Date:
August 12th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6200 0 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
233/15:32:27
000 0
0 0
0 0
0
012/16:55:45
047 0
0 0
0 184
6
000/00:00:00
000 0
0 0
0 184
3
Coasting Arc #1 (Orbit 1952)
---------------------------------------
Vector Time (GMT): 2007/223/15:32:27
000
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3602234
20 A = 6717608
88 meter
Y = 3660045
04 meter E =
0008524
Z = -4337081
58 I = 51
64538
XDOT = -6491
296115 Wp = 167
87229
YDOT = -2318
367245 meter/sec RA = 176
47947 deg
ZDOT = 3428
021189 TA = 136
76154
MA = 136
69460
Ha = 186
445 n
mi
Hp = 182
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11818353
66 X = -3621825
40
Y = 12008021
79 feet Y = 3619653
66 meter
Z = -14229270
28 Z = -4354628
08
XDOT = -21296
903265 XDOT = -6481
541638
YDOT = -7606
191749 feet/sec YDOT = -2390
902325 meter/sec
ZDOT = 11246
788678 ZDOT = 3396
510751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8961791
51 X = 2731554
05
Y = -14200998
40 feet Y = -4328464
31 meter
Z = -14295318
84 Z = -4357213
18
XDOT = 21443
715372 XDOT = 6536
044445
YDOT = 2308
574627 feet/sec YDOT = 703
653546 meter/sec
ZDOT = 11127
042417 ZDOT = 3391
522529
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 07223
65737267
00020000 00000-0 20000-3 0 9006
2 25544 51
6335 177
4451 0008378 232
4419 127
5985 15
76215856 19536
Satellite: ISS
Catalog Number: 25544
Epoch time: 07223
65737267 = yrday
fracday
Element set: 900
Inclination: 51
6335 deg
RA of node: 177
4451 deg
Eccentricity:
0008378
Arg of perigee: 232
4419 deg
Mean anomaly: 127
5985 deg
Mean motion: 15
76215856 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1953
Checksum: 314
Coasting Arc #2 (Orbit 1968)
---------------------------------------
Vector Time (GMT): 2007/224/15:37:05
805
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3749894
87 A = 6716577
63 meter
Y = 3122332
40 meter E =
0003059
Z = -4617371
59 I = 51
67155
XDOT = -6324
702225 Wp = 109
42161
YDOT = 3291
006242 meter/sec RA = 171
35867 deg
ZDOT = -2913
597033 TA = 131
76081
MA = 131
73466
Ha = 186
281 n
mi
Hp = 182
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12302804
68 X = 3737131
58
Y = 10243872
72 feet Y = 3164194
74 meter
Z = -15148856
93 Z = -4599185
88
XDOT = -20750
335384 XDOT = -6346
879310
YDOT = 10797
264575 feet/sec YDOT = 3220
156028 meter/sec
ZDOT = -9559
045383 ZDOT = -2944
375345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14527448
77 X = -4427966
39
Y = -6880800
59 feet Y = -2097268
02 meter
Z = -15079509
71 Z = -4596234
56
XDOT = 16901
392557 XDOT = 5151
544451
YDOT = -14498
646615 feet/sec YDOT = -4419
187488 meter/sec
ZDOT = -9675
308601 ZDOT = -2949
034062
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 07224
67177215
00020000 00000-0 20000-3 0 9011
2 25544 51
6343 172
2179 0008378 236
8906 123
1455 15
76246452 19691
Satellite: ISS
Catalog Number: 25544
Epoch time: 07224
67177215 = yrday
fracday
Element set: 901
Inclination: 51
6343 deg
RA of node: 172
2179 deg
Eccentricity:
0008378
Arg of perigee: 236
8906 deg
Mean anomaly: 123
1455 deg
Mean motion: 15
76246452 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1969
Checksum: 304
Coasting Arc #3 (Orbit 1984)
---------------------------------------
Vector Time (GMT): 2007/225/15:41:36
106
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6465793
01 A = 6725878
53 meter
Y = -1801898
92 meter E =
0013056
Z = 258559
95 I = 51
73136
XDOT = 1507
979465 Wp = 170
61660
YDOT = 4539
472636 meter/sec RA = 166
16918 deg
ZDOT = -6044
571489 TA = 6
57319
MA = 6
55608
Ha = 186
172 n
mi
Hp = 182
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21213231
66 X = 6484205
55
Y = -5911741
85 feet Y = -1729491
83 meter
Z = 848293
79 Z = 290014
71
XDOT = 4947
439188 XDOT = 1486
469091
YDOT = 14893
282925 feet/sec YDOT = 4556
215643 meter/sec
ZDOT = -19831
271289 ZDOT = -6037
297990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18684304
45 X = -5694976
00
Y = 11646052
95 feet Y = 3549716
94 meter
Z = 967320
86 Z = 294839
40
XDOT = -8199
614931 XDOT = -2499
242631
YDOT = -11503
035369 feet/sec YDOT = -3506
125180 meter/sec
ZDOT = -19803
105814 ZDOT = -6035
986652
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 07225
68616377
00020000 00000-0 20000-3 0 9021
2 25544 51
6345 166
9906 0008490 239
6660 120
3665 15
76204916 19853
Satellite: ISS
Catalog Number: 25544
Epoch time: 07225
68616377 = yrday
fracday
Element set: 902
Inclination: 51
6345 deg
RA of node: 166
9906 deg
Eccentricity:
0008490
Arg of perigee: 239
6660 deg
Mean anomaly: 120
3665 deg
Mean motion: 15
76204916 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1985
Checksum: 316
Coasting Arc #4 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2007/226/15:46:13
272
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1310686
01 A = 6715435
37 meter
Y = -4481163
48 meter E =
0001847
Z = 4828447
95 I = 51
72533
XDOT = 7293
440940 Wp = 272
78895
YDOT = -484
622490 meter/sec RA = 160
98956 deg
ZDOT = -2430
282634 TA = 200
90337
MA = 200
91093
Ha = 185
734 n
mi
Hp = 183
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4300150
95 X = 1337242
36
Y = -14701979
91 feet Y = -4466358
23 meter
Z = 15841364
67 Z = 4834879
58
XDOT = 23928
612007 XDOT = 7310
123643
YDOT = -1589
968800 feet/sec YDOT = -402
969809 meter/sec
ZDOT = -7973
368223 ZDOT = -2394
811274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 672409
26 X = 204950
34
Y = 15278502
64 feet Y = 4656887
60 meter
Z = 15865168
41 Z = 4835703
33
XDOT = -21114
991746 XDOT = -6435
849484
YDOT = 9066
805932 feet/sec YDOT = 2763
562448 meter/sec
ZDOT = -7838
933688 ZDOT = -2389
306988
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 07226
70054231
00020000 00000-0 20000-3 0 9031
2 25544 51
6349 161
7630 0008504 245
8195 114
2081 15
76302108 20018
Satellite: ISS
Catalog Number: 25544
Epoch time: 07226
70054231 = yrday
fracday
Element set: 903
Inclination: 51
6349 deg
RA of node: 161
7630 deg
Eccentricity:
0008504
Arg of perigee: 245
8195 deg
Mean anomaly: 114
2081 deg
Mean motion: 15
76302108 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2001
Checksum: 251
Coasting Arc #5 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2007/227/15:50:49
977
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5229445
70 A = 6718708
80 meter
Y = -1160581
08 meter E =
0005915
Z = 4056981
25 I = 51
76234
XDOT = 4159
771655 Wp = 153
36255
YDOT = -5201
643336 meter/sec RA = 155
87216 deg
ZDOT = 3866
558963 TA = 256
87211
MA = 256
93813
Ha = 185
602 n
mi
Hp = 183
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17156974
07 X = -5235787
03
Y = -3807680
72 feet Y = -1219095
16 meter
Z = 13310305
94 Z = 4031561
58
XDOT = 13647
544800 XDOT = 4198
845277
YDOT = -17065
758976 feet/sec YDOT = -5154
907963 meter/sec
ZDOT = 12685
560901 ZDOT = 3886
861723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17467388
39 X = 5324059
98
Y = -2512206
38 feet Y = -765720
51 meter
Z = 13213765
47 Z = 4027555
71
XDOT = -6870
426214 XDOT = -2094
105910
YDOT = 19482
815413 feet/sec YDOT = 5938
362138 meter/sec
ZDOT = 12761
868862 ZDOT = 3889
817629
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 07227
71491555
00020000 00000-0 20000-3 0 9048
2 25544 51
6346 156
5350 0008376 249
7472 110
2792 15
76253073 20172
Satellite: ISS
Catalog Number: 25544
Epoch time: 07227
71491555 = yrday
fracday
Element set: 904
Inclination: 51
6346 deg
RA of node: 156
5350 deg
Eccentricity:
0008376
Arg of perigee: 249
7472 deg
Mean anomaly: 110
2792 deg
Mean motion: 15
76253073 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2017
Checksum: 292
Coasting Arc #6 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2007/228/15:55:20
527
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5222593
32 A = 6724977
13 meter
Y = 4047102
30 meter E =
0005539
Z = -1233894
43 I = 51
80940
XDOT = -3837
514426 Wp = 331
13132
YDOT = -3155
554863 meter/sec RA = 150
67496 deg
ZDOT = 5886
508801 TA = 15
36125
MA = 15
34444
Ha = 185
349 n
mi
Hp = 183
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17134492
54 X = -5261466
50
Y = 13277894
68 feet Y = 3988482
96 meter
Z = -4048210
09 Z = -1259359
95
XDOT = -12590
270426 XDOT = -3830
538630
YDOT = -10352
870286 feet/sec YDOT = -3198
429107 meter/sec
ZDOT = 19312
692917 ZDOT = 5867
883296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10641856
41 X = 3243637
84
Y = -18864183
21 feet Y = -5749803
04 meter
Z = -4144250
28 Z = -1263167
48
XDOT = 14339
468675 XDOT = 4370
670052
YDOT = 3857
819198 feet/sec YDOT = 1175
863292 meter/sec
ZDOT = 19241
652432 ZDOT = 5864
855661
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 07228
66587871
00020000 00000-0 20000-3 0 9051
2 25544 51
6341 151
6338 0008550 253
8232 106
1991 15
76286895 20323
Satellite: ISS
Catalog Number: 25544
Epoch time: 07228
66587871 = yrday
fracday
Element set: 905
Inclination: 51
6341 deg
RA of node: 151
6338 deg
Eccentricity:
0008550
Arg of perigee: 253
8232 deg
Mean anomaly: 106
1991 deg
Mean motion: 15
76286895 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2032
Checksum: 306
Coasting Arc #7 (Orbit 2047)
---------------------------------------
Vector Time (GMT): 2007/229/15:59:41
430
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1135512
39 A = 6714003
04 meter
Y = 4148095
69 meter E =
0007081
Z = -5161377
22 I = 51
79612
XDOT = -6771
855205 Wp = 126
72528
YDOT = 3438
076921 meter/sec RA = 145
51838 deg
ZDOT = 1270
337881 TA = 155
41059
MA = 155
37681
Ha = 185
122 n
mi
Hp = 183
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3725434
36 X = 1114116
25
Y = 13609237
81 feet Y = 4160674
01 meter
Z = -16933652
30 Z = -5155912
89
XDOT = -22217
372720 XDOT = -6815
968026
YDOT = 11279
779923 feet/sec YDOT = 3362
103565 meter/sec
ZDOT = 4167
775201 ZDOT = 1237
333284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9183475
51 X = -2799123
34
Y = -10745862
86 feet Y = -3275339
00 meter
Z = -16912392
03 Z = -5154897
09
XDOT = 14661
854772 XDOT = 4468
933334
YDOT = -18908
558423 feet/sec YDOT = -5763
328607 meter/sec
ZDOT = 4043
059290 ZDOT = 1232
324472
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 07229
68023109
00020000 00000-0 20000-3 0 9064
2 25544 51
6329 146
4053 0008585 257
5395 102
4809 15
76318419 20486
Satellite: ISS
Catalog Number: 25544
Epoch time: 07229
68023109 = yrday
fracday
Element set: 906
Inclination: 51
6329 deg
RA of node: 146
4053 deg
Eccentricity:
0008585
Arg of perigee: 257
5395 deg
Mean anomaly: 102
4809 deg
Mean motion: 15
76318419 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2048
Checksum: 302
Coasting Arc #8 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2007/230/16:04:23
910
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5683740
37 A = 6720843
69 meter
Y = -1297105
43 meter E =
0004160
Z = -3339074
53 I = 51
84120
XDOT = -1402
031836 Wp = 247
99497
YDOT = 5946
288302 meter/sec RA = 140
39789 deg
ZDOT = -4693
330773 TA = 331
20874
MA = 331
23169
Ha = 185
055 n
mi
Hp = 184
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18647442
17 X = 5714042
94
Y = -4255595
23 feet Y = -1233377
16 meter
Z = -10954968
94 Z = -3311389
43
XDOT = -4599
841982 XDOT = -1445
620635
YDOT = 19508
819888 feet/sec YDOT = 5930
366344 meter/sec
ZDOT = -15398
066840 ZDOT = -4700
247609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14736984
51 X = -4491832
88
Y = 12285937
09 feet Y = 3744753
62 meter
Z = -10850141
57 Z = -3307123
15
XDOT = -3940
448845 XDOT = -1201
048808
YDOT = -18356
713234 feet/sec YDOT = -5595
126194 meter/sec
ZDOT = -15423
532039 ZDOT = -4701
092566
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 07230
69457423
00020000 00000-0 20000-3 0 9078
2 25544 51
6320 141
1779 0008673 261
4905 98
5277 15
76309100 20642
Satellite: ISS
Catalog Number: 25544
Epoch time: 07230
69457423 = yrday
fracday
Element set: 907
Inclination: 51
6320 deg
RA of node: 141
1779 deg
Eccentricity:
0008673
Arg of perigee: 261
4905 deg
Mean anomaly: 98
5277 deg
Mean motion: 15
76309100 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2064
Checksum: 292
Coasting Arc #9 (Orbit 2079)
---------------------------------------
Vector Time (GMT): 2007/231/16:09:05
639
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3190811
67 A = 6723434
79 meter
Y = -5518328
64 meter E =
0006993
Z = 2123889
39 I = 51
87249
XDOT = 5267
172409 Wp = 139
29868
YDOT = 907
765792 meter/sec RA = 135
19721 deg
ZDOT = -5549
546817 TA = 17
00790
MA = 16
98447
Ha = 184
566 n
mi
Hp = 184
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10468542
22 X = 3241963
83
Y = -18104752
76 feet Y = -5482361
24 meter
Z = 6968141
04 Z = 2139514
41
XDOT = 17280
749372 XDOT = 5283
588822
YDOT = 2978
234226 feet/sec YDOT = 966
758239 meter/sec
ZDOT = -18207
174597 ZDOT = -5523
919030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -283967
26 X = -86553
22
Y = 20891920
49 feet Y = 6367857
36 meter
Z = 7026696
19 Z = 2141737
00
XDOT = -15106
833615 XDOT = -4604
562886
YDOT = 5891
106934 feet/sec YDOT = 1795
609393 meter/sec
ZDOT = -18109
860017 ZDOT = -5519
885333
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 07231
70890654
00020000 00000-0 20000-3 0 9089
2 25544 51
6323 135
9493 0008692 266
4908 93
5262 15
76373058 20808
Satellite: ISS
Catalog Number: 25544
Epoch time: 07231
70890654 = yrday
fracday
Element set: 908
Inclination: 51
6323 deg
RA of node: 135
9493 deg
Eccentricity:
0008692
Arg of perigee: 266
4908 deg
Mean anomaly: 93
5262 deg
Mean motion: 15
76373058 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2080
Checksum: 309
Coasting Arc #10 (Orbit 2095)
---------------------------------------
Vector Time (GMT): 2007/232/16:13:58
605
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2851621
33 A = 6713555
47 meter
Y = -3038317
07 meter E =
0006160
Z = 5269176
70 I = 51
85701
XDOT = 5208
166292 Wp = 276
19125
YDOT = -5655
007619 meter/sec RA = 130
05689 deg
ZDOT = -441
980347 TA = 177
99506
MA = 177
99259
Ha = 184
116 n
mi
Hp = 183
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9355713
04 X = -2843031
16
Y = -9968231
85 feet Y = -3070157
72 meter
Z = 17287325
12 Z = 5255344
26
XDOT = 17087
159752 XDOT = 5273
161403
YDOT = -18553
174602 feet/sec YDOT = -5596
403541 meter/sec
ZDOT = -1450
066755 ZDOT = -416
521498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13260319
13 X = 4041745
27
Y = 3589356
09 feet Y = 1094035
74 meter
Z = 17234473
65 Z = 5253067
57
XDOT = -4674
155250 XDOT = -1424
682520
YDOT = 23773
637220 feet/sec YDOT = 7246
204625 meter/sec
ZDOT = -1354
219020 ZDOT = -412
765957
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 07232
72323203
00020000 00000-0 20000-3 0 9094
2 25544 51
6311 130
7202 0008615 268
8574 91
1603 15
76320393 20960
Satellite: ISS
Catalog Number: 25544
Epoch time: 07232
72323203 = yrday
fracday
Element set: 909
Inclination: 51
6311 deg
RA of node: 130
7202 deg
Eccentricity:
0008615
Arg of perigee: 268
8574 deg
Mean anomaly: 91
1603 deg
Mean motion: 15
76320393 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2096
Checksum: 266
Coasting Arc #11 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2007/233/15:32:27
000
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025142
46 A = 6722661
74 meter
Y = -3645247
19 meter E =
0005463
Z = -2571296
89 I = 51
90512
XDOT = 1243
001306 Wp = 239
16031
YDOT = 5453
858810 meter/sec RA = 125
09512 deg
ZDOT = -5297
032786 TA = 329
93317
MA = 329
96452
Ha = 184
578 n
mi
Hp = 184
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16486687
87 X = 5078021
54
Y = -11959472
39 feet Y = -3588757
39 meter
Z = -8436013
42 Z = -2546756
59
XDOT = 4078
088273 XDOT = 1207
655024
YDOT = 17893
237565 feet/sec YDOT = 5467
561444 meter/sec
ZDOT = -17378
716489 ZDOT = -5291
079823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10864710
65 X = -3311563
81
Y = 17272874
53 feet Y = 5264772
16 meter
Z = -8343383
43 Z = -2543063
27
XDOT = -9301
960600 XDOT = -2835
237591
YDOT = -14243
066577 feet/sec YDOT = -4341
286693 meter/sec
ZDOT = -17355
448891 ZDOT = -5289
940822
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 07233
67415102
00020000 00000-0 20000-3 0 9101
2 25544 51
6311 125
8196 0008707 273
1451 86
8716 15
76355884 21119
Satellite: ISS
Catalog Number: 25544
Epoch time: 07233
67415102 = yrday
fracday
Element set: 910
Inclination: 51
6311 deg
RA of node: 125
8196 deg
Eccentricity:
0008707
Arg of perigee: 273
1451 deg
Mean anomaly: 86
8716 deg
Mean motion: 15
76355884 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2111
Checksum: 282
Coasting Arc #12 (Orbit 2126)
---------------------------------------
Vector Time (GMT): 2007/234/15:37:35
002
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 944602
71 A = 6721891
85 meter
Y = -6037228
79 meter E =
0004698
Z = 2795128
91 I = 51
91926
XDOT = 5526
093561 Wp = 104
36667
YDOT = -1520
966041 meter/sec RA = 119
89530 deg
ZDOT = -5146
660326 TA = 43
73249
MA = 43
69529
Ha = 184
723 n
mi
Hp = 183
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3099090
26 X = 998463
54
Y = -19807181
06 feet Y = -6026364
76 meter
Z = 9170370
45 Z = 2799848
17
XDOT = 18130
228217 XDOT = 5567
691927
YDOT = -4990
046065 feet/sec YDOT = -1458
937191 meter/sec
ZDOT = -16885
368525 ZDOT = -5119
713774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5347448
65 X = 1629902
35
Y = 19313693
51 feet Y = 5886813
78 meter
Z = 9187519
36 Z = 2800355
90
XDOT = -13164
466377 XDOT = -4012
529352
YDOT = 11638
083372 feet/sec YDOT = 3547
287812 meter/sec
ZDOT = -16783
332527 ZDOT = -5115
559754
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 07234
68845472
00020000 00000-0 20000-3 0 9111
2 25544 51
6316 120
5904 0008868 277
5711 82
4446 15
76416599 21278
Satellite: ISS
Catalog Number: 25544
Epoch time: 07234
68845472 = yrday
fracday
Element set: 911
Inclination: 51
6316 deg
RA of node: 120
5904 deg
Eccentricity:
0008868
Arg of perigee: 277
5711 deg
Mean anomaly: 82
4446 deg
Mean motion: 15
76416599 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2127
Checksum: 311
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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