Date:
September 18th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4843 76 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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
There are no maneuvers
Coasting Arc #1 (Orbit 2533)
---------------------------------------
Vector Time (GMT): 2007/260/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6623859
74 A = 6723709
29 meter
Y = 829310
51 meter E =
0009149
Z = -816766
81 I = 51
58372
XDOT = 118
044072 Wp = 83
36258
YDOT = -4871
160082 meter/sec RA = 347
29543 deg
ZDOT = -5959
171428 TA = 105
55428
MA = 105
45326
Ha = 188
205 n
mi
Hp = 177
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21731823
29 X = -6628673
16
Y = 2720835
00 feet Y = 755211
84 meter
Z = -2679681
14 Z = -848957
62
XDOT = 387
283700 XDOT = 201
454270
YDOT = -15981
496332 feet/sec YDOT = -4869
373779 meter/sec
ZDOT = -19551
087361 ZDOT = -5958
395273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21359482
20 X = 6510370
17
Y = 4772673
59 feet Y = 1454710
91 meter
Z = -2801764
51 Z = -853977
82
XDOT = -5516
873750 XDOT = -1681
543119
YDOT = 13317
060486 feet/sec YDOT = 4059
040036 meter/sec
ZDOT = -19548
705122 ZDOT = -5958
445321
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 07260
48842507
00020000 00000-0 20000-3 0 9002
2 25544 51
6363 347
6225 0009361 16
5605 343
5864 15
76865938 25342
Satellite: ISS
Catalog Number: 25544
Epoch time: 07260
48842507 = yrday
fracday
Element set: 900
Inclination: 51
6363 deg
RA of node: 347
6225 deg
Eccentricity:
0009361
Arg of perigee: 16
5605 deg
Mean anomaly: 343
5864 deg
Mean motion: 15
76865938 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2534
Checksum: 306
Coasting Arc #2 (Orbit 2549)
---------------------------------------
Vector Time (GMT): 2007/261/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -929078
10 A = 6713222
34 meter
Y = 4434635
63 meter E =
0014884
Z = 4950296
02 I = 51
52104
XDOT = -7407
089095 Wp = 33
60598
YDOT = 710
976506 meter/sec RA = 342
10664 deg
ZDOT = -2012
004786 TA = 75
95344
MA = 75
78802
Ha = 188
323 n
mi
Hp = 177
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3048156
49 X = -1002645
70
Y = 14549329
50 feet Y = 4423834
83 meter
Z = 16241128
69 Z = 4945603
81
XDOT = -24301
473409 XDOT = -7404
714769
YDOT = 2332
600085 feet/sec YDOT = 628
159521 meter/sec
ZDOT = -6601
065571 ZDOT = -2047
983038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7649782
19 X = 2331653
61
Y = -12767797
29 feet Y = -3891624
61 meter
Z = 16223831
01 Z = 4945023
69
XDOT = 22794
930369 XDOT = 6947
894776
YDOT = 5033
275202 feet/sec YDOT = 1534
142282 meter/sec
ZDOT = -6737
539931 ZDOT = -2053
602171
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 07261
50240436
00020000 00000-0 20000-3 0 9010
2 25544 51
6367 342
3923 0009547 20
2514 339
9028 15
76910431 25508
Satellite: ISS
Catalog Number: 25544
Epoch time: 07261
50240436 = yrday
fracday
Element set: 901
Inclination: 51
6367 deg
RA of node: 342
3923 deg
Eccentricity:
0009547
Arg of perigee: 20
2514 deg
Mean anomaly: 339
9028 deg
Mean motion: 15
76910431 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2550
Checksum: 270
Coasting Arc #3 (Orbit 2565)
---------------------------------------
Vector Time (GMT): 2007/262/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6162318
03 A = 6720776
29 meter
Y = -348990
22 meter E =
0020802
Z = 2627554
74 I = 51
51960
XDOT = -1934
094223 Wp = 56
01368
YDOT = 5335
858436 meter/sec RA = 336
98005 deg
ZDOT = 5226
750648 TA = 334
01018
MA = 334
11449
Ha = 188
271 n
mi
Hp = 177
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20217578
84 X = 6152998
21
Y = -1144981
03 feet Y = -280131
82 meter
Z = 8620586
43 Z = 2657468
87
XDOT = -6345
453488 XDOT = -2019
007648
YDOT = 17506
097230 feet/sec YDOT = 5313
755495 meter/sec
ZDOT = 17148
132048 ZDOT = 5217
148522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19556373
85 X = -5960782
75
Y = -5063587
45 feet Y = -1543381
45 meter
Z = 8734088
96 Z = 2662150
31
XDOT = 11106
835990 XDOT = 3385
363610
YDOT = -13279
551650 feet/sec YDOT = -4047
607343 meter/sec
ZDOT = 17112
301638 ZDOT = 5215
829539
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 07262
51636688
00020000 00000-0 20000-3 0 9021
2 25544 51
6366 337
1624 0009536 24
4077 335
7537 15
76925971 25666
Satellite: ISS
Catalog Number: 25544
Epoch time: 07262
51636688 = yrday
fracday
Element set: 902
Inclination: 51
6366 deg
RA of node: 337
1624 deg
Eccentricity:
0009536
Arg of perigee: 24
4077 deg
Mean anomaly: 335
7537 deg
Mean motion: 15
76925971 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2566
Checksum: 319
Coasting Arc #4 (Orbit 2580)
---------------------------------------
Vector Time (GMT): 2007/263/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2363794
40 A = 6716890
41 meter
Y = -4868314
74 meter E =
0012811
Z = -3983308
70 I = 51
48019
XDOT = 6617
301628 Wp = 60
07513
YDOT = 4
127225 meter/sec RA = 331
76428 deg
ZDOT = 3937
536547 TA = 250
66761
MA = 250
80617
Ha = 188
410 n
mi
Hp = 177
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7755230
97 X = 2437407
21
Y = -15972161
20 feet Y = -4841469
83 meter
Z = -13068598
11 Z = -3971646
57
XDOT = 21710
307178 XDOT = 6597
635744
YDOT = 13
540764 feet/sec YDOT = 78
015647 meter/sec
ZDOT = 12918
426990 ZDOT = 3969
635761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12106362
28 X = -3690019
22
Y = 13031880
06 feet Y = 3972117
04 meter
Z = -13024895
09 Z = -3969988
02
XDOT = -19761
834502 XDOT = -6023
407156
YDOT = -5376
765645 feet/sec YDOT = -1638
838169 meter/sec
ZDOT = 13040
267946 ZDOT = 3974
673670
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 07263
46694151
00020000 00000-0 20000-3 0 9036
2 25544 51
6363 332
2601 0009581 27
7803 332
3871 15
76958461 25818
Satellite: ISS
Catalog Number: 25544
Epoch time: 07263
46694151 = yrday
fracday
Element set: 903
Inclination: 51
6363 deg
RA of node: 332
2601 deg
Eccentricity:
0009581
Arg of perigee: 27
7803 deg
Mean anomaly: 332
3871 deg
Mean motion: 15
76958461 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2581
Checksum: 296
Coasting Arc #5 (Orbit 2596)
---------------------------------------
Vector Time (GMT): 2007/264/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5285992
24 A = 6716241
85 meter
Y = -465105
15 meter E =
0016622
Z = -4135176
70 I = 51
45259
XDOT = 3420
272333 Wp = 48
44278
YDOT = -5798
722159 meter/sec RA = 326
64506 deg
ZDOT = -3718
695069 TA = 183
36494
MA = 183
37613
Ha = 188
491 n
mi
Hp = 176
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17342494
24 X = -5260310
55
Y = -1525935
52 feet Y = -524072
51 meter
Z = -13566852
70 Z = -4160793
69
XDOT = 11221
365921 XDOT = 3502
925068
YDOT = -19024
678998 feet/sec YDOT = -5760
012614 meter/sec
ZDOT = -12200
443141 ZDOT = -3701
878600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16198740
29 X = 4937376
04
Y = 6167820
73 feet Y = 1879951
76 meter
Z = -13664145
72 Z = -4164831
62
XDOT = -15592
023909 XDOT = -4752
448887
YDOT = 14052
140492 feet/sec YDOT = 4283
092422 meter/sec
ZDOT = -12137
285445 ZDOT = -3699
444604
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 07264
48087105
00020000 00000-0 20000-3 0 9045
2 25544 51
6356 327
0296 0009620 31
4280 328
7458 15
76953396 25976
Satellite: ISS
Catalog Number: 25544
Epoch time: 07264
48087105 = yrday
fracday
Element set: 904
Inclination: 51
6356 deg
RA of node: 327
0296 deg
Eccentricity:
0009620
Arg of perigee: 31
4280 deg
Mean anomaly: 328
7458 deg
Mean motion: 15
76953396 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2597
Checksum: 313
Coasting Arc #6 (Orbit 2612)
---------------------------------------
Vector Time (GMT): 2007/265/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3493416
72 A = 6721188
61 meter
Y = 5218493
86 meter E =
0019488
Z = 2386111
35 I = 51
44627
XDOT = -5410
897105 Wp = 77
42474
YDOT = -1151
414159 meter/sec RA = 321
42648 deg
ZDOT = -5362
797954 TA = 75
56246
MA = 75
34627
Ha = 188
570 n
mi
Hp = 176
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11461340
94 X = -3563102
33
Y = 17121042
85 feet Y = 5179038
92 meter
Z = 7828449
32 Z = 2368971
00
XDOT = -17752
287090 XDOT = -5371
568220
YDOT = -3777
605508 feet/sec YDOT = -1211
702079 meter/sec
ZDOT = -17594
481477 ZDOT = -5388
988484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15499066
63 X = 4724115
51
Y = -13611624
53 feet Y = -4148823
16 meter
Z = 7763998
64 Z = 2366466
78
XDOT = 15108
631417 XDOT = 4605
110856
YDOT = 7033
859536 feet/sec YDOT = 2143
920387 meter/sec
ZDOT = -17694
035492 ZDOT = -5393
142018
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 07265
49478266
00020000 00000-0 20000-3 0 9050
2 25544 51
6357 321
7991 0009847 35
0771 325
1041 15
77010100 26132
Satellite: ISS
Catalog Number: 25544
Epoch time: 07265
49478266 = yrday
fracday
Element set: 905
Inclination: 51
6357 deg
RA of node: 321
7991 deg
Eccentricity:
0009847
Arg of perigee: 35
0771 deg
Mean anomaly: 325
1041 deg
Mean motion: 15
77010100 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2613
Checksum: 284
Coasting Arc #7 (Orbit 2628)
---------------------------------------
Vector Time (GMT): 2007/266/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4120645
46 A = 6712332
24 meter
Y = 1621688
47 meter E =
0011199
Z = 5034500
66 I = 51
39489
XDOT = -4435
379844 Wp = 64
90449
YDOT = 6086
750190 meter/sec RA = 316
28720 deg
ZDOT = 1671
442077 TA = 9
00949
MA = 8
98941
Ha = 188
428 n
mi
Hp = 176
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13519178
02 X = 4077748
62
Y = 5320500
23 feet Y = 1667528
24 meter
Z = 16517390
63 Z = 5054414
43
XDOT = -14551
771142 XDOT = -4511
232688
YDOT = 19969
652855 feet/sec YDOT = 6036
727227 meter/sec
ZDOT = 5483
733848 ZDOT = 1649
710544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11766050
12 X = -3586292
08
Y = -8374164
81 feet Y = -2552445
43 meter
Z = 16593176
86 Z = 5057600
31
XDOT = 18320
673734 XDOT = 5584
141354
YDOT = -15049
112586 feet/sec YDOT = -4586
969516 meter/sec
ZDOT = 5401
964274 ZDOT = 1646
518711
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 07266
50867626
00020000 00000-0 20000-3 0 9066
2 25544 51
6356 316
5684 0009754 38
6430 321
5431 15
77040688 26294
Satellite: ISS
Catalog Number: 25544
Epoch time: 07266
50867626 = yrday
fracday
Element set: 906
Inclination: 51
6356 deg
RA of node: 316
5684 deg
Eccentricity:
0009754
Arg of perigee: 38
6430 deg
Mean anomaly: 321
5431 deg
Mean motion: 15
77040688 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2629
Checksum: 312
Coasting Arc #8 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2007/267/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4114280
15 A = 6723578
22 meter
Y = -5284641
63 meter E =
0021403
Z = -467261
50 I = 51
41148
XDOT = 4054
211443 Wp = 41
34678
YDOT = 2640
642678 meter/sec RA = 311
09344 deg
ZDOT = 6004
144596 TA = 313
54477
MA = 313
72234
Ha = 188
764 n
mi
Hp = 176
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13498294
45 X = 4175337
89
Y = -17338063
10 feet Y = -5238292
07 meter
Z = -1533010
19 Z = -447125
67
XDOT = 13301
218646 XDOT = 3995
215055
YDOT = 8663
525845 feet/sec YDOT = 2685
649735 meter/sec
ZDOT = 19698
637125 ZDOT = 6023
696429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17021412
81 X = -5188126
62
Y = 13903616
44 feet Y = 4237822
29 meter
Z = -1457210
15 Z = -444157
65
XDOT = -9921
758690 XDOT = -3024
152049
YDOT = -10136
347198 feet/sec YDOT = -3089
558626 meter/sec
ZDOT = 19773
174215 ZDOT = 6026
863501
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 07267
45918716
00020000 00000-0 20000-3 0 9079
2 25544 51
6347 311
6650 0010083 41
6576 318
5355 15
76996498 26441
Satellite: ISS
Catalog Number: 25544
Epoch time: 07267
45918716 = yrday
fracday
Element set: 907
Inclination: 51
6347 deg
RA of node: 311
6650 deg
Eccentricity:
0010083
Arg of perigee: 41
6576 deg
Mean anomaly: 318
5355 deg
Mean motion: 15
76996498 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2644
Checksum: 322
Coasting Arc #9 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2007/268/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2950965
29 A = 6711587
17 meter
Y = -3043648
94 meter E =
0022637
Z = -5221512
72 I = 51
35297
XDOT = 4911
180927 Wp = 75
46345
YDOT = -5880
768368 meter/sec RA = 305
91436 deg
ZDOT = 660
333635 TA = 200
80246
MA = 200
89473
Ha = 188
706 n
mi
Hp = 176
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9681644
64 X = -2891346
19
Y = -9985724
85 feet Y = -3076315
45 meter
Z = -17130947
23 Z = -5235703
44
XDOT = 16112
798317 XDOT = 4973
367758
YDOT = -19293
859476 feet/sec YDOT = -5825
500998 meter/sec
ZDOT = 2166
448933 ZDOT = 684
343825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7329929
68 X = 2234162
57
Y = 11741373
50 feet Y = 3578770
64 meter
Z = -17185184
78 Z = -5238044
32
XDOT = -18863
604101 XDOT = -5749
626530
YDOT = 15041
270486 feet/sec YDOT = 4584
579244 meter/sec
ZDOT = 2256
875409 ZDOT = 687
895625
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 07268
47304755
00020000 00000-0 20000-3 0 9085
2 25544 51
6342 306
4337 0009992 45
9054 314
2931 15
77048844 26600
Satellite: ISS
Catalog Number: 25544
Epoch time: 07268
47304755 = yrday
fracday
Element set: 908
Inclination: 51
6342 deg
RA of node: 306
4337 deg
Eccentricity:
0009992
Arg of perigee: 45
9054 deg
Mean anomaly: 314
2931 deg
Mean motion: 15
77048844 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2660
Checksum: 307
Coasting Arc #10 (Orbit 2675)
---------------------------------------
Vector Time (GMT): 2007/269/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4381606
89 A = 6722144
16 meter
Y = 4839119
14 meter E =
0012634
Z = -1615313
60 I = 51
37370
XDOT = -2724
851589 Wp = 88
63206
YDOT = -4365
246812 meter/sec RA = 300
75600 deg
ZDOT = -5724
262991 TA = 109
27412
MA = 109
13741
Ha = 188
743 n
mi
Hp = 175
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14375350
70 X = -4427546
02
Y = 15876375
14 feet Y = 4789864
51 meter
Z = -5299585
29 Z = -1636711
72
XDOT = -8939
801801 XDOT = -2648
028532
YDOT = -14321
675892 feet/sec YDOT = -4395
288696 meter/sec
ZDOT = -18780
390390 ZDOT = -5737
313385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17081128
28 X = 5206327
90
Y = -12887355
16 feet Y = -3928065
85 meter
Z = -5380216
82 Z = -1639890
09
XDOT = 5036
001811 XDOT = 1534
973352
YDOT = 14484
569779 feet/sec YDOT = 4414
896869 meter/sec
ZDOT = -18830
462273 ZDOT = -5739
524901
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 07269
48688947
00020000 00000-0 20000-3 0 9096
2 25544 51
6345 301
2021 0010198 50
2316 309
9746 15
77116051 26764
Satellite: ISS
Catalog Number: 25544
Epoch time: 07269
48688947 = yrday
fracday
Element set: 909
Inclination: 51
6345 deg
RA of node: 301
2021 deg
Eccentricity:
0010198
Arg of perigee: 50
2316 deg
Mean anomaly: 309
9746 deg
Mean motion: 15
77116051 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2676
Checksum: 302
Coasting Arc #11 (Orbit 2691)
---------------------------------------
Vector Time (GMT): 2007/270/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1873543
37 A = 6714047
12 meter
Y = 4546934
58 meter E =
0018497
Z = 4562072
40 I = 51
33212
XDOT = -5028
105968 Wp = 58
45833
YDOT = 5049
273724 meter/sec RA = 295
53778 deg
ZDOT = -2949
264357 TA = 60
96153
MA = 60
77634
Ha = 188
669 n
mi
Hp = 175
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6146795
85 X = 1800397
54
Y = 14917764
37 feet Y = 4567477
05 meter
Z = 14967429
14 Z = 4570996
12
XDOT = -16496
410656 XDOT = -5069
866776
YDOT = 16565
858675 feet/sec YDOT = 4992
812824 meter/sec
ZDOT = -9676
064164 ZDOT = -2973
793200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3412752
39 X = -1040206
93
Y = -15736710
39 feet Y = -4796549
33 meter
Z = 15001859
73 Z = 4572566
85
XDOT = 17893
024475 XDOT = 5453
793860
YDOT = -13249
946839 feet/sec YDOT = -4038
583796 meter/sec
ZDOT = -9768
549598 ZDOT = -2977
453917
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 07270
50071192
00020000 00000-0 20000-3 0 9101
2 25544 51
6336 295
9707 0010154 53
5117 306
6982 15
77162852 26925
Satellite: ISS
Catalog Number: 25544
Epoch time: 07270
50071192 = yrday
fracday
Element set: 910
Inclination: 51
6336 deg
RA of node: 295
9707 deg
Eccentricity:
0010154
Arg of perigee: 53
5117 deg
Mean anomaly: 306
6982 deg
Mean motion: 15
77162852 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2692
Checksum: 288
Coasting Arc #12 (Orbit 2707)
---------------------------------------
Vector Time (GMT): 2007/271/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4334028
85 A = 6718063
15 meter
Y = -3809700
16 meter E =
0021896
Z = 3416622
37 I = 51
33396
XDOT = 1662
406113 Wp = 75
96043
YDOT = 5998
478907 meter/sec RA = 290
40389 deg
ZDOT = 4560
716909 TA = 324
77109
MA = 324
91563
Ha = 188
790 n
mi
Hp = 175
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14219254
76 X = 4359709
69
Y = -12499016
26 feet Y = -3761090
77 meter
Z = 11209390
98 Z = 3437740
17
XDOT = 5454
088297 XDOT = 1573
051063
YDOT = 19680
048907 feet/sec YDOT = 6016
569583 meter/sec
ZDOT = 14962
981986 ZDOT = 4568
575579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15918452
02 X = -4851944
18
Y = 10159852
21 feet Y = 3096722
95 meter
Z = 11289080
91 Z = 3440911
86
XDOT = -1521
347691 XDOT = -463
706776
YDOT = -19112
790953 feet/sec YDOT = -5825
578683 meter/sec
ZDOT = 14993
547077 ZDOT = 4570
033149
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 07271
51451876
00020000 00000-0 20000-3 0 9115
2 25544 51
6332 290
7385 0010416 58
1843 302
0334 15
77147110 27083
Satellite: ISS
Catalog Number: 25544
Epoch time: 07271
51451876 = yrday
fracday
Element set: 911
Inclination: 51
6332 deg
RA of node: 290
7385 deg
Eccentricity:
0010416
Arg of perigee: 58
1843 deg
Mean anomaly: 302
0334 deg
Mean motion: 15
77147110 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2708
Checksum: 270
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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