Date:
August 7th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7319 46 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
112 4
0 10
6 10
6
N/A 9
1 0
1 195
6
000/00:18:52
224 -3
6 -0
2 188
8
Coasting Arc #1 (Orbit 3645)
---------------------------------------
Vector Time (GMT): 2008/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4544688
92 A = 6724983
70 meter
Y = 409657
52 meter E =
0012437
Z = 4928590
01 I = 51
91811
XDOT = 1733
387990 Wp = 67
33987
YDOT = -7182
849861 meter/sec RA = 117
03240 deg
ZDOT = 2195
727497 TA = 1
44602
MA = 1
44243
Ha = 195
271 n
mi
Hp = 182
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14910396
71 X = -4572874
01
Y = 1344020
74 feet Y = 358678
43 meter
Z = 16169914
72 Z = 4906443
64
XDOT = 5686
968470 XDOT = 1802
912572
YDOT = -23565
780384 feet/sec YDOT = -7163
077469 meter/sec
ZDOT = 7203
830371 ZDOT = 2204
316838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11498362
12 X = 3504700
77
Y = 9729963
69 feet Y = 2965692
93 meter
Z = 16084400
48 Z = 4902525
27
XDOT = -20024
750608 XDOT = -6103
543985
YDOT = 11703
796784 feet/sec YDOT = 3567
317260 meter/sec
ZDOT = 7236
314796 ZDOT = 2205
628750
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
55146591
00020000 00000-0 20000-3 0 9005
2 25544 51
6414 117
6193 0010284 36
3001 323
8858 15
72847723 36461
Satellite: ISS
Catalog Number: 25544
Epoch time: 08219
55146591 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 117
6193 deg
Eccentricity:
0010284
Arg of perigee: 36
3001 deg
Mean anomaly: 323
8858 deg
Mean motion: 15
72847723 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3646
Checksum: 288
Coasting Arc #2 (Orbit 3660)
---------------------------------------
Vector Time (GMT): 2008/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -616800
66 A = 6733149
33 meter
Y = 6303533
60 meter E =
0016198
Z = -2271943
44 I = 51
95850
XDOT = -5206
798728 Wp = 41
17785
YDOT = 1454
112238 meter/sec RA = 111
88904 deg
ZDOT = 5481
890614 TA = 293
43579
MA = 293
60601
Ha = 195
167 n
mi
Hp = 182
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2023624
21 X = -676205
31
Y = 20680884
51 feet Y = 6296304
14 meter
Z = -7453882
68 Z = -2275083
82
XDOT = -17082
672992 XDOT = -5249
301750
YDOT = 4770
709441 feet/sec YDOT = 1395
648902 meter/sec
ZDOT = 17985
205425 ZDOT = 5456
492956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15878417
20 X = 4839741
56
Y = -13397683
15 feet Y = -4083613
82 meter
Z = -7465410
90 Z = -2275457
24
XDOT = 14643
560575 XDOT = 4463
357263
YDOT = 7449
741824 feet/sec YDOT = 2270
681308 meter/sec
ZDOT = 17887
226170 ZDOT = 5452
026537
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
50450848
00020000 00000-0 20000-3 0 9016
2 25544 51
6419 112
7333 0010295 39
3582 320
8327 15
72866195 36616
Satellite: ISS
Catalog Number: 25544
Epoch time: 08220
50450848 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 112
7333 deg
Eccentricity:
0010295
Arg of perigee: 39
3582 deg
Mean anomaly: 320
8327 deg
Mean motion: 15
72866195 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3661
Checksum: 284
Coasting Arc #3 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2008/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4423429
31 A = 6726159
28 meter
Y = -2087425
45 meter E =
0020196
Z = -4636758
48 I = 51
94486
XDOT = 261
261418 Wp = 56
50518
YDOT = 7092
253618 meter/sec RA = 106
82583 deg
ZDOT = -2941
896344 TA = 184
38775
MA = 184
40549
Ha = 195
179 n
mi
Hp = 182
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14512563
36 X = 4468966
91
Y = -6848508
70 feet Y = -2037705
20 meter
Z = -15212462
19 Z = -4615159
08
XDOT = 857
156883 XDOT = 196
226424
YDOT = 23268
548614 feet/sec YDOT = 7094
811757 meter/sec
ZDOT = -9651
890892 ZDOT = -2940
784645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15314261
42 X = -4667786
88
Y = -5051333
67 feet Y = -1539646
50 meter
Z = -15129210
10 Z = -4611383
24
XDOT = 14952
078688 XDOT = 4557
393584
YDOT = -16420
095728 feet/sec YDOT = -5004
845178 meter/sec
ZDOT = -9646
926021 ZDOT = -2940
383051
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
52107683
00020000 00000-0 20000-3 0 9026
2 25544 51
6420 107
5214 0010288 42
4560 317
7397 15
72884752 36779
Satellite: ISS
Catalog Number: 25544
Epoch time: 08221
52107683 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 107
5214 deg
Eccentricity:
0010288
Arg of perigee: 42
4560 deg
Mean anomaly: 317
7397 deg
Mean motion: 15
72884752 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3677
Checksum: 287
Coasting Arc #4 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2008/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1051061
76 A = 6731803
62 meter
Y = -5994016
38 meter E =
0021411
Z = 2867071
97 I = 51
97112
XDOT = 4747
664510 Wp = 76
42723
YDOT = -3286
724109 meter/sec RA = 101
67566 deg
ZDOT = -5094
365045 TA = 70
81625
MA = 70
58464
Ha = 195
281 n
mi
Hp = 182
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3448365
35 X = -997885
24
Y = -19665408
06 feet Y = -6005472
86 meter
Z = 9406404
10 Z = 2862094
61
XDOT = 15576
327134 XDOT = 4808
811708
YDOT = -10783
215582 feet/sec YDOT = -3233
290689 meter/sec
ZDOT = -16713
796081 ZDOT = -5071
152746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10674461
25 X = -3253575
79
Y = 16883342
99 feet Y = 5146042
94 meter
Z = 9386615
08 Z = 2861040
28
XDOT = -17612
817095 XDOT = -5368
386651
YDOT = -1826
273173 feet/sec YDOT = -556
648063 meter/sec
ZDOT = -16624
415532 ZDOT = -5067
121854
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
53763634
00020000 00000-0 20000-3 0 9033
2 25544 51
6419 102
3094 0010353 46
6943 313
5081 15
72885606 36931
Satellite: ISS
Catalog Number: 25544
Epoch time: 08222
53763634 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 102
3094 deg
Eccentricity:
0010353
Arg of perigee: 46
6943 deg
Mean anomaly: 313
5081 deg
Mean motion: 15
72885606 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3693
Checksum: 286
Coasting Arc #5 (Orbit 3708)
---------------------------------------
Vector Time (GMT): 2008/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3754653
51 A = 6727620
59 meter
Y = 3617687
24 meter E =
0017981
Z = 4234127
73 I = 51
96189
XDOT = -2114
344993 Wp = 77
74157
YDOT = -6461
253029 meter/sec RA = 96
61939 deg
ZDOT = 3636
522458 TA = 335
42677
MA = 335
51235
Ha = 195
426 n
mi
Hp = 182
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12318417
04 X = -3815396
50
Y = 11869052
63 feet Y = 3575360
52 meter
Z = 13891495
18 Z = 4215740
54
XDOT = -6936
827406 XDOT = -2059
602536
YDOT = -21198
336708 feet/sec YDOT = -6484
591110 meter/sec
ZDOT = 11930
847959 ZDOT = 3626
383400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17148982
79 X = 5227009
95
Y = -699934
59 feet Y = -213340
06 meter
Z = 13820778
85 Z = 4212573
39
XDOT = -8820
631143 XDOT = -2688
528372
YDOT = 19280
690213 feet/sec YDOT = 5876
754377 meter/sec
ZDOT = 11891
077287 ZDOT = 3624
400357
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
55418500
00020000 00000-0 20000-3 0 9046
2 25544 51
6421 97
0973 0010360 49
8974 310
3095 15
72885939 37094
Satellite: ISS
Catalog Number: 25544
Epoch time: 08223
55418500 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 97
0973 deg
Eccentricity:
0010360
Arg of perigee: 49
8974 deg
Mean anomaly: 310
3095 deg
Mean motion: 15
72885939 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3709
Checksum: 302
Coasting Arc #6 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2008/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2573146
29 A = 6730114
39 meter
Y = 5172063
34 meter E =
0014379
Z = -3458199
36 I = 51
97246
XDOT = -3724
140329 Wp = 65
43399
YDOT = 4914
497676 meter/sec RA = 91
46482 deg
ZDOT = 4599
765594 TA = 253
86909
MA = 254
02742
Ha = 195
269 n
mi
Hp = 182
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8442081
00 X = 2531919
36
Y = 16968711
73 feet Y = 5200607
57 meter
Z = -11345798
43 Z = -3445798
75
XDOT = -12218
308165 XDOT = -3801
162856
YDOT = 16123
680038 feet/sec YDOT = 4872
421079 meter/sec
ZDOT = 15091
094470 ZDOT = 4581
487300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4528927
07 X = 1380416
97
Y = -18433404
87 feet Y = -5618501
81 meter
Z = -11297409
25 Z = -3443450
34
XDOT = 18478
421198 XDOT = 5632
222781
YDOT = -4624
188099 feet/sec YDOT = -1409
452533 meter/sec
ZDOT = 15020
907389 ZDOT = 4578
372572
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
50718916
00020000 00000-0 20000-3 0 9057
2 25544 51
6419 92
2111 0010179 52
4710 307
7376 15
72914899 37245
Satellite: ISS
Catalog Number: 25544
Epoch time: 08224
50718916 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 92
2111 deg
Eccentricity:
0010179
Arg of perigee: 52
4710 deg
Mean anomaly: 307
7376 deg
Mean motion: 15
72914899 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3724
Checksum: 294
Coasting Arc #7 (Orbit 3739)
---------------------------------------
Vector Time (GMT): 2008/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2680649
84 A = 6729020
94 meter
Y = -4869900
31 meter E =
0016032
Z = -3810027
89 I = 51
96770
XDOT = 3636
956297 Wp = 63
56636
YDOT = 5295
873628 meter/sec RA = 86
41176 deg
ZDOT = -4216
832582 TA = 162
30261
MA = 162
24670
Ha = 195
242 n
mi
Hp = 182
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8794782
93 X = 2753414
80
Y = -15977363
21 feet Y = -4839516
51 meter
Z = -12500091
51 Z = -3796829
21
XDOT = 11932
271314 XDOT = 3597
951030
YDOT = 17374
913478 feet/sec YDOT = 5336
326498 meter/sec
ZDOT = -13834
752564 ZDOT = -4199
258684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16997641
61 X = -5180881
16
Y = 6705685
01 feet Y = 2043892
79 meter
Z = -12449522
00 Z = -3794614
30
XDOT = 2251
982559 XDOT = 686
404284
YDOT = -19809
176921 feet/sec YDOT = -6037
837125 meter/sec
ZDOT = -13766
359781 ZDOT = -4195
986461
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
52371836
00020000 00000-0 20000-3 0 9067
2 25544 51
6413 86
9989 0010081 56
2944 303
9178 15
72918743 37403
Satellite: ISS
Catalog Number: 25544
Epoch time: 08225
52371836 = yrday
fracday
Element set: 906
Inclination: 51
6413 deg
RA of node: 86
9989 deg
Eccentricity:
0010081
Arg of perigee: 56
2944 deg
Mean anomaly: 303
9178 deg
Mean motion: 15
72918743 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3740
Checksum: 312
Coasting Arc #8 (Orbit 3752)
---------------------------------------
Vector Time (GMT): 2008/226/08:03:52
224
Vector Time (MET): N/A
Weight (LBS) : 661093
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4217766
88 A = 6730228
04 meter
Y = 932723
26 meter E =
0014605
Z = -5173719
81 I = 51
94787
XDOT = -18
699195 Wp = 94
36488
YDOT = 7565
031549 meter/sec RA = 82
10755 deg
ZDOT = 1350
756635 TA = 188
52075
MA = 188
54558
Ha = 195
568 n
mi
Hp = 188
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13837817
85 X = 4232156
14
Y = 3060115
69 feet Y = 979969
70 meter
Z = -16974146
37 Z = -5153195
19
XDOT = -61
349066 XDOT = -109
852824
YDOT = 24819
657313 feet/sec YDOT = 7564
312650 meter/sec
ZDOT = 4431
616255 ZDOT = 1350
445100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4888334
99 X = 1489964
50
Y = -13403102
26 feet Y = -4085265
57 meter
Z = -16894738
44 Z = -5149516
28
XDOT = 23609
731720 XDOT = 7196
246228
YDOT = 3034
446092 feet/sec YDOT = 924
899169 meter/sec
ZDOT = 4431
089837 ZDOT = 1350
596182
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
34965566
00020000 00000-0 20000-3 0 9078
2 25544 51
6415 82
7645 0001565 27
2885 332
8358 15
70665873 37533
Satellite: ISS
Catalog Number: 25544
Epoch time: 08226
34965566 = yrday
fracday
Element set: 907
Inclination: 51
6415 deg
RA of node: 82
7645 deg
Eccentricity:
0001565
Arg of perigee: 27
2885 deg
Mean anomaly: 332
8358 deg
Mean motion: 15
70665873 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3753
Checksum: 323
Coasting Arc #9 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2008/227/08:03:52
224
Vector Time (MET): N/A
Weight (LBS) : 661093
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1425339
71 A = 6741692
93 meter
Y = -6583426
63 meter E =
0011721
Z = -112995
58 I = 51
98138
XDOT = 4652
643624 Wp = 128
47770
YDOT = -910
633073 meter/sec RA = 77
03232 deg
ZDOT = -6060
728739 TA = 52
74223
MA = 52
63539
Ha = 195
589 n
mi
Hp = 188
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4676311
38 X = -1351067
94
Y = -21599168
74 feet Y = -6598950
32 meter
Z = -370720
42 Z = -119739
87
XDOT = 15264
578818 XDOT = 4691
922041
YDOT = -2987
641314 feet/sec YDOT = -858
384437 meter/sec
ZDOT = -19884
280641 ZDOT = -6038
031290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21995754
32 X = -6704305
92
Y = 2135016
72 feet Y = 650753
10 meter
Z = -397375
90 Z = -121120
17
XDOT = -1026
558529 XDOT = -312
895040
YDOT = -14016
977095 feet/sec YDOT = -4272
374619 meter/sec
ZDOT = -19796
634430 ZDOT = -6034
014174
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 08227
36764255
00020000 00000-0 20000-3 0 9084
2 25544 51
6418 77
5624 0001502 31
8791 328
2461 15
70660154 37691
Satellite: ISS
Catalog Number: 25544
Epoch time: 08227
36764255 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 77
5624 deg
Eccentricity:
0001502
Arg of perigee: 31
8791 deg
Mean anomaly: 328
2461 deg
Mean motion: 15
70660154 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3769
Checksum: 297
Coasting Arc #10 (Orbit 3784)
---------------------------------------
Vector Time (GMT): 2008/228/08:03:52
224
Vector Time (MET): N/A
Weight (LBS) : 661093
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3490255
87 A = 6729871
66 meter
Y = 2445932
06 meter E =
0004036
Z = 5205078
22 I = 51
93411
XDOT = -3178
195147 Wp = 101
45175
YDOT = -6922
218910 meter/sec RA = 71
95235 deg
ZDOT = 1120
194205 TA = 337
88954
MA = 337
90694
Ha = 195
621 n
mi
Hp = 188
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11450970
69 X = -3542632
07
Y = 8024711
50 feet Y = 2406608
86 meter
Z = 17077028
28 Z = 5187995
83
XDOT = -10427
149434 XDOT = -3105
995167
YDOT = -22710
691962 feet/sec YDOT = -6957
355690 meter/sec
ZDOT = 3675
177839 ZDOT = 1104
929823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6842178
97 X = 2085496
15
Y = 12286115
71 feet Y = 3744808
07 meter
Z = 17011218
86 Z = 5185019
51
XDOT = -22737
462656 XDOT = -6930
378617
YDOT = 7649
617202 feet/sec YDOT = 2331
603323 meter/sec
ZDOT = 3615
558349 ZDOT = 1102
022185
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 08228
38561928
00020000 00000-0 20000-3 0 9090
2 25544 51
6415 72
3603 0001528 31
1297 328
9955 15
70717212 37851
Satellite: ISS
Catalog Number: 25544
Epoch time: 08228
38561928 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 72
3603 deg
Eccentricity:
0001528
Arg of perigee: 31
1297 deg
Mean anomaly: 328
9955 deg
Mean motion: 15
70717212 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3785
Checksum: 303
Coasting Arc #11 (Orbit 3799)
---------------------------------------
Vector Time (GMT): 2008/229/08:03:52
224
Vector Time (MET): N/A
Weight (LBS) : 661093
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3907509
78 A = 6739788
00 meter
Y = 5099940
83 meter E =
0008336
Z = -2027307
82 I = 51
95763
XDOT = -2874
992236 Wp = 38
55299
YDOT = 4421
851886 meter/sec RA = 66
83563 deg
ZDOT = 5600
975342 TA = 298
98368
MA = 299
06721
Ha = 195
573 n
mi
Hp = 188
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12819913
97 X = 3860039
10
Y = 16732089
34 feet Y = 5143371
49 meter
Z = -6651272
39 Z = -2008440
68
XDOT = -9432
389225 XDOT = -2951
432375
YDOT = 14507
388077 feet/sec YDOT = 4389
274490 meter/sec
ZDOT = 18375
903354 ZDOT = 5586
823393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17728428
63 X = 5403625
05
Y = -11444939
88 feet Y = -3488417
68 meter
Z = -6577887
33 Z = -2004940
06
XDOT = 12843
473061 XDOT = 3914
690589
YDOT = 9400
122982 feet/sec YDOT = 2865
157485 meter/sec
ZDOT = 18321
596383 ZDOT = 5584
422578
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 08229
33996681
00020000 00000-0 20000-3 0 9106
2 25544 51
6419 67
4829 0001604 33
7494 326
3769 15
70717575 38007
Satellite: ISS
Catalog Number: 25544
Epoch time: 08229
33996681 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 67
4829 deg
Eccentricity:
0001604
Arg of perigee: 33
7494 deg
Mean anomaly: 326
3769 deg
Mean motion: 15
70717575 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3800
Checksum: 315
Coasting Arc #12 (Orbit 3815)
---------------------------------------
Vector Time (GMT): 2008/230/08:03:52
224
Vector Time (MET): N/A
Weight (LBS) : 661093
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1255557
65 A = 6733160
24 meter
Y = -4949963
75 meter E =
0010558
Z = -4399068
41 I = 51
92311
XDOT = 5348
109335 Wp = 63
67718
YDOT = 4361
913066 meter/sec RA = 61
78769 deg
ZDOT = -3383
389025 TA = 172
33010
MA = 172
31394
Ha = 195
522 n
mi
Hp = 188
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4119283
61 X = 1332185
10
Y = -16240038
55 feet Y = -4935494
91 meter
Z = -14432639
14 Z = -4392782
94
XDOT = 17546
290468 XDOT = 5315
371828
YDOT = 14310
738406 feet/sec YDOT = 4421
535681 meter/sec
ZDOT = -11100
357693 ZDOT = -3357
487886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15934188
40 X = -4856740
62
Y = -5243751
17 feet Y = -1598295
36 meter
Z = -14408786
77 Z = -4391798
21
XDOT = 15037
718669 XDOT = 4583
496650
YDOT = -15484
722968 feet/sec YDOT = -4719
743561 meter/sec
ZDOT = -10999
848295 ZDOT = -3352
753760
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 08230
35792800
00020000 00000-0 20000-3 0 9118
2 25544 51
6422 62
2804 0001660 32
4837 327
6426 15
70731005 38161
Satellite: ISS
Catalog Number: 25544
Epoch time: 08230
35792800 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 62
2804 deg
Eccentricity:
0001660
Arg of perigee: 32
4837 deg
Mean anomaly: 327
6426 deg
Mean motion: 15
70731005 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3816
Checksum: 261
Coasting Arc #13 (Orbit 3831)
---------------------------------------
Vector Time (GMT): 2008/231/08:03:52
224
Vector Time (MET): N/A
Weight (LBS) : 661093
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5066975
53 A = 6735351
34 meter
Y = -2307783
00 meter E =
0012881
Z = 3781735
98 I = 51
91533
XDOT = -249
925935 Wp = 77
21234
YDOT = -6421
401611 meter/sec RA = 56
64695 deg
ZDOT = -4238
657343 TA = 57
23898
MA = 57
11491
Ha = 195
637 n
mi
Hp = 188
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16623935
48 X = -5059163
67
Y = -7571466
54 feet Y = -2364401
11 meter
Z = 12407270
26 Z = 3757139
98
XDOT = -819
966978 XDOT = -157
511892
YDOT = -21067
590588 feet/sec YDOT = -6423
679771 meter/sec
ZDOT = -13906
356112 ZDOT = -4239
646907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8356333
74 X = -2547010
52
Y = 16315920
31 feet Y = 4973092
51 meter
Z = 12311991
01 Z = 3752694
86
XDOT = -19889
237966 XDOT = -6062
239732
YDOT = 347
618225 feet/sec YDOT = 105
954035 meter/sec
ZDOT = -13910
756163 ZDOT = -4239
998478
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 08231
37588137
00020000 00000-0 20000-3 0 9128
2 25544 51
6419 57
0778 0001751 36
0033 324
1246 15
70746635 38323
Satellite: ISS
Catalog Number: 25544
Epoch time: 08231
37588137 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 57
0778 deg
Eccentricity:
0001751
Arg of perigee: 36
0033 deg
Mean anomaly: 324
1246 deg
Mean motion: 15
70746635 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3832
Checksum: 283
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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