Date:
February 11th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 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 367)
---------------------------------------
Vector Time (GMT): 2010/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4216087
76 A = 6717671
58 meter
Y = 2382850
16 meter E =
0010675
Z = -4661545
18 I = 51
74607
XDOT = -5635
880796 Wp = 7
78628
YDOT = 4413
822719 meter/sec RA = 160
10456 deg
ZDOT = -2831
472846 TA = 234
23462
MA = 234
33392
Ha = 187
812 n
mi
Hp = 182
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13832308
92 X = 4211773
25
Y = 7817749
88 feet Y = 2429972
97 meter
Z = -15293783
39 Z = -4641074
42
XDOT = -18490
422560 XDOT = -5671
063687
YDOT = 14481
045666 feet/sec YDOT = 4350
602325 meter/sec
ZDOT = -9289
609075 ZDOT = -2858
936497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5557966
18 X = 1694068
09
Y = 14967967
49 feet Y = 4562236
49 meter
Z = -15212453
93 Z = -4636755
96
XDOT = -22334
546641 XDOT = -6807
569816
YDOT = -1290
832162 feet/sec YDOT = -393
445643 meter/sec
ZDOT = -9398
418845 ZDOT = -2864
638064
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
52084275
00016717 00000-0 10270-3 0 9006
2 25544 51
6446 160
9963 0011205 308
5494 51
4666 15
75809537 3689
Satellite: ISS
Catalog Number: 25544
Epoch time: 10041
52084275 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 160
9963 deg
Eccentricity:
0011205
Arg of perigee: 308
5494 deg
Mean anomaly: 51
4666 deg
Mean motion: 15
75809537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 368
Checksum: 309
Coasting Arc #2 (Orbit 383)
---------------------------------------
Vector Time (GMT): 2010/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5054864
78 A = 6725297
39 meter
Y = -4011184
40 meter E =
0005306
Z = 1894734
58 I = 51
80078
XDOT = 4386
282477 Wp = 66
98905
YDOT = 2853
427307 meter/sec RA = 154
92587 deg
ZDOT = -5646
694891 TA = 92
00327
MA = 91
94251
Ha = 187
913 n
mi
Hp = 182
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16584202
02 X = 5090138
87
Y = -13160053
80 feet Y = -3954460
70 meter
Z = 6216320
79 Z = 1919375
98
XDOT = 14390
690541 XDOT = 4381
478727
YDOT = 9361
638147 feet/sec YDOT = 2902
450530 meter/sec
ZDOT = -18525
901873 ZDOT = -5625
398621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21140121
94 X = 6443509
17
Y = 307582
65 feet Y = 93751
19 meter
Z = 6313957
10 Z = 1924494
12
XDOT = 5305
237995 XDOT = 1617
036541
YDOT = 14888
680871 feet/sec YDOT = 4538
069930 meter/sec
ZDOT = -18441
267131 ZDOT = -5620
898222
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
53548869
00016717 00000-0 10270-3 0 9013
2 25544 51
6450 155
7721 0011124 312
8345 47
1883 15
75851699 3848
Satellite: ISS
Catalog Number: 25544
Epoch time: 10042
53548869 = yrday
fracday
Element set: 901
Inclination: 51
6450 deg
RA of node: 155
7721 deg
Eccentricity:
0011124
Arg of perigee: 312
8345 deg
Mean anomaly: 47
1883 deg
Mean motion: 15
75851699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 315
Coasting Arc #3 (Orbit 399)
---------------------------------------
Vector Time (GMT): 2010/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3428915
99 A = 6715315
69 meter
Y = -2669204
11 meter E =
0006700
Z = 5122003
25 I = 51
79563
XDOT = 5880
341527 Wp = 325
08034
YDOT = -4754
252091 meter/sec RA = 149
81720 deg
ZDOT = 1465
346171 TA = 110
94513
MA = 110
87342
Ha = 188
091 n
mi
Hp = 182
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11249724
38 X = -3423694
61
Y = -8757231
32 feet Y = -2707519
05 meter
Z = 16804472
59 Z = 5105358
80
XDOT = 19292
459079 XDOT = 5925
949218
YDOT = -15597
939932 feet/sec YDOT = -4688
239611 meter/sec
ZDOT = 4807
566179 ZDOT = 1494
022772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3468182
69 X = -1057102
09
Y = -13908153
20 feet Y = -4239205
10 meter
Z = 16738299
83 Z = 5101833
79
XDOT = 23771
061808 XDOT = 7245
419639
YDOT = -30
085877 feet/sec YDOT = -9
170175 meter/sec
ZDOT = 4921
197616 ZDOT = 1499
981034
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
55010525
00016717 00000-0 10270-3 0 9020
2 25544 51
6460 150
5473 0011247 317
0958 42
9328 15
75937757 4005
Satellite: ISS
Catalog Number: 25544
Epoch time: 10043
55010525 = yrday
fracday
Element set: 902
Inclination: 51
6460 deg
RA of node: 150
5473 deg
Eccentricity:
0011247
Arg of perigee: 317
0958 deg
Mean anomaly: 42
9328 deg
Mean motion: 15
75937757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 400
Checksum: 289
Coasting Arc #4 (Orbit 414)
---------------------------------------
Vector Time (GMT): 2010/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5147828
08 A = 6726519
43 meter
Y = 4264321
93 meter E =
0017167
Z = -638272
97 I = 51
85914
XDOT = -3493
294365 Wp = 359
96651
YDOT = -3318
438564 meter/sec RA = 144
66256 deg
ZDOT = 6020
404963 TA = 353
09210
MA = 353
11573
Ha = 188
319 n
mi
Hp = 181
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16889199
73 X = -5192029
37
Y = 13990557
50 feet Y = 4206508
70 meter
Z = -2094071
44 Z = -663387
82
XDOT = -11460
939519 XDOT = -3485
172504
YDOT = -10887
265631 feet/sec YDOT = -3357
457088 meter/sec
ZDOT = 19751
984787 ZDOT = 6003
454878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21903863
65 X = -6676297
64
Y = 880232
93 feet Y = 268295
00 meter
Z = -2193592
69 Z = -668607
05
XDOT = -2531
950791 XDOT = -771
738601
YDOT = -14080
899236 feet/sec YDOT = -4291
858087 meter/sec
ZDOT = 19684
565961 ZDOT = 5999
855705
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
50128569
00016717 00000-0 10270-3 0 9035
2 25544 51
6463 145
6499 0011368 321
8168 38
2190 15
75922805 4150
Satellite: ISS
Catalog Number: 25544
Epoch time: 10044
50128569 = yrday
fracday
Element set: 903
Inclination: 51
6463 deg
RA of node: 145
6499 deg
Eccentricity:
0011368
Arg of perigee: 321
8168 deg
Mean anomaly: 38
2190 deg
Mean motion: 15
75922805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 415
Checksum: 309
Coasting Arc #5 (Orbit 430)
---------------------------------------
Vector Time (GMT): 2010/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2669955
56 A = 6714437
01 meter
Y = 3179671
68 meter E =
0012737
Z = -5284169
01 I = 51
84269
XDOT = -5874
402733 Wp = 42
91559
YDOT = 4975
203538 meter/sec RA = 139
53453 deg
ZDOT = 34
751918 TA = 227
35961
MA = 227
46705
Ha = 188
460 n
mi
Hp = 181
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8759696
73 X = 2659870
28
Y = 10431993
71 feet Y = 3209472
09 meter
Z = -17336512
49 Z = -5271223
37
XDOT = -19272
974846 XDOT = -5929
768559
YDOT = 16322
846253 feet/sec YDOT = 4909
202917 meter/sec
ZDOT = 114
015478 ZDOT = 6
080194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 948988
99 X = 289251
84
Y = 13654374
43 feet Y = 4161853
33 meter
Z = -17284991
29 Z = -5268465
34
XDOT = -24202
711339 XDOT = -7376
986416
YDOT = 1644
362802 feet/sec YDOT = 501
201782 meter/sec
ZDOT =
396574 ZDOT =
120876
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
51585020
00016717 00000-0 10270-3 0 9047
2 25544 51
6461 140
4260 0011381 325
4725 34
5699 15
75987067 4313
Satellite: ISS
Catalog Number: 25544
Epoch time: 10045
51585020 = yrday
fracday
Element set: 904
Inclination: 51
6461 deg
RA of node: 140
4260 deg
Eccentricity:
0011381
Arg of perigee: 325
4725 deg
Mean anomaly: 34
5699 deg
Mean motion: 15
75987067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 431
Checksum: 294
Coasting Arc #6 (Orbit 446)
---------------------------------------
Vector Time (GMT): 2010/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5068080
24 A = 6726203
23 meter
Y = -4364605
73 meter E =
0001919
Z = -722379
77 I = 51
90413
XDOT = 2626
331273 Wp = 36
46515
YDOT = 4041
705533 meter/sec RA = 134
40788 deg
ZDOT = -6000
658849 TA = 151
37706
MA = 151
36652
Ha = 188
516 n
mi
Hp = 181
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16627559
85 X = 5120018
47
Y = -14319572
61 feet Y = -4307641
09 meter
Z = -2370012
36 Z = -697633
25
XDOT = 8616
572418 XDOT = 2610
090392
YDOT = 13260
188757 feet/sec YDOT = 4070
983567 meter/sec
ZDOT = -19687
200948 ZDOT = -5987
940141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21859289
33 X = 6662711
39
Y = -2037793
22 feet Y = -621119
37 meter
Z = -2271944
92 Z = -692488
81
XDOT = -708
018581 XDOT = -215
804064
YDOT = 14272
848545 feet/sec YDOT = 4350
364237 meter/sec
ZDOT = -19636
543205 ZDOT = -5985
218369
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
53038770
00016717 00000-0 10270-3 0 9056
2 25544 51
6453 135
2012 0011304 329
7259 30
3251 15
76025262 4471
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
53038770 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 135
2012 deg
Eccentricity:
0011304
Arg of perigee: 329
7259 deg
Mean anomaly: 30
3251 deg
Mean motion: 15
76025262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 447
Checksum: 271
Coasting Arc #7 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2010/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1953454
42 A = 6714928
67 meter
Y = -3922341
15 meter E =
0013186
Z = 5092210
93 I = 51
88774
XDOT = 5678
566694 Wp = 355
27121
YDOT = -4944
134360 meter/sec RA = 129
25432 deg
ZDOT = -1617
321175 TA = 110
28071
MA = 110
13893
Ha = 188
631 n
mi
Hp = 180
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6408971
21 X = -1934185
44
Y = -12868573
33 feet Y = -3944077
75 meter
Z = 16706728
78 Z = 5082768
32
XDOT = 18630
468155 XDOT = 5741
287328
YDOT = -16220
913256 feet/sec YDOT = -4880
282679 meter/sec
ZDOT = -5306
171834 ZDOT = -1589
582602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1901128
63 X = 579464
01
Y = -14293959
64 feet Y = -4356798
90 meter
Z = 16669082
33 Z = 5080736
29
XDOT = 23519
737524 XDOT = 7168
815997
YDOT = -2979
695407 feet/sec YDOT = -908
211160 meter/sec
ZDOT = -5196
242144 ZDOT = -1583
814606
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
54489557
00016717 00000-0 10270-3 0 9062
2 25544 51
6458 129
9754 0011488 333
5522 26
5055 15
76109666 4636
Satellite: ISS
Catalog Number: 25544
Epoch time: 10047
54489557 = yrday
fracday
Element set: 906
Inclination: 51
6458 deg
RA of node: 129
9754 deg
Eccentricity:
0011488
Arg of perigee: 333
5522 deg
Mean anomaly: 26
5055 deg
Mean motion: 15
76109666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 332
Coasting Arc #8 (Orbit 478)
---------------------------------------
Vector Time (GMT): 2010/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4811694
57 A = 6724340
55 meter
Y = 4193128
24 meter E =
0018009
Z = 2078562
87 I = 51
93691
XDOT = -1913
648418 Wp = 29
87636
YDOT = -4965
948166 meter/sec RA = 124
15480 deg
ZDOT = 5582
742739 TA = 353
28413
MA = 353
30823
Ha = 188
868 n
mi
Hp = 180
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15786399
49 X = -4868322
37
Y = 13756982
43 feet Y = 4139004
54 meter
Z = 6819431
99 Z = 2055050
21
XDOT = -6278
374075 XDOT = -1885
095580
YDOT = -16292
480860 feet/sec YDOT = -4987
187681 meter/sec
ZDOT = 18316
085101 ZDOT = 5573
516093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20786211
18 X = -6335637
17
Y = 2767798
34 feet Y = 843624
93 meter
Z = 6726242
94 Z = 2050158
85
XDOT = 3843
422355 XDOT = 1171
475134
YDOT = -15600
012285 feet/sec YDOT = -4754
883745 meter/sec
ZDOT = 18279
256786 ZDOT = 5571
517468
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
55937853
00016717 00000-0 10270-3 0 9072
2 25544 51
6451 124
7502 0011460 338
2941 21
7736 15
76113652 4790
Satellite: ISS
Catalog Number: 25544
Epoch time: 10048
55937853 = yrday
fracday
Element set: 907
Inclination: 51
6451 deg
RA of node: 124
7502 deg
Eccentricity:
0011460
Arg of perigee: 338
2941 deg
Mean anomaly: 21
7736 deg
Mean motion: 15
76113652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 479
Checksum: 306
Coasting Arc #9 (Orbit 493)
---------------------------------------
Vector Time (GMT): 2010/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1434951
02 A = 6717037
65 meter
Y = 4742760
60 meter E =
0009586
Z = -4536285
90 I = 51
92794
XDOT = -5338
663913 Wp = 39
06865
YDOT = 4591
005356 meter/sec RA = 118
98273 deg
ZDOT = 3122
031626 TA = 261
86679
MA = 261
97554
Ha = 188
937 n
mi
Hp = 180
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4707844
56 X = 1403846
16
Y = 15560238
17 feet Y = 4758632
86 meter
Z = -14882827
76 Z = -4529390
85
XDOT = -17515
301551 XDOT = -5404
770640
YDOT = 15062
353530 feet/sec YDOT = 4530
935824 meter/sec
ZDOT = 10242
885911 ZDOT = 3095
935871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4296630
77 X = -1309613
06
Y = 15704881
08 feet Y = 4786847
75 meter
Z = -14855270
07 Z = -4527886
32
XDOT = -21766
605645 XDOT = -6634
461400
YDOT = 3602
226879 feet/sec YDOT = 1097
958753 meter/sec
ZDOT = 10139
447282 ZDOT = 3090
503532
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 10049
51042999
00016717 00000-0 10270-3 0 9088
2 25544 51
6440 119
8516 0011515 342
5027 17
5739 15
76178224 4941
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
51042999 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 119
8516 deg
Eccentricity:
0011515
Arg of perigee: 342
5027 deg
Mean anomaly: 17
5739 deg
Mean motion: 15
76178224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 494
Checksum: 313
Coasting Arc #10 (Orbit 509)
---------------------------------------
Vector Time (GMT): 2010/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4505322
22 A = 6721162
60 meter
Y = -3716539
20 meter E =
0011133
Z = -3339452
85 I = 51
95513
XDOT = 1398
032899 Wp = 10
68537
YDOT = 5926
874160 meter/sec RA = 113
90004 deg
ZDOT = -4701
802868 TA = 208
38607
MA = 208
44677
Ha = 189
030 n
mi
Hp = 179
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14781240
86 X = 4562768
67
Y = -12193370
06 feet Y = -3665836
98 meter
Z = -10956210
14 Z = -3317426
49
XDOT = 4586
722110 XDOT = 1354
493915
YDOT = 19445
125198 feet/sec YDOT = 5942
264117 meter/sec
ZDOT = -15425
862429 ZDOT = -4695
117348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19026284
33 X = 5799211
46
Y = -2658891
46 feet Y = -810430
12 meter
Z = -10868886
62 Z = -3312836
64
XDOT = -6346
917312 XDOT = -1934
540397
YDOT = 17641
931018 feet/sec YDOT = 5377
260574 meter/sec
ZDOT = -15399
098928 ZDOT = -4693
645353
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 10050
52485870
00016717 00000-0 10270-3 0 9091
2 25544 51
6437 114
6252 0011543 346
5650 13
5205 15
76194588 5108
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
52485870 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 114
6252 deg
Eccentricity:
0011543
Arg of perigee: 346
5650 deg
Mean anomaly: 13
5205 deg
Mean motion: 15
76194588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 510
Checksum: 293
Coasting Arc #11 (Orbit 525)
---------------------------------------
Vector Time (GMT): 2010/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1061910
94 A = 6720145
44 meter
Y = -5589750
71 meter E =
0015903
Z = 3578742
94 I = 51
96423
XDOT = 4979
705091 Wp = 39
37047
YDOT = -3817
743926 meter/sec RA = 108
71874 deg
ZDOT = -4462
664903 TA = 98
09904
MA = 97
91859
Ha = 189
105 n
mi
Hp = 179
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3483959
77 X = -1016711
16
Y = -18339077
14 feet Y = -5601372
78 meter
Z = 11741282
61 Z = 3573694
20
XDOT = 16337
615127 XDOT = 5043
704305
YDOT = -12525
406581 feet/sec YDOT = -3761
700221 meter/sec
ZDOT = -14641
289052 ZDOT = -4438
318132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6233398
32 X = 1899939
81
Y = -17609072
64 feet Y = -5367245
34 meter
Z = 11721038
76 Z = 3572572
61
XDOT = 19222
256909 XDOT = 5858
943906
YDOT = -2926
719555 feet/sec YDOT = -892
064120 meter/sec
ZDOT = -14544
744159 ZDOT = -4433
238020
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 10051
53925750
00016717 00000-0 10270-3 0 9101
2 25544 51
6443 109
3987 0011758 350
1023 9
9908 15
76277972 5269
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051
53925750 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 109
3987 deg
Eccentricity:
0011758
Arg of perigee: 350
1023 deg
Mean anomaly: 9
9908 deg
Mean motion: 15
76277972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 526
Checksum: 314
Coasting Arc #12 (Orbit 541)
---------------------------------------
Vector Time (GMT): 2010/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4210935
79 A = 6717407
36 meter
Y = 2867666
50 meter E =
0011553
Z = 4366493
34 I = 51
96331
XDOT = -1099
958112 Wp = 43
38645
YDOT = -6822
539917 meter/sec RA = 103
63901 deg
ZDOT = 3422
807375 TA = 12
32809
MA = 12
29985
Ha = 189
335 n
mi
Hp = 179
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13815406
14 X = -4263901
01
Y = 9408354
65 feet Y = 2820281
24 meter
Z = 14325765
54 Z = 4345908
12
XDOT = -3608
786458 XDOT = -1040
212725
YDOT = -22383
661144 feet/sec YDOT = -6834
506191 meter/sec
ZDOT = 11229
682990 ZDOT = 3417
609062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16729783
28 X = -5099237
94
Y = 1352667
62 feet Y = 412293
09 meter
Z = 14244114
02 Z = 4341605
95
XDOT = 7912
100766 XDOT = 2411
608313
YDOT = -20074
873881 feet/sec YDOT = -6118
821559 meter/sec
ZDOT = 11208
812033 ZDOT = 3416
445908
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 10052
55363077
00016717 00000-0 10270-3 0 9113
2 25544 51
6439 104
1721 0011659 354
8947 5
2097 15
76295491 5421
Satellite: ISS
Catalog Number: 25544
Epoch time: 10052
55363077 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 104
1721 deg
Eccentricity:
0011659
Arg of perigee: 354
8947 deg
Mean anomaly: 5
2097 deg
Mean motion: 15
76295491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 542
Checksum: 308
Coasting Arc #13 (Orbit 556)
---------------------------------------
Vector Time (GMT): 2010/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 902197
14 A = 6723190
35 meter
Y = 6237569
63 meter E =
0016306
Z = -2316589
86 I = 51
98959
XDOT = -4719
743998 Wp = 13
72073
YDOT = 2703
242635 meter/sec RA = 98
46524 deg
ZDOT = 5463
792256 TA = 320
31096
MA = 320
43018
Ha = 189
338 n
mi
Hp = 178
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2959964
36 X = 843633
91
Y = 20464467
28 feet Y = 6247331
08 meter
Z = -7600360
44 Z = -2312349
30
XDOT = -15484
724404 XDOT = -4776
163137
YDOT = 8868
906283 feet/sec YDOT = 2650
148207 meter/sec
ZDOT = 17925
827612 ZDOT = 5440
726986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7119684
04 X = -2170079
70
Y = 19419697
05 feet Y = 5919123
66 meter
Z = -7583320
80 Z = -2311396
18
XDOT = -16516
470096 XDOT = -5034
220085
YDOT = 879
092435 feet/sec YDOT = 267
947374 meter/sec
ZDOT = 17834
310597 ZDOT = 5435
897870
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 10053
50458029
00016717 00000-0 10270-3 0 9122
2 25544 51
6443 99
2724 0011721 358
8760 1
2376 15
76339545 5571
Satellite: ISS
Catalog Number: 25544
Epoch time: 10053
50458029 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 99
2724 deg
Eccentricity:
0011721
Arg of perigee: 358
8760 deg
Mean anomaly: 1
2376 deg
Mean motion: 15
76339545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 557
Checksum: 307
Coasting Arc #14 (Orbit 572)
---------------------------------------
Vector Time (GMT): 2010/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4067985
01 A = 6714457
01 meter
Y = -1761123
05 meter E =
0020127
Z = -5058733
91 I = 51
96431
XDOT = 968
234248 Wp = 42
53894
YDOT = 7416
609979 meter/sec RA = 93
37090 deg
ZDOT = -1793
008598 TA = 210
18703
MA = 210
30315
Ha = 189
426 n
mi
Hp = 178
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13346407
51 X = 4111949
86
Y = -5777962
76 feet Y = -1715386
57 meter
Z = -16596896
01 Z = -5038865
19
XDOT = 3176
621547 XDOT = 893
938400
YDOT = 24332
709905 feet/sec YDOT = 7427
021953 meter/sec
ZDOT = -5882
574139 ZDOT = -1788
485398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14592852
39 X = 4447901
41
Y = 1082394
26 feet Y = 329913
77 meter
Z = -16518035
18 Z = -5034697
12
XDOT = -8308
667023 XDOT = -2532
481709
YDOT = 22001
726370 feet/sec YDOT = 6706
126198 meter/sec
ZDOT = -5864
382370 ZDOT = -1787
463746
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 10054
51889876
00016717 00000-0 10270-3 0 9133
2 25544 51
6451 94
0455 0011731 2
9081 357
2149 15
76358307 5735
Satellite: ISS
Catalog Number: 25544
Epoch time: 10054
51889876 = yrday
fracday
Element set: 913
Inclination: 51
6451 deg
RA of node: 94
0455 deg
Eccentricity:
0011731
Arg of perigee: 2
9081 deg
Mean anomaly: 357
2149 deg
Mean motion: 15
76358307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 573
Checksum: 312
Coasting Arc #15 (Orbit 588)
---------------------------------------
Vector Time (GMT): 2010/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -798245
95 A = 6725013
89 meter
Y = -6635648
15 meter E =
0012764
Z = 757297
04 I = 52
00073
XDOT = 4652
678082 Wp = 73
39254
YDOT = -1254
576285 meter/sec RA = 88
21918 deg
ZDOT = -6002
339529 TA = 98
39321
MA = 98
24848
Ha = 189
472 n
mi
Hp = 178
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2618917
14 X = -727664
35
Y = -21770499
18 feet Y = -6644179
97 meter
Z = 2484570
35 Z = 753590
65
XDOT = 15264
691870 XDOT = 4695
518819
YDOT = -4116
063926 feet/sec YDOT = -1202
307707 meter/sec
ZDOT = -19692
714990 ZDOT = -5979
633267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7362663
88 X = 2244139
95
Y = -20656196
53 feet Y = -6296008
70 meter
Z = 2469651
17 Z = 752749
68
XDOT = 14093
905157 XDOT = 4295
822292
YDOT = 2645
856648 feet/sec YDOT = 806
457106 meter/sec
ZDOT = -19602
559634 ZDOT = -5974
860177
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 10055
53318806
00016717 00000-0 10270-3 0 9147
2 25544 51
6446 88
8184 0011864 7
2618 352
8716 15
76431395 5897
Satellite: ISS
Catalog Number: 25544
Epoch time: 10055
53318806 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 88
8184 deg
Eccentricity:
0011864
Arg of perigee: 7
2618 deg
Mean anomaly: 352
8716 deg
Mean motion: 15
76431395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 589
Checksum: 328
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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