Date:
June 15th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 519)
---------------------------------------
Vector Time (GMT): 2009/163/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5933123
18 A = 6733152
48 meter
Y = -3171966
00 meter E =
0018711
Z = 93221
99 I = 51
50310
XDOT = 2174
442163 Wp = 69
18654
YDOT = 4272
682100 meter/sec RA = 331
23871 deg
ZDOT = 6024
822149 TA = 291
82780
MA = 292
02674
Ha = 193
773 n
mi
Hp = 181
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19465627
24 X = 5967698
83
Y = -10406712
60 feet Y = -3105425
04 meter
Z = 305846
41 Z = 122128
44
XDOT = 7133
996597 XDOT = 2097
235342
YDOT = 14017
985893 feet/sec YDOT = 4296
565326 meter/sec
ZDOT = 19766
476868 ZDOT = 6035
198696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13615340
70 X = 4149955
84
Y = -17370975
96 feet Y = -5294673
47 meter
Z = 418981
05 Z = 127705
42
XDOT = 10808
789091 XDOT = 3294
518915
YDOT = 9005
375246 feet/sec YDOT = 2744
838375 meter/sec
ZDOT = 19807
304032 ZDOT = 6037
266269
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 09163
40701161
00010596 00000-0 82463-4 0 9009
2 25544 51
6425 331
4429 0008704 103
9991 256
2141 15
73655091 5202
Satellite: ISS
Catalog Number: 25544
Epoch time: 09163
40701161 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 331
4429 deg
Eccentricity:
0008704
Arg of perigee: 103
9991 deg
Mean anomaly: 256
2141 deg
Mean motion: 15
73655091 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 520
Checksum: 281
Coasting Arc #2 (Orbit 534)
---------------------------------------
Vector Time (GMT): 2009/164/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2321830
96 A = 6721033
11 meter
Y = -3499425
69 meter E =
0023439
Z = -5267473
89 I = 51
43600
XDOT = 6385
791927 Wp = 96
11125
YDOT = -4272
210262 meter/sec RA = 326
09141 deg
ZDOT = 21
084348 TA = 174
10367
MA = 174
07603
Ha = 193
682 n
mi
Hp = 181
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7617555
64 X = -2256938
89
Y = -11481055
43 feet Y = -3525026
18 meter
Z = -17281738
49 Z = -5278596
19
XDOT = 20950
760915 XDOT = 6432
987475
YDOT = -14016
437869 feet/sec YDOT = -4200
536725 meter/sec
ZDOT = 69
174369 ZDOT = 52
220430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11635180
68 X = -3546403
07
Y = -7276761
30 feet Y = -2217956
85 meter
Z = -17325460
70 Z = -5280800
42
XDOT = 12621
635182 XDOT = 3847
074404
YDOT = -20654
598871 feet/sec YDOT = -6295
521736 meter/sec
ZDOT = 190
997530 ZDOT = 58
216047
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 09164
35956748
00010596 00000-0 82463-4 0 9018
2 25544 51
6416 326
5528 0008618 107
0543 253
1565 15
73676312 5350
Satellite: ISS
Catalog Number: 25544
Epoch time: 09164
35956748 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 326
5528 deg
Eccentricity:
0008618
Arg of perigee: 107
0543 deg
Mean anomaly: 253
1565 deg
Mean motion: 15
73676312 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 535
Checksum: 318
Coasting Arc #3 (Orbit 550)
---------------------------------------
Vector Time (GMT): 2009/165/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5196962
29 A = 6733126
56 meter
Y = 4268120
49 meter E =
0020507
Z = 50158
50 I = 51
45282
XDOT = -3091
402006 Wp = 124
59239
YDOT = -3673
035024 meter/sec RA = 320
94519 deg
ZDOT = -6024
302821 TA = 54
86121
MA = 54
66921
Ha = 193
646 n
mi
Hp = 181
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17050401
22 X = -5244546
55
Y = 14003019
97 feet Y = 4209738
95 meter
Z = 164562
00 Z = 24796
67
XDOT = -10142
395033 XDOT = -3020
834825
YDOT = -12050
639841 feet/sec YDOT = -3707
209544 meter/sec
ZDOT = -19764
773034 ZDOT = -6039
149897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9274485
35 X = -2826863
14
Y = 20020176
80 feet Y = 6102149
89 meter
Z = 65368
08 Z = 19924
19
XDOT = -12807
307170 XDOT = -3903
667225
YDOT = -5821
694893 feet/sec YDOT = -1774
452603 meter/sec
ZDOT = -19823
100010 ZDOT = -6042
080883
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 09165
37561027
00010596 00000-0 82463-4 0 9024
2 25544 51
6417 321
3382 0008620 111
3355 248
8729 15
73667152 5517
Satellite: ISS
Catalog Number: 25544
Epoch time: 09165
37561027 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 321
3382 deg
Eccentricity:
0008620
Arg of perigee: 111
3355 deg
Mean anomaly: 248
8729 deg
Mean motion: 15
73667152 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 551
Checksum: 301
Coasting Arc #4 (Orbit 566)
---------------------------------------
Vector Time (GMT): 2009/166/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3054960
65 A = 6720948
91 meter
Y = 2871179
64 meter E =
0010847
Z = 5244407
30 I = 51
38903
XDOT = -5431
535539 Wp = 110
29526
YDOT = 5467
853365 meter/sec RA = 315
79744 deg
ZDOT = 166
466292 TA = 338
09801
MA = 338
14434
Ha = 193
474 n
mi
Hp = 181
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10022836
77 X = 2997151
16
Y = 9419880
70 feet Y = 2905018
13 meter
Z = 17206060
69 Z = 5259108
25
XDOT = -17819
998489 XDOT = -5493
082982
YDOT = 17939
151461 feet/sec YDOT = 5406
770611 meter/sec
ZDOT = 546
149251 ZDOT = 139
931008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13099838
16 X = 3992830
67
Y = 3949171
47 feet Y = 1203707
46 meter
Z = 17263783
44 Z = 5262001
19
XDOT = -7559
313528 XDOT = -2304
078763
YDOT = 23084
047207 feet/sec YDOT = 7036
017589 meter/sec
ZDOT = 442
413503 ZDOT = 134
847636
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 09166
39163413
00010596 00000-0 82463-4 0 9035
2 25544 51
6409 316
1221 0008539 114
6579 245
5474 15
73699064 5670
Satellite: ISS
Catalog Number: 25544
Epoch time: 09166
39163413 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 316
1221 deg
Eccentricity:
0008539
Arg of perigee: 114
6579 deg
Mean anomaly: 245
5474 deg
Mean motion: 15
73699064 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 567
Checksum: 325
Coasting Arc #5 (Orbit 581)
---------------------------------------
Vector Time (GMT): 2009/167/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4242392
44 A = 6732911
52 meter
Y = -5219796
27 meter E =
0016267
Z = -226494
42 I = 51
40794
XDOT = 3848
096597 Wp = 73
23839
YDOT = 2882
348918 meter/sec RA = 310
64239 deg
ZDOT = 6011
148688 TA = 284
29388
MA = 284
47446
Ha = 193
453 n
mi
Hp = 181
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13918610
37 X = 4301546
06
Y = -17125315
84 feet Y = -5172024
59 meter
Z = -743091
91 Z = -205741
69
XDOT = 12624
988835 XDOT = 3786
378445
YDOT = 9456
525320 feet/sec YDOT = 2925
034777 meter/sec
ZDOT = 19721
616431 ZDOT = 6029
693283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4358650
06 X = 1328516
54
Y = -21636086
98 feet Y = -6594679
31 meter
Z = -662006
75 Z = -201779
66
XDOT = 13895
693238 XDOT = 4235
407299
YDOT = 2234
280795 feet/sec YDOT = 681
008786 meter/sec
ZDOT = 19794
400299 ZDOT = 6033
333211
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 09167
34413977
00010596 00000-0 82463-4 0 9045
2 25544 51
6397 311
2316 0008424 118
0986 242
1029 15
73733401 5820
Satellite: ISS
Catalog Number: 25544
Epoch time: 09167
34413977 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 311
2316 deg
Eccentricity:
0008424
Arg of perigee: 118
0986 deg
Mean anomaly: 242
1029 deg
Mean motion: 15
73733401 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 582
Checksum: 305
Coasting Arc #6 (Orbit 597)
---------------------------------------
Vector Time (GMT): 2009/168/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3615480
12 A = 6720789
63 meter
Y = -2166873
97 meter E =
0022553
Z = -5253665
31 I = 51
34795
XDOT = 4259
693990 Wp = 99
75797
YDOT = -6388
450971 meter/sec RA = 305
49355 deg
ZDOT = -301
391116 TA = 167
39152
MA = 167
33502
Ha = 193
371 n
mi
Hp = 181
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11861811
41 X = -3565459
45
Y = -7109166
56 feet Y = -2207024
03 meter
Z = -17236434
73 Z = -5271108
26
XDOT = 13975
373984 XDOT = 4332
278258
YDOT = -20959
484814 feet/sec YDOT = -6340
410705 meter/sec
ZDOT = -988
815997 ZDOT = -280
521827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13730809
84 X = -4185150
84
Y = -586328
50 feet Y = -178712
93 meter
Z = -17304871
61 Z = -5274524
87
XDOT = 2152
483171 XDOT = 656
076871
YDOT = -24097
468997 feet/sec YDOT = -7344
908550 meter/sec
ZDOT = -907
327428 ZDOT = -276
553400
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 09168
36012928
00010596 00000-0 82463-4 0 9050
2 25544 51
6387 306
0146 0008488 121
9130 238
2860 15
73769897 5980
Satellite: ISS
Catalog Number: 25544
Epoch time: 09168
36012928 = yrday
fracday
Element set: 905
Inclination: 51
6387 deg
RA of node: 306
0146 deg
Eccentricity:
0008488
Arg of perigee: 121
9130 deg
Mean anomaly: 238
2860 deg
Mean motion: 15
73769897 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 598
Checksum: 340
Coasting Arc #7 (Orbit 613)
---------------------------------------
Vector Time (GMT): 2009/169/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3184308
98 A = 6732621
32 meter
Y = 5913664
19 meter E =
0021023
Z = 298251
79 I = 51
37274
XDOT = -4371
480118 Wp = 128
87961
YDOT = -2037
181275 meter/sec RA = 300
33444 deg
ZDOT = -6009
322142 TA = 47
86507
MA = 47
68661
Ha = 193
151 n
mi
Hp = 181
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10447207
96 X = -3251648
79
Y = 19401785
40 feet Y = 5877678
83 meter
Z = 978516
38 Z = 282619
51
XDOT = -14342
126373 XDOT = -4319
182546
YDOT = -6683
665602 feet/sec YDOT = -2085
772442 meter/sec
ZDOT = -19715
623826 ZDOT = -6030
432326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 530152
37 X = 161590
44
Y = 22031976
98 feet Y = 6715346
58 meter
Z = 917526
01 Z = 279661
93
XDOT = -14063
634899 XDOT = -4286
595917
YDOT = 1202
320991 feet/sec YDOT = 366
467438 meter/sec
ZDOT = -19798
424019 ZDOT = -6034
559641
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 09169
37609970
00010596 00000-0 82463-4 0 9062
2 25544 51
6393 300
7987 0008287 124
7213 235
4731 15
73833622 6144
Satellite: ISS
Catalog Number: 25544
Epoch time: 09169
37609970 = yrday
fracday
Element set: 906
Inclination: 51
6393 deg
RA of node: 300
7987 deg
Eccentricity:
0008287
Arg of perigee: 124
7213 deg
Mean anomaly: 235
4731 deg
Mean motion: 15
73833622 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 614
Checksum: 326
Coasting Arc #8 (Orbit 629)
---------------------------------------
Vector Time (GMT): 2009/170/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3984778
13 A = 6720767
24 meter
Y = 1365352
90 meter E =
0010968
Z = 5229499
60 I = 51
31751
XDOT = -2976
649888 Wp = 123
77063
YDOT = 7098
221812 meter/sec RA = 295
18477 deg
ZDOT = 408
266123 TA = 322
30032
MA = 322
37713
Ha = 193
167 n
mi
Hp = 181
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13073419
05 X = 3943810
05
Y = 4479504
26 feet Y = 1409683
06 meter
Z = 17157150
92 Z = 5248758
64
XDOT = -9765
911706 XDOT = -3057
785485
YDOT = 23288
129303 feet/sec YDOT = 7064
481451 meter/sec
ZDOT = 1339
455783 ZDOT = 393
609477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13443601
06 X = 4097609
60
Y = -2766354
53 feet Y = -843184
86 meter
Z = 17232670
86 Z = 5252518
08
XDOT = 3274
307331 XDOT = 998
008874
YDOT = 24035
211197 feet/sec YDOT = 7325
932373 meter/sec
ZDOT = 1282
337334 ZDOT = 390
856419
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 09170
39205569
00010596 00000-0 82463-4 0 9073
2 25544 51
6384 295
5817 0008501 128
9964 231
1958 15
73779476 6303
Satellite: ISS
Catalog Number: 25544
Epoch time: 09170
39205569 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 295
5817 deg
Eccentricity:
0008501
Arg of perigee: 128
9964 deg
Mean anomaly: 231
1958 deg
Mean motion: 15
73779476 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 630
Checksum: 346
Coasting Arc #9 (Orbit 644)
---------------------------------------
Vector Time (GMT): 2009/171/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1998572
51 A = 6732526
86 meter
Y = -6415518
84 meter E =
0014110
Z = -398300
64 I = 51
34635
XDOT = 4699
830618 Wp = 78
95439
YDOT = 1103
326772 meter/sec RA = 290
02029 deg
ZDOT = 5993
262650 TA = 276
70022
MA = 276
86078
Ha = 193
123 n
mi
Hp = 181
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6556996
43 X = 2072098
29
Y = -21048290
15 feet Y = -6392758
45 meter
Z = -1306760
63 Z = -388414
13
XDOT = 15419
391791 XDOT = 4658
029184
YDOT = 3619
838492 feet/sec YDOT = 1155
648110 meter/sec
ZDOT = 19662
935205 ZDOT = 6015
993398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5461449
50 X = -1664649
81
Y = -21361093
81 feet Y = -6510861
39 meter
Z = -1268299
81 Z = -386577
78
XDOT = 13369
467312 XDOT = 4075
013637
YDOT = -4554
398320 feet/sec YDOT = -1388
180608 meter/sec
ZDOT = 19752
051129 ZDOT = 6020
425184
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 09171
34449474
00010596 00000-0 82463-4 0 9085
2 25544 51
6385 290
6908 0008497 133
2143 226
9731 15
73851189 6452
Satellite: ISS
Catalog Number: 25544
Epoch time: 09171
34449474 = yrday
fracday
Element set: 908
Inclination: 51
6385 deg
RA of node: 290
6908 deg
Eccentricity:
0008497
Arg of perigee: 133
2143 deg
Mean anomaly: 226
9731 deg
Mean motion: 15
73851189 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 645
Checksum: 337
Coasting Arc #10 (Orbit 660)
---------------------------------------
Vector Time (GMT): 2009/172/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4188558
97 A = 6720509
62 meter
Y = -586360
99 meter E =
0021527
Z = -5240419
83 I = 51
29743
XDOT = 1613
033631 Wp = 104
13009
YDOT = -7500
593395 meter/sec RA = 284
87092 deg
ZDOT = -456
753399 TA = 161
54162
MA = 161
46340
Ha = 193
046 n
mi
Hp = 181
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13741991
36 X = -4156233
66
Y = -1923756
54 feet Y = -633017
99 meter
Z = -17192978
45 Z = -5260689
63
XDOT = 5292
105087 XDOT = 1699
005496
YDOT = -24608
246048 feet/sec YDOT = -7482
074715 meter/sec
ZDOT = -1498
534775 ZDOT = -448
710067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12524433
29 X = -3817447
27
Y = 5739617
90 feet Y = 1749435
54 meter
Z = -17272435
58 Z = -5264638
37
XDOT = -8394
171860 XDOT = -2558
543583
YDOT = -22666
372750 feet/sec YDOT = -6908
710414 meter/sec
ZDOT = -1467
341486 ZDOT = -447
245685
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 09172
36041446
00010596 00000-0 82463-4 0 9096
2 25544 51
6388 285
4745 0008587 136
2595 223
9249 15
73881694 6613
Satellite: ISS
Catalog Number: 25544
Epoch time: 09172
36041446 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 285
4745 deg
Eccentricity:
0008587
Arg of perigee: 136
2595 deg
Mean anomaly: 223
9249 deg
Mean motion: 15
73881694 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 661
Checksum: 349
Coasting Arc #11 (Orbit 676)
---------------------------------------
Vector Time (GMT): 2009/173/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -813519
63 A = 6732281
68 meter
Y = 6660109
26 meter E =
0021181
Z = 400860
87 I = 51
33102
XDOT = -4833
170261 Wp = 134
20709
YDOT = -218
408694 meter/sec RA = 279
70449 deg
ZDOT = -5999
063337 TA = 41
41219
MA = 41
25183
Ha = 192
775 n
mi
Hp = 181
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2669027
66 X = -889880
95
Y = 21850752
16 feet Y = 6650584
95 meter
Z = 1315160
34 Z = 396724
88
XDOT = -15856
857813 XDOT = -4801
226377
YDOT = -716
563956 feet/sec YDOT = -272
276002 meter/sec
ZDOT = -19681
966329 ZDOT = -6022
465368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9874447
04 X = 3009731
46
Y = 19675263
30 feet Y = 5997020
25 meter
Z = 1299244
16 Z = 396009
62
XDOT = -12069
222942 XDOT = -3678
699153
YDOT = 7402
581734 feet/sec YDOT = 2256
306913 meter/sec
ZDOT = -19773
691243 ZDOT = -6027
021091
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 09173
37631476
00010596 00000-0 82463-4 0 9108
2 25544 51
6386 280
2574 0008272 139
7963 220
3813 15
73941484 6771
Satellite: ISS
Catalog Number: 25544
Epoch time: 09173
37631476 = yrday
fracday
Element set: 910
Inclination: 51
6386 deg
RA of node: 280
2574 deg
Eccentricity:
0008272
Arg of perigee: 139
7963 deg
Mean anomaly: 220
3813 deg
Mean motion: 15
73941484 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 677
Checksum: 329
Coasting Arc #12 (Orbit 692)
---------------------------------------
Vector Time (GMT): 2009/174/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4216424
76 A = 6720454
13 meter
Y = -212362
20 meter E =
0010878
Z = 5222844
76 I = 51
28689
XDOT = -222
966423 Wp = 135
43934
YDOT = 7688
313150 meter/sec RA = 274
55427 deg
ZDOT = 484
345537 TA = 309
89309
MA = 309
98868
Ha = 192
767 n
mi
Hp = 181
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13833414
55 X = 4193114
59
Y = -696726
39 feet Y = -165343
22 meter
Z = 17135317
46 Z = 5243271
36
XDOT = -731
517136 XDOT = -311
274721
YDOT = 25224
124508 feet/sec YDOT = 7685
325940 meter/sec
ZDOT = 1589
060162 ZDOT = 483
049652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10906305
86 X = 3324242
03
Y = -8375642
18 feet Y = -2552895
74 meter
Z = 17215371
06 Z = 5247245
10
XDOT = 13110
301798 XDOT = 3996
019988
YDOT = 20383
439313 feet/sec YDOT = 6212
872303 meter/sec
ZDOT = 1584
327749 ZDOT = 482
903098
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 09174
39220186
00010596 00000-0 82463-4 0 9114
2 25544 51
6385 275
0410 0008479 143
2108 216
9638 15
73899368 6938
Satellite: ISS
Catalog Number: 25544
Epoch time: 09174
39220186 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 275
0410 deg
Eccentricity:
0008479
Arg of perigee: 143
2108 deg
Mean anomaly: 216
9638 deg
Mean motion: 15
73899368 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 693
Checksum: 332
Coasting Arc #13 (Orbit 707)
---------------------------------------
Vector Time (GMT): 2009/175/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -413471
36 A = 6732193
35 meter
Y = -6705714
89 meter E =
0012233
Z = -426970
49 I = 51
32691
XDOT = 4786
081271 Wp = 84
09126
YDOT = -666
952398 meter/sec RA = 269
38728 deg
ZDOT = 5988
328197 TA = 271
24904
MA = 271
38919
Ha = 192
741 n
mi
Hp = 181
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1356533
33 X = -336382
07
Y = -22000376
94 feet Y = -6709907
45 meter
Z = -1400821
83 Z = -428793
28
XDOT = 15702
366375 XDOT = 4764
093681
YDOT = -2188
164035 feet/sec YDOT = -613
555840 meter/sec
ZDOT = 19646
746052 ZDOT = 6011
525152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13904992
39 X = -4238241
68
Y = -17102251
41 feet Y = -5212766
23 meter
Z = -1408280
21 Z = -429243
81
XDOT = 10152
855863 XDOT = 3094
590467
YDOT = -9840
200308 feet/sec YDOT = -2999
293054 meter/sec
ZDOT = 19737
646156 ZDOT = 6016
034548
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 09175
34457688
00010596 00000-0 82463-4 0 9120
2 25544 51
6394 270
1509 0008551 147
2900 212
8794 15
73962698 7080
Satellite: ISS
Catalog Number: 25544
Epoch time: 09175
34457688 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 270
1509 deg
Eccentricity:
0008551
Arg of perigee: 147
2900 deg
Mean anomaly: 212
8794 deg
Mean motion: 15
73962698 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 708
Checksum: 340
Coasting Arc #14 (Orbit 723)
---------------------------------------
Vector Time (GMT): 2009/176/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4127384
53 A = 6720177
71 meter
Y = 920361
69 meter E =
0020165
Z = -5238915
55 I = 51
28818
XDOT = -1129
587093 Wp = 108
67773
YDOT = -7590
424440 meter/sec RA = 264
23729 deg
ZDOT = -451
326544 TA = 157
05231
MA = 156
96209
Ha = 192
576 n
mi
Hp = 181
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13541287
84 X = -4111920
10
Y = 3019559
34 feet Y = 874294
28 meter
Z = -17188043
13 Z = -5258928
36
XDOT = -3705
994401 XDOT = -1042
433296
YDOT = -24902
967323 feet/sec YDOT = -7602
568759 meter/sec
ZDOT = -1480
730131 ZDOT = -456
603677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8992292
66 X = -2740850
80
Y = 10436534
31 feet Y = 3181055
66 meter
Z = -17266454
94 Z = -5262815
47
XDOT = -17052
311587 XDOT = -5197
544572
YDOT = -17135
104518 feet/sec YDOT = -5222
779857 meter/sec
ZDOT = -1501
786710 ZDOT = -457
744589
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 09176
36042823
00010596 00000-0 82463-4 0 9135
2 25544 51
6393 264
9351 0008474 150
4339 209
7305 15
73998533 7249
Satellite: ISS
Catalog Number: 25544
Epoch time: 09176
36042823 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 264
9351 deg
Eccentricity:
0008474
Arg of perigee: 150
4339 deg
Mean anomaly: 209
7305 deg
Mean motion: 15
73998533 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 724
Checksum: 324
Coasting Arc #15 (Orbit 739)
---------------------------------------
Vector Time (GMT): 2009/177/08:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1557653
77 A = 6732082
37 meter
Y = 6527497
51 meter E =
0020846
Z = 364448
38 I = 51
33183
XDOT = -4613
436316 Wp = 140
39895
YDOT = 1445
686668 meter/sec RA = 259
06936 deg
ZDOT = -6003
040329 TA = 35
61843
MA = 35
47949
Ha = 192
410 n
mi
Hp = 181
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5110412
63 X = 1482776
02
Y = 21415674
24 feet Y = 6544497
39 meter
Z = 1195696
77 Z = 371834
47
XDOT = -15135
945920 XDOT = -4600
098081
YDOT = 4743
066495 feet/sec YDOT = 1394
172017 meter/sec
ZDOT = -19695
014202 ZDOT = -6025
419472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17104447
68 X = 5213435
65
Y = 13860533
75 feet Y = 4224690
69 meter
Z = 1224983
63 Z = 373375
01
XDOT = -8001
957044 XDOT = -2438
996507
YDOT = 11671
865671 feet/sec YDOT = 3557
584656 meter/sec
ZDOT = -19782
680404 ZDOT = -6029
760987
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 09177
37626246
00010596 00000-0 82463-4 0 9145
2 25544 51
6385 259
7169 0008343 154
8608 205
2963 15
74014427 7402
Satellite: ISS
Catalog Number: 25544
Epoch time: 09177
37626246 = yrday
fracday
Element set: 914
Inclination: 51
6385 deg
RA of node: 259
7169 deg
Eccentricity:
0008343
Arg of perigee: 154
8608 deg
Mean anomaly: 205
2963 deg
Mean motion: 15
74014427 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 740
Checksum: 327
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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