Date:
January 4th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
012/00:42:49
247 -0
5 8
2 8
2
N/A 7
9 0
0 183
9
000/00:01:38
494 -2
2 -0
0 180
8
Coasting Arc #1 (Orbit 222)
---------------------------------------
Vector Time (GMT): 2008/002/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1814334
05 A = 6711528
59 meter
Y = -4697924
66 meter E =
0010288
Z = 4431434
10 I = 51
76298
XDOT = 6970
116979 Wp = 61
54425
YDOT = -404
117736 meter/sec RA = 155
01323 deg
ZDOT = -3271
633151 TA = 61
20579
MA = 61
10252
Ha = 183
859 n
mi
Hp = 177
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5952539
53 X = 1845204
98
Y = -15413138
65 feet Y = -4677463
63 meter
Z = 14538825
80 Z = 4440322
62
XDOT = 22867
837859 XDOT = 6990
010877
YDOT = -1325
845590 feet/sec YDOT = -326
062335 meter/sec
ZDOT = -10733
704565 ZDOT = -3237
723988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16392773
21 X = 4996517
27
Y = 1817016
81 feet Y = 553826
73 meter
Z = 14572249
73 Z = 4441621
72
XDOT = 7166
370741 XDOT = 2184
309802
YDOT = 20667
428727 feet/sec YDOT = 6299
432276 meter/sec
ZDOT = -10604
269675 ZDOT = -3232
181397
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 08002
55224790
00020000 00000-0 20000-3 0 9003
2 25544 51
6355 155
7958 0001670 20
1535 339
9696 15
78232236 2238
Satellite: ISS
Catalog Number: 25544
Epoch time: 08002
55224790 = yrday
fracday
Element set: 900
Inclination: 51
6355 deg
RA of node: 155
7958 deg
Eccentricity:
0001670
Arg of perigee: 20
1535 deg
Mean anomaly: 339
9696 deg
Mean motion: 15
78232236 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 223
Checksum: 283
Coasting Arc #2 (Orbit 238)
---------------------------------------
Vector Time (GMT): 2008/003/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5418237
93 A = 6713280
84 meter
Y = -434900
80 meter E =
0011598
Z = 3930203
14 I = 51
79634
XDOT = 3386
403418 Wp = 92
23018
YDOT = -5632
762182 meter/sec RA = 149
90497 deg
ZDOT = 4034
649899 TA = 315
98274
MA = 316
07503
Ha = 183
879 n
mi
Hp = 176
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17776371
15 X = -5432064
35
Y = -1426839
90 feet Y = -495568
43 meter
Z = 12894367
27 Z = 3903847
66
XDOT = 11110
247433 XDOT = 3429
538513
YDOT = -18480
190887 feet/sec YDOT = -5594
652837 meter/sec
ZDOT = 13237
040351 ZDOT = 4051
205122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3398220
82 X = -1035777
71
Y = -17580499
35 feet Y = -5358536
20 meter
Z = 12793673
78 Z = 3899511
77
XDOT = 19476
159536 XDOT = 5936
333427
YDOT = 5939
274960 feet/sec YDOT = 1810
291008 meter/sec
ZDOT = 13299
648313 ZDOT = 4053
732806
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 08003
56532530
00020000 00000-0 20000-3 0 9010
2 25544 51
6365 150
5598 0001670 19
8593 340
2637 15
78313005 2392
Satellite: ISS
Catalog Number: 25544
Epoch time: 08003
56532530 = yrday
fracday
Element set: 901
Inclination: 51
6365 deg
RA of node: 150
5598 deg
Eccentricity:
0001670
Arg of perigee: 19
8593 deg
Mean anomaly: 340
2637 deg
Mean motion: 15
78313005 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 239
Checksum: 274
Coasting Arc #3 (Orbit 253)
---------------------------------------
Vector Time (GMT): 2008/004/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3867583
51 A = 6717520
93 meter
Y = 4974547
77 meter E =
0007451
Z = -2322561
77 I = 51
83635
XDOT = -5233
901688 Wp = 40
76141
YDOT = -1535
276694 meter/sec RA = 144
70274 deg
ZDOT = 5442
561695 TA = 293
14293
MA = 293
22142
Ha = 183
819 n
mi
Hp = 176
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12688922
27 X = -3911639
63
Y = 16320694
79 feet Y = 4931052
27 meter
Z = -7619953
31 Z = -2341456
78
XDOT = -17171
593466 XDOT = -5242
783965
YDOT = -5036
997026 feet/sec YDOT = -1593
855606 meter/sec
ZDOT = 17856
173539 ZDOT = 5417
113605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19239647
12 X = -5864244
44
Y = -7490865
82 feet Y = -2283215
90 meter
Z = -7691581
33 Z = -2344393
99
XDOT = -621
058109 XDOT = -189
298512
YDOT = -16588
597092 feet/sec YDOT = -5056
204393 meter/sec
ZDOT = 17758
816149 ZDOT = 5412
887162
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 08004
51507069
00020000 00000-0 20000-3 0 9026
2 25544 51
6373 145
6514 0001824 24
8698 335
2555 15
78313464 2546
Satellite: ISS
Catalog Number: 25544
Epoch time: 08004
51507069 = yrday
fracday
Element set: 902
Inclination: 51
6373 deg
RA of node: 145
6514 deg
Eccentricity:
0001824
Arg of perigee: 24
8698 deg
Mean anomaly: 335
2555 deg
Mean motion: 15
78313464 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 254
Checksum: 284
Coasting Arc #4 (Orbit 269)
---------------------------------------
Vector Time (GMT): 2008/005/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3554208
35 A = 6708117
50 meter
Y = 2341083
21 meter E =
0015645
Z = -5198690
53 I = 51
82823
XDOT = -5222
121879 Wp = 76
06712
YDOT = 5551
736698 meter/sec RA = 139
57867 deg
ZDOT = -1069
140941 TA = 183
74950
MA = 183
76124
Ha = 183
819 n
mi
Hp = 176
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11660788
55 X = 3553020
05
Y = 7680719
21 feet Y = 2380822
56 meter
Z = -17056071
31 Z = -5181426
76
XDOT = -17132
945798 XDOT = -5278
620453
YDOT = 18214
359244 feet/sec YDOT = 5493
024236 meter/sec
ZDOT = -3507
680251 ZDOT = -1094
646286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3794116
83 X = -1156446
81
Y = 13521305
22 feet Y = 4121293
83 meter
Z = -16989878
99 Z = -5178515
12
XDOT = -21527
823337 XDOT = -6561
680553
YDOT = -10574
148612 feet/sec YDOT = -3223
000497 meter/sec
ZDOT = -3604
509450 ZDOT = -1098
654480
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 08005
52811314
00020000 00000-0 20000-3 0 9030
2 25544 51
6377 140
4159 0001927 26
7474 333
3790 15
78355808 2701
Satellite: ISS
Catalog Number: 25544
Epoch time: 08005
52811314 = yrday
fracday
Element set: 903
Inclination: 51
6377 deg
RA of node: 140
4159 deg
Eccentricity:
0001927
Arg of perigee: 26
7474 deg
Mean anomaly: 333
3790 deg
Mean motion: 15
78355808 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 270
Checksum: 283
Coasting Arc #5 (Orbit 285)
---------------------------------------
Vector Time (GMT): 2008/006/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4977554
38 A = 6719613
44 meter
Y = -4475954
98 meter E =
0010679
Z = -538318
65 I = 51
88906
XDOT = 2834
943884 Wp = 129
28556
YDOT = 3867
872989 meter/sec RA = 134
42061 deg
ZDOT = -6032
543729 TA = 56
56172
MA = 56
45965
Ha = 183
825 n
mi
Hp = 176
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16330558
98 X = 5029850
28
Y = -14684891
68 feet Y = -4420000
66 meter
Z = -1766137
29 Z = -514011
58
XDOT = 9300
996995 XDOT = 2820
786815
YDOT = 12689
872011 feet/sec YDOT = 3899
496773 meter/sec
ZDOT = -19791
810135 ZDOT = -6018
805429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19104702
02 X = 5823113
17
Y = 10847181
49 feet Y = 3306220
92 meter
Z = -1673754
93 Z = -510160
50
XDOT = -8263
764331 XDOT = -2518
795368
YDOT = 11554
594498 feet/sec YDOT = 3521
840403 meter/sec
ZDOT = -19738
916900 ZDOT = -6016
421871
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 08006
54113686
00020000 00000-0 20000-3 0 9041
2 25544 51
6380 135
1788 0001954 29
8097 330
3179 15
78385185 2865
Satellite: ISS
Catalog Number: 25544
Epoch time: 08006
54113686 = yrday
fracday
Element set: 904
Inclination: 51
6380 deg
RA of node: 135
1788 deg
Eccentricity:
0001954
Arg of perigee: 29
8097 deg
Mean anomaly: 330
3179 deg
Mean motion: 15
78385185 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 286
Checksum: 308
Coasting Arc #6 (Orbit 301)
---------------------------------------
Vector Time (GMT): 2008/007/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1398682
58 A = 6709248
36 meter
Y = -4362992
16 meter E =
0008457
Z = 4897309
03 I = 51
87481
XDOT = 5898
485595 Wp = 52
05239
YDOT = -4427
066248 meter/sec RA = 129
24634 deg
ZDOT = -2251
720219 TA = 59
77912
MA = 59
69540
Ha = 183
930 n
mi
Hp = 176
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4588853
61 X = -1373580
92
Y = -14314278
73 feet Y = -4378493
46 meter
Z = 16067286
84 Z = 4890574
58
XDOT = 19351
986861 XDOT = 5958
489651
YDOT = -14524
495565 feet/sec YDOT = -4360
770169 meter/sec
ZDOT = -7387
533528 ZDOT = -2222
920700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11938661
88 X = 3638904
14
Y = -9179621
87 feet Y = -2797948
75 meter
Z = 16041095
79 Z = 4889326
00
XDOT = 19484
643858 XDOT = 5938
919448
YDOT = 12578
663679 feet/sec YDOT = 3833
976689 meter/sec
ZDOT = -7277
967620 ZDOT = -2218
324531
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 08007
55414279
00020000 00000-0 20000-3 0 9056
2 25544 51
6391 129
9431 0002105 34
7870 325
3433 15
78389033 3028
Satellite: ISS
Catalog Number: 25544
Epoch time: 08007
55414279 = yrday
fracday
Element set: 905
Inclination: 51
6391 deg
RA of node: 129
9431 deg
Eccentricity:
0002105
Arg of perigee: 34
7870 deg
Mean anomaly: 325
3433 deg
Mean motion: 15
78389033 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 302
Checksum: 276
Coasting Arc #7 (Orbit 317)
---------------------------------------
Vector Time (GMT): 2008/008/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5073652
11 A = 6715013
32 meter
Y = 2963693
36 meter E =
0014325
Z = 3236003
47 I = 51
91308
XDOT = -452
831660 Wp = 80
96908
YDOT = -6025
552896 meter/sec RA = 124
13859 deg
ZDOT = 4792
865438 TA = 316
83146
MA = 316
94368
Ha = 183
869 n
mi
Hp = 176
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16645840
26 X = -5122135
15
Y = 9723403
41 feet Y = 2906685
33 meter
Z = 10616809
30 Z = 3211238
77
XDOT = -1485
668176 XDOT = -408
701827
YDOT = -19768
874331 feet/sec YDOT = -6030
370702 meter/sec
ZDOT = 15724
624142 ZDOT = 4790
771894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14944947
29 X = -4555219
93
Y = -12258503
98 feet Y = -3736392
01 meter
Z = 10522492
21 Z = 3207255
63
XDOT = 17080
602903 XDOT = 5206
167765
YDOT = -7288
991322 feet/sec YDOT = -2221
684555 meter/sec
ZDOT = 15715
988986 ZDOT = 4790
233443
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 08008
56712687
00020000 00000-0 20000-3 0 9063
2 25544 51
6399 124
7067 0002056 37
0188 323
1119 15
78462845 3184
Satellite: ISS
Catalog Number: 25544
Epoch time: 08008
56712687 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 124
7067 deg
Eccentricity:
0002056
Arg of perigee: 37
0188 deg
Mean anomaly: 323
1119 deg
Mean motion: 15
78462845 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 318
Checksum: 299
Coasting Arc #8 (Orbit 332)
---------------------------------------
Vector Time (GMT): 2008/009/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -500989
93 A = 6715347
45 meter
Y = 5933553
53 meter E =
0006350
Z = -3105943
95 I = 51
92978
XDOT = -5553
597695 Wp = 63
14676
YDOT = 2095
867304 meter/sec RA = 118
93987 deg
ZDOT = 4910
158467 TA = 260
87747
MA = 260
94932
Ha = 183
840 n
mi
Hp = 176
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1643667
74 X = -552214
79
Y = 19467039
15 feet Y = 5927665
18 meter
Z = -10190104
81 Z = -3108501
34
XDOT = -18220
464879 XDOT = -5600
473424
YDOT = 6876
205066 feet/sec YDOT = 2033
501072 meter/sec
ZDOT = 16109
443789 ZDOT = 4883
066055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18701213
82 X = -5700129
97
Y = 5634301
22 feet Y = 1717335
01 meter
Z = -10199252
16 Z = -3108732
06
XDOT = -12678
781550 XDOT = -3864
492617
YDOT = -13170
618986 feet/sec YDOT = -4014
404667 meter/sec
ZDOT = 16006
129142 ZDOT = 4878
668163
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 08009
51678525
00020000 00000-0 20000-3 0 9072
2 25544 51
6402 119
7986 0002206 34
4716 325
6592 15
78437969 3336
Satellite: ISS
Catalog Number: 25544
Epoch time: 08009
51678525 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 119
7986 deg
Eccentricity:
0002206
Arg of perigee: 34
4716 deg
Mean anomaly: 325
6592 deg
Mean motion: 15
78437969 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 333
Checksum: 310
Coasting Arc #9 (Orbit 348)
---------------------------------------
Vector Time (GMT): 2008/010/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4480029
69 A = 6708749
26 meter
Y = -477404
11 meter E =
0014742
Z = -4984127
72 I = 51
92086
XDOT = -1478
778625 Wp = 70
14357
YDOT = 7276
552147 meter/sec RA = 113
83230 deg
ZDOT = -2026
112489 TA = 180
31866
MA = 180
31960
Ha = 183
812 n
mi
Hp = 176
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14698260
13 X = 4509246
59
Y = -1566286
44 feet Y = -427141
97 meter
Z = -16352125
07 Z = -4962293
30
XDOT = -4851
635909 XDOT = -1550
193968
YDOT = 23873
202583 feet/sec YDOT = 7259
616522 meter/sec
ZDOT = -6647
350685 ZDOT = -2033
468909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7086575
20 X = 2159988
12
Y = 13076433
38 feet Y = 3985696
89 meter
Z = -16268725
83 Z = -4958707
63
XDOT = -22951
985514 XDOT = -6995
765185
YDOT = 4133
969562 feet/sec YDOT = 1260
033922 meter/sec
ZDOT = -6674
697490 ZDOT = -2034
447795
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 08010
52973493
00020000 00000-0 20000-3 0 9088
2 25544 51
6404 114
5623 0002172 39
4616 320
6708 15
78475002 3496
Satellite: ISS
Catalog Number: 25544
Epoch time: 08010
52973493 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 114
5623 deg
Eccentricity:
0002172
Arg of perigee: 39
4616 deg
Mean anomaly: 320
6708 deg
Mean motion: 15
78475002 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 349
Checksum: 276
Coasting Arc #10 (Orbit 364)
---------------------------------------
Vector Time (GMT): 2008/011/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1940896
14 A = 6719342
12 meter
Y = -6421649
67 meter E =
0013172
Z = 276581
83 I = 51
96698
XDOT = 4624
423519 Wp = 122
06079
YDOT = 1127
902136 meter/sec RA = 108
66512 deg
ZDOT = -6062
498927 TA = 54
94136
MA = 54
81788
Ha = 183
857 n
mi
Hp = 176
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6367769
49 X = 2011216
20
Y = -21068404
42 feet Y = -6399552
31 meter
Z = 907420
70 Z = 286180
77
XDOT = 15171
993173 XDOT = 4640
917337
YDOT = 3700
466324 feet/sec YDOT = 1179
707794 meter/sec
ZDOT = -19890
088343 ZDOT = -6039
993803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21862695
07 X = 6663749
46
Y = -2526275
78 feet Y = -770008
86 meter
Z = 943430
18 Z = 287557
52
XDOT = 2488
535244 XDOT = 758
505542
YDOT = 13902
792185 feet/sec YDOT = 4237
571058 meter/sec
ZDOT = -19803
949629 ZDOT = -6036
243847
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 08011
54266626
00020000 00000-0 20000-3 0 9095
2 25544 51
6398 109
3261 0002306 45
6946 314
4408 15
78509358 3650
Satellite: ISS
Catalog Number: 25544
Epoch time: 08011
54266626 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 109
3261 deg
Eccentricity:
0002306
Arg of perigee: 45
6946 deg
Mean anomaly: 314
4408 deg
Mean motion: 15
78509358 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 365
Checksum: 297
Coasting Arc #11 (Orbit 372)
---------------------------------------
Vector Time (GMT): 2008/012/00:43:38
494
Vector Time (MET): N/A
Weight (LBS) : 540063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4347009
12 A = 6712515
57 meter
Y = -768055
83 meter E =
0009380
Z = -5065174
05 I = 51
93478
XDOT = -717
665305 Wp = 71
33052
YDOT = 7463
401962 meter/sec RA = 106
00792 deg
ZDOT = -1747
301410 TA = 181
91313
MA = 181
91672
Ha = 183
927 n
mi
Hp = 180
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14261840
93 X = 4379879
75
Y = -2519868
22 feet Y = -719260
96 meter
Z = -16618025
09 Z = -5043976
92
XDOT = -2354
544964 XDOT = -792
580969
YDOT = 24486
226910 feet/sec YDOT = 7454
957871 meter/sec
ZDOT = -5732
616176 ZDOT = -1750
969192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9566736
49 X = -2915941
28
Y = -10995953
77 feet Y = -3351566
71 meter
Z = -16537084
21 Z = -5040503
27
XDOT = 21370
254034 XDOT = 6513
653430
YDOT = -9949
715117 feet/sec YDOT = -3032
673168 meter/sec
ZDOT = -5745
845458 ZDOT = -1751
333696
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 08012
04913168
00020000 00000-0 20000-3 0 9103
2 25544 51
6404 106
7100 0004238 269
3231 90
7448 15
77021891 3736
Satellite: ISS
Catalog Number: 25544
Epoch time: 08012
04913168 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 106
7100 deg
Eccentricity:
0004238
Arg of perigee: 269
3231 deg
Mean anomaly: 90
7448 deg
Mean motion: 15
77021891 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 373
Checksum: 261
Coasting Arc #12 (Orbit 388)
---------------------------------------
Vector Time (GMT): 2008/013/00:43:38
494
Vector Time (MET): N/A
Weight (LBS) : 540063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 857776
31 A = 6723541
11 meter
Y = -6642153
11 meter E =
0010152
Z = 521941
10 I = 51
97832
XDOT = 4782
819147 Wp = 144
49498
YDOT = 139
019489 meter/sec RA = 100
85203 deg
ZDOT = -6041
041258 TA = 29
84482
MA = 29
78696
Ha = 183
962 n
mi
Hp = 180
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2814226
73 X = 929450
67
Y = -21791840
91 feet Y = -6632160
24 meter
Z = 1712405
18 Z = 526281
85
XDOT = 15691
663867 XDOT = 4810
254931
YDOT = 456
100685 feet/sec YDOT = 192
657412 meter/sec
ZDOT = -19819
689167 ZDOT = -6017
740067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19958062
17 X = -6083217
35
Y = 9188323
18 feet Y = 2800600
91 meter
Z = 1728295
52 Z = 526784
47
XDOT = -7330
589218 XDOT = -2234
363594
YDOT = -12180
976580 feet/sec YDOT = -3712
761662 meter/sec
ZDOT = -19730
606062 ZDOT = -6013
888728
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 08013
06302238
00020000 00000-0 20000-3 0 9117
2 25544 51
6401 101
4796 0004264 271
9520 88
1157 15
76998237 3896
Satellite: ISS
Catalog Number: 25544
Epoch time: 08013
06302238 = yrday
fracday
Element set: 911
Inclination: 51
6401 deg
RA of node: 101
4796 deg
Eccentricity:
0004264
Arg of perigee: 271
9520 deg
Mean anomaly: 88
1157 deg
Mean motion: 15
76998237 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 389
Checksum: 285
Coasting Arc #13 (Orbit 404)
---------------------------------------
Vector Time (GMT): 2008/014/00:43:38
494
Vector Time (MET): N/A
Weight (LBS) : 540063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4035427
31 A = 6711417
63 meter
Y = -1044331
73 meter E =
0002510
Z = 5261677
68 I = 51
94257
XDOT = 1211
836444 Wp = 315
02441
YDOT = -7587
445044 meter/sec RA = 95
71586 deg
ZDOT = -574
960896 TA = 140
42281
MA = 140
40449
Ha = 183
943 n
mi
Hp = 180
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13239590
92 X = -4049009
48
Y = -3426285
21 feet Y = -1089534
35 meter
Z = 17262722
03 Z = 5242040
77
XDOT = 3975
841351 XDOT = 1299
383372
YDOT = -24893
192403 feet/sec YDOT = -7573
404075 meter/sec
ZDOT = -1886
354645 ZDOT = -568
861560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4399325
40 X = 1340914
38
Y = 13048443
92 feet Y = 3977165
71 meter
Z = 17187548
32 Z = 5238764
73
XDOT = -22089
819404 XDOT = -6732
976954
YDOT = 9909
545060 feet/sec YDOT = 3020
429334 meter/sec
ZDOT = -1863
837166 ZDOT = -568
097568
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 08014
07689321
00020000 00000-0 20000-3 0 9121
2 25544 51
6402 96
2489 0004401 278
4203 81
6463 15
77088104 4051
Satellite: ISS
Catalog Number: 25544
Epoch time: 08014
07689321 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 96
2489 deg
Eccentricity:
0004401
Arg of perigee: 278
4203 deg
Mean anomaly: 81
6463 deg
Mean motion: 15
77088104 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 405
Checksum: 274
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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