Date:
February 6th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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
There are no maneuvers
Coasting Arc #1 (Orbit 241)
---------------------------------------
Vector Time (GMT): 2010/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2917649
44 A = 6716487
98 meter
Y = -3337149
60 meter E =
0008138
Z = 5052916
56 I = 51
52789
XDOT = 6731
228793 Wp = 303
83728
YDOT = 3333
876095 meter/sec RA = 196
09654 deg
ZDOT = -1682
389144 TA = 162
38691
MA = 162
35867
Ha = 185
807 n
mi
Hp = 183
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9572340
68 X = 2930203
45
Y = -10948653
54 feet Y = -3304452
43 meter
Z = 16577810
22 Z = 5067120
81
XDOT = 22084
083968 XDOT = 6701
621126
YDOT = 10937
913696 feet/sec YDOT = 3408
983109 meter/sec
ZDOT = -5519
649422 ZDOT = -1649
761367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14470765
42 X = 4410689
30
Y = -483400
15 feet Y = -147340
36 meter
Z = 16633994
85 Z = 5070041
63
XDOT = 6960
525226 XDOT = 2121
568089
YDOT = 22605
223140 feet/sec YDOT = 6890
072013 meter/sec
ZDOT = -5390
137080 ZDOT = -1642
913782
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 10034
54478490
00016717 00000-0 10270-3 0 9006
2 25544 51
6406 196
9055 0011011 278
2414 81
7501 15
75582575 2421
Satellite: ISS
Catalog Number: 25544
Epoch time: 10034
54478490 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 196
9055 deg
Eccentricity:
0011011
Arg of perigee: 278
2414 deg
Mean anomaly: 81
7501 deg
Mean motion: 15
75582575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 242
Checksum: 291
Coasting Arc #2 (Orbit 257)
---------------------------------------
Vector Time (GMT): 2010/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5797324
89 A = 6725717
17 meter
Y = -2744366
44 meter E =
0007866
Z = 2005974
00 I = 51
59001
XDOT = 3723
214129 Wp = 16
97557
YDOT = -3786
310708 meter/sec RA = 190
97490 deg
ZDOT = 5582
075611 TA = 5
41549
MA = 5
40699
Ha = 186
131 n
mi
Hp = 183
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19020094
77 X = -5775950
55
Y = -9003826
91 feet Y = -2809076
05 meter
Z = 6581279
52 Z = 1977862
92
XDOT = 12215
269453 XDOT = 3738
160279
YDOT = -12422
279225 feet/sec YDOT = -3744
591939 meter/sec
ZDOT = 18313
896360 ZDOT = 5600
199040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6683037
13 X = -2036989
72
Y = -19990653
69 feet Y = -6093151
24 meter
Z = 6469692
75 Z = 1971962
35
XDOT = 15887
911952 XDOT = 4842
635563
YDOT = 636
717332 feet/sec YDOT = 194
071443 meter/sec
ZDOT = 18385
609061 ZDOT = 5603
933642
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 10035
55955433
00016717 00000-0 10270-3 0 9016
2 25544 51
6415 191
6814 0011089 281
9771 78
0149 15
75676602 2587
Satellite: ISS
Catalog Number: 25544
Epoch time: 10035
55955433 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 191
6814 deg
Eccentricity:
0011089
Arg of perigee: 281
9771 deg
Mean anomaly: 78
0149 deg
Mean motion: 15
75676602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 258
Checksum: 317
Coasting Arc #3 (Orbit 272)
---------------------------------------
Vector Time (GMT): 2010/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3572748
21 A = 6717966
84 meter
Y = 3319492
92 meter E =
0000694
Z = -4620243
24 I = 51
59472
XDOT = -6495
087991 Wp = 216
59625
YDOT = -2963
006141 meter/sec RA = 185
78407 deg
ZDOT = 2892
938055 TA = 82
04471
MA = 82
03683
Ha = 186
374 n
mi
Hp = 183
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11721614
85 X = -3587157
83
Y = 10890724
80 feet Y = 3279459
84 meter
Z = -15158278
34 Z = -4637634
36
XDOT = -21309
343802 XDOT = -6475
525583
YDOT = -9721
148755 feet/sec YDOT = -3035
528729 meter/sec
ZDOT = 9491
266586 ZDOT = 2861
432815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15923634
09 X = -4853523
67
Y = -591954
04 feet Y = -180427
59 meter
Z = -15227114
36 Z = -4641224
46
XDOT = -8183
668565 XDOT = -2494
382179
YDOT = -20854
268288 feet/sec YDOT = -6356
380974 meter/sec
ZDOT = 9366
200617 ZDOT = 2854
817948
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 10036
51088204
00016717 00000-0 10270-3 0 9027
2 25544 51
6421 186
7847 0011036 286
1348 73
8601 15
75693239 2732
Satellite: ISS
Catalog Number: 25544
Epoch time: 10036
51088204 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 186
7847 deg
Eccentricity:
0011036
Arg of perigee: 286
1348 deg
Mean anomaly: 73
8601 deg
Mean motion: 15
75693239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 273
Checksum: 303
Coasting Arc #4 (Orbit 288)
---------------------------------------
Vector Time (GMT): 2010/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5477058
00 A = 6723334
43 meter
Y = 2458564
79 meter E =
0006553
Z = -3024315
92 I = 51
64297
XDOT = -4468
406110 Wp = 291
34241
YDOT = 3859
602489 meter/sec RA = 180
68039 deg
ZDOT = -4943
822385 TA = 283
66816
MA = 283
74111
Ha = 186
726 n
mi
Hp = 183
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17969350
40 X = 5463850
19
Y = 8066157
45 feet Y = 2519738
75 meter
Z = -9922296
32 Z = -2997740
77
XDOT = -14660
125032 XDOT = -4487
216926
YDOT = 12662
737826 feet/sec YDOT = 3809
529103 meter/sec
ZDOT = -16219
889714 ZDOT = -4965
575151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7282641
30 X = 2219749
07
Y = 18357726
91 feet Y = 5595435
16 meter
Z = -9816792
38 Z = -2992158
32
XDOT = -17929
536684 XDOT = -5464
922781
YDOT = -1626
186779 feet/sec YDOT = -495
661730 meter/sec
ZDOT = -16306
012836 ZDOT = -4970
072712
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 10037
52560813
00016717 00000-0 10270-3 0 9031
2 25544 51
6419 181
5604 0011078 290
5935 69
4040 15
75738184 2894
Satellite: ISS
Catalog Number: 25544
Epoch time: 10037
52560813 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 181
5604 deg
Eccentricity:
0011078
Arg of perigee: 290
5935 deg
Mean anomaly: 69
4040 deg
Mean motion: 15
75738184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 289
Checksum: 309
Coasting Arc #5 (Orbit 304)
---------------------------------------
Vector Time (GMT): 2010/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4207563
05 A = 6720367
85 meter
Y = -3458671
85 meter E =
0006679
Z = 3941043
59 I = 51
66363
XDOT = 5988
160404 Wp = 6
75886
YDOT = 2707
583133 meter/sec RA = 175
48235 deg
ZDOT = -4009
738048 TA = 124
87974
MA = 124
81693
Ha = 186
939 n
mi
Hp = 183
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13804340
73 X = 4226781
28
Y = -11347348
60 feet Y = -3411513
10 meter
Z = 12929933
04 Z = 3961530
11
XDOT = 19646
195552 XDOT = 5976
916916
YDOT = 8883
146761 feet/sec YDOT = 2774
483594 meter/sec
ZDOT = -13155
308556 ZDOT = -3980
675273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17773574
20 X = 5417385
42
Y = 1147890
88 feet Y = 349877
14 meter
Z = 13011061
38 Z = 3965771
51
XDOT = 8355
855104 XDOT = 2546
864636
YDOT = 18690
866389 feet/sec YDOT = 5696
976075 meter/sec
ZDOT = -13039
914666 ZDOT = -3974
565990
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 10038
54031194
00016717 00000-0 10270-3 0 9040
2 25544 51
6420 176
3360 0011018 294
2711 65
7302 15
75745372 3050
Satellite: ISS
Catalog Number: 25544
Epoch time: 10038
54031194 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 176
3360 deg
Eccentricity:
0011018
Arg of perigee: 294
2711 deg
Mean anomaly: 65
7302 deg
Mean motion: 15
75745372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 305
Checksum: 274
Coasting Arc #6 (Orbit 320)
---------------------------------------
Vector Time (GMT): 2010/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4925473
31 A = 6720306
16 meter
Y = -2319401
19 meter E =
0003497
Z = 3936336
34 I = 51
69515
XDOT = 5140
045613 Wp = 20
18849
YDOT = -4092
824598 meter/sec RA = 170
38799 deg
ZDOT = 4022
212773 TA = 28
11300
MA = 28
09412
Ha = 187
197 n
mi
Hp = 183
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16159689
34 X = -4918292
89
Y = -7609583
94 feet Y = -2374440
78 meter
Z = 12914489
30 Z = 3912426
24
XDOT = 16863
666709 XDOT = 5165
891522
YDOT = -13427
902225 feet/sec YDOT = -4035
201235 meter/sec
ZDOT = 13196
236132 ZDOT = 4047
245170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6891268
11 X = -2100458
52
Y = -16552800
80 feet Y = -5045293
68 meter
Z = 12819538
64 Z = 3907395
38
XDOT = 20245
581557 XDOT = 6170
853259
YDOT = 1862
596878 feet/sec YDOT = 567
719528 meter/sec
ZDOT = 13295
385642 ZDOT = 4052
433544
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 10039
55498973
00016717 00000-0 10270-3 0 9055
2 25544 51
6431 171
1114 0011139 298
3094 61
6946 15
75833405 3217
Satellite: ISS
Catalog Number: 25544
Epoch time: 10039
55498973 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 171
1114 deg
Eccentricity:
0011139
Arg of perigee: 298
3094 deg
Mean anomaly: 61
6946 deg
Mean motion: 15
75833405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 321
Checksum: 306
Coasting Arc #7 (Orbit 335)
---------------------------------------
Vector Time (GMT): 2010/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4711869
54 A = 6722932
33 meter
Y = 3711743
68 meter E =
0008977
Z = -3022906
36 I = 51
73414
XDOT = -5270
274263 Wp = 325
94694
YDOT = -2652
371666 meter/sec RA = 165
19429 deg
ZDOT = 4958
362965 TA = 359
07942
MA = 359
08107
Ha = 187
376 n
mi
Hp = 182
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15458889
56 X = -4738340
36
Y = 12177636
73 feet Y = 3658904
88 meter
Z = -9917671
78 Z = -3045860
18
XDOT = -17290
926061 XDOT = -5264
309495
YDOT = -8702
006778 feet/sec YDOT = -2711
273849 meter/sec
ZDOT = 16267
595031 ZDOT = 4932
775002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19606851
50 X = -5976168
34
Y = -1015664
62 feet Y = -309574
58 meter
Z = -10008602
09 Z = -3050621
92
XDOT = -7392
751765 XDOT = -2253
310738
YDOT = -16582
302675 feet/sec YDOT = -5054
285855 meter/sec
ZDOT = 16165
961239 ZDOT = 4927
384986
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 10040
50623146
00016717 00000-0 10270-3 0 9065
2 25544 51
6435 166
2141 0011216 302
9767 57
0319 15
75822455 3363
Satellite: ISS
Catalog Number: 25544
Epoch time: 10040
50623146 = yrday
fracday
Element set: 906
Inclination: 51
6435 deg
RA of node: 166
2141 deg
Eccentricity:
0011216
Arg of perigee: 302
9767 deg
Mean anomaly: 57
0319 deg
Mean motion: 15
75822455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 336
Checksum: 282
Coasting Arc #8 (Orbit 351)
---------------------------------------
Vector Time (GMT): 2010/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4227698
48 A = 6717531
99 meter
Y = 2373221
94 meter E =
0010366
Z = -4655392
97 I = 51
74550
XDOT = -5624
216739 Wp = 6
47887
YDOT = 4421
100554 meter/sec RA = 160
09866 deg
ZDOT = -2844
240528 TA = 235
40687
MA = 235
50470
Ha = 187
625 n
mi
Hp = 182
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13870401
84 X = 4223460
89
Y = 7786161
23 feet Y = 2420475
01 meter
Z = -15273599
00 Z = -4634865
63
XDOT = -18452
154657 XDOT = -5659
419858
YDOT = 14504
923079 feet/sec YDOT = 4358
010482 meter/sec
ZDOT = -9331
497795 ZDOT = -2871
647565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5607358
29 X = 1709122
81
Y = 14968449
19 feet Y = 4562383
31 meter
Z = -15192045
35 Z = -4630535
42
XDOT = -22320
592111 XDOT = -6803
316475
YDOT = -1251
310722 feet/sec YDOT = -381
399508 meter/sec
ZDOT = -9440
082624 ZDOT = -2877
337184
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 10041
52086557
00016717 00000-0 10270-3 0 9078
2 25544 51
6440 160
9899 0011224 306
6988 53
3144 15
75866988 3527
Satellite: ISS
Catalog Number: 25544
Epoch time: 10041
52086557 = yrday
fracday
Element set: 907
Inclination: 51
6440 deg
RA of node: 160
9899 deg
Eccentricity:
0011224
Arg of perigee: 306
6988 deg
Mean anomaly: 53
3144 deg
Mean motion: 15
75866988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 352
Checksum: 329
Coasting Arc #9 (Orbit 367)
---------------------------------------
Vector Time (GMT): 2010/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5057944
93 A = 6725159
87 meter
Y = -4009197
20 meter E =
0004958
Z = 1889851
53 I = 51
80015
XDOT = 4380
917079 Wp = 68
72261
YDOT = 2857
689275 meter/sec RA = 154
91945 deg
ZDOT = -5648
976409 TA = 90
32542
MA = 90
26860
Ha = 187
739 n
mi
Hp = 182
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16594307
50 X = 5093220
29
Y = -13153534
11 feet Y = -3952439
05 meter
Z = 6200300
29 Z = 1914507
90
XDOT = 14373
087531 XDOT = 4376
077153
YDOT = 9375
620982 feet/sec YDOT = 2906
652297 meter/sec
ZDOT = -18533
387168 ZDOT = -5627
706291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21143879
77 X = 6444654
55
Y = 319089
52 feet Y = 97258
49 meter
Z = 6297996
08 Z = 1919629
21
XDOT = 5283
633243 XDOT = 1610
451413
YDOT = 14888
094736 feet/sec YDOT = 4537
891276 meter/sec
ZDOT = -18448
856046 ZDOT = -5623
211323
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 10042
53547650
00016717 00000-0 10270-3 0 9087
2 25544 51
6444 155
7654 0011140 310
9550 49
0649 15
75902929 3687
Satellite: ISS
Catalog Number: 25544
Epoch time: 10042
53547650 = yrday
fracday
Element set: 908
Inclination: 51
6444 deg
RA of node: 155
7654 deg
Eccentricity:
0011140
Arg of perigee: 310
9550 deg
Mean anomaly: 49
0649 deg
Mean motion: 15
75902929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 368
Checksum: 308
Coasting Arc #10 (Orbit 383)
---------------------------------------
Vector Time (GMT): 2010/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3408557
61 A = 6715164
77 meter
Y = -2685624
77 meter E =
0006722
Z = 5127147
81 I = 51
79489
XDOT = 5895
509381 Wp = 321
81902
YDOT = -4742
417418 meter/sec RA = 149
81012 deg
ZDOT = 1441
445145 TA = 114
43821
MA = 114
36807
Ha = 187
929 n
mi
Hp = 182
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11182931
79 X = -3403179
12
Y = -8811104
88 feet Y = -2723711
17 meter
Z = 16821351
09 Z = 5110602
65
XDOT = 19342
222378 XDOT = 5941
099710
YDOT = -15559
112264 feet/sec YDOT = -4676
235419 meter/sec
ZDOT = 4729
150739 ZDOT = 1470
195387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3382454
05 X = -1030971
99
Y = -13909033
24 feet Y = -4239473
33 meter
Z = 16755571
73 Z = 5107098
26
XDOT = 23786
302250 XDOT = 7250
064926
YDOT = 25
270925 feet/sec YDOT = 7
702578 meter/sec
ZDOT = 4843
074961 ZDOT = 1476
169248
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 10043
55006212
00016717 00000-0 10270-3 0 9095
2 25544 51
6454 150
5403 0011263 315
2224 44
8030 15
75982805 3841
Satellite: ISS
Catalog Number: 25544
Epoch time: 10043
55006212 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 150
5403 deg
Eccentricity:
0011263
Arg of perigee: 315
2224 deg
Mean anomaly: 44
8030 deg
Mean motion: 15
75982805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 270
Coasting Arc #11 (Orbit 398)
---------------------------------------
Vector Time (GMT): 2010/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5167858
37 A = 6726428
22 meter
Y = 4245249
20 meter E =
0016981
Z = -602660
18 I = 51
85853
XDOT = -3453
689590 Wp = 359
29002
YDOT = -3351
044560 meter/sec RA = 144
65559 deg
ZDOT = 6025
111340 TA = 354
15759
MA = 354
17737
Ha = 188
170 n
mi
Hp = 181
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16954915
91 X = -5212017
89
Y = 13927982
95 feet Y = 4187212
22 meter
Z = -1977231
57 Z = -627872
23
XDOT = -11331
002593 XDOT = -3445
228929
YDOT = -10994
240683 feet/sec YDOT = -3389
618305 meter/sec
ZDOT = 19767
425656 ZDOT = 6008
354472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21918676
84 X = -6680812
70
Y = 790205
39 feet Y = 240854
60 meter
Z = -2077139
45 Z = -633112
11
XDOT = -2370
396560 XDOT = -722
496872
YDOT = -14086
063170 feet/sec YDOT = -4293
432054 meter/sec
ZDOT = 19700
772492 ZDOT = 6004
795456
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 10044
50121727
00016717 00000-0 10270-3 0 9102
2 25544 51
6457 145
6427 0011372 319
9440 40
0884 15
75962004 3997
Satellite: ISS
Catalog Number: 25544
Epoch time: 10044
50121727 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 145
6427 deg
Eccentricity:
0011372
Arg of perigee: 319
9440 deg
Mean anomaly: 40
0884 deg
Mean motion: 15
75962004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 399
Checksum: 293
Coasting Arc #12 (Orbit 414)
---------------------------------------
Vector Time (GMT): 2010/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2624040
03 A = 6714342
80 meter
Y = 3218192
56 meter E =
0012293
Z = -5283397
48 I = 51
84202
XDOT = -5901
159875 Wp = 42
87304
YDOT = 4943
306386 meter/sec RA = 139
52642 deg
ZDOT = 89
122793 TA = 227
91822
MA = 228
02283
Ha = 188
323 n
mi
Hp = 181
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8609055
22 X = 2613523
66
Y = 10558374
55 feet Y = 3247477
10 meter
Z = -17333981
25 Z = -5270675
95
XDOT = -19360
760744 XDOT = -5956
431149
YDOT = 16218
196803 feet/sec YDOT = 4877
007081 meter/sec
ZDOT = 292
397616 ZDOT = 60
321318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 752738
06 X = 229434
56
Y = 13666794
58 feet Y = 4165638
99 meter
Z = -17283348
11 Z = -5267964
50
XDOT = -24211
276056 XDOT = -7379
596942
YDOT = 1521
735158 feet/sec YDOT = 463
824876 meter/sec
ZDOT = 178
262311 ZDOT = 54
334352
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 10045
51575877
00016717 00000-0 10270-3 0 9114
2 25544 51
6455 140
4185 0011387 323
6056 36
4333 15
76020393 4154
Satellite: ISS
Catalog Number: 25544
Epoch time: 10045
51575877 = yrday
fracday
Element set: 911
Inclination: 51
6455 deg
RA of node: 140
4185 deg
Eccentricity:
0011387
Arg of perigee: 323
6056 deg
Mean anomaly: 36
4333 deg
Mean motion: 15
76020393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 415
Checksum: 292
Coasting Arc #13 (Orbit 430)
---------------------------------------
Vector Time (GMT): 2010/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5091695
80 A = 6726093
68 meter
Y = -4326942
84 meter E =
0001577
Z = -778589
42 I = 51
90332
XDOT = 2564
338484 Wp = 25
18531
YDOT = 4095
130437 meter/sec RA = 134
40047 deg
ZDOT = -5991
494852 TA = 163
27180
MA = 163
26660
Ha = 188
391 n
mi
Hp = 181
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16705038
71 X = 5143484
17
Y = -14196006
70 feet Y = -4269714
96 meter
Z = -2554427
22 Z = -753728
54
XDOT = 8413
184002 XDOT = 2547
460287
YDOT = 13435
467313 feet/sec YDOT = 4123
711668 meter/sec
ZDOT = -19657
135342 ZDOT = -5979
078849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21851785
82 X = 6660424
32
Y = -1891563
90 feet Y = -576548
68 meter
Z = -2455904
24 Z = -748559
61
XDOT = -964
813834 XDOT = -294
075256
YDOT = 14298
417388 feet/sec YDOT = 4358
157620 meter/sec
ZDOT = -19607
677183 ZDOT = -5976
420005
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 10046
53027737
00016717 00000-0 10270-3 0 9125
2 25544 51
6446 135
1936 0011310 327
8133 32
2340 15
76051530 4314
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
53027737 = yrday
fracday
Element set: 912
Inclination: 51
6446 deg
RA of node: 135
1936 deg
Eccentricity:
0011310
Arg of perigee: 327
8133 deg
Mean anomaly: 32
2340 deg
Mean motion: 15
76051530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 431
Checksum: 263
Coasting Arc #14 (Orbit 446)
---------------------------------------
Vector Time (GMT): 2010/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1893405
14 A = 6714949
61 meter
Y = -3974603
18 meter E =
0013130
Z = 5074646
35 I = 51
88731
XDOT = 5704
726546 Wp = 354
40501
YDOT = -4889
473515 meter/sec RA = 129
24559 deg
ZDOT = -1688
645263 TA = 111
84756
MA = 111
70786
Ha = 188
519 n
mi
Hp = 180
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6211959
12 X = -1873470
90
Y = -13040036
68 feet Y = -3995664
56 meter
Z = 16649102
19 Z = 5065497
07
XDOT = 18716
294443 XDOT = 5767
180481
YDOT = -16041
579775 feet/sec YDOT = -4825
330795 meter/sec
ZDOT = -5540
174749 ZDOT = -1660
780260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2160834
52 X = 658622
36
Y = -14323941
70 feet Y = -4365937
43 meter
Z = 16612618
24 Z = 5063526
04
XDOT = 23488
185592 XDOT = 7159
198968
YDOT = -2801
402614 feet/sec YDOT = -853
867517 meter/sec
ZDOT = -5429
740898 ZDOT = -1654
985026
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 10047
54477047
00016717 00000-0 10270-3 0 9131
2 25544 51
6452 129
9675 0011497 331
6773 28
3765 15
76129407 4474
Satellite: ISS
Catalog Number: 25544
Epoch time: 10047
54477047 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 129
9675 deg
Eccentricity:
0011497
Arg of perigee: 331
6773 deg
Mean anomaly: 28
3765 deg
Mean motion: 15
76129407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 447
Checksum: 329
Coasting Arc #15 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2010/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4833166
95 A = 6724180
38 meter
Y = 4135521
23 meter E =
0017544
Z = 2143556
44 I = 51
93580
XDOT = -1840
240779 Wp = 29
62917
YDOT = -5029
591645 meter/sec RA = 124
14687 deg
ZDOT = 5550
022572 TA = 354
29985
MA = 354
31979
Ha = 188
768 n
mi
Hp = 180
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15856846
96 X = -4889464
71
Y = 13567983
02 feet Y = 4081159
26 meter
Z = 7032665
50 Z = 2119940
28
XDOT = -6037
535365 XDOT = -1810
822778
YDOT = -16501
284925 feet/sec YDOT = -5050
005437 meter/sec
ZDOT = 18208
735472 ZDOT = 5541
154640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20741980
89 X = -6322155
77
Y = 2570558
99 feet Y = 783506
38 meter
Z = 6939063
22 Z = 2115026
47
XDOT = 4145
580732 XDOT = 1263
573007
YDOT = -15644
556527 feet/sec YDOT = -4768
460829 meter/sec
ZDOT = 18173
328890 ZDOT = 5539
230646
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 10048
55924271
00016717 00000-0 10270-3 0 9140
2 25544 51
6445 124
7422 0011459 336
3680 23
6956 15
76128322 4639
Satellite: ISS
Catalog Number: 25544
Epoch time: 10048
55924271 = yrday
fracday
Element set: 914
Inclination: 51
6445 deg
RA of node: 124
7422 deg
Eccentricity:
0011459
Arg of perigee: 336
3680 deg
Mean anomaly: 23
6956 deg
Mean motion: 15
76128322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 303
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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