Date:
January 29th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 200 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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
357/10:54:56
325 -43
9 50
7 50
7
N/A -0
3 0
0 133
9
000/00:00:36
650 -25
3 -0
0 118
9
357/11:31:07
795 12
8 24
4 24
4
N/A -9
8 -0
0 136
8
000/00:00:17
591 18
3 0
0 127
7
357/12:07:43
653 -1
2 -0
0 3
4
N/A 2
4 -3
4 136
8
000/00:00:02
447 2
1 -0
0 127
6
359/07:54:40
538 -6
3 9
8 9
8
N/A -5
9 0
0 136
9
000/00:00:07
077 4
7 0
0 131
8
360/06:15:57
021 -25
4 36
3 36
3
N/A -19
5 -0
0 154
1
000/00:00:26
042 17
1 0
0 135
3
360/07:00:50
655 58
2 83
2 83
2
N/A 44
6 -0
0 182
6
000/00:00:59
309 -39
2 0
1 153
3
360/07:46:31
677 -33
3 44
1 44
3
N/A -22
4 0
0 183
1
000/00:00:31
354 18
8 -4
2 177
5
Coasting Arc #1 (Orbit 1)
---------------------------------------
Vector Time (GMT): 2007/357/07:13:19
000
Vector Time (MET): N/A
Weight (LBS) : 15432
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2284552
13 A = 6585732
04 meter
Y = -4768454
40 meter E =
0040804
Z = 3889324
59 I = 51
48651
XDOT = 6715
785278 Wp = 84
85803
YDOT = 52
479072 meter/sec RA = 208
57089 deg
ZDOT = 3977
916883 TA = 324
36632
MA = 324
63805
Ha = 125
479 n
mi
Hp = 97
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7495249
78 X = -2249954
46
Y = -15644535
42 feet Y = -4793808
88 meter
Z = 12760251
29 Z = 3878309
28
XDOT = 22033
416266 XDOT = 6695
375243
YDOT = 172
175433 feet/sec YDOT = 127
463878 meter/sec
ZDOT = 13050
908408 ZDOT = 4010
492736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12257214
44 X = 3735998
96
Y = 12319675
67 feet Y = 3755037
14 meter
Z = 12717726
06 Z = 3876362
90
XDOT = -19915
599143 XDOT = -6070
274619
YDOT = 6107
703910 feet/sec YDOT = 1861
628152 meter/sec
ZDOT = 13175
165527 ZDOT = 4015
790453
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 07357
35412034
00020000 00000-0 20000-3 0 9003
2 25544 51
6448 209
2179 0030128 78
4753 281
9817 16
24369710 25
Satellite: ISS
Catalog Number: 25544
Epoch time: 07357
35412034 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 209
2179 deg
Eccentricity:
0030128
Arg of perigee: 78
4753 deg
Mean anomaly: 281
9817 deg
Mean motion: 16
24369710 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2
Checksum: 280
Coasting Arc #2 (Orbit 3)
---------------------------------------
Vector Time (GMT): 2007/357/10:55:14
650
Vector Time (MET): N/A
Weight (LBS) : 15351
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2136530
07 A = 6610957
49 meter
Y = 4762847
11 meter E =
0017968
Z = -4050044
80 I = 51
49029
XDOT = -6782
353240 Wp = 160
97858
YDOT = -159
453966 meter/sec RA = 207
71638 deg
ZDOT = -3786
895822 TA = 70
59215
MA = 70
39804
Ha = 133
921 n
mi
Hp = 118
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7009613
10 X = 2102786
83
Y = 15626138
81 feet Y = 4786551
14 meter
Z = -13287548
55 Z = -4039746
51
XDOT = -22251
815092 XDOT = -6761
670020
YDOT = -523
142934 feet/sec YDOT = -235
181679 meter/sec
ZDOT = -12424
198891 ZDOT = -3819
794382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16942888
08 X = -5164192
29
Y = 2702831
09 feet Y = 823822
92 meter
Z = -13247757
70 Z = -4037916
55
XDOT = 6563
939195 XDOT = 2000
688666
YDOT = -20018
820848 feet/sec YDOT = -6101
736594 meter/sec
ZDOT = -12549
701585 ZDOT = -3825
149043
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 07357
47722491
00020000 00000-0 20000-3 0 9018
2 25544 51
6460 208
5389 0019673 184
0736 176
0292 16
14840982 48
Satellite: ISS
Catalog Number: 25544
Epoch time: 07357
47722491 = yrday
fracday
Element set: 901
Inclination: 51
6460 deg
RA of node: 208
5389 deg
Eccentricity:
0019673
Arg of perigee: 184
0736 deg
Mean anomaly: 176
0292 deg
Mean motion: 16
14840982 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4
Checksum: 298
Coasting Arc #3 (Orbit 4)
---------------------------------------
Vector Time (GMT): 2007/357/11:31:16
591
Vector Time (MET): N/A
Weight (LBS) : 15312
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5071139
22 A = 6630014
94 meter
Y = -3989223
26 meter E =
0017461
Z = 1495926
11 I = 51
51279
XDOT = 4134
157227 Wp = 71
42114
YDOT = -3056
670235 meter/sec RA = 207
56799 deg
ZDOT = 5814
462654 TA = 305
34974
MA = 305
51282
Ha = 136
833 n
mi
Hp = 127
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16637595
87 X = -5033421
18
Y = -13088002
81 feet Y = -4045721
02 meter
Z = 4907894
05 Z = 1471381
26
XDOT = 13563
507964 XDOT = 4139
784446
YDOT = -10028
445652 feet/sec YDOT = -3010
409449 meter/sec
ZDOT = 19076
321043 ZDOT = 5834
559499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14835579
04 X = 4521884
49
Y = -15130278
65 feet Y = -4611708
93 meter
Z = 4813844
66 Z = 1467259
85
XDOT = 7390
026112 XDOT = 2252
479959
YDOT = 13391
721289 feet/sec YDOT = 4081
796649 meter/sec
ZDOT = 19152
649876 ZDOT = 5837
727682
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 07357
53928631
00020000 00000-0 20000-3 0 9020
2 25544 51
6456 208
2025 0004067 107
3821 252
7806 16
10260058 51
Satellite: ISS
Catalog Number: 25544
Epoch time: 07357
53928631 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 208
2025 deg
Eccentricity:
0004067
Arg of perigee: 107
3821 deg
Mean anomaly: 252
7806 deg
Mean motion: 16
10260058 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 5
Checksum: 263
Coasting Arc #4 (Orbit 4)
---------------------------------------
Vector Time (GMT): 2007/357/12:07:44
877
Vector Time (MET): N/A
Weight (LBS) : 15307
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6173959
21 A = 6630026
68 meter
Y = 1919891
23 meter E =
0018407
Z = 1429962
82 I = 51
50598
XDOT = -226
257291 Wp = 116
13939
YDOT = 5112
325514 meter/sec RA = 207
40409 deg
ZDOT = -5838
013952 TA = 47
84438
MA = 47
68816
Ha = 136
818 n
mi
Hp = 127
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20255771
70 X = 6145085
32
Y = 6298855
73 feet Y = 1988770
21 meter
Z = 4691479
07 Z = 1459886
24
XDOT = -742
313948 XDOT = -255
047201
YDOT = 16772
721501 feet/sec YDOT = 5109
635576 meter/sec
ZDOT = -19153
589082 ZDOT = -5839
182017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5284972
44 X = -1610859
60
Y = 20517187
36 feet Y = 6253638
71 meter
Z = 4805823
11 Z = 1464814
88
XDOT = -15287
341371 XDOT = -4659
581650
YDOT = 586
265213 feet/sec YDOT = 178
693637 meter/sec
ZDOT = -19157
497100 ZDOT = -5839
205116
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 07357
53928738
00020000 00000-0 20000-3 0 9039
2 25544 51
6380 208
2051 0004139 105
8457 254
3182 16
10247232 58
Satellite: ISS
Catalog Number: 25544
Epoch time: 07357
53928738 = yrday
fracday
Element set: 903
Inclination: 51
6380 deg
RA of node: 208
2051 deg
Eccentricity:
0004139
Arg of perigee: 105
8457 deg
Mean anomaly: 254
3182 deg
Mean motion: 16
10247232 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 5
Checksum: 269
Coasting Arc #5 (Orbit 20)
---------------------------------------
Vector Time (GMT): 2007/358/12:07:44
877
Vector Time (MET): N/A
Weight (LBS) : 15307
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4890398
86 A = 6628056
22 meter
Y = 3880950
26 meter E =
0009702
Z = -2221330
64 I = 51
52759
XDOT = -4708
046182 Wp = 128
20672
YDOT = 2802
653299 meter/sec RA = 202
01147 deg
ZDOT = -5490
346501 TA = 77
14441
MA = 77
03603
Ha = 136
338 n
mi
Hp = 127
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16044615
69 X = 4857428
78
Y = 12732776
46 feet Y = 3935453
57 meter
Z = -7287830
17 Z = -2197652
52
XDOT = -15446
345741 XDOT = -4712
365005
YDOT = 9195
056754 feet/sec YDOT = 2749
982188 meter/sec
ZDOT = -18012
947839 ZDOT = -5513
228010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11627984
00 X = -3544209
52
Y = 16901413
22 feet Y = 5151550
75 meter
Z = -7197081
15 Z = -2193670
33
XDOT = -8968
618881 XDOT = -2733
635035
YDOT = -13846
798494 feet/sec YDOT = -4220
504181 meter/sec
ZDOT = -18099
939311 ZDOT = -5516
861502
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 07358
53215062
00020000 00000-0 20000-3 0 9040
2 25544 51
6361 202
8262 0003831 111
3793 248
7798 16
10517156 217
Satellite: ISS
Catalog Number: 25544
Epoch time: 07358
53215062 = yrday
fracday
Element set: 904
Inclination: 51
6361 deg
RA of node: 202
8262 deg
Eccentricity:
0003831
Arg of perigee: 111
3793 deg
Mean anomaly: 248
7798 deg
Mean motion: 16
10517156 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 21
Checksum: 269
Coasting Arc #6 (Orbit 33)
---------------------------------------
Vector Time (GMT): 2007/359/07:54:44
077
Vector Time (MET): N/A
Weight (LBS) : 15291
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4871384
99 A = 6626941
34 meter
Y = 1870744
58 meter E =
0005109
Z = -4088955
64 I = 51
53483
XDOT = -4929
753635 Wp = 85
90851
YDOT = -4669
660021 meter/sec RA = 197
49201 deg
ZDOT = 3740
956202 TA = 222
11708
MA = 222
15636
Ha = 136
910 n
mi
Hp = 131
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15982234
21 X = -4872078
69
Y = 6137613
44 feet Y = 1816266
85 meter
Z = -13415208
81 Z = -4112621
93
XDOT = -16173
732399 XDOT = -4895
343090
YDOT = -15320
406892 feet/sec YDOT = -4724
595601 meter/sec
ZDOT = 12273
478354 ZDOT = 3717
090443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10380042
54 X = 3163836
97
Y = -13525213
04 feet Y = -4122484
93 meter
Z = -13505305
10 Z = -4116416
99
XDOT = 20859
511555 XDOT = 6357
979122
YDOT = 3858
851598 feet/sec YDOT = 1176
177967 meter/sec
ZDOT = 12181
913491 ZDOT = 3713
047232
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 07359
33871659
00020000 00000-0 20000-3 0 9050
2 25544 51
6382 198
4562 0004117 321
7112 38
3776 16
08909618 341
Satellite: ISS
Catalog Number: 25544
Epoch time: 07359
33871659 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 198
4562 deg
Eccentricity:
0004117
Arg of perigee: 321
7112 deg
Mean anomaly: 38
3776 deg
Mean motion: 16
08909618 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 34
Checksum: 303
Coasting Arc #7 (Orbit 48)
---------------------------------------
Vector Time (GMT): 2007/360/06:16:10
042
Vector Time (MET): N/A
Weight (LBS) : 15234
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4667597
63 A = 6645185
54 meter
Y = 2305073
91 meter E =
0024944
Z = -4103718
33 I = 51
56109
XDOT = -5353
002018 Wp = 315
28587
YDOT = -4211
238530 meter/sec RA = 192
44946 deg
ZDOT = 3727
149911 TA = 352
49350
MA = 352
53078
Ha = 154
108 n
mi
Hp = 135
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15313640
52 X = -4673091
58
Y = 7562578
44 feet Y = 2252848
11 meter
Z = -13463642
82 Z = -4126406
19
XDOT = -17562
342579 XDOT = -5323
619023
YDOT = -13816
399377 feet/sec YDOT = -4270
935130 meter/sec
ZDOT = 12228
182123 ZDOT = 3701
216102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14091328
03 X = 4295036
78
Y = -9529044
54 feet Y = -2904452
77 meter
Z = -13549968
31 Z = -4130030
34
XDOT = 18622
952169 XDOT = 5676
275821
YDOT = 10311
412485 feet/sec YDOT = 3142
918525 meter/sec
ZDOT = 12128
758903 ZDOT = 3696
845714
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 07360
27030398
00020000 00000-0 20000-3 0 9063
2 25544 51
6371 193
4195 0032599 308
9061 50
9211 16
02268344 499
Satellite: ISS
Catalog Number: 25544
Epoch time: 07360
27030398 = yrday
fracday
Element set: 906
Inclination: 51
6371 deg
RA of node: 193
4195 deg
Eccentricity:
0032599
Arg of perigee: 308
9061 deg
Mean anomaly: 50
9211 deg
Mean motion: 16
02268344 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 49
Checksum: 284
Coasting Arc #8 (Orbit 49)
---------------------------------------
Vector Time (GMT): 2007/360/07:01:20
309
Vector Time (MET): N/A
Weight (LBS) : 15103
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4780958
14 A = 6689219
73 meter
Y = -2254055
74 meter E =
0040841
Z = 4056594
55 I = 51
56301
XDOT = 5247
154817 Wp = 113
34836
YDOT = 4240
229936 meter/sec RA = 192
28194 deg
ZDOT = -3814
056922 TA = 15
63998
MA = 15
51418
Ha = 182
558 n
mi
Hp = 153
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15685558
21 X = 4786102
09
Y = -7395195
99 feet Y = -2200564
22 meter
Z = 13309037
25 Z = 4079832
26
XDOT = 17215
074860 XDOT = 5217
877674
YDOT = 13911
515538 feet/sec YDOT = 4298
743495 meter/sec
ZDOT = -12513
310113 ZDOT = -3788
637056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12352942
43 X = -3765176
85
Y = 12073476
21 feet Y = 3679995
55 meter
Z = 13397466
85 Z = 4083547
89
XDOT = -19991
916979 XDOT = -6093
536295
YDOT = -6626
804906 feet/sec YDOT = -2019
850135 meter/sec
ZDOT = -12415
844390 ZDOT = -3784
349370
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 07360
33317854
00020000 00000-0 20000-3 0 9076
2 25544 51
6372 193
0883 0033116 124
2210 236
2105 15
86570115 507
Satellite: ISS
Catalog Number: 25544
Epoch time: 07360
33317854 = yrday
fracday
Element set: 907
Inclination: 51
6372 deg
RA of node: 193
0883 deg
Eccentricity:
0033116
Arg of perigee: 124
2210 deg
Mean anomaly: 236
2105 deg
Mean motion: 15
86570115 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 50
Checksum: 255
Coasting Arc #9 (Orbit 49)
---------------------------------------
Vector Time (GMT): 2007/360/07:46:47
354
Vector Time (MET): N/A
Weight (LBS) : 15034
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4829947
03 A = 6712535
82 meter
Y = 2271792
63 meter E =
0006148
Z = -4076465
71 I = 51
56517
XDOT = -5198
008964 Wp = 101
07638
YDOT = -4212
380272 meter/sec RA = 192
11668 deg
ZDOT = 3814
936055 TA = 208
13100
MA = 208
16423
Ha = 183
076 n
mi
Hp = 177
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15846282
91 X = -4835189
15
Y = 7453387
91 feet Y = 2217752
75 meter
Z = -13374231
33 Z = -4099941
64
XDOT = -17053
835184 XDOT = -5169
051161
YDOT = -13820
145249 feet/sec YDOT = -4270
346036 meter/sec
ZDOT = 12516
194405 ZDOT = 3789
754170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9833252
39 X = 2997175
33
Y = -14407193
07 feet Y = -4391312
45 meter
Z = -13463568
34 Z = -4103695
63
XDOT = 20712
193370 XDOT = 6313
076539
YDOT = 2541
580981 feet/sec YDOT = 774
673883 meter/sec
ZDOT = 12419
639323 ZDOT = 3785
506066
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 07360
33317170
00020000 00000-0 20000-3 0 9088
2 25544 51
6383 193
0888 0001888 319
7968 40
3058 15
78325878 502
Satellite: ISS
Catalog Number: 25544
Epoch time: 07360
33317170 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 193
0888 deg
Eccentricity:
0001888
Arg of perigee: 319
7968 deg
Mean anomaly: 40
3058 deg
Mean motion: 15
78325878 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 50
Checksum: 312
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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