Date:
August 3rd 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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
226/07:54:26
102 4
0 10
6 10
6
N/A 9
1 0
1 195
6
000/00:18:52
205 -3
6 -0
2 188
8
Coasting Arc #1 (Orbit 3566)
---------------------------------------
Vector Time (GMT): 2008/214/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4766026
54 A = 6726350
20 meter
Y = -951821
78 meter E =
0012124
Z = 4638231
55 I = 51
82799
XDOT = 4001
649534 Wp = 60
23777
YDOT = -5915
237715 meter/sec RA = 142
68297 deg
ZDOT = 2898
306138 TA = 1
18724
MA = 1
18436
Ha = 194
887 n
mi
Hp = 183
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15636570
00 X = -4777560
00
Y = -3122774
87 feet Y = -1005183
19 meter
Z = 15217295
13 Z = 4615050
69
XDOT = 13128
771437 XDOT = 4053
418176
YDOT = -19406
947884 feet/sec YDOT = -5870
199817 meter/sec
ZDOT = 9508
878405 ZDOT = 2917
870780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5734568
94 X = 1747896
61
Y = 14969577
59 feet Y = 4562727
25 meter
Z = 15127676
00 Z = 4610915
64
XDOT = -22297
246017 XDOT = -6796
200586
YDOT = -1142
479209 feet/sec YDOT = -348
227663 meter/sec
ZDOT = 9583
858763 ZDOT = 2921
160151
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 08214
53195304
00020000 00000-0 20000-3 0 9004
2 25544 51
6409 143
3468 0010141 17
7053 342
4461 15
72794588 35677
Satellite: ISS
Catalog Number: 25544
Epoch time: 08214
53195304 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 143
3468 deg
Eccentricity:
0010141
Arg of perigee: 17
7053 deg
Mean anomaly: 342
4461 deg
Mean motion: 15
72794588 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3567
Checksum: 283
Coasting Arc #2 (Orbit 3581)
---------------------------------------
Vector Time (GMT): 2008/215/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2634544
93 A = 6732036
43 meter
Y = 5479347
79 meter E =
0013967
Z = -2882343
76 I = 51
86954
XDOT = -5780
815840 Wp = 34
62738
YDOT = -117
633424 meter/sec RA = 137
52635 deg
ZDOT = 5083
408456 TA = 292
37567
MA = 292
52360
Ha = 194
926 n
mi
Hp = 183
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8643520
12 X = -2681618
51
Y = 17976862
82 feet Y = 5449623
80 meter
Z = -9456508
41 Z = -2895256
01
XDOT = -18965
931232 XDOT = -5803
764467
YDOT = -385
936432 feet/sec YDOT = -182
406512 meter/sec
ZDOT = 16677
849265 ZDOT = 5055
270200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19746507
76 X = 6018735
57
Y = -2649152
59 feet Y = -807461
71 meter
Z = -9505840
84 Z = -2897380
29
XDOT = 9915
245087 XDOT = 3022
166703
YDOT = 14724
496926 feet/sec YDOT = 4488
026663 meter/sec
ZDOT = 16569
156546 ZDOT = 5050
278915
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 08215
48504323
00020000 00000-0 20000-3 0 9015
2 25544 51
6408 138
4614 0010302 21
0898 339
0688 15
72766352 35826
Satellite: ISS
Catalog Number: 25544
Epoch time: 08215
48504323 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 138
4614 deg
Eccentricity:
0010302
Arg of perigee: 21
0898 deg
Mean anomaly: 339
0688 deg
Mean motion: 15
72766352 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3582
Checksum: 283
Coasting Arc #3 (Orbit 3597)
---------------------------------------
Vector Time (GMT): 2008/216/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5189779
82 A = 6727927
35 meter
Y = -749856
51 meter E =
0017132
Z = -4233512
93 I = 51
87742
XDOT = -2037
324409 Wp = 45
03052
YDOT = 6454
480886 meter/sec RA = 132
46495 deg
ZDOT = -3637
852888 TA = 187
95726
MA = 187
98447
Ha = 194
995 n
mi
Hp = 183
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17026836
68 X = 5218344
32
Y = -2460159
17 feet Y = -691661
49 meter
Z = -13889478
13 Z = -4208232
18
XDOT = -6684
135201 XDOT = -2091
676372
YDOT = 21176
118391 feet/sec YDOT = 6431
394634 meter/sec
ZDOT = -11935
212886 ZDOT = -3647
881700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11642000
66 X = -3548481
80
Y = -12772251
90 feet Y = -3892982
38 meter
Z = -13791901
80 Z = -4203771
67
XDOT = 20305
487943 XDOT = 6189
112725
YDOT = -5569
051298 feet/sec YDOT = -1697
446836 meter/sec
ZDOT = -11973
312937 ZDOT = -3649
465783
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 08216
50166184
00020000 00000-0 20000-3 0 9029
2 25544 51
6417 133
2498 0010348 25
3848 334
7821 15
72807980 35982
Satellite: ISS
Catalog Number: 25544
Epoch time: 08216
50166184 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 133
2498 deg
Eccentricity:
0010348
Arg of perigee: 25
3848 deg
Mean anomaly: 334
7821 deg
Mean motion: 15
72807980 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3598
Checksum: 303
Coasting Arc #4 (Orbit 3613)
---------------------------------------
Vector Time (GMT): 2008/217/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 917027
88 A = 6730345
00 meter
Y = -5690664
64 meter E =
0019689
Z = 3468888
26 I = 51
90415
XDOT = 5913
702123 Wp = 61
83522
YDOT = -1850
054243 meter/sec RA = 127
30614 deg
ZDOT = -4569
664806 TA = 77
22925
MA = 77
00929
Ha = 195
053 n
mi
Hp = 183
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3008621
65 X = 963742
69
Y = -18670159
57 feet Y = -5680148
83 meter
Z = 11380866
99 Z = 3473456
38
XDOT = 19401
909854 XDOT = 5956
148445
YDOT = -6069
731770 feet/sec YDOT = -1783
686337 meter/sec
ZDOT = -14992
338602 ZDOT = -4540
833481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16960102
20 X = -5169439
15
Y = 8342207
84 feet Y = 2542704
95 meter
Z = 11397951
48 Z = 3474095
61
XDOT = -15573
996119 XDOT = -4746
954017
YDOT = -11202
295094 feet/sec YDOT = -3414
459545 meter/sec
ZDOT = -14881
150966 ZDOT = -4535
774815
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 08217
51827070
00020000 00000-0 20000-3 0 9030
2 25544 51
6413 128
0386 0010301 29
0141 331
1592 15
72805586 36147
Satellite: ISS
Catalog Number: 25544
Epoch time: 08217
51827070 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 128
0386 deg
Eccentricity:
0010301
Arg of perigee: 29
0141 deg
Mean anomaly: 331
1592 deg
Mean motion: 15
72805586 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3614
Checksum: 259
Coasting Arc #5 (Orbit 3629)
---------------------------------------
Vector Time (GMT): 2008/218/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5012860
60 A = 6729611
53 meter
Y = 2479784
64 meter E =
0018866
Z = 3721720
64 I = 51
91841
XDOT = 42
761771 Wp = 66
71733
YDOT = -6393
655900 meter/sec RA = 122
24994 deg
ZDOT = 4307
882930 TA = 338
01757
MA = 338
09839
Ha = 195
251 n
mi
Hp = 182
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16446393
05 X = -5058296
61
Y = 8135776
39 feet Y = 2423473
79 meter
Z = 12210369
55 Z = 3697258
17
XDOT = 140
294525 XDOT = 93
326806
YDOT = -20976
561352 feet/sec YDOT = -6392
895124 meter/sec
ZDOT = 14133
474180 ZDOT = 4308
213287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16310210
56 X = 4971352
18
Y = 8540761
89 feet Y = 2603224
23 meter
Z = 12116115
07 Z = 3692991
87
XDOT = -16353
241354 XDOT = -4984
467965
YDOT = 11132
629263 feet/sec YDOT = 3393
225399 meter/sec
ZDOT = 14134
123377 ZDOT = 4308
080805
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 08218
53486960
00020000 00000-0 20000-3 0 9043
2 25544 51
6413 122
8270 0010349 32
7943 327
3860 15
72817244 36301
Satellite: ISS
Catalog Number: 25544
Epoch time: 08218
53486960 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 122
8270 deg
Eccentricity:
0010349
Arg of perigee: 32
7943 deg
Mean anomaly: 327
3860 deg
Mean motion: 15
72817244 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3630
Checksum: 286
Coasting Arc #6 (Orbit 3644)
---------------------------------------
Vector Time (GMT): 2008/219/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 810858
22 A = 6728454
55 meter
Y = 5336029
75 meter E =
0014281
Z = -4024252
69 I = 51
92992
XDOT = -5409
199405 Wp = 64
96824
YDOT = 3785
990115 meter/sec RA = 117
09198 deg
ZDOT = 3946
936558 TA = 245
63157
MA = 245
78070
Ha = 195
171 n
mi
Hp = 182
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2660295
99 X = 770678
55
Y = 17506659
30 feet Y = 5344872
73 meter
Z = -13202928
77 Z = -4020410
97
XDOT = -17746
717209 XDOT = -5470
306277
YDOT = 12421
227411 feet/sec YDOT = 3725
159526 meter/sec
ZDOT = 12949
266923 ZDOT = 3920
510590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12307886
75 X = 3751443
88
Y = -12746825
12 feet Y = -3885232
30 meter
Z = -13187569
74 Z = -4019571
26
XDOT = 19729
515807 XDOT = 6013
556418
YDOT = 5815
274337 feet/sec YDOT = 1772
495618 meter/sec
ZDOT = 12847
547927 ZDOT = 3915
932608
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 08219
48792146
00020000 00000-0 20000-3 0 9055
2 25544 51
6418 117
9411 0010343 35
9930 324
1927 15
72843895 36459
Satellite: ISS
Catalog Number: 25544
Epoch time: 08219
48792146 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 117
9411 deg
Eccentricity:
0010343
Arg of perigee: 35
9930 deg
Mean anomaly: 324
1927 deg
Mean motion: 15
72843895 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3645
Checksum: 306
Coasting Arc #7 (Orbit 3660)
---------------------------------------
Vector Time (GMT): 2008/220/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4333152
00 A = 6731118
48 meter
Y = -4061982
74 meter E =
0013042
Z = -3184772
02 I = 51
95143
XDOT = 1784
270805 Wp = 57
40075
YDOT = 5694
906191 meter/sec RA = 112
03630 deg
ZDOT = -4843
300481 TA = 159
47564
MA = 159
42319
Ha = 195
178 n
mi
Hp = 182
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14216377
94 X = 4393722
65
Y = -13326715
02 feet Y = -4013188
12 meter
Z = -10448727
09 Z = -3163574
75
XDOT = 5853
906842 XDOT = 1743
984592
YDOT = 18684
075429 feet/sec YDOT = 5714
633920 meter/sec
ZDOT = -15890
093440 ZDOT = -4834
730114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19296421
22 X = -5881549
19
Y = -3008554
51 feet Y = -917007
41 meter
Z = -10367225
31 Z = -3159930
28
XDOT = 10813
505450 XDOT = 3295
956461
YDOT = -14801
109944 feet/sec YDOT = -4511
378311 meter/sec
ZDOT = -15856
437779 ZDOT = -4833
042235
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 08220
50450084
00020000 00000-0 20000-3 0 9063
2 25544 51
6422 112
7291 0010279 39
3801 320
8107 15
72851748 36613
Satellite: ISS
Catalog Number: 25544
Epoch time: 08220
50450084 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 112
7291 deg
Eccentricity:
0010279
Arg of perigee: 39
3801 deg
Mean anomaly: 320
8107 deg
Mean motion: 15
72851748 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3661
Checksum: 268
Coasting Arc #8 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2008/221/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2257626
00 A = 6726823
13 meter
Y = -4517836
91 meter E =
0019067
Z = 4435944
56 I = 51
94684
XDOT = 4349
212684 Wp = 55
03682
YDOT = -5434
284469 meter/sec RA = 106
88282 deg
ZDOT = -3300
497136 TA = 68
02832
MA = 67
82581
Ha = 195
247 n
mi
Hp = 182
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7406909
44 X = -2228487
95
Y = -14822299
56 feet Y = -4542920
35 meter
Z = 14553623
87 Z = 4425047
54
XDOT = 14269
070487 XDOT = 4425
689624
YDOT = -17829
017286 feet/sec YDOT = -5385
221252 meter/sec
ZDOT = -10828
402678 ZDOT = -3279
183348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6780787
41 X = -2066784
00
Y = 15159810
00 feet Y = 4620710
09 meter
Z = 14511096
52 Z = 4422982
22
XDOT = -21768
778598 XDOT = -6635
123717
YDOT = 614
775652 feet/sec YDOT = 187
383619 meter/sec
ZDOT = -10746
570324 ZDOT = -3275
554635
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 08221
52107024
00020000 00000-0 20000-3 0 9070
2 25544 51
6418 107
5173 0010369 42
7665 317
4303 15
72893930 36771
Satellite: ISS
Catalog Number: 25544
Epoch time: 08221
52107024 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 107
5173 deg
Eccentricity:
0010369
Arg of perigee: 42
7665 deg
Mean anomaly: 317
4303 deg
Mean motion: 15
72893930 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3677
Checksum: 283
Coasting Arc #9 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2008/222/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3162748
55 A = 6732606
48 meter
Y = 5349017
04 meter E =
0023406
Z = 2557026
92 I = 51
97380
XDOT = -3302
105977 Wp = 63
48980
YDOT = -4505
286184 meter/sec RA = 101
82343 deg
ZDOT = 5313
357250 TA = 325
39655
MA = 325
54864
Ha = 195
365 n
mi
Hp = 182
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10376471
62 X = -3234748
56
Y = 17549268
51 feet Y = 5313246
59 meter
Z = 8389195
95 Z = 2541487
91
XDOT = -10833
681027 XDOT = -3277
292928
YDOT = -14781
122651 feet/sec YDOT = -4542
073926 meter/sec
ZDOT = 17432
274443 ZDOT = 5297
375602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20139586
64 X = 6138546
01
Y = -3322723
50 feet Y = -1012766
12 meter
Z = 8329655
22 Z = 2538878
91
XDOT = -4512
935919 XDOT = -1375
542868
YDOT = 16413
665324 feet/sec YDOT = 5002
885191 meter/sec
ZDOT = 17370
106108 ZDOT = 5294
408342
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 08222
53763135
00020000 00000-0 20000-3 0 9084
2 25544 51
6423 102
3053 0010405 46
5202 313
6824 15
72868940 36934
Satellite: ISS
Catalog Number: 25544
Epoch time: 08222
53763135 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 102
3053 deg
Eccentricity:
0010405
Arg of perigee: 46
5202 deg
Mean anomaly: 313
6824 deg
Mean motion: 15
72868940 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3693
Checksum: 270
Coasting Arc #10 (Orbit 3707)
---------------------------------------
Vector Time (GMT): 2008/223/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3402969
18 A = 6725374
58 meter
Y = 3271633
49 meter E =
0019102
Z = -4805189
32 I = 51
95491
XDOT = -2807
036018 Wp = 80
88996
YDOT = 6677
945554 meter/sec RA = 96
67763 deg
ZDOT = 2570
382889 TA = 214
17555
MA = 214
29865
Ha = 195
266 n
mi
Hp = 182
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11164597
03 X = 3389474
91
Y = 10733705
66 feet Y = 3309612
44 meter
Z = -15765056
83 Z = -4788690
28
XDOT = -9209
435754 XDOT = -2893
987618
YDOT = 21909
270189 feet/sec YDOT = 6646
069251 meter/sec
ZDOT = 8433
014729 ZDOT = 2556
535820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 699656
43 X = 213255
28
Y = -15536622
47 feet Y = -4735562
53 meter
Z = -15701003
92 Z = -4785665
99
XDOT = 21467
365969 XDOT = 6543
253147
YDOT = -7463
502435 feet/sec YDOT = -2274
875542 meter/sec
ZDOT = 8380
122638 ZDOT = 2554
261380
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 08223
49064661
00020000 00000-0 20000-3 0 9099
2 25544 51
6427 97
4194 0010258 49
4939 310
7115 15
72905671 37084
Satellite: ISS
Catalog Number: 25544
Epoch time: 08223
49064661 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 97
4194 deg
Eccentricity:
0010258
Arg of perigee: 49
4939 deg
Mean anomaly: 310
7115 deg
Mean motion: 15
72905671 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3708
Checksum: 305
Coasting Arc #11 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2008/224/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1702283
08 A = 6733709
25 meter
Y = -6219120
46 meter E =
0012521
Z = -1953122
75 I = 51
98504
XDOT = 4324
558092 Wp = 87
03940
YDOT = 2944
178002 meter/sec RA = 91
61101 deg
ZDOT = -5635
904082 TA = 114
55076
MA = 114
42019
Ha = 195
276 n
mi
Hp = 182
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5584918
23 X = 1781187
58
Y = -20403938
50 feet Y = -6199643
17 meter
Z = -6407883
03 Z = -1944662
10
XDOT = 14188
182718 XDOT = 4318
692356
YDOT = 9659
376646 feet/sec YDOT = 2992
505466 meter/sec
ZDOT = -18490
498956 ZDOT = -5614
909526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18916319
06 X = -5765694
05
Y = 9491871
75 feet Y = 2893122
51 meter
Z = -6375753
02 Z = -1943329
52
XDOT = -1708
847434 XDOT = -520
856698
YDOT = -15704
123374 feet/sec YDOT = -4786
616804 meter/sec
ZDOT = -18409
102276 ZDOT = -5611
094374
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 08224
50718849
00020000 00000-0 20000-3 0 9108
2 25544 51
6428 92
2075 0010107 53
5352 306
6741 15
72884076 37246
Satellite: ISS
Catalog Number: 25544
Epoch time: 08224
50718849 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 92
2075 deg
Eccentricity:
0010107
Arg of perigee: 53
5352 deg
Mean anomaly: 306
6741 deg
Mean motion: 15
72884076 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3724
Checksum: 286
Coasting Arc #12 (Orbit 3739)
---------------------------------------
Vector Time (GMT): 2008/225/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4059806
93 A = 6724177
23 meter
Y = -1814358
52 meter E =
0015727
Z = 5035195
61 I = 51
95334
XDOT = 997
270090 Wp = 55
75164
YDOT = -7413
486364 meter/sec RA = 86
47392 deg
ZDOT = -1854
506546 TA = 52
11155
MA = 51
96943
Ha = 195
321 n
mi
Hp = 182
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13319576
54 X = -4063676
50
Y = -5952619
83 feet Y = -1859779
76 meter
Z = 16519670
63 Z = 5015463
74
XDOT = 3271
883497 XDOT = 1089
103501
YDOT = -24322
461823 feet/sec YDOT = -7401
820663 meter/sec
ZDOT = -6084
339061 ZDOT = -1849
439555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4803420
30 X = 1464082
51
Y = 13866901
31 feet Y = 4226631
52 meter
Z = 16443251
55 Z = 5011903
07
XDOT = -19023
446548 XDOT = -5798
346508
YDOT = 13831
777655 feet/sec YDOT = 4215
925829 meter/sec
ZDOT = -6065
424321 ZDOT = -1848
741333
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 08225
52371867
00020000 00000-0 20000-3 0 9117
2 25544 51
6429 86
9954 0010179 56
2875 303
9256 15
72967028 37400
Satellite: ISS
Catalog Number: 25544
Epoch time: 08225
52371867 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 86
9954 deg
Eccentricity:
0010179
Arg of perigee: 56
2875 deg
Mean anomaly: 303
9256 deg
Mean motion: 15
72967028 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3740
Checksum: 319
Coasting Arc #13 (Orbit 3752)
---------------------------------------
Vector Time (GMT): 2008/226/08:03:52
205
Vector Time (MET): N/A
Weight (LBS) : 661093
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4217816
81 A = 6730240
19 meter
Y = 930031
76 meter E =
0014636
Z = -5174207
89 I = 51
94823
XDOT = -16
462517 Wp = 94
37877
YDOT = 7565
393091 meter/sec RA = 82
10413 deg
ZDOT = 1348
577924 TA = 188
48572
MA = 188
51049
Ha = 195
584 n
mi
Hp = 188
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13837981
64 X = 4232238
53
Y = 3051285
29 feet Y = 977278
93 meter
Z = -16975747
67 Z = -5153682
94
XDOT = -54
010883 XDOT = -107
609771
YDOT = 24820
843476 feet/sec YDOT = 7564
699240 meter/sec
ZDOT = 4424
468253 ZDOT = 1348
277270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4879624
81 X = 1487309
64
Y = -13404442
76 feet Y = -4085674
15 meter
Z = -16896338
73 Z = -5150004
05
XDOT = 23611
787433 XDOT = 7196
872810
YDOT = 3027
960013 feet/sec YDOT = 922
922212 meter/sec
ZDOT = 4423
983916 ZDOT = 1348
430298
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 08226
34965928
00020000 00000-0 20000-3 0 9126
2 25544 51
6420 82
7609 0001569 28
3220 331
8026 15
70660906 37531
Satellite: ISS
Catalog Number: 25544
Epoch time: 08226
34965928 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 82
7609 deg
Eccentricity:
0001569
Arg of perigee: 28
3220 deg
Mean anomaly: 331
8026 deg
Mean motion: 15
70660906 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3753
Checksum: 289
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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