Date:
September 25th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 3875 01 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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
262/00:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 190
2
000/00:00:00
000 0
0 0
0 179
5
263/05:38:00
000 0
0 0
0 0
0
N/A 0
0 0
0 190
3
000/00:00:00
000 0
0 0
0 179
2
Coasting Arc #1 (Orbit 779)
---------------------------------------
Vector Time (GMT): 2006/260/22:47:48
000
Vector Time (MET): N/A
Weight (LBS) : 465373
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4553035
20 A = 6717688
61 meter
Y = -1748061
56 meter E =
0016684
Z = 4621363
41 I = 51
91701
XDOT = -270
316394 Wp = 23
08510
YDOT = -7113
868020 meter/sec RA = 68
95125 deg
ZDOT = -2938
606036 TA = 96
00601
MA = 95
81586
Ha = 190
006 n
mi
Hp = 179
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14937779
52 X = -4555599
28
Y = -5735110
11 feet Y = -1798990
35 meter
Z = 15161953
44 Z = 4599238
78
XDOT = -886
864810 XDOT = -176
472967
YDOT = -23339
462007 feet/sec YDOT = -7116
366210 meter/sec
ZDOT = -9641
095918 ZDOT = -2939
691114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11769154
62 X = -3587238
33
Y = -10955161
30 feet Y = -3339133
16 meter
Z = 15079291
02 Z = 4596167
90
XDOT = 7190
754876 XDOT = 2191
742086
YDOT = -21086
855537 feet/sec YDOT = -6427
273568 meter/sec
ZDOT = -9646
107984 ZDOT = -2940
133714
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 06260
99232069
00020000 00000-0 20000-3 0 9003
2 25544 51
6331 69
3911 0011792 355
4686 4
6369 15
75860262 7802
Satellite: ISS
Catalog Number: 25544
Epoch time: 06260
99232069 = yrday
fracday
Element set: 900
Inclination: 51
6331 deg
RA of node: 69
3911 deg
Eccentricity:
0011792
Arg of perigee: 355
4686 deg
Mean anomaly: 4
6369 deg
Mean motion: 15
75860262 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 780
Checksum: 297
Coasting Arc #2 (Orbit 795)
---------------------------------------
Vector Time (GMT): 2006/261/22:47:48
000
Vector Time (MET): N/A
Weight (LBS) : 465373
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 225384
74 A = 6722698
51 meter
Y = 5953349
29 meter E =
0018238
Z = 3088477
84 I = 51
92233
XDOT = -5451
583132 Wp = 44
48306
YDOT = -2351
139666 meter/sec RA = 63
86819 deg
ZDOT = 4925
273909 TA = 351
29683
MA = 351
32841
Ha = 190
095 n
mi
Hp = 179
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 739451
25 X = 143793
68
Y = 19531985
86 feet Y = 5955413
60 meter
Z = 10132801
32 Z = 3089374
31
XDOT = -17885
771431 XDOT = -5448
813074
YDOT = -7713
712815 feet/sec YDOT = -2412
086583 meter/sec
ZDOT = 16159
035135 ZDOT = 4898
797184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6382508
75 X = -1945388
67
Y = 18472267
71 feet Y = 5630347
20 meter
Z = 10136953
69 Z = 3089743
48
XDOT = -12653
730000 XDOT = -3856
856904
YDOT = -13193
629952 feet/sec YDOT = -4021
418409 meter/sec
ZDOT = 16060
074272 ZDOT = 4895
110638
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 06262
00695956
00020000 00000-0 20000-3 0 9016
2 25544 51
6328 64
1655 0011841 359
0362 1
0777 15
75869658 7961
Satellite: ISS
Catalog Number: 25544
Epoch time: 06262
00695956 = yrday
fracday
Element set: 901
Inclination: 51
6328 deg
RA of node: 64
1655 deg
Eccentricity:
0011841
Arg of perigee: 359
0362 deg
Mean anomaly: 1
0777 deg
Mean motion: 15
75869658 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 796
Checksum: 309
Coasting Arc #3 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2006/262/00:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 450157
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2522060
11 A = 6716051
68 meter
Y = 3711792
35 meter E =
0009781
Z = 4990328
84 I = 51
89801
XDOT = -4645
627236 Wp = 27
16574
YDOT = -5821
907208 meter/sec RA = 63
50194 deg
ZDOT = 1989
471465 TA = 43
72931
MA = 43
65187
Ha = 190
201 n
mi
Hp = 179
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8274475
43 X = -2587620
35
Y = 12177796
43 feet Y = 3683222
94 meter
Z = 16372469
96 Z = 4977917
37
XDOT = -15241
559172 XDOT = -4589
845005
YDOT = -19100
745432 feet/sec YDOT = -5873
545200 meter/sec
ZDOT = 6527
137351 ZDOT = 1967
038962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7482958
90 X = -2280805
87
Y = 12738383
72 feet Y = 3882659
36 meter
Z = 16326737
22 Z = 4976389
51
XDOT = -15660
313817 XDOT = -4773
263651
YDOT = -17427
533761 feet/sec YDOT = -5311
912290 meter/sec
ZDOT = 6442
769543 ZDOT = 1963
756157
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 06262
07037477
00020000 00000-0 20000-3 0 9022
2 25544 51
6318 63
8383 0011983 358
7280 1
3852 15
75865698 7974
Satellite: ISS
Catalog Number: 25544
Epoch time: 06262
07037477 = yrday
fracday
Element set: 902
Inclination: 51
6318 deg
RA of node: 63
8383 deg
Eccentricity:
0011983
Arg of perigee: 358
7280 deg
Mean anomaly: 1
3852 deg
Mean motion: 15
75865698 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 797
Checksum: 318
Coasting Arc #4 (Orbit 811)
---------------------------------------
Vector Time (GMT): 2006/263/00:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 450157
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4197911
09 A = 6726289
93 meter
Y = 5116193
87 meter E =
0020548
Z = -1133604
41 I = 51
91871
XDOT = -3091
444668 Wp = 18
19851
YDOT = 3839
986655 meter/sec RA = 58
34409 deg
ZDOT = 5930
238716 TA = 329
41593
MA = 329
53558
Ha = 190
274 n
mi
Hp = 179
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13772674
17 X = 4145895
92
Y = 16785412
95 feet Y = 5162846
33 meter
Z = -3719174
59 Z = -1113337
76
XDOT = -10142
535001 XDOT = -3162
962016
YDOT = 12598
381415 feet/sec YDOT = 3805
016912 meter/sec
ZDOT = 19456
163766 ZDOT = 5915
046615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15213950
12 X = 4637212
00
Y = 15509138
72 feet Y = 4727185
48 meter
Z = -3642971
16 Z = -1110377
61
XDOT = -7972
606233 XDOT = -2430
050380
YDOT = 12340
281344 feet/sec YDOT = 3761
317754 meter/sec
ZDOT = 19400
089552 ZDOT = 5913
147295
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 06263
02158786
00020000 00000-0 20000-3 0 9036
2 25544 51
6317 58
9391 0011981 3
1144 357
0093 15
75882311 8122
Satellite: ISS
Catalog Number: 25544
Epoch time: 06263
02158786 = yrday
fracday
Element set: 903
Inclination: 51
6317 deg
RA of node: 58
9391 deg
Eccentricity:
0011981
Arg of perigee: 3
1144 deg
Mean anomaly: 357
0093 deg
Mean motion: 15
75882311 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 812
Checksum: 280
Coasting Arc #5 (Orbit 815)
---------------------------------------
Vector Time (GMT): 2006/263/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5009898
12 A = 6719739
07 meter
Y = -1917873
55 meter E =
0018320
Z = 4047750
43 I = 51
89726
XDOT = -630
234408 Wp = 37
62592
YDOT = -6615
857473 meter/sec RA = 57
22555 deg
ZDOT = -3891
310511 TA = 92
42866
MA = 92
21891
Ha = 190
323 n
mi
Hp = 179
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16436673
63 X = -5007742
98
Y = -6292236
04 feet Y = -1973884
68 meter
Z = 13280021
10 Z = 4023417
85
XDOT = -2067
698190 XDOT = -537
304958
YDOT = -21705
569136 feet/sec YDOT = -6622
385768 meter/sec
ZDOT = -12766
766769 ZDOT = -3894
146006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8325312
41 X = -2537555
22
Y = 15583711
51 feet Y = 4749915
27 meter
Z = 13189107
01 Z = 4020039
82
XDOT = -20647
564385 XDOT = -6293
377624
YDOT = -150
426821 feet/sec YDOT = -45
850095 meter/sec
ZDOT = -12778
234581 ZDOT = -3894
805900
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 06263
27524283
00020000 00000-0 20000-3 0 9043
2 25544 51
6355 57
6335 0012175 3
3354 356
7889 15
75901127 8169
Satellite: ISS
Catalog Number: 25544
Epoch time: 06263
27524283 = yrday
fracday
Element set: 904
Inclination: 51
6355 deg
RA of node: 57
6335 deg
Eccentricity:
0012175
Arg of perigee: 3
3354 deg
Mean anomaly: 356
7889 deg
Mean motion: 15
75901127 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 816
Checksum: 294
Coasting Arc #6 (Orbit 831)
---------------------------------------
Vector Time (GMT): 2006/264/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 425763
92 A = 6720305
57 meter
Y = 5475297
65 meter E =
0016349
Z = 3854230
83 I = 51
88334
XDOT = -6025
416860 Wp = 50
55098
YDOT = -2451
218421 meter/sec RA = 52
14398 deg
ZDOT = 4146
398215 TA = 356
34883
MA = 356
36074
Ha = 190
450 n
mi
Hp = 178
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1396863
24 X = 345783
61
Y = 17963574
96 feet Y = 5479611
89 meter
Z = 12645114
27 Z = 3856104
48
XDOT = -19768
428020 XDOT = -6017
701603
YDOT = -8042
055186 feet/sec YDOT = -2518
554504 meter/sec
ZDOT = 13603
668683 ZDOT = 4117
145720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18000982
62 X = 5486699
50
Y = 640599
86 feet Y = 195254
84 meter
Z = 12652842
52 Z = 3856586
40
XDOT = -10112
366789 XDOT = -3082
249397
YDOT = 17534
647007 feet/sec YDOT = 5344
560408 meter/sec
ZDOT = 13494
354286 ZDOT = 4113
079186
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 06264
28985606
00020000 00000-0 20000-3 0 9056
2 25544 51
6361 52
4070 0012223 7
2242 352
9096 15
75889842 8323
Satellite: ISS
Catalog Number: 25544
Epoch time: 06264
28985606 = yrday
fracday
Element set: 905
Inclination: 51
6361 deg
RA of node: 52
4070 deg
Eccentricity:
0012223
Arg of perigee: 7
2242 deg
Mean anomaly: 352
9096 deg
Mean motion: 15
75889842 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 832
Checksum: 291
Coasting Arc #7 (Orbit 846)
---------------------------------------
Vector Time (GMT): 2006/265/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5490348
99 A = 6722558
12 meter
Y = 2290613
76 meter E =
0014741
Z = -3120755
26 I = 51
87279
XDOT = 291
491502 Wp = 25
73118
YDOT = 5942
767286 meter/sec RA = 46
95969 deg
ZDOT = 4896
332320 TA = 298
07340
MA = 298
22236
Ha = 190
568 n
mi
Hp = 178
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18012956
01 X = 5479487
10
Y = 7515136
99 feet Y = 2351948
88 meter
Z = -10238698
35 Z = -3094109
63
XDOT = 956
336950 XDOT = 201
231413
YDOT = 19497
267999 feet/sec YDOT = 5945
522653 meter/sec
ZDOT = 16064
082414 ZDOT = 4897
528642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9145474
24 X = 2787540
55
Y = -17301252
45 feet Y = -5273421
75 meter
Z = -10139121
10 Z = -3090404
11
XDOT = 18232
604793 XDOT = 5557
297941
YDOT = 262
462921 feet/sec YDOT = 79
998698 meter/sec
ZDOT = 16069
349332 ZDOT = 4897
937676
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 06265
24104401
00020000 00000-0 20000-3 0 9060
2 25544 51
6363 47
5078 0012282 9
7755 350
3646 15
75915295 8470
Satellite: ISS
Catalog Number: 25544
Epoch time: 06265
24104401 = yrday
fracday
Element set: 906
Inclination: 51
6363 deg
RA of node: 47
5078 deg
Eccentricity:
0012282
Arg of perigee: 9
7755 deg
Mean anomaly: 350
3646 deg
Mean motion: 15
75915295 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 847
Checksum: 292
Coasting Arc #8 (Orbit 862)
---------------------------------------
Vector Time (GMT): 2006/266/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4162
48 A = 6717345
63 meter
Y = -4883588
38 meter E =
0020212
Z = -4630630
30 I = 51
83514
XDOT = 6544
962635 Wp = 39
24938
YDOT = 2783
380720 meter/sec RA = 41
87082 deg
ZDOT = -2921
137681 TA = 201
81168
MA = 201
89786
Ha = 190
545 n
mi
Hp = 178
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13656
43 X = 81266
09
Y = -16022271
59 feet Y = -4883111
12 meter
Z = -15192356
62 Z = -4630422
37
XDOT = 21472
974524 XDOT = 6527
542532
YDOT = 9131
826508 feet/sec YDOT = 2856
472468 meter/sec
ZDOT = -9583
785042 ZDOT = -2889
384539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15969859
10 X = -4867613
05
Y = -1296286
54 feet Y = -395108
14 meter
Z = -15192245
21 Z = -4630596
34
XDOT = 10622
817785 XDOT = 3237
834861
YDOT = -19617
131380 feet/sec YDOT = -5979
301645 meter/sec
ZDOT = -9465
118399 ZDOT = -2884
968088
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 06266
25563377
00020000 00000-0 20000-3 0 9074
2 25544 51
6362 42
2815 0012301 13
2725 346
8760 15
75943146 8630
Satellite: ISS
Catalog Number: 25544
Epoch time: 06266
25563377 = yrday
fracday
Element set: 907
Inclination: 51
6362 deg
RA of node: 42
2815 deg
Eccentricity:
0012301
Arg of perigee: 13
2725 deg
Mean anomaly: 346
8760 deg
Mean motion: 15
75943146 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 863
Checksum: 286
Coasting Arc #9 (Orbit 878)
---------------------------------------
Vector Time (GMT): 2006/267/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5926785
94 A = 6725052
46 meter
Y = -2520633
88 meter E =
0017896
Z = 1934869
94 I = 51
83949
XDOT = 374
295228 Wp = 69
21972
YDOT = -5238
301048 meter/sec RA = 36
69470 deg
ZDOT = -5629
744734 TA = 89
31598
MA = 89
11092
Ha = 190
683 n
mi
Hp = 178
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19444835
77 X = -5907558
75
Y = -8269796
19 feet Y = -2586802
82 meter
Z = 6347998
51 Z = 1906124
15
XDOT = 1228
002718 XDOT = 460
191456
YDOT = -17186
027059 feet/sec YDOT = -5233
635647 meter/sec
ZDOT = -18470
291121 ZDOT = -5627
717324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9379645
01 X = -2858915
80
Y = 18970127
15 feet Y = 5782094
76 meter
Z = 6240575
89 Z = 1902127
53
XDOT = -15697
168358 XDOT = -4784
496916
YDOT = -1634
890591 feet/sec YDOT = -498
314652 meter/sec
ZDOT = -18463
445854 ZDOT = -5627
658296
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 06267
27021295
00020000 00000-0 20000-3 0 9086
2 25544 51
6366 37
0555 0012345 17
8052 342
3542 15
75953300 8797
Satellite: ISS
Catalog Number: 25544
Epoch time: 06267
27021295 = yrday
fracday
Element set: 908
Inclination: 51
6366 deg
RA of node: 37
0555 deg
Eccentricity:
0012345
Arg of perigee: 17
8052 deg
Mean anomaly: 342
3542 deg
Mean motion: 15
75953300 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 879
Checksum: 285
Coasting Arc #10 (Orbit 894)
---------------------------------------
Vector Time (GMT): 2006/268/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -697237
71 A = 6715207
93 meter
Y = 4292680
58 meter E =
0012080
Z = 5107815
07 I = 51
78271
XDOT = -6983
598514 Wp = 42
37134
YDOT = -2909
041159 meter/sec RA = 31
58562 deg
ZDOT = 1498
229573 TA = 33
35102
MA = 33
27498
Ha = 190
810 n
mi
Hp = 178
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2287525
28 X = -770000
49
Y = 14083597
71 feet Y = 4284477
19 meter
Z = 16757923
44 Z = 5104250
80
XDOT = -22912
068614 XDOT = -6957
828425
YDOT = -9544
098290 feet/sec YDOT = -2986
991438 meter/sec
ZDOT = 4915
451355 ZDOT = 1464
365484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13975467
36 X = 4259722
45
Y = 2948281
02 feet Y = 898636
05 meter
Z = 16745221
57 Z = 5103943
54
XDOT = -10250
281852 XDOT = -3124
285908
YDOT = 21514
394388 feet/sec YDOT = 6557
587409 meter/sec
ZDOT = 4788
915537 ZDOT = 1459
661456
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 06268
28477926
00020000 00000-0 20000-3 0 9095
2 25544 51
6363 31
8290 0012390 21
2898 338
8779 15
75960599 8957
Satellite: ISS
Catalog Number: 25544
Epoch time: 06268
28477926 = yrday
fracday
Element set: 909
Inclination: 51
6363 deg
RA of node: 31
8290 deg
Eccentricity:
0012390
Arg of perigee: 21
2898 deg
Mean anomaly: 338
8779 deg
Mean motion: 15
75960599 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 895
Checksum: 344
Coasting Arc #11 (Orbit 909)
---------------------------------------
Vector Time (GMT): 2006/269/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6196401
74 A = 6726369
50 meter
Y = 2500152
00 meter E =
0023063
Z = -659149
31 I = 51
79491
XDOT = -1253
497896 Wp = 31
30121
YDOT = 4662
477637 meter/sec RA = 26
42642 deg
ZDOT = 6013
656567 TA = 321
52193
MA = 321
68615
Ha = 190
839 n
mi
Hp = 177
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20329402
03 X = 6171186
25
Y = 8202598
42 feet Y = 2569302
58 meter
Z = -2162563
35 Z = -629108
00
XDOT = -4112
525907 XDOT = -1334
755003
YDOT = 15296
842642 feet/sec YDOT = 4648
006287 meter/sec
ZDOT = 19729
844380 ZDOT = 6007
369361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8674412
62 X = 2643960
97
Y = -20144344
51 feet Y = -6139996
21 meter
Z = -2050326
28 Z = -624939
45
XDOT = 13725
139409 XDOT = 4183
422492
YDOT = 3944
036297 feet/sec YDOT = 1202
142263 meter/sec
ZDOT = 19707
043963 ZDOT = 6006
707000
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 06269
23592359
00020000 00000-0 20000-3 0 9101
2 25544 51
6356 26
9292 0012429 24
1096 336
0647 15
75984161 9104
Satellite: ISS
Catalog Number: 25544
Epoch time: 06269
23592359 = yrday
fracday
Element set: 910
Inclination: 51
6356 deg
RA of node: 26
9292 deg
Eccentricity:
0012429
Arg of perigee: 24
1096 deg
Mean anomaly: 336
0647 deg
Mean motion: 15
75984161 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 910
Checksum: 297
Coasting Arc #12 (Orbit 925)
---------------------------------------
Vector Time (GMT): 2006/270/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1545000
32 A = 6714356
63 meter
Y = -3870635
82 meter E =
0023530
Z = -5282153
30 I = 51
72766
XDOT = 7153
370426 Wp = 62
28971
YDOT = 2819
096720 meter/sec RA = 21
28921 deg
ZDOT = 37
396366 TA = 208
00183
MA = 208
12862
Ha = 190
836 n
mi
Hp = 177
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5068898
68 X = 1613827
70
Y = -12698936
42 feet Y = -3852974
08 meter
Z = -17329899
27 Z = -5274480
26
XDOT = 23469
063078 XDOT = 7121
133573
YDOT = 9249
004988 feet/sec YDOT = 2898
909425 meter/sec
ZDOT = 122
691488 ZDOT = 72
069709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12666981
34 X = -3860895
91
Y = -5241802
58 feet Y = -1597701
43 meter
Z = -17301827
02 Z = -5273596
88
XDOT = 9009
827165 XDOT = 2746
195320
YDOT = -22487
450893 feet/sec YDOT = -6854
175032 meter/sec
ZDOT = 252
223075 ZDOT = 76
877593
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 06270
25046655
00020000 00000-0 20000-3 0 9119
2 25544 51
6346 21
7021 0012410 28
1296 332
0536 15
76021086 9261
Satellite: ISS
Catalog Number: 25544
Epoch time: 06270
25046655 = yrday
fracday
Element set: 911
Inclination: 51
6346 deg
RA of node: 21
7021 deg
Eccentricity:
0012410
Arg of perigee: 28
1296 deg
Mean anomaly: 332
0536 deg
Mean motion: 15
76021086 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 926
Checksum: 252
Coasting Arc #13 (Orbit 941)
---------------------------------------
Vector Time (GMT): 2006/271/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6236813
19 A = 6726151
94 meter
Y = -2415157
78 meter E =
0013401
Z = -741419
02 I = 51
74080
XDOT = 2340
540158 Wp = 79
03266
YDOT = -4234
485579 meter/sec RA = 16
15326 deg
ZDOT = -5983
371659 TA = 109
03367
MA = 108
88846
Ha = 190
903 n
mi
Hp = 177
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20461985
52 X = -6205741
28
Y = -7923745
98 feet Y = -2484727
55 meter
Z = -2432477
11 Z = -771642
48
XDOT = 7678
937526 XDOT = 2416
783441
YDOT = -13892
669222 feet/sec YDOT = -4207
886111 meter/sec
ZDOT = -19630
484446 ZDOT = -5971
815891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7696284
79 X = -2345827
60
Y = 20534940
71 feet Y = 6259049
93 meter
Z = -2545379
53 Z = -775831
68
XDOT = -12480
586567 XDOT = -3804
082786
YDOT = -7071
198623 feet/sec YDOT = -2155
301340 meter/sec
ZDOT = -19587
991876 ZDOT = -5970
419924
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 06271
26499770
00020000 00000-0 20000-3 0 9122
2 25544 51
6347 16
4762 0012412 31
8731 328
3182 15
76024350 9422
Satellite: ISS
Catalog Number: 25544
Epoch time: 06271
26499770 = yrday
fracday
Element set: 912
Inclination: 51
6347 deg
RA of node: 16
4762 deg
Eccentricity:
0012412
Arg of perigee: 31
8731 deg
Mean anomaly: 328
3182 deg
Mean motion: 15
76024350 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 942
Checksum: 276
Coasting Arc #14 (Orbit 957)
---------------------------------------
Vector Time (GMT): 2006/272/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2540460
77 A = 6715207
31 meter
Y = 3588540
42 meter E =
0017273
Z = 5069172
58 I = 51
67577
XDOT = -7047
007092 Wp = 40
60944
YDOT = -2674
306822 meter/sec RA = 10
98486 deg
ZDOT = -1622
518525 TA = 65
04009
MA = 64
86074
Ha = 191
017 n
mi
Hp = 177
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8334845
04 X = -2605024
97
Y = 11773426
58 feet Y = 3559770
56 meter
Z = 16631143
62 Z = 5056674
04
XDOT = -23120
102007 XDOT = -7008
696863
YDOT = -8773
972513 feet/sec YDOT = -2752
896144 meter/sec
ZDOT = -5323
223507 ZDOT = -1656
660316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12006971
87 X = 3659725
03
Y = 8089924
17 feet Y = 2465808
89 meter
Z = 16585050
70 Z = 5055123
45
XDOT = -7527
080660 XDOT = -2294
254185
YDOT = 22453
857871 feet/sec YDOT = 6843
935879 meter/sec
ZDOT = -5450
758736 ZDOT = -1661
391263
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 06272
27951611
00020000 00000-0 20000-3 0 9132
2 25544 51
6342 11
2487 0012371 35
6426 324
5562 15
76041283 9582
Satellite: ISS
Catalog Number: 25544
Epoch time: 06272
27951611 = yrday
fracday
Element set: 913
Inclination: 51
6342 deg
RA of node: 11
2487 deg
Eccentricity:
0012371
Arg of perigee: 35
6426 deg
Mean anomaly: 324
5562 deg
Mean motion: 15
76041283 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 958
Checksum: 276
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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