Date:
February 22nd 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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
059/05:22:06
066 -8
1 10
5 10
5
N/A -6
6 0
0 187
2
000/00:02:12
132 -0
8 0
0 181
4
Coasting Arc #1 (Orbit 995)
---------------------------------------
Vector Time (GMT): 2008/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4198937
52 A = 6712234
26 meter
Y = -1993037
06 meter E =
0017885
Z = -4857756
54 I = 51
30100
XDOT = 844
187665 Wp = 87
93379
YDOT = -7301
270254 meter/sec RA = 262
24632 deg
ZDOT = 2273
705435 TA = 204
27563
MA = 204
36000
Ha = 187
383 n
mi
Hp = 176
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13776041
75 X = -4152741
65
Y = -6538835
49 feet Y = -2039733
85 meter
Z = -15937521
46 Z = -4878042
05
XDOT = 2769
644569 XDOT = 914
723955
YDOT = -23954
298734 feet/sec YDOT = -7291
435598 meter/sec
ZDOT = 7459
663501 ZDOT = 2277
977952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8376170
32 X = -2553056
71
Y = -12644671
92 feet Y = -3854096
00 meter
Z = -16015377
88 Z = -4881487
18
XDOT = 13733
163809 XDOT = 4185
868329
YDOT = -18532
651190 feet/sec YDOT = -5648
752083 meter/sec
ZDOT = 7475
193129 ZDOT = 2278
438866
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 08051
51195489
00020000 00000-0 20000-3 0 9005
2 25544 51
6375 262
9825 0007342 55
1747 305
0107 15
77367736 9960
Satellite: ISS
Catalog Number: 25544
Epoch time: 08051
51195489 = yrday
fracday
Element set: 900
Inclination: 51
6375 deg
RA of node: 262
9825 deg
Eccentricity:
0007342
Arg of perigee: 55
1747 deg
Mean anomaly: 305
0107 deg
Mean motion: 15
77367736 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 996
Checksum: 307
Coasting Arc #2 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2008/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1108538
70 A = 6718611
55 meter
Y = 5914905
81 meter E =
0010760
Z = -2999353
23 I = 51
32712
XDOT = -4829
708692 Wp = 77
56646
YDOT = -3400
673037 meter/sec RA = 257
10476 deg
ZDOT = -4933
913696 TA = 137
27834
MA = 137
19464
Ha = 187
398 n
mi
Hp = 176
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3636937
98 X = -1160027
80
Y = 19405858
94 feet Y = 5902221
43 meter
Z = -9840397
75 Z = -3004863
77
XDOT = -15845
500957 XDOT = -4767
355509
YDOT = -11157
063769 feet/sec YDOT = -3454
333247 meter/sec
ZDOT = -16187
380891 ZDOT = -4957
224099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12792395
45 X = -3899122
13
Y = 15025548
99 feet Y = 4579787
33 meter
Z = -9860811
49 Z = -3005575
34
XDOT = -6982
566178 XDOT = -2128
286171
YDOT = -16599
793919 feet/sec YDOT = -5059
617186 meter/sec
ZDOT = -16276
980274 ZDOT = -4961
223588
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 08052
52561237
00020000 00000-0 20000-3 0 9016
2 25544 51
6366 257
7506 0007315 58
5858 301
6022 15
77387738 10120
Satellite: ISS
Catalog Number: 25544
Epoch time: 08052
52561237 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 257
7506 deg
Eccentricity:
0007315
Arg of perigee: 58
5858 deg
Mean anomaly: 301
6022 deg
Mean motion: 15
77387738 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1012
Checksum: 288
Coasting Arc #3 (Orbit 1027)
---------------------------------------
Vector Time (GMT): 2008/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4233055
88 A = 6716801
82 meter
Y = 3815590
21 meter E =
0018902
Z = 3543038
64 I = 51
32993
XDOT = -1742
347253 Wp = 77
19078
YDOT = 6067
151928 meter/sec RA = 251
86870 deg
ZDOT = -4428
253232 TA = 60
25807
MA = 60
07013
Ha = 187
222 n
mi
Hp = 176
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13887978
62 X = 4172863
72
Y = 12518340
57 feet Y = 3862590
36 meter
Z = 11624142
51 Z = 3563455
85
XDOT = -5716
362379 XDOT = -1788
550445
YDOT = 19905
354095 feet/sec YDOT = 6047
409346 meter/sec
ZDOT = -14528
389868 ZDOT = -4436
830023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6029374
45 X = 1837753
33
Y = 17646483
82 feet Y = 5378648
27 meter
Z = 11702723
72 Z = 3566990
19
XDOT = -13283
138820 XDOT = -4048
700712
YDOT = 14246
457857 feet/sec YDOT = 4342
320355 meter/sec
ZDOT = -14560
513026 ZDOT = -4438
044370
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 08053
53924812
00020000 00000-0 20000-3 0 9021
2 25544 51
6370 252
5172 0007213 61
1900 298
9989 15
77456814 10281
Satellite: ISS
Catalog Number: 25544
Epoch time: 08053
53924812 = yrday
fracday
Element set: 902
Inclination: 51
6370 deg
RA of node: 252
5172 deg
Eccentricity:
0007213
Arg of perigee: 61
1900 deg
Mean anomaly: 298
9989 deg
Mean motion: 15
77456814 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1028
Checksum: 294
Coasting Arc #4 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2008/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1999228
39 A = 6713407
62 meter
Y = -4523776
75 meter E =
0014507
Z = 4527449
73 I = 51
32734
XDOT = 4857
234238 Wp = 92
12288
YDOT = 5177
651099 meter/sec RA = 246
73267 deg
ZDOT = 3019
760534 TA = 327
74340
MA = 327
83204
Ha = 187
331 n
mi
Hp = 176
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6559148
25 X = 2027672
25
Y = -14841787
25 feet Y = -4501260
85 meter
Z = 14853837
68 Z = 4537231
24
XDOT = 15935
807869 XDOT = 4784
306769
YDOT = 16987
044289 feet/sec YDOT = 5231
559943 meter/sec
ZDOT = 9907
350833 ZDOT = 3043
178986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12681857
55 X = 3865430
18
Y = -10068452
74 feet Y = -3068864
40 meter
Z = 14890746
01 Z = 4538699
38
XDOT = 5317
993619 XDOT = 1620
924455
YDOT = 21527
050588 feet/sec YDOT = 6561
445019 meter/sec
ZDOT = 9997
582659 ZDOT = 3047
263194
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 08054
55286693
00020000 00000-0 20000-3 0 9033
2 25544 51
6359 247
2838 0007313 65
6091 294
5837 15
77432225 10441
Satellite: ISS
Catalog Number: 25544
Epoch time: 08054
55286693 = yrday
fracday
Element set: 903
Inclination: 51
6359 deg
RA of node: 247
2838 deg
Eccentricity:
0007313
Arg of perigee: 65
6091 deg
Mean anomaly: 294
5837 deg
Mean motion: 15
77432225 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1044
Checksum: 306
Coasting Arc #5 (Orbit 1058)
---------------------------------------
Vector Time (GMT): 2008/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4163251
41 A = 6721163
37 meter
Y = -5031428
09 meter E =
0014681
Z = -1575389
18 I = 51
36659
XDOT = 2936
138960 Wp = 53
11437
YDOT = -4213
618981 meter/sec RA = 241
51050 deg
ZDOT = 5743
513663 TA = 289
41571
MA = 289
57432
Ha = 187
292 n
mi
Hp = 175
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13658961
30 X = -4099026
93
Y = -16507310
00 feet Y = -5077624
96 meter
Z = -5168599
67 Z = -1595457
59
XDOT = 9633
001837 XDOT = 2955
137524
YDOT = -13824
209255 feet/sec YDOT = -4180
678749 meter/sec
ZDOT = 18843
548764 ZDOT = 5757
823679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4650523
77 X = -1417479
65
Y = -20895575
16 feet Y = -6368971
31 meter
Z = -5245998
19 Z = -1598980
25
XDOT = 13239
803271 XDOT = 4035
492037
YDOT = -7654
200183 feet/sec YDOT = -2333
000216 meter/sec
ZDOT = 18897
823331 ZDOT = 5760
056551
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 08055
50311305
00020000 00000-0 20000-3 0 9049
2 25544 51
6355 242
3774 0007264 70
2436 289
9511 15
77481597 10591
Satellite: ISS
Catalog Number: 25544
Epoch time: 08055
50311305 = yrday
fracday
Element set: 904
Inclination: 51
6355 deg
RA of node: 242
3774 deg
Eccentricity:
0007264
Arg of perigee: 70
2436 deg
Mean anomaly: 289
9511 deg
Mean motion: 15
77481597 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1059
Checksum: 292
Coasting Arc #6 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2008/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3198507
81 A = 6710185
22 meter
Y = 2753166
50 meter E =
0022229
Z = -5236059
76 I = 51
34473
XDOT = -4557
215884 Wp = 82
52251
YDOT = -6177
105862 meter/sec RA = 236
34678 deg
ZDOT = -462
978212 TA = 183
04918
MA = 183
06275
Ha = 187
340 n
mi
Hp = 175
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10493792
02 X = -3203620
87
Y = 9032698
48 feet Y = 2717370
05 meter
Z = -17178673
75 Z = -5251610
53
XDOT = -14951
495681 XDOT = -4485
554790
YDOT = -20266
095348 feet/sec YDOT = -6227
666600 meter/sec
ZDOT = -1518
957388 ZDOT = -484
942483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13304526
22 X = -4055219
59
Y = 3558311
22 feet Y = 1084573
26 meter
Z = -17237869
59 Z = -5254102
65
XDOT = -4281
495676 XDOT = -1304
999882
YDOT = -23796
260263 feet/sec YDOT = -7253
100128 meter/sec
ZDOT = -1603
751505 ZDOT = -488
823459
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 08056
51668973
00020000 00000-0 20000-3 0 9058
2 25544 51
6354 237
1443 0007380 74
4476 285
7503 15
77516422 10753
Satellite: ISS
Catalog Number: 25544
Epoch time: 08056
51668973 = yrday
fracday
Element set: 905
Inclination: 51
6354 deg
RA of node: 237
1443 deg
Eccentricity:
0007380
Arg of perigee: 74
4476 deg
Mean anomaly: 285
7503 deg
Mean motion: 15
77516422 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1075
Checksum: 303
Coasting Arc #7 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2008/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3667009
15 A = 6721707
24 meter
Y = 5572945
86 meter E =
0015174
Z = -799091
80 I = 51
40212
XDOT = -4429
284819 Wp = 114
81386
YDOT = 2074
549150 meter/sec RA = 231
16835 deg
ZDOT = -5952
163510 TA = 73
93921
MA = 73
77217
Ha = 187
243 n
mi
Hp = 175
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12030869
92 X = 3608300
88
Y = 18283943
10 feet Y = 5613624
16 meter
Z = -2621692
27 Z = -781420
48
XDOT = -14531
774339 XDOT = -4423
239282
YDOT = 6806
263615 feet/sec YDOT = 2025
051907 meter/sec
ZDOT = -19528
095504 ZDOT = -5973
666182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3179745
57 X = 969186
45
Y = 21663034
50 feet Y = 6602892
92 meter
Z = -2553396
01 Z = -778275
10
XDOT = -14366
514729 XDOT = -4378
913689
YDOT = -165
190369 feet/sec YDOT = -50
350024 meter/sec
ZDOT = -19610
155615 ZDOT = -5977
175432
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 08057
53024350
00020000 00000-0 20000-3 0 9067
2 25544 51
6358 231
9110 0007388 76
0588 284
1398 15
77592277 10915
Satellite: ISS
Catalog Number: 25544
Epoch time: 08057
53024350 = yrday
fracday
Element set: 906
Inclination: 51
6358 deg
RA of node: 231
9110 deg
Eccentricity:
0007388
Arg of perigee: 76
0588 deg
Mean anomaly: 284
1398 deg
Mean motion: 15
77592277 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1091
Checksum: 304
Coasting Arc #8 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2008/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4522519
98 A = 6711599
20 meter
Y = -912603
69 meter E =
0013512
Z = 4864959
55 I = 51
38655
XDOT = 3700
251503 Wp = 70
64066
YDOT = 6390
551028 meter/sec RA = 225
96175 deg
ZDOT = -2231
568463 TA = 41
13905
MA = 41
03726
Ha = 187
187 n
mi
Hp = 175
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14837663
98 X = 4508755
84
Y = -2994106
58 feet Y = -862107
13 meter
Z = 15961153
38 Z = 4886896
35
XDOT = 12139
932753 XDOT = 3639
356825
YDOT = 20966
374763 feet/sec YDOT = 6431
588814 meter/sec
ZDOT = -7321
418843 ZDOT = -2213
740873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14687473
24 X = 4476741
84
Y = 3273361
95 feet Y = 997720
72 meter
Z = 16045017
76 Z = 4890521
41
XDOT = 2821
737769 XDOT = 860
065672
YDOT = 23039
142061 feet/sec YDOT = 7022
330500 meter/sec
ZDOT = -7252
423008 ZDOT = -2210
538533
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 08058
54377851
00020000 00000-0 20000-3 0 9077
2 25544 51
6353 226
6776 0007373 81
9549 278
2453 15
77556009 11072
Satellite: ISS
Catalog Number: 25544
Epoch time: 08058
54377851 = yrday
fracday
Element set: 907
Inclination: 51
6353 deg
RA of node: 226
6776 deg
Eccentricity:
0007373
Arg of perigee: 81
9549 deg
Mean anomaly: 278
2453 deg
Mean motion: 15
77556009 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1107
Checksum: 321
Coasting Arc #9 (Orbit 1117)
---------------------------------------
Vector Time (GMT): 2008/059/05:23:12
132
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2720713
69 A = 6715378
47 meter
Y = 3195371
03 meter E =
0014144
Z = -5254641
99 I = 51
40065
XDOT = -5759
060096 Wp = 87
74301
YDOT = -5099
785416 meter/sec RA = 222
23346 deg
ZDOT = -119
041277 TA = 181
12096
MA = 181
12413
Ha = 187
216 n
mi
Hp = 181
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8926226
03 X = -2730716
76
Y = 10483500
74 feet Y = 3164890
45 meter
Z = -17239639
08 Z = -5267883
43
XDOT = -18894
554121 XDOT = -5701
027207
YDOT = -16731
579448 feet/sec YDOT = -5163
862033 meter/sec
ZDOT = -390
555372 ZDOT = -146
877496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4092215
39 X = -1247307
25
Y = -13080435
18 feet Y = -3986916
64 meter
Z = -17289952
09 Z = -5269977
40
XDOT = 23311
322655 XDOT = 7105
291145
YDOT = -6633
877650 feet/sec YDOT = -2022
005908 meter/sec
ZDOT = -497
717722 ZDOT = -151
704362
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 08059
24057411
00020000 00000-0 20000-3 0 9083
2 25544 51
6397 223
0849 0000978 289
2427 70
8631 15
75661683 11183
Satellite: ISS
Catalog Number: 25544
Epoch time: 08059
24057411 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 223
0849 deg
Eccentricity:
0000978
Arg of perigee: 289
2427 deg
Mean anomaly: 70
8631 deg
Mean motion: 15
75661683 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1118
Checksum: 308
Coasting Arc #10 (Orbit 1133)
---------------------------------------
Vector Time (GMT): 2008/060/05:23:12
132
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5113200
56 A = 6727411
00 meter
Y = 4338051
03 meter E =
0010429
Z = -475464
66 I = 51
46353
XDOT = -3432
865829 Wp = 141
68062
YDOT = 3397
075767 meter/sec RA = 217
07381 deg
ZDOT = -6001
274659 TA = 43
50727
MA = 43
42504
Ha = 187
230 n
mi
Hp = 181
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16775592
40 X = 5066621
48
Y = 14232450
90 feet Y = 4394969
32 meter
Z = -1559923
41 Z = -450738
16
XDOT = -11262
683167 XDOT = -3441
444539
YDOT = 11145
261703 feet/sec YDOT = 3358
639523 meter/sec
ZDOT = -19689
221323 ZDOT = -6017
972179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20909766
53 X = -6373296
84
Y = 6859497
35 feet Y = 2090774
79 meter
Z = -1464745
61 Z = -446454
46
XDOT = -3165
479744 XDOT = -964
838226
YDOT = -13808
928075 feet/sec YDOT = -4208
961277 meter/sec
ZDOT = -19752
746153 ZDOT = -6020
637027
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 08060
25533551
00020000 00000-0 20000-3 0 9091
2 25544 51
6396 217
8607 0001030 287
5598 72
5453 15
75646244 11340
Satellite: ISS
Catalog Number: 25544
Epoch time: 08060
25533551 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 217
8607 deg
Eccentricity:
0001030
Arg of perigee: 287
5598 deg
Mean anomaly: 72
5453 deg
Mean motion: 15
75646244 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1134
Checksum: 293
Coasting Arc #11 (Orbit 1149)
---------------------------------------
Vector Time (GMT): 2008/061/05:23:12
132
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3300763
50 A = 6715568
59 meter
Y = -2776058
29 meter E =
0003589
Z = 5146168
91 I = 51
44860
XDOT = 5907
698929 Wp = 37
60526
YDOT = 4800
073897 meter/sec RA = 211
89766 deg
ZDOT = -1196
611147 TA = 63
86679
MA = 63
82987
Ha = 186
941 n
mi
Hp = 181
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10829276
58 X = 3306561
69
Y = -9107802
77 feet Y = -2739114
86 meter
Z = 16883756
27 Z = 5162217
87
XDOT = 19382
214335 XDOT = 5859
397528
YDOT = 15748
273939 feet/sec YDOT = 4865
867091 meter/sec
ZDOT = -3925
889589 ZDOT = -1168
029262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2386602
03 X = 727436
30
Y = 13873060
38 feet Y = 4228508
80 meter
Z = 16944876
96 Z = 5164798
50
XDOT = -22414
305856 XDOT = -6831
880425
YDOT = 8529
706166 feet/sec YDOT = 2599
854439 meter/sec
ZDOT = -3815
883547 ZDOT = -1163
081305
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 08061
27007469
00020000 00000-0 20000-3 0 9100
2 25544 51
6395 212
6362 0001250 300
4534 59
6506 15
75747672 11509
Satellite: ISS
Catalog Number: 25544
Epoch time: 08061
27007469 = yrday
fracday
Element set: 910
Inclination: 51
6395 deg
RA of node: 212
6362 deg
Eccentricity:
0001250
Arg of perigee: 300
4534 deg
Mean anomaly: 59
6506 deg
Mean motion: 15
75747672 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1150
Checksum: 271
Coasting Arc #12 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2008/062/05:23:12
132
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5136371
09 A = 6726175
46 meter
Y = -4022345
04 meter E =
0013664
Z = 1608001
21 I = 51
50949
XDOT = 4165
240951 Wp = 58
18607
YDOT = -3012
314429 meter/sec RA = 206
76227 deg
ZDOT = 5741
204346 TA = 319
61734
MA = 319
71870
Ha = 187
128 n
mi
Hp = 181
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16851611
20 X = -5098822
11
Y = -13196670
07 feet Y = -4079572
92 meter
Z = 5275594
54 Z = 1583140
37
XDOT = 13665
488686 XDOT = 4170
726307
YDOT = -9882
921356 feet/sec YDOT = -2965
705665 meter/sec
ZDOT = 18835
972264 ZDOT = 5761
452050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19808484
84 X = 6037626
18
Y = -8170263
55 feet Y = -2490296
33 meter
Z = 5179915
13 Z = 1578838
13
XDOT = 1309
138467 XDOT = 399
025405
YDOT = 15225
145268 feet/sec YDOT = 4640
624278 meter/sec
ZDOT = 18913
148230 ZDOT = 5764
727580
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 08062
28479748
00020000 00000-0 20000-3 0 9116
2 25544 51
6395 207
4112 0001291 310
6814 49
4238 15
75732548 11665
Satellite: ISS
Catalog Number: 25544
Epoch time: 08062
28479748 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 207
4112 deg
Eccentricity:
0001291
Arg of perigee: 310
6814 deg
Mean anomaly: 49
4238 deg
Mean motion: 15
75732548 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1166
Checksum: 293
Coasting Arc #13 (Orbit 1180)
---------------------------------------
Vector Time (GMT): 2008/063/05:23:12
132
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3985379
17 A = 6717032
55 meter
Y = 2522699
03 meter E =
0010656
Z = -4792300
76 I = 51
50590
XDOT = -5788
154238 Wp = 104
89520
YDOT = -4417
464137 meter/sec RA = 201
56907 deg
ZDOT = 2490
073542 TA = 189
51557
MA = 189
53577
Ha = 187
016 n
mi
Hp = 181
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13075390
96 X = -3990012
54
Y = 8276571
61 feet Y = 2478106
29 meter
Z = -15722771
52 Z = -4811672
60
XDOT = -18990
007344 XDOT = -5750
423358
YDOT = -14492
992577 feet/sec YDOT = -4481
979592 meter/sec
ZDOT = 8169
532619 ZDOT = 2462
046970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1054697
54 X = -321471
81
Y = -15363145
46 feet Y = -4682686
74 meter
Z = -15796658
04 Z = -4814821
37
XDOT = 20713
991777 XDOT = 6313
624694
YDOT = -9704
795917 feet/sec YDOT = -2958
021795 meter/sec
ZDOT = 8061
667865 ZDOT = 2457
196365
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 08063
23608002
00020000 00000-0 20000-3 0 9120
2 25544 51
6395 202
5129 0001396 312
3439 47
7607 15
75778809 11815
Satellite: ISS
Catalog Number: 25544
Epoch time: 08063
23608002 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 202
5129 deg
Eccentricity:
0001396
Arg of perigee: 312
3439 deg
Mean anomaly: 47
7607 deg
Mean motion: 15
75778809 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1181
Checksum: 287
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 may contain past, current and future orbital data 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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