651841
49 X = -4110403
91
Y = -16745693
38 feet Y = -5150335
72 meter
Z = 4529430
94 Z = 1360478
52
XDOT = 15022
820765 XDOT = 4574
398669
YDOT = -7042
818166 feet/sec YDOT = -2095
472407 meter/sec
ZDOT = 19059
527219 ZDOT = 5831
577408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9533951
54 X = -2905948
43
Y = -19406151
82 feet Y = -5914995
07 meter
Z = 4451045
61 Z = 1356678
70
XDOT = 14704
643724 XDOT = 4481
975407
YDOT = -2790
444089 feet/sec YDOT = -850
527358 meter/sec
ZDOT = 19145
635534 ZDOT = 5835
589711
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 08339
82137117
00020000 00000-0 20000-3 0 9125
2 25544 51
6397 221
8169 0006335 65
4437 294
7385 15
71732800 15387
Satellite: ISS
Catalog Number: 25544
Epoch time: 08339
82137117 = yrday
fracday
Element set: 912
Inclination: 51
6397 deg
RA of node: 221
8169 deg
Eccentricity:
0006335
Arg of perigee: 65
4437 deg
Mean anomaly: 294
7385 deg
Mean motion: 15
71732800 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1538
Checksum: 304
Coasting Arc #14 (Orbit 1552)
---------------------------------------
Vector Time (GMT): 2008/340/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3150983
71 A = 6726727
37 meter
Y = 2862100
95 meter E =
0020689
Z = -5226223
16 I = 51
42578
XDOT = -5798
119510 Wp = 87
91681
YDOT = -4980
051493 meter/sec RA = 216
03975 deg
ZDOT = 771
874992 TA = 189
44775
MA = 189
48673
Ha = 195
846 n
mi
Hp = 184
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10337873
07 X = -3157365
67
Y = 9390094
98 feet Y = 2826829
51 meter
Z = -17146401
43 Z = -5241546
11
XDOT = -19022
701805 XDOT = -5745
750500
YDOT = -16338
751617 feet/sec YDOT = -5044
596664 meter/sec
ZDOT = 2532
398267 ZDOT = 743
834265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11978946
13 X = -3651182
78
Y = 7036727
38 feet Y = 2144794
51 meter
Z = -17205635
79 Z = -5244277
79
XDOT = -14678
855774 XDOT = -4474
115240
YDOT = -19090
523788 feet/sec YDOT = -5818
791650 meter/sec
ZDOT = 2423
164229 ZDOT = 738
580457
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 08340
77509589
00020000 00000-0 20000-3 0 9138
2 25544 51
6402 216
9365 0006436 68
7349 291
4500 15
71743962 15538
Satellite: ISS
Catalog Number: 25544
Epoch time: 08340
77509589 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 216
9365 deg
Eccentricity:
0006436
Arg of perigee: 68
7349 deg
Mean anomaly: 291
4500 deg
Mean motion: 15
71743962 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1553
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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