Date:
January 15th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16414 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 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
022/09:06:27
407 1
5 3
3 3
3
N/A 2
7 0
0 185
4
000/00:00:54
815 1
1 0
0 179
6
024/09:02:53
473 -4
3 8
2 8
2
N/A -6
7 0
0 187
6
000/00:02:16
945 -1
9 0
0 183
4
Coasting Arc #1 (Orbit 3910)
---------------------------------------
Vector Time (GMT): 2010/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3917700
86 A = 6722532
47 meter
Y = -5459891
06 meter E =
0009126
Z = 133432
55 I = 51
38882
XDOT = 3831
904096 Wp = 80
42879
YDOT = 2905
063791 meter/sec RA = 304
75244 deg
ZDOT = 6015
907268 TA = 281
02701
MA = 281
12964
Ha = 186
226 n
mi
Hp = 178
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12853349
29 X = 3977814
97
Y = -17913028
42 feet Y = -5415744
92 meter
Z = 437770
82 Z = 152609
72
XDOT = 12571
863832 XDOT = 3769
910695
YDOT = 9531
049184 feet/sec YDOT = 2947
567013 meter/sec
ZDOT = 19737
228568 ZDOT = 6034
372125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21430617
29 X = 6532052
15
Y = 5171233
89 feet Y = 1576192
09 meter
Z = 513615
74 Z = 156550
08
XDOT = -3770
882327 XDOT = -1149
364933
YDOT = 13563
183534 feet/sec YDOT = 4134
058341 meter/sec
ZDOT = 19810
387018 ZDOT = 6038
205963
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 10013
56305587
00016717 00000-0 10270-3 0 9001
2 25544 51
6441 305
0416 0007146 181
5663 178
5481 15
77390747 39118
Satellite: ISS
Catalog Number: 25544
Epoch time: 10013
56305587 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 305
0416 deg
Eccentricity:
0007146
Arg of perigee: 181
5663 deg
Mean anomaly: 178
5481 deg
Mean motion: 15
77390747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3911
Checksum: 303
Coasting Arc #2 (Orbit 3925)
---------------------------------------
Vector Time (GMT): 2010/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2730157
62 A = 6711107
31 meter
Y = -3439338
37 meter E =
0016284
Z = -5088370
25 I = 51
33496
XDOT = 4702
092271 Wp = 126
89683
YDOT = -5912
240558 meter/sec RA = 299
55700 deg
ZDOT = 1466
904032 TA = 157
27017
MA = 157
19799
Ha = 186
037 n
mi
Hp = 178
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8957210
05 X = -2666777
57
Y = -11283918
53 feet Y = -3469513
63 meter
Z = -16694128
12 Z = -5101479
53
XDOT = 15426
811913 XDOT = 4760
728716
YDOT = -19397
114691 feet/sec YDOT = -5859
331300 meter/sec
ZDOT = 4812
677271 ZDOT = 1489
888047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6909402
23 X = 2105985
80
Y = -12573016
02 feet Y = -3832255
28 meter
Z = -16746097
21 Z = -5104210
43
XDOT = 22963
347818 XDOT = 6999
228415
YDOT = 6060
302655 feet/sec YDOT = 1847
180249 meter/sec
ZDOT = 4903
584821 ZDOT = 1494
612653
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 10014
51333734
00016717 00000-0 10270-3 0 9013
2 25544 51
6448 300
1371 0007110 185
2970 174
8121 15
77422348 39263
Satellite: ISS
Catalog Number: 25544
Epoch time: 10014
51333734 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 300
1371 deg
Eccentricity:
0007110
Arg of perigee: 185
2970 deg
Mean anomaly: 174
8121 deg
Mean motion: 15
77422348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3926
Checksum: 280
Coasting Arc #3 (Orbit 3941)
---------------------------------------
Vector Time (GMT): 2010/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4201136
96 A = 6719848
46 meter
Y = 4670296
05 meter E =
0011234
Z = -2370606
94 I = 51
35153
XDOT = -2473
865057 Wp = 164
83678
YDOT = -4943
691929 meter/sec RA = 294
40833 deg
ZDOT = -5371
772434 TA = 42
04048
MA = 41
95433
Ha = 185
799 n
mi
Hp = 178
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13783257
73 X = -4241533
09
Y = 15322493
59 feet Y = 4623090
82 meter
Z = -7777581
83 Z = -2391113
23
XDOT = -8116
355173 XDOT = -2392
305483
YDOT = -16219
461709 feet/sec YDOT = -4970
899585 meter/sec
ZDOT = -17623
925310 ZDOT = -5383
592581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19591738
09 X = -5971561
77
Y = -6297021
29 feet Y = -1919332
09 meter
Z = -7858696
09 Z = -2395330
57
XDOT = 11084
705966 XDOT = 3378
618378
YDOT = -12500
790037 feet/sec YDOT = -3810
240803 meter/sec
ZDOT = -17670
826290 ZDOT = -5386
067853
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 10015
52695061
00016717 00000-0 10270-3 0 9020
2 25544 51
6453 294
9060 0007119 189
3342 170
7691 15
77456424 39428
Satellite: ISS
Catalog Number: 25544
Epoch time: 10015
52695061 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 294
9060 deg
Eccentricity:
0007119
Arg of perigee: 189
3342 deg
Mean anomaly: 170
7691 deg
Mean motion: 15
77456424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3942
Checksum: 312
Coasting Arc #4 (Orbit 3957)
---------------------------------------
Vector Time (GMT): 2010/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1649083
94 A = 6715113
04 meter
Y = 5097344
50 meter E =
0009931
Z = 4037704
17 I = 51
32358
XDOT = -4851
814430 Wp = 116
73361
YDOT = 4608
471941 meter/sec RA = 289
17829 deg
ZDOT = -3833
496307 TA = 12
82737
MA = 12
80212
Ha = 185
650 n
mi
Hp = 178
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5410380
39 X = 1572348
03
Y = 16723571
20 feet Y = 5115356
15 meter
Z = 13247060
93 Z = 4045529
26
XDOT = -15918
026344 XDOT = -4884
364613
YDOT = 15119
658600 feet/sec YDOT = 4554
034400 meter/sec
ZDOT = -12577
087623 ZDOT = -3857
144520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12893849
62 X = -3930045
36
Y = 11911083
40 feet Y = 3630498
22 meter
Z = 13278155
27 Z = 4047181
73
XDOT = -19536
517165 XDOT = -5954
730432
YDOT = -7013
259879 feet/sec YDOT = -2137
641611 meter/sec
ZDOT = -12670
640177 ZDOT = -3862
011126
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 10016
54054319
00016717 00000-0 10270-3 0 9039
2 25544 51
6445 289
6749 0007088 192
9313 167
1671 15
77483318 39584
Satellite: ISS
Catalog Number: 25544
Epoch time: 10016
54054319 = yrday
fracday
Element set: 903
Inclination: 51
6445 deg
RA of node: 289
6749 deg
Eccentricity:
0007088
Arg of perigee: 192
9313 deg
Mean anomaly: 167
1671 deg
Mean motion: 15
77483318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 337
Coasting Arc #5 (Orbit 3973)
---------------------------------------
Vector Time (GMT): 2010/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4218654
72 A = 6714577
60 meter
Y = -3173144
91 meter E =
0012323
Z = 4149219
47 I = 51
31359
XDOT = 1368
181323 Wp = 140
53902
YDOT = 6636
105407 meter/sec RA = 284
04405 deg
ZDOT = 3668
574923 TA = 271
80357
MA = 271
94471
Ha = 185
482 n
mi
Hp = 178
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13840730
70 X = 4233668
18
Y = -10410580
41 feet Y = -3125885
73 meter
Z = 13612924
77 Z = 4169749
46
XDOT = 4488
783867 XDOT = 1276
052699
YDOT = 21771
999366 feet/sec YDOT = 6650
889872 meter/sec
ZDOT = 12036
006965 ZDOT = 3674
998026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15393196
31 X = 4691846
24
Y = 7795982
42 feet Y = 2376215
44 meter
Z = 13694155
58 Z = 4173978
62
XDOT = -17056
148791 XDOT = -5198
714151
YDOT = 12402
471543 feet/sec YDOT = 3780
273326 meter/sec
ZDOT = 12061
594556 ZDOT = 3676
374021
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 10017
55411406
00016717 00000-0 10270-3 0 9046
2 25544 51
6447 284
4428 0007053 197
1716 162
9211 15
77518224 39745
Satellite: ISS
Catalog Number: 25544
Epoch time: 10017
55411406 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node: 284
4428 deg
Eccentricity:
0007053
Arg of perigee: 197
1716 deg
Mean anomaly: 162
9211 deg
Mean motion: 15
77518224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3974
Checksum: 305
Coasting Arc #6 (Orbit 3988)
---------------------------------------
Vector Time (GMT): 2010/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -787134
23 A = 6719948
28 meter
Y = -6309505
93 meter E =
0002542
Z = -2179576
34 I = 51
32628
XDOT = 4815
193903 Wp = 141
65882
YDOT = -2489
264014 meter/sec RA = 278
81308 deg
ZDOT = 5468
475832 TA = 193
80036
MA = 193
80731
Ha = 185
303 n
mi
Hp = 178
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2582461
39 X = -705933
97
Y = -20700478
77 feet Y = -6317854
02 meter
Z = -7150841
00 Z = -2183203
20
XDOT = 15797
880258 XDOT = 4816
107152
YDOT = -8166
876685 feet/sec YDOT = -2435
412802 meter/sec
ZDOT = 17941
193673 ZDOT = 5491
869623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17287611
17 X = 5269263
88
Y = -11666601
18 feet Y = -3555980
04 meter
Z = -7165359
19 Z = -2184001
48
XDOT = 13552
825224 XDOT = 4130
901128
YDOT = 9009
586359 feet/sec YDOT = 2746
121922 meter/sec
ZDOT = 18033
778907 ZDOT = 5496
695811
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 10018
50431743
00016717 00000-0 10270-3 0 9059
2 25544 51
6449 279
5376 0007068 201
4416 158
6454 15
77569963 39899
Satellite: ISS
Catalog Number: 25544
Epoch time: 10018
50431743 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 279
5376 deg
Eccentricity:
0007068
Arg of perigee: 201
4416 deg
Mean anomaly: 158
6454 deg
Mean motion: 15
77569963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 342
Coasting Arc #7 (Orbit 4004)
---------------------------------------
Vector Time (GMT): 2010/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4194784
64 A = 6710287
11 meter
Y = 1050876
78 meter E =
0011830
Z = -5139902
35 I = 51
29057
XDOT = -463
051826 Wp = 109
83001
YDOT = -7594
227151 meter/sec RA = 273
65644 deg
ZDOT = -1180
928231 TA = 148
86939
MA = 148
79926
Ha = 184
994 n
mi
Hp = 178
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13762416
79 X = -4181255
74
Y = 3447758
46 feet Y = 1004044
01 meter
Z = -16863196
70 Z = -5160247
32
XDOT = -1519
198903 XDOT = -372
360799
YDOT = -24915
443410 feet/sec YDOT = -7598
898155 meter/sec
ZDOT = -3874
436454 ZDOT = -1182
957639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9458801
19 X = -2883042
60
Y = -10445056
97 feet Y = -3183653
36 meter
Z = -16943742
86 Z = -5164452
82
XDOT = 20534
317254 XDOT = 6258
859899
YDOT = -12329
643285 feet/sec YDOT = -3758
075273 meter/sec
ZDOT = -3882
672225 ZDOT = -1183
438494
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 10019
51784752
00016717 00000-0 10270-3 0 9063
2 25544 51
6449 274
3053 0006987 206
0184 154
0631 15
77609546 40055
Satellite: ISS
Catalog Number: 25544
Epoch time: 10019
51784752 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 274
3053 deg
Eccentricity:
0006987
Arg of perigee: 206
0184 deg
Mean anomaly: 154
0631 deg
Mean motion: 15
77609546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4005
Checksum: 312
Coasting Arc #8 (Orbit 4020)
---------------------------------------
Vector Time (GMT): 2010/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 38663
85 A = 6721999
13 meter
Y = 6709680
07 meter E =
0015583
Z = -176809
05 I = 51
32894
XDOT = -4821
213500 Wp = 162
47883
YDOT = -126
793740 meter/sec RA = 268
46143 deg
ZDOT = -6017
665450 TA = 19
45465
MA = 19
39525
Ha = 184
979 n
mi
Hp = 179
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 126849
91 X = -35508
96
Y = 22013386
05 feet Y = 6709697
71 meter
Z = -580082
19 Z = -176801
23
XDOT = -15817
629594 XDOT = -4790
205087
YDOT = -415
989960 feet/sec YDOT = -180
533889 meter/sec
ZDOT = -19742
996884 ZDOT = -6041
011213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19192395
71 X = -5849842
21
Y = 10782274
96 feet Y = 3286437
41 meter
Z = -579866
56 Z = -176743
33
XDOT = -6458
869349 XDOT = -1968
663378
YDOT = -12536
718677 feet/sec YDOT = -3821
191853 meter/sec
ZDOT = -19835
459863 ZDOT = -6045
848166
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 10020
53135824
00016717 00000-0 10270-3 0 9078
2 25544 51
6447 269
0730 0007176 209
7428 150
3330 15
77580270 40213
Satellite: ISS
Catalog Number: 25544
Epoch time: 10020
53135824 = yrday
fracday
Element set: 907
Inclination: 51
6447 deg
RA of node: 269
0730 deg
Eccentricity:
0007176
Arg of perigee: 209
7428 deg
Mean anomaly: 150
3330 deg
Mean motion: 15
77580270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4021
Checksum: 285
Coasting Arc #9 (Orbit 4036)
---------------------------------------
Vector Time (GMT): 2010/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4227747
49 A = 6710415
05 meter
Y = 1271522
06 meter E =
0002864
Z = 5053048
33 I = 51
29296
XDOT = -383
053874 Wp = 182
31898
YDOT = 7534
589038 meter/sec RA = 263
25921 deg
ZDOT = -1578
330405 TA = 282
87828
MA = 282
91027
Ha = 184
479 n
mi
Hp = 179
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13870562
62 X = 4188668
40
Y = 4171660
31 feet Y = 1318580
62 meter
Z = 16578242
55 Z = 5073491
58
XDOT = -1256
738433 XDOT = -459
611361
YDOT = 24719
780309 feet/sec YDOT = 7529
877484 meter/sec
ZDOT = -5178
249360 ZDOT = -1580
377040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3267009
40 X = 995784
46
Y = 14015333
92 feet Y = 4271873
78 meter
Z = 16659245
11 Z = 5077737
91
XDOT = -21004
153551 XDOT = -6402
066002
YDOT = 11049
506306 feet/sec YDOT = 3367
889522 meter/sec
ZDOT = -5186
139568 ZDOT = -1580
735340
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 10021
54484496
00016717 00000-0 10270-3 0 9083
2 25544 51
6446 263
8401 0007026 215
7002 144
3694 15
77690871 40370
Satellite: ISS
Catalog Number: 25544
Epoch time: 10021
54484496 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 263
8401 deg
Eccentricity:
0007026
Arg of perigee: 215
7002 deg
Mean anomaly: 144
3694 deg
Mean motion: 15
77690871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4037
Checksum: 307
Coasting Arc #10 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2010/022/09:06:54
815
Vector Time (MET): N/A
Weight (LBS) : 751525
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3200370
32 A = 6713443
01 meter
Y = -3479050
26 meter E =
0009115
Z = 4766432
11 I = 51
29969
XDOT = 3328
272637 Wp = 151
84310
YDOT = 6488
222460 meter/sec RA = 258
72803 deg
ZDOT = 2491
191066 TA = 273
63326
MA = 273
73750
Ha = 185
415 n
mi
Hp = 179
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10499902
62 X = 3215881
57
Y = -11414206
88 feet Y = -3443175
23 meter
Z = 15637900
62 Z = 4782016
93
XDOT = 10919
529650 XDOT = 3243
371183
YDOT = 21286
819095 feet/sec YDOT = 6524
966394 meter/sec
ZDOT = 8173
199037 ZDOT = 2507
153625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8905864
81 X = 2714507
59
Y = 12620875
90 feet Y = 3846842
98 meter
Z = 15699524
61 Z = 4785215
10
XDOT = -22207
811748 XDOT = -6768
941021
YDOT = 5384
919602 feet/sec YDOT = 1641
323495 meter/sec
ZDOT = 8236
611333 ZDOT = 2510
519134
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 10022
43165763
00016717 00000-0 10270-3 0 9096
2 25544 51
6430 259
2610 0004809 204
0026 156
0916 15
77073549 40517
Satellite: ISS
Catalog Number: 25544
Epoch time: 10022
43165763 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 259
2610 deg
Eccentricity:
0004809
Arg of perigee: 204
0026 deg
Mean anomaly: 156
0916 deg
Mean motion: 15
77073549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 287
Coasting Arc #11 (Orbit 4065)
---------------------------------------
Vector Time (GMT): 2010/023/09:06:54
815
Vector Time (MET): N/A
Weight (LBS) : 751525
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2773347
63 A = 6722770
09 meter
Y = -6004754
24 meter E =
0004658
Z = -1194085
64 I = 51
33873
XDOT = 3996
684502 Wp = 46
52813
YDOT = -3007
114059 meter/sec RA = 253
51418 deg
ZDOT = 5856
860737 TA = 300
32074
MA = 300
36681
Ha = 185
300 n
mi
Hp = 179
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9098909
55 X = -2700194
68
Y = -19700637
28 feet Y = -6035358
39 meter
Z = -3917603
81 Z = -1207381
03
XDOT = 13112
481961 XDOT = 4001
562184
YDOT = -9865
859772 feet/sec YDOT = -2962
393739 meter/sec
ZDOT = 19215
422364 ZDOT = 5876
288206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21109876
79 X = 6434290
45
Y = -4986136
59 feet Y = -1519774
43 meter
Z = -3970444
26 Z = -1210191
41
XDOT = 6726
168565 XDOT = 2050
136179
YDOT = 13159
213565 feet/sec YDOT = 4010
928295 meter/sec
ZDOT = 19292
281393 ZDOT = 5880
287368
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 10023
38214307
00016717 00000-0 10270-3 0 9102
2 25544 51
6433 254
3576 0004697 208
6274 151
4633 15
77083466 40667
Satellite: ISS
Catalog Number: 25544
Epoch time: 10023
38214307 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 254
3576 deg
Eccentricity:
0004697
Arg of perigee: 208
6274 deg
Mean anomaly: 151
4633 deg
Mean motion: 15
77083466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4066
Checksum: 303
Coasting Arc #12 (Orbit 4081)
---------------------------------------
Vector Time (GMT): 2010/024/09:04:01
945
Vector Time (MET): N/A
Weight (LBS) : 750815
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3249337
67 A = 6716148
86 meter
Y = 2909166
28 meter E =
0006163
Z = -5111181
47 I = 51
31255
XDOT = -3771
451002 Wp = 122
53899
YDOT = -6576
610117 meter/sec RA = 248
36590 deg
ZDOT = -1350
076373 TA = 134
50633
MA = 134
45595
Ha = 187
595 n
mi
Hp = 183
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10660556
67 X = -3256797
97
Y = 9544508
79 feet Y = 2872788
85 meter
Z = -16768968
06 Z = -5126984
58
XDOT = -12373
526909 XDOT = -3691
071504
YDOT = -21576
804845 feet/sec YDOT = -6618
335208 meter/sec
ZDOT = -4429
384427 ZDOT = -1368
203102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7314739
87 X = -2229532
71
Y = -12212262
15 feet Y = -3722297
50 meter
Z = -16831477
66 Z = -5130234
39
XDOT = 22671
191184 XDOT = 6910
179073
YDOT = -7395
335683 feet/sec YDOT = -2254
098316 meter/sec
ZDOT = -4501
385848 ZDOT = -1372
022406
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 10024
39598009
00016717 00000-0 10270-3 0 9119
2 25544 51
6440 249
1274 0010452 235
9750 124
0422 15
75602551 40820
Satellite: ISS
Catalog Number: 25544
Epoch time: 10024
39598009 = yrday
fracday
Element set: 911
Inclination: 51
6440 deg
RA of node: 249
1274 deg
Eccentricity:
0010452
Arg of perigee: 235
9750 deg
Mean anomaly: 124
0422 deg
Mean motion: 15
75602551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4082
Checksum: 283
Coasting Arc #13 (Orbit 4097)
---------------------------------------
Vector Time (GMT): 2010/025/09:08:01
945
Vector Time (MET): N/A
Weight (LBS) : 750815
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2425473
39 A = 6727421
81 meter
Y = 6213864
48 meter E =
0013687
Z = -799658
20 I = 51
36271
XDOT = -4774
940503 Wp = 190
89919
YDOT = 1097
633843 meter/sec RA = 243
17875 deg
ZDOT = -5950
426522 TA = 357
86584
MA = 357
87168
Ha = 187
512 n
mi
Hp = 183
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7957589
85 X = 2359693
15
Y = 20386694
50 feet Y = 6240619
83 meter
Z = -2623550
54 Z = -788034
64
XDOT = -15665
815300 XDOT = -4757
953720
YDOT = 3601
160903 feet/sec YDOT = 1044
333084 meter/sec
ZDOT = -19522
396727 ZDOT = -5973
581628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21398551
36 X = -6522278
45
Y = 4613352
77 feet Y = 1406149
92 meter
Z = -2577313
04 Z = -785565
01
XDOT = -733
495799 XDOT = -223
569519
YDOT = -14366
074963 feet/sec YDOT = -4378
779649 meter/sec
ZDOT = -19614
091221 ZDOT = -5978
375004
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 10025
41078270
00016717 00000-0 10270-3 0 9127
2 25544 51
6441 243
9041 0010613 239
7090 120
3024 15
75579161 40987
Satellite: ISS
Catalog Number: 25544
Epoch time: 10025
41078270 = yrday
fracday
Element set: 912
Inclination: 51
6441 deg
RA of node: 243
9041 deg
Eccentricity:
0010613
Arg of perigee: 239
7090 deg
Mean anomaly: 120
3024 deg
Mean motion: 15
75579161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4098
Checksum: 278
Coasting Arc #14 (Orbit 4113)
---------------------------------------
Vector Time (GMT): 2010/026/09:08:01
945
Vector Time (MET): N/A
Weight (LBS) : 750815
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4352415
60 A = 6716086
54 meter
Y = -692819
52 meter E =
0005980
Z = 5072310
84 I = 51
33992
XDOT = 2900
244278 Wp = 253
40281
YDOT = 6964
550355 meter/sec RA = 237
98975 deg
ZDOT = -1540
527207 TA = 211
42488
MA = 211
46062
Ha = 186
972 n
mi
Hp = 183
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14279578
74 X = 4335199
30
Y = -2273029
92 feet Y = -644244
99 meter
Z = 16641439
76 Z = 5093412
72
XDOT = 9515
237132 XDOT = 2829
633398
YDOT = 22849
574657 feet/sec YDOT = 6996
587946 meter/sec
ZDOT = -5054
223119 ZDOT = -1526
608839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 224733
46 X = 68498
76
Y = 14360838
40 feet Y = 4377183
54 meter
Z = 16725022
17 Z = 5097786
76
XDOT = -22930
818834 XDOT = -6989
313581
YDOT = 6168
557062 feet/sec YDOT = 1880
176193 meter/sec
ZDOT = -4998
861382 ZDOT = -1523
652949
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 10026
42556499
00016717 00000-0 10270-3 0 9134
2 25544 51
6438 238
6806 0010595 244
9977 115
0087 15
75676918 41141
Satellite: ISS
Catalog Number: 25544
Epoch time: 10026
42556499 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 238
6806 deg
Eccentricity:
0010595
Arg of perigee: 244
9977 deg
Mean anomaly: 115
0087 deg
Mean motion: 15
75676918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4114
Checksum: 339
Coasting Arc #15 (Orbit 4129)
---------------------------------------
Vector Time (GMT): 2010/027/09:08:01
945
Vector Time (MET): N/A
Weight (LBS) : 750815
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2586490
81 A = 6725939
71 meter
Y = -5912180
79 meter E =
0003676
Z = 1889097
09 I = 51
38969
XDOT = 5246
617128 Wp = 60
30615
YDOT = -499
358040 meter/sec RA = 232
85186 deg
ZDOT = 5614
321103 TA = 320
76579
MA = 320
79242
Ha = 186
815 n
mi
Hp = 183
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8485862
23 X = -2529364
24
Y = -19396918
61 feet Y = -5940785
25 meter
Z = 6197825
10 Z = 1876670
29
XDOT = 17213
310787 XDOT = 5224
538257
YDOT = -1638
313779 feet/sec YDOT = -440
811298 meter/sec
ZDOT = 18419
688659 ZDOT = 5639
755012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20314236
43 X = 6191779
26
Y = -6016011
50 feet Y = -1833680
31 meter
Z = 6148394
03 Z = 1874030
50
XDOT = -964
189780 XDOT = -293
885045
YDOT = 15693
753256 feet/sec YDOT = 4783
455992 meter/sec
ZDOT = 18520
453083 ZDOT = 5645
034100
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 10027
44033255
00016717 00000-0 10270-3 0 9148
2 25544 51
6436 233
4562 0010493 249
2561 110
7479 15
75655856 41308
Satellite: ISS
Catalog Number: 25544
Epoch time: 10027
44033255 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 233
4562 deg
Eccentricity:
0010493
Arg of perigee: 249
2561 deg
Mean anomaly: 110
7479 deg
Mean motion: 15
75655856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4130
Checksum: 300
Coasting Arc #16 (Orbit 4144)
---------------------------------------
Vector Time (GMT): 2010/028/09:08:01
945
Vector Time (MET): N/A
Weight (LBS) : 750815
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4837053
57 A = 6717755
31 meter
Y = 219234
03 meter E =
0006727
Z = -4659768
43 I = 51
38160
XDOT = -2970
640975 Wp = 177
41546
YDOT = -6542
268366 meter/sec RA = 227
64653 deg
ZDOT = 2769
388978 TA = 120
02460
MA = 119
95784
Ha = 186
408 n
mi
Hp = 183
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15869598
34 X = -4816509
85
Y = 719271
74 feet Y = 165258
55 meter
Z = -15287954
17 Z = -4683216
32
XDOT = -9746
197423 XDOT = -2910
716238
YDOT = -21464
135059 feet/sec YDOT = -6575
153042 meter/sec
ZDOT = 9085
921843 ZDOT = 2755
102891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 999534
35 X = 304658
07
Y = -15764288
46 feet Y = -4804955
12 meter
Z = -15380870
79 Z = -4688089
42
XDOT = 21251
861939 XDOT = 6477
567519
YDOT = -7482
594918 feet/sec YDOT = -2280
694931 meter/sec
ZDOT = 9029
086634 ZDOT = 2752
065606
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 10028
39165839
00016717 00000-0 10270-3 0 9158
2 25544 51
6433 228
5587 0010612 253
1695 106
8306 15
75703914 41452
Satellite: ISS
Catalog Number: 25544
Epoch time: 10028
39165839 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 228
5587 deg
Eccentricity:
0010612
Arg of perigee: 253
1695 deg
Mean anomaly: 106
8306 deg
Mean motion: 15
75703914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4145
Checksum: 314
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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