Date:
September 17th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4800 7 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 2486)
---------------------------------------
Vector Time (GMT): 2007/257/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4179986
49 A = 6716644
95 meter
Y = 3142152
04 meter E =
0015948
Z = 4213800
17 I = 51
64484
XDOT = -6031
266271 Wp = 41
47065
YDOT = -3147
530914 meter/sec RA = 2
68411 deg
ZDOT = -3616
296938 TA = 85
38641
MA = 85
20427
Ha = 188
034 n
mi
Hp = 178
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13713866
44 X = -4235281
89
Y = 10308897
76 feet Y = 3095100
17 meter
Z = 13824803
71 Z = 4193359
11
XDOT = -19787
618999 XDOT = -5978
054385
YDOT = -10326
544994 feet/sec YDOT = -3214
678655 meter/sec
ZDOT = -11864
491265 ZDOT = -3645
467617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16390079
20 X = 4995696
14
Y = -5276161
98 feet Y = -1608174
17 meter
Z = 13747586
03 Z = 4190264
22
XDOT = 14918
278618 XDOT = 4547
091323
YDOT = 14971
340083 feet/sec YDOT = 4563
264457 meter/sec
ZDOT = -11975
582313 ZDOT = -3650
157489
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 07257
50977301
00020000 00000-0 20000-3 0 9002
2 25544 51
6363 2
9821 0009098 5
5516 354
5748 15
76771652 24870
Satellite: ISS
Catalog Number: 25544
Epoch time: 07257
50977301 = yrday
fracday
Element set: 900
Inclination: 51
6363 deg
RA of node: 2
9821 deg
Eccentricity:
0009098
Arg of perigee: 5
5516 deg
Mean anomaly: 354
5748 deg
Mean motion: 15
76771652 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2487
Checksum: 304
Coasting Arc #2 (Orbit 2502)
---------------------------------------
Vector Time (GMT): 2007/258/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4696022
23 A = 6717496
30 meter
Y = 2852109
58 meter E =
0014399
Z = 3848485
06 I = 51
62050
XDOT = -5504
169648 Wp = 59
58829
YDOT = 3498
401314 meter/sec RA = 357
57778 deg
ZDOT = 4119
469454 TA = 347
45368
MA = 347
48948
Ha = 187
874 n
mi
Hp = 178
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15406897
07 X = 4645085
04
Y = 9357314
88 feet Y = 2904338
54 meter
Z = 12626263
34 Z = 3871174
72
XDOT = -18058
299369 XDOT = -5562
892073
YDOT = 11477
694601 feet/sec YDOT = 3436
522456 meter/sec
ZDOT = 13515
319731 ZDOT = 4092
587085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11705963
85 X = -3567977
78
Y = -13627604
70 feet Y = -4153693
91 meter
Z = 12712715
89 Z = 3874835
80
XDOT = 19794
626776 XDOT = 6033
402241
YDOT = -4477
434739 feet/sec YDOT = -1364
722109 meter/sec
ZDOT = 13413
695778 ZDOT = 4088
494473
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 07258
52379192
00020000 00000-0 20000-3 0 9010
2 25544 51
6369 357
7523 0009166 8
7209 351
4113 15
76856344 25039
Satellite: ISS
Catalog Number: 25544
Epoch time: 07258
52379192 = yrday
fracday
Element set: 901
Inclination: 51
6369 deg
RA of node: 357
7523 deg
Eccentricity:
0009166
Arg of perigee: 8
7209 deg
Mean anomaly: 351
4113 deg
Mean motion: 15
76856344 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2503
Checksum: 301
Coasting Arc #3 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2007/259/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5306820
19 A = 6720711
76 meter
Y = -2981071
38 meter E =
0012957
Z = -2839010
96 I = 51
60188
XDOT = 4648
014463 Wp = 27
22530
YDOT = 3446
862774 meter/sec RA = 352
36958 deg
ZDOT = 5089
375874 TA = 300
13473
MA = 300
26308
Ha = 188
232 n
mi
Hp = 178
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17410827
40 X = 5353552
14
Y = -9780417
92 feet Y = -2921466
33 meter
Z = -9314340
43 Z = -2813116
50
XDOT = 15249
391283 XDOT = 4584
402100
YDOT = 11308
604900 feet/sec YDOT = 3498
483998 meter/sec
ZDOT = 16697
427407 ZDOT = 5111
801572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19556555
65 X = -5960838
16
Y = 4260214
65 feet Y = 1298513
42 meter
Z = -9216405
24 Z = -2809160
32
XDOT = -10886
179444 XDOT = -3318
107495
YDOT = -13811
896865 feet/sec YDOT = -4209
866164 meter/sec
ZDOT = 16782
944153 ZDOT = 5115
441378
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 07259
47442257
00020000 00000-0 20000-3 0 9029
2 25544 51
6369 352
8503 0009417 11
6626 348
4755 15
76819911 25181
Satellite: ISS
Catalog Number: 25544
Epoch time: 07259
47442257 = yrday
fracday
Element set: 902
Inclination: 51
6369 deg
RA of node: 352
8503 deg
Eccentricity:
0009417
Arg of perigee: 11
6626 deg
Mean anomaly: 348
4755 deg
Mean motion: 15
76819911 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2518
Checksum: 312
Coasting Arc #4 (Orbit 2533)
---------------------------------------
Vector Time (GMT): 2007/260/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3312906
28 A = 6713605
01 meter
Y = -3226210
47 meter E =
0019129
Z = -4883824
42 I = 51
54991
XDOT = 6562
655418 Wp = 48
87830
YDOT = -3318
887633 meter/sec RA = 347
24958 deg
ZDOT = -2252
651361 TA = 199
12475
MA = 199
19667
Ha = 188
178 n
mi
Hp = 177
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10869115
09 X = -3252859
06
Y = -10584680
03 feet Y = -3262921
61 meter
Z = -16023045
98 Z = -4899772
80
XDOT = 21531
021714 XDOT = 6610
223070
YDOT = -10888
738955 feet/sec YDOT = -3245
234387 meter/sec
ZDOT = -7390
588456 ZDOT = -2220
653994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7449175
41 X = 2270508
67
Y = 13142580
56 feet Y = 4005858
55 meter
Z = -16083950
97 Z = -4902388
26
XDOT = -22777
665335 XDOT = -6942
632394
YDOT = 3987
231164 feet/sec YDOT = 1215
308059 meter/sec
ZDOT = -7269
527332 ZDOT = -2215
751931
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
48841103
00020000 00000-0 20000-3 0 9036
2 25544 51
6369 347
6206 0009322 15
6988 344
4464 15
76858934 25342
Satellite: ISS
Catalog Number: 25544
Epoch time: 07260
48841103 = yrday
fracday
Element set: 903
Inclination: 51
6369 deg
RA of node: 347
6206 deg
Eccentricity:
0009322
Arg of perigee: 15
6988 deg
Mean anomaly: 344
4464 deg
Mean motion: 15
76858934 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2534
Checksum: 310
Coasting Arc #5 (Orbit 2549)
---------------------------------------
Vector Time (GMT): 2007/261/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6026436
33 A = 6723538
85 meter
Y = 2799780
82 meter E =
0014631
Z = 1016762
39 I = 51
55508
XDOT = -2872
121631 Wp = 85
49460
YDOT = -4006
765854 meter/sec RA = 342
05816 deg
ZDOT = -5916
196237 TA = 83
37068
MA = 83
20416
Ha = 188
283 n
mi
Hp = 177
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19771772
74 X = -6062235
30
Y = 9185632
61 feet Y = 2732189
64 meter
Z = 3335834
60 Z = 987398
69
XDOT = -9422
971229 XDOT = -2798
363798
YDOT = -13145
557265 feet/sec YDOT = -4038
471156 meter/sec
ZDOT = -19410
092640 ZDOT = -5929
969980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21492701
85 X = 6550975
52
Y = -3753887
12 feet Y = -1144184
80 meter
Z = 3224706
96 Z = 982890
68
XDOT = 5322
693445 XDOT = 1622
356962
YDOT = 13539
938465 feet/sec YDOT = 4126
973244 meter/sec
ZDOT = -19462
833590 ZDOT = -5932
271678
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
50238287
00020000 00000-0 20000-3 0 9044
2 25544 51
6363 342
3908 0009410 20
4573 339
6966 15
76892085 25505
Satellite: ISS
Catalog Number: 25544
Epoch time: 07261
50238287 = yrday
fracday
Element set: 904
Inclination: 51
6363 deg
RA of node: 342
3908 deg
Eccentricity:
0009410
Arg of perigee: 20
4573 deg
Mean anomaly: 339
6966 deg
Mean motion: 15
76892085 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2550
Checksum: 301
Coasting Arc #6 (Orbit 2565)
---------------------------------------
Vector Time (GMT): 2007/262/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1686712
66 A = 6711653
48 meter
Y = 3821012
40 meter E =
0010628
Z = 5248428
57 I = 51
48917
XDOT = -7076
337687 Wp = 34
68414
YDOT = 3063
464573 meter/sec RA = 336
90138 deg
ZDOT = 52
424024 TA = 54
86782
MA = 54
76826
Ha = 188
231 n
mi
Hp = 177
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5533834
19 X = 1618364
06
Y = 12536129
92 feet Y = 3839491
99 meter
Z = 17219253
85 Z = 5256456
69
XDOT = -23216
330994 XDOT = -7110
322544
YDOT = 10050
736789 feet/sec YDOT = 2984
142948 meter/sec
ZDOT = 171
994829 ZDOT = 17
964382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2241432
15 X = -683188
52
Y = -13479180
81 feet Y = -4108454
31 meter
Z = 17250166
48 Z = 5257850
74
XDOT = 23976
258496 XDOT = 7307
963589
YDOT = -3969
678093 feet/sec YDOT = -1209
957883 meter/sec
ZDOT = 41
552433 ZDOT = 12
665182
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
51633557
00020000 00000-0 20000-3 0 9056
2 25544 51
6369 337
1601 0009489 23
3921 336
7674 15
76965490 25660
Satellite: ISS
Catalog Number: 25544
Epoch time: 07262
51633557 = yrday
fracday
Element set: 905
Inclination: 51
6369 deg
RA of node: 337
1601 deg
Eccentricity:
0009489
Arg of perigee: 23
3921 deg
Mean anomaly: 336
7674 deg
Mean motion: 15
76965490 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2566
Checksum: 318
Coasting Arc #7 (Orbit 2581)
---------------------------------------
Vector Time (GMT): 2007/263/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6167105
88 A = 6723435
42 meter
Y = -2478151
40 meter E =
0022744
Z = 926446
40 I = 51
50235
XDOT = 1030
311599 Wp = 43
45314
YDOT = 4811
261939 meter/sec RA = 331
74276 deg
ZDOT = 5941
507047 TA = 326
70698
MA = 326
84983
Ha = 188
425 n
mi
Hp = 177
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20233287
00 X = 6189858
05
Y = -8130417
99 feet Y = -2409060
13 meter
Z = 3039522
30 Z = 956461
57
XDOT = 3380
287399 XDOT = 947
571889
YDOT = 15784
980115 feet/sec YDOT = 4822
320806 meter/sec
ZDOT = 19493
133355 ZDOT = 5946
311376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21527866
79 X = -6561693
80
Y = 3367015
63 feet Y = 1026266
36 meter
Z = 3153165
50 Z = 961084
84
XDOT = 615
102636 XDOT = 187
483283
YDOT = -14546
066361 feet/sec YDOT = -4433
641027 meter/sec
ZDOT = 19511
926248 ZDOT = 5947
235120
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
53027482
00020000 00000-0 20000-3 0 9064
2 25544 51
6367 331
9305 0009689 27
6741 332
4937 15
76940894 25824
Satellite: ISS
Catalog Number: 25544
Epoch time: 07263
53027482 = yrday
fracday
Element set: 906
Inclination: 51
6367 deg
RA of node: 331
9305 deg
Eccentricity:
0009689
Arg of perigee: 27
6741 deg
Mean anomaly: 332
4937 deg
Mean motion: 15
76940894 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2582
Checksum: 320
Coasting Arc #8 (Orbit 2596)
---------------------------------------
Vector Time (GMT): 2007/264/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -136431
63 A = 6713201
78 meter
Y = -4595580
91 meter E =
0017755
Z = -4904730
72 I = 51
44252
XDOT = 6941
432006 Wp = 73
79253
YDOT = -2511
706394 meter/sec RA = 326
54609 deg
ZDOT = 2171
670063 TA = 217
30214
MA = 217
42557
Ha = 188
464 n
mi
Hp = 176
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -447610
33 X = -61206
71
Y = -15077365
17 feet Y = -4596685
97 meter
Z = -16091636
23 Z = -4905210
78
XDOT = 22773
727055 XDOT = 6958
452793
YDOT = -8240
506543 feet/sec YDOT = -2433
988206 meter/sec
ZDOT = 7124
901783 ZDOT = 2205
432908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2794260
98 X = -851690
75
Y = 14820375
13 feet Y = 4517250
34 meter
Z = -16093993
87 Z = -4905449
33
XDOT = -22871
110249 XDOT = -6971
114404
YDOT = 3523
406552 feet/sec YDOT = 1073
934317 meter/sec
ZDOT = 7252
768668 ZDOT = 2210
643890
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
48082503
00020000 00000-0 20000-3 0 9075
2 25544 51
6359 327
0276 0009753 31
2110 328
9632 15
76989952 25977
Satellite: ISS
Catalog Number: 25544
Epoch time: 07264
48082503 = yrday
fracday
Element set: 907
Inclination: 51
6359 deg
RA of node: 327
0276 deg
Eccentricity:
0009753
Arg of perigee: 31
2110 deg
Mean anomaly: 328
9632 deg
Mean motion: 15
76989952 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2597
Checksum: 314
Coasting Arc #9 (Orbit 2612)
---------------------------------------
Vector Time (GMT): 2007/265/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5841558
42 A = 6720120
42 meter
Y = 1790862
56 meter E =
0011382
Z = -2814461
89 I = 51
44215
XDOT = 687
556485 Wp = 58
66322
YDOT = -5733
197256 meter/sec RA = 321
41478 deg
ZDOT = -5084
422192 TA = 153
68291
MA = 153
62505
Ha = 188
542 n
mi
Hp = 176
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19165217
91 X = -5847477
84
Y = 5875533
32 feet Y = 1725505
79 meter
Z = -9233798
85 Z = -2842854
54
XDOT = 2255
762745 XDOT = 776
314007
YDOT = -18809
702285 feet/sec YDOT = -5725
012448 meter/sec
ZDOT = -16681
175169 ZDOT = -5080
866340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19884749
36 X = 6060871
61
Y = -2103837
68 feet Y = -641249
73 meter
Z = -9341366
08 Z = -2847248
38
XDOT = -6064
084852 XDOT = -1848
333063
YDOT = 16560
672503 feet/sec YDOT = 5047
692979 meter/sec
ZDOT = -16668
351505 ZDOT = -5080
513539
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
49472986
00020000 00000-0 20000-3 0 9086
2 25544 51
6353 321
7968 0009771 35
2944 324
8866 15
76999197 26134
Satellite: ISS
Catalog Number: 25544
Epoch time: 07265
49472986 = yrday
fracday
Element set: 908
Inclination: 51
6353 deg
RA of node: 321
7968 deg
Eccentricity:
0009771
Arg of perigee: 35
2944 deg
Mean anomaly: 324
8866 deg
Mean motion: 15
76999197 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2613
Checksum: 352
Coasting Arc #10 (Orbit 2628)
---------------------------------------
Vector Time (GMT): 2007/266/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1241539
81 A = 6717182
98 meter
Y = 5392907
83 meter E =
0019814
Z = 3800064
98 I = 51
41140
XDOT = -6326
070412 Wp = 61
46935
YDOT = 1483
484443 meter/sec RA = 316
19073 deg
ZDOT = -4146
466828 TA = 72
12807
MA = 71
91208
Ha = 188
539 n
mi
Hp = 176
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4073293
34 X = -1320211
81
Y = 17693267
17 feet Y = 5378584
53 meter
Z = 12467404
80 Z = 3793842
26
XDOT = -20754
824187 XDOT = -6322
046063
YDOT = 4867
074943 feet/sec YDOT = 1412
765058 meter/sec
ZDOT = -13603
893794 ZDOT = -4177
189077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7171135
26 X = 2185762
03
Y = -16697027
16 feet Y = -5089253
88 meter
Z = 12444424
75 Z = 3793060
66
XDOT = 19992
780717 XDOT = 6093
799562
YDOT = -1702
129166 feet/sec YDOT = -518
808970 meter/sec
ZDOT = -13720
339952 ZDOT = -4181
959617
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
50861526
00020000 00000-0 20000-3 0 9092
2 25544 51
6358 316
5660 0009871 37
8735 322
3122 15
77068103 26297
Satellite: ISS
Catalog Number: 25544
Epoch time: 07266
50861526 = yrday
fracday
Element set: 909
Inclination: 51
6358 deg
RA of node: 316
5660 deg
Eccentricity:
0009871
Arg of perigee: 37
8735 deg
Mean anomaly: 322
3122 deg
Mean motion: 15
77068103 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2629
Checksum: 301
Coasting Arc #11 (Orbit 2644)
---------------------------------------
Vector Time (GMT): 2007/267/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5123407
92 A = 6715351
19 meter
Y = -688292
24 meter E =
0016425
Z = 4270134
19 I = 51
38474
XDOT = -2031
399389 Wp = 74
91989
YDOT = 6575
063901 meter/sec RA = 311
06581 deg
ZDOT = 3490
236985 TA = 339
67429
MA = 339
73959
Ha = 188
475 n
mi
Hp = 176
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16809081
10 X = 5109980
21
Y = -2258176
64 feet Y = -631074
16 meter
Z = 14009626
60 Z = 4294991
10
XDOT = -6664
696158 XDOT = -2121
726677
YDOT = 21571
731958 feet/sec YDOT = 6551
842854 meter/sec
ZDOT = 11450
908744 ZDOT = 3480
148576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16876803
66 X = -5144049
76
Y = -409481
33 feet Y = -124809
91 meter
Z = 14103901
22 Z = 4298869
09
XDOT = 10018
169694 XDOT = 3053
538123
YDOT = -19009
195773 feet/sec YDOT = -5794
002872 meter/sec
ZDOT = 11413
404413 ZDOT = 3478
805665
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
52248506
00020000 00000-0 20000-3 0 9104
2 25544 51
6350 311
3354 0009893 42
5810 317
6120 15
77074474 26454
Satellite: ISS
Catalog Number: 25544
Epoch time: 07267
52248506 = yrday
fracday
Element set: 910
Inclination: 51
6350 deg
RA of node: 311
3354 deg
Eccentricity:
0009893
Arg of perigee: 42
5810 deg
Mean anomaly: 317
6120 deg
Mean motion: 15
77074474 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2645
Checksum: 280
Coasting Arc #12 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2007/268/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2193227
83 A = 6721412
14 meter
Y = -5972902
67 meter E =
0016345
Z = -2153281
73 I = 51
38655
XDOT = 5402
206601 Wp = 44
01888
YDOT = 15
949166 meter/sec RA = 305
84417 deg
ZDOT = 5494
652735 TA = 291
76075
MA = 291
93463
Ha = 188
691 n
mi
Hp = 176
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7195629
36 X = 2270315
00
Y = -19596137
38 feet Y = -5947945
95 meter
Z = -7064572
60 Z = -2142439
19
XDOT = 17723
774937 XDOT = 5374
934640
YDOT = 52
326659 feet/sec YDOT = 76
207732 meter/sec
ZDOT = 18027
075902 ZDOT = 5520
830482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9921533
12 X = -3024083
29
Y = 18382559
36 feet Y = 5603004
09 meter
Z = -7024141
24 Z = -2140958
25
XDOT = -16098
860103 XDOT = -4906
932559
YDOT = -1808
666461 feet/sec YDOT = -551
281537 meter/sec
ZDOT = 18126
447387 ZDOT = 5524
941164
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
47297236
00020000 00000-0 20000-3 0 9114
2 25544 51
6344 306
4315 0010038 45
9741 314
2250 15
77081816 26604
Satellite: ISS
Catalog Number: 25544
Epoch time: 07268
47297236 = yrday
fracday
Element set: 911
Inclination: 51
6344 deg
RA of node: 306
4315 deg
Eccentricity:
0010038
Arg of perigee: 45
9741 deg
Mean anomaly: 314
2250 deg
Mean motion: 15
77081816 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2660
Checksum: 280
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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