Date:
September 5th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5651 05 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 2313)
---------------------------------------
Vector Time (GMT): 2007/246/12:56:13
833
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4814087
91 A = 6721808
46 meter
Y = 3771288
12 meter E =
0009433
Z = -2776126
14 I = 51
91862
XDOT = -1376
614111 Wp = 352
45282
YDOT = 5553
331121 meter/sec RA = 58
91158 deg
ZDOT = 5164
036073 TA = 335
86930
MA = 335
91346
Ha = 186
865 n
mi
Hp = 181
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15794251
67 X = 4785044
97
Y = 12372992
52 feet Y = 3824959
66 meter
Z = -9108025
40 Z = -2752809
66
XDOT = -4516
450497 XDOT = -1463
696011
YDOT = 18219
590291 feet/sec YDOT = 5537
449995 meter/sec
ZDOT = 16942
375568 ZDOT = 5157
137098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14849615
40 X = -4526162
77
Y = -13551773
62 feet Y = -4130580
60 meter
Z = -9019080
37 Z = -2749015
70
XDOT = 5007
013876 XDOT = 1526
137829
YDOT = -16729
319612 feet/sec YDOT = -5099
096618 meter/sec
ZDOT = 16916
847844 ZDOT = 5156
255223
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 07246
54458802
00020000 00000-0 20000-3 0 9004
2 25544 51
6340 59
5136 0008660 322
4674 37
5885 15
76486150 23147
Satellite: ISS
Catalog Number: 25544
Epoch time: 07246
54458802 = yrday
fracday
Element set: 900
Inclination: 51
6340 deg
RA of node: 59
5136 deg
Eccentricity:
0008660
Arg of perigee: 322
4674 deg
Mean anomaly: 37
5885 deg
Mean motion: 15
76486150 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2314
Checksum: 293
Coasting Arc #2 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2007/247/12:56:13
833
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1579082
93 A = 6714617
60 meter
Y = -4336648
65 meter E =
0012968
Z = -4886959
20 I = 51
87934
XDOT = 5662
813905 Wp = 32
98404
YDOT = 4672
976180 meter/sec RA = 53
81772 deg
ZDOT = -2309
188665 TA = 214
55509
MA = 214
63944
Ha = 186
912 n
mi
Hp = 180
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5180718
27 X = 1651198
56
Y = -14227849
91 feet Y = -4318587
03 meter
Z = -16033330
71 Z = -4879113
04
XDOT = 18578
785779 XDOT = 5621
356727
YDOT = 15331
286680 feet/sec YDOT = 4736
069259 meter/sec
ZDOT = -7576
078297 ZDOT = -2281
779244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6108313
83 X = -1861814
06
Y = 13888768
74 feet Y = 4233296
71 meter
Z = -16004057
41 Z = -4878036
70
XDOT = -16662
606299 XDOT = -5078
762400
YDOT = -15967
190654 feet/sec YDOT = -4866
799711 meter/sec
ZDOT = -7471
490815 ZDOT = -2277
310400
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 07247
55880683
00020000 00000-0 20000-3 0 9013
2 25544 51
6345 54
2861 0008703 327
2326 32
8297 15
76533379 23303
Satellite: ISS
Catalog Number: 25544
Epoch time: 07247
55880683 = yrday
fracday
Element set: 901
Inclination: 51
6345 deg
RA of node: 54
2861 deg
Eccentricity:
0008703
Arg of perigee: 327
2326 deg
Mean anomaly: 32
8297 deg
Mean motion: 15
76533379 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2330
Checksum: 298
Coasting Arc #3 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2007/248/12:56:13
833
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5028391
04 A = 6724317
69 meter
Y = -4301733
13 meter E =
0007327
Z = 1189247
70 I = 51
89333
XDOT = 2328
227481 Wp = 87
85494
YDOT = -4362
103929 meter/sec RA = 48
64939 deg
ZDOT = -5902
990744 TA = 79
15429
MA = 79
07183
Ha = 187
029 n
mi
Hp = 180
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16497345
94 X = -4985691
82
Y = -14113297
67 feet Y = -4357724
74 meter
Z = 3901731
29 Z = 1164923
46
XDOT = 7638
541604 XDOT = 2405
507623
YDOT = -14311
364595 feet/sec YDOT = -4335
636034 meter/sec
ZDOT = -19366
767533 ZDOT = -5891
492754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15906513
56 X = 4848305
33
Y = 14800210
98 feet Y = 4511104
31 meter
Z = 3808895
18 Z = 1160951
25
XDOT = -7267
091309 XDOT = -2215
009431
YDOT = 12810
407337 feet/sec YDOT = 3904
612156 meter/sec
ZDOT = -19323
630360 ZDOT = -5889
842534
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 07248
57300619
00020000 00000-0 20000-3 0 9023
2 25544 51
6338 49
0562 0008848 330
2955 29
7706 15
76558717 23467
Satellite: ISS
Catalog Number: 25544
Epoch time: 07248
57300619 = yrday
fracday
Element set: 902
Inclination: 51
6338 deg
RA of node: 49
0562 deg
Eccentricity:
0008848
Arg of perigee: 330
2955 deg
Mean anomaly: 29
7706 deg
Mean motion: 15
76558717 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2346
Checksum: 312
Coasting Arc #4 (Orbit 2361)
---------------------------------------
Vector Time (GMT): 2007/249/12:56:13
833
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2550486
93 A = 6712826
84 meter
Y = 3287935
94 meter E =
0007425
Z = 5268293
95 I = 51
83555
XDOT = -5780
935592 Wp = 349
21751
YDOT = -5079
874097 meter/sec RA = 43
52435 deg
ZDOT = 378
909195 TA = 97
23870
MA = 97
15429
Ha = 187
266 n
mi
Hp = 180
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8367739
26 X = -2612655
70
Y = 10787191
40 feet Y = 3259067
20 meter
Z = 17284428
98 Z = 5255752
91
XDOT = -18966
324121 XDOT = -5725
542685
YDOT = -16666
253598 feet/sec YDOT = -5144
210075 meter/sec
ZDOT = 1243
140405 ZDOT = 350
960115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8733409
43 X = 2661943
19
Y = -10570733
14 feet Y = -3221959
46 meter
Z = 17237204
08 Z = 5253899
80
XDOT = 17776
917234 XDOT = 5418
404373
YDOT = 16501
423061 feet/sec YDOT = 5029
633749 meter/sec
ZDOT = 1136
448949 ZDOT = 346
389640
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 07249
58718821
00020000 00000-0 20000-3 0 9034
2 25544 51
6347 43
8273 0008857 334
7883 25
2847 15
76568453 23620
Satellite: ISS
Catalog Number: 25544
Epoch time: 07249
58718821 = yrday
fracday
Element set: 903
Inclination: 51
6347 deg
RA of node: 43
8273 deg
Eccentricity:
0008857
Arg of perigee: 334
7883 deg
Mean anomaly: 25
2847 deg
Mean motion: 15
76568453 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2362
Checksum: 326
Coasting Arc #5 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2007/250/12:56:13
833
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4971540
55 A = 6724621
76 meter
Y = 4478633
82 meter E =
0017977
Z = 539158
51 I = 51
85502
XDOT = -3562
806434 Wp = 22
74741
YDOT = 3222
579126 meter/sec RA = 38
38607 deg
ZDOT = 6033
283866 TA = 343
11405
MA = 343
17381
Ha = 187
256 n
mi
Hp = 180
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16310828
58 X = 4918471
21
Y = 14693680
50 feet Y = 4533931
66 meter
Z = 1768892
73 Z = 563181
04
XDOT = -11688
997486 XDOT = -3627
885196
YDOT = 10572
766161 feet/sec YDOT = 3182
373896 meter/sec
ZDOT = 19794
238406 ZDOT = 6015
817941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16183204
97 X = -4932640
88
Y = -14822899
66 feet Y = -4518019
82 meter
Z = 1860612
62 Z = 567114
73
XDOT = 10802
887521 XDOT = 3292
720116
YDOT = -9298
322523 feet/sec YDOT = -2834
128705 meter/sec
ZDOT = 19728
308344 ZDOT = 6013
188383
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 07250
60134887
00020000 00000-0 20000-3 0 9044
2 25544 51
6359 38
5986 0008804 338
6693 21
4104 15
76614783 23788
Satellite: ISS
Catalog Number: 25544
Epoch time: 07250
60134887 = yrday
fracday
Element set: 904
Inclination: 51
6359 deg
RA of node: 38
5986 deg
Eccentricity:
0008804
Arg of perigee: 338
6693 deg
Mean anomaly: 21
4104 deg
Mean motion: 15
76614783 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2378
Checksum: 314
Coasting Arc #6 (Orbit 2392)
---------------------------------------
Vector Time (GMT): 2007/251/12:56:13
833
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3693548
80 A = 6713439
66 meter
Y = -2368731
44 meter E =
0011997
Z = -5088793
16 I = 51
79419
XDOT = 5507
686866 Wp = 62
21067
YDOT = 5130
042525 meter/sec RA = 33
22554 deg
ZDOT = 1618
022539 TA = 223
25535
MA = 223
34962
Ha = 187
401 n
mi
Hp = 179
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12117942
24 X = 3744481
87
Y = -7771428
63 feet Y = -2327143
41 meter
Z = -16695515
63 Z = -5070726
41
XDOT = 18069
838798 XDOT = 5442
052677
YDOT = 16830
848180 feet/sec YDOT = 5191
265641 meter/sec
ZDOT = 5308
472898 ZDOT = 1644
618973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12139201
42 X = -3700028
59
Y = 7883889
52 feet Y = 2403009
53 meter
Z = -16627204
95 Z = -5067972
07
XDOT = -17619
657407 XDOT = -5370
471578
YDOT = -15778
103335 feet/sec YDOT = -4809
165896 meter/sec
ZDOT = 5410
044055 ZDOT = 1648
981428
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 07251
55210751
00020000 00000-0 20000-3 0 9055
2 25544 51
6360 33
6976 0008888 342
4130 17
6726 15
76653579 23936
Satellite: ISS
Catalog Number: 25544
Epoch time: 07251
55210751 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 33
6976 deg
Eccentricity:
0008888
Arg of perigee: 342
4130 deg
Mean anomaly: 17
6726 deg
Mean motion: 15
76653579 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2393
Checksum: 303
Coasting Arc #7 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2007/252/12:56:13
833
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4521163
40 A = 6722291
32 meter
Y = -4434964
74 meter E =
0004901
Z = -2263543
84 I = 51
79990
XDOT = 4934
155493 Wp = 22
91831
YDOT = -2240
251001 meter/sec RA = 28
11358 deg
ZDOT = -5465
592738 TA = 182
43942
MA = 182
44181
Ha = 187
485 n
mi
Hp = 179
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14833213
24 X = -4460239
19
Y = -14550409
24 feet Y = -4485182
39 meter
Z = -7426324
95 Z = -2285359
20
XDOT = 16188
174191 XDOT = 4985
390117
YDOT = -7349
904860 feet/sec YDOT = -2184
788254 meter/sec
ZDOT = -17931
734706 ZDOT = -5441
498381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15170851
65 X = 4624075
58
Y = 14154119
81 feet Y = 4314175
72 meter
Z = -7509665
68 Z = -2288946
10
XDOT = -15056
496887 XDOT = -4589
220251
YDOT = 6671
686937 feet/sec YDOT = 2033
530178 meter/sec
ZDOT = -17840
527482 ZDOT = -5437
792777
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 07252
56623047
00020000 00000-0 20000-3 0 9064
2 25544 51
6364 28
4674 0008980 346
2664 13
8255 15
76674390 24091
Satellite: ISS
Catalog Number: 25544
Epoch time: 07252
56623047 = yrday
fracday
Element set: 906
Inclination: 51
6364 deg
RA of node: 28
4674 deg
Eccentricity:
0008980
Arg of perigee: 346
2664 deg
Mean anomaly: 13
8255 deg
Mean motion: 15
76674390 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2409
Checksum: 307
Coasting Arc #8 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2007/253/12:56:13
833
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4901604
44 A = 6716618
99 meter
Y = 1608472
04 meter E =
0014288
Z = 4301709
91 I = 51
75510
XDOT = -4718
425573 Wp = 33
22191
YDOT = -4986
151325 meter/sec RA = 22
92272 deg
ZDOT = -3494
863895 TA = 92
14709
MA = 91
98347
Ha = 187
701 n
mi
Hp = 179
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16081379
40 X = -4940123
05
Y = 5277139
24 feet Y = 1553444
43 meter
Z = 14113221
49 Z = 4277804
48
XDOT = -15480
398860 XDOT = -4645
341745
YDOT = -16358
764188 feet/sec YDOT = -5038
507009 meter/sec
ZDOT = -11466
088895 ZDOT = -3517
607959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15914777
60 X = 4850824
21
Y = -5977193
30 feet Y = -1821848
52 meter
Z = 14022660
12 Z = 4274106
80
XDOT = 15678
998041 XDOT = 4778
958603
YDOT = 14509
896083 feet/sec YDOT = 4422
616326 meter/sec
ZDOT = -11553
020115 ZDOT = -3521
360531
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 07253
58033431
00020000 00000-0 20000-3 0 9070
2 25544 51
6371 23
2387 0008994 350
7341 9
3656 15
76672684 24257
Satellite: ISS
Catalog Number: 25544
Epoch time: 07253
58033431 = yrday
fracday
Element set: 907
Inclination: 51
6371 deg
RA of node: 23
2387 deg
Eccentricity:
0008994
Arg of perigee: 350
7341 deg
Mean anomaly: 9
3656 deg
Mean motion: 15
76672684 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2425
Checksum: 299
Coasting Arc #9 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2007/254/12:56:13
833
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3595594
65 A = 6718147
50 meter
Y = 4254723
97 meter E =
0012974
Z = 3739895
49 I = 51
73512
XDOT = -6243
042476 Wp = 53
86544
YDOT = 1525
474731 meter/sec RA = 17
82450 deg
ZDOT = 4263
998098 TA = 351
36321
MA = 351
38552
Ha = 187
591 n
mi
Hp = 179
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11796570
36 X = 3529582
81
Y = 13959068
13 feet Y = 4294563
12 meter
Z = 12269998
34 Z = 3757202
15
XDOT = -20482
422821 XDOT = -6280
350198
YDOT = 5004
838356 feet/sec YDOT = 1455
453216 meter/sec
ZDOT = 13989
495073 ZDOT = 4233
578819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12554630
78 X = -3826651
46
Y = -13219944
63 feet Y = -4029439
12 meter
Z = 12336199
76 Z = 3760073
69
XDOT = 19254
288172 XDOT = 5868
707035
YDOT = -5330
369632 feet/sec YDOT = -1624
696664 meter/sec
ZDOT = 13874
200299 ZDOT = 4228
856251
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 07254
59441447
00020000 00000-0 20000-3 0 9083
2 25544 51
6380 18
0093 0009093 353
9563 6
1490 15
76763040 24411
Satellite: ISS
Catalog Number: 25544
Epoch time: 07254
59441447 = yrday
fracday
Element set: 908
Inclination: 51
6380 deg
RA of node: 18
0093 deg
Eccentricity:
0009093
Arg of perigee: 353
9563 deg
Mean anomaly: 6
1490 deg
Mean motion: 15
76763040 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2441
Checksum: 286
Coasting Arc #10 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2007/255/12:56:13
833
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5901321
65 A = 6720538
63 meter
Y = -1110786
75 meter E =
0011595
Z = -3007273
12 I = 51
71498
XDOT = 3426
730835 Wp = 18
61645
YDOT = 4788
933177 meter/sec RA = 12
62447 deg
ZDOT = 4971
580852 TA = 306
60044
MA = 306
70705
Ha = 187
954 n
mi
Hp = 178
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19361291
50 X = 5927912
83
Y = -3644313
50 feet Y = -1044646
39 meter
Z = -9866381
62 Z = -2978539
82
XDOT = 11242
555233 XDOT = 3348
774541
YDOT = 15711
723022 feet/sec YDOT = 4826
817325 meter/sec
ZDOT = 16310
960802 ZDOT = 4988
038186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19073156
83 X = -5813498
20
Y = 5147145
97 feet Y = 1568850
09 meter
Z = -9757442
92 Z = -2974068
60
XDOT = -11966
538744 XDOT = -3647
401009
YDOT = -13403
454470 feet/sec YDOT = -4085
372922 meter/sec
ZDOT = 16373
998174 ZDOT = 4990
794643
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 07255
54509922
00020000 00000-0 20000-3 0 9093
2 25544 51
6383 13
1079 0009370 357
1622 2
9488 15
76734317 24566
Satellite: ISS
Catalog Number: 25544
Epoch time: 07255
54509922 = yrday
fracday
Element set: 909
Inclination: 51
6383 deg
RA of node: 13
1079 deg
Eccentricity:
0009370
Arg of perigee: 357
1622 deg
Mean anomaly: 2
9488 deg
Mean motion: 15
76734317 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2456
Checksum: 301
Coasting Arc #11 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2007/256/12:56:13
833
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2266660
62 A = 6714204
93 meter
Y = -4127869
38 meter E =
0017286
Z = -4800596
46 I = 51
66587
XDOT = 7201
387025 Wp = 41
32701
YDOT = -1041
476997 meter/sec RA = 7
51579 deg
ZDOT = -2497
048327 TA = 204
18811
MA = 204
26936
Ha = 187
890 n
mi
Hp = 178
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7436550
59 X = -2197013
16
Y = -13542878
55 feet Y = -4152827
40 meter
Z = -15749988
39 Z = -4811438
47
XDOT = 23626
597852 XDOT = 7224
628022
YDOT = -3416
919283 feet/sec YDOT = -960
817254 meter/sec
ZDOT = -8192
415772 ZDOT = -2462
007294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8602694
00 X = 2622101
13
Y = 12782491
35 feet Y = 3896103
36 meter
Z = -15791629
09 Z = -4813288
55
XDOT = -22307
847823 XDOT = -6799
432016
YDOT = 5025
581706 feet/sec YDOT = 1531
797304 meter/sec
ZDOT = -8059
530729 ZDOT = -2456
544966
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 07256
55914174
00020000 00000-0 20000-3 0 9106
2 25544 51
6385 7
8789 0009285 1
1335 358
9849 15
76778782 24725
Satellite: ISS
Catalog Number: 25544
Epoch time: 07256
55914174 = yrday
fracday
Element set: 910
Inclination: 51
6385 deg
RA of node: 7
8789 deg
Eccentricity:
0009285
Arg of perigee: 1
1335 deg
Mean anomaly: 358
9849 deg
Mean motion: 15
76778782 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2472
Checksum: 333
Coasting Arc #12 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2007/257/12:56:13
833
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6560528
03 A = 6723510
55 meter
Y = 737626
61 meter E =
0012995
Z = 1269441
91 I = 51
66810
XDOT = -1673
407245 Wp = 80
63032
YDOT = -4705
928603 meter/sec RA = 2
32963 deg
ZDOT = -5860
972026 TA = 85
44079
MA = 85
29236
Ha = 188
011 n
mi
Hp = 178
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21524042
10 X = -6574455
46
Y = 2420034
81 feet Y = 664185
29 meter
Z = 4164835
65 Z = 1237536
71
XDOT = -5490
181251 XDOT = -1592
188685
YDOT = -15439
398305 feet/sec YDOT = -4724
187849 meter/sec
ZDOT = -19228
910846 ZDOT = -5868
903925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21139421
96 X = 6443295
81
Y = -4822774
63 feet Y = -1469981
71 meter
Z = 4043822
06 Z = 1232556
96
XDOT = 6728
970450 XDOT = 2050
990193
YDOT = 13196
244690 feet/sec YDOT = 4022
215381 meter/sec
ZDOT = -19259
570009 ZDOT = -5870
316939
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
57316370
00020000 00000-0 20000-3 0 9114
2 25544 51
6379 2
6499 0009359 5
9684 354
1590 15
76817132 24881
Satellite: ISS
Catalog Number: 25544
Epoch time: 07257
57316370 = yrday
fracday
Element set: 911
Inclination: 51
6379 deg
RA of node: 2
6499 deg
Eccentricity:
0009359
Arg of perigee: 5
9684 deg
Mean anomaly: 354
1590 deg
Mean motion: 15
76817132 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2488
Checksum: 317
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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