Date:
December 24th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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 1313)
---------------------------------------
Vector Time (GMT): 2010/356/17:40:45
857
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5141151
42 A = 6730871
86 meter
Y = 1838651
84 meter E =
0014989
Z = 3922527
08 I = 51
55661
XDOT = -4714
858054 Wp = 86
63228
YDOT = 4577
828571 meter/sec RA = 344
90849 deg
ZDOT = 4021
518132 TA = 321
52142
MA = 321
62820
Ha = 194
640 n
mi
Hp = 185
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16867294
68 X = 5101154
39
Y = 6032322
33 feet Y = 1895919
09 meter
Z = 12869183
34 Z = 3947405
72
XDOT = -15468
694403 XDOT = -4785
233426
YDOT = 15019
122607 feet/sec YDOT = 4524
710115 meter/sec
ZDOT = 13193
957125 ZDOT = 3998
443248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16275238
06 X = 4960692
56
Y = 7309386
55 feet Y = 2227901
02 meter
Z = 12969191
06 Z = 3953009
44
XDOT = -16125
710579 XDOT = -4915
116584
YDOT = 12589
518685 feet/sec YDOT = 3837
285295 meter/sec
ZDOT = 13100
950868 ZDOT = 3993
169825
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 10356
79164617
00016717 00000-0 10270-3 0 9003
2 25544 51
6465 345
1206 0005037 55
6207 304
5431 15
72074112 13149
Satellite: ISS
Catalog Number: 25544
Epoch time: 10356
79164617 = yrday
fracday
Element set: 900
Inclination: 51
6465 deg
RA of node: 345
1206 deg
Eccentricity:
0005037
Arg of perigee: 55
6207 deg
Mean anomaly: 304
5431 deg
Mean motion: 15
72074112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 276
Coasting Arc #2 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2010/357/17:40:45
857
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3097887
08 A = 6730864
30 meter
Y = -4490829
49 meter E =
0010763
Z = -3950780
38 I = 51
52825
XDOT = 6499
069792 Wp = 86
19543
YDOT = 980
718491 meter/sec RA = 339
72930 deg
ZDOT = 3991
311008 TA = 225
28774
MA = 225
37544
Ha = 194
718 n
mi
Hp = 185
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10163671
51 X = 3167066
10
Y = -14733692
56 feet Y = -4455799
77 meter
Z = -12961877
90 Z = -3935563
53
XDOT = 21322
407453 XDOT = 6468
231335
YDOT = 3217
580352 feet/sec YDOT = 1053
222084 meter/sec
ZDOT = 13094
852387 ZDOT = 4022
808361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11105409
86 X = 3384928
93
Y = -14093950
93 feet Y = -4295836
24 meter
Z = -12900488
85 Z = -3932069
00
XDOT = 19985
193076 XDOT = 6091
486850
YDOT = 3675
790669 feet/sec YDOT = 1120
380996 meter/sec
ZDOT = 13221
523711 ZDOT = 4029
920427
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 10357
74514600
00016717 00000-0 10270-3 0 9011
2 25544 51
6473 340
2382 0005006 58
2728 301
8921 15
72107956 13295
Satellite: ISS
Catalog Number: 25544
Epoch time: 10357
74514600 = yrday
fracday
Element set: 901
Inclination: 51
6473 deg
RA of node: 340
2382 deg
Eccentricity:
0005006
Arg of perigee: 58
2728 deg
Mean anomaly: 301
8921 deg
Mean motion: 15
72107956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1329
Checksum: 290
Coasting Arc #3 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2010/358/17:40:45
857
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6012612
29 A = 6733455
65 meter
Y = 178404
62 meter E =
0008702
Z = -3034691
26 I = 51
50956
XDOT = 2318
755665 Wp = 82
65915
YDOT = -5431
496055 meter/sec RA = 334
64978 deg
ZDOT = -4924
406964 TA = 132
47311
MA = 132
39952
Ha = 194
652 n
mi
Hp = 184
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19726418
26 X = -5999418
56
Y = 585316
98 feet Y = 111242
03 meter
Z = -9956336
16 Z = -3063868
12
XDOT = 7607
466093 XDOT = 2403
240928
YDOT = -17819
868948 feet/sec YDOT = -5405
093468 meter/sec
ZDOT = -16156
190826 ZDOT = -4912
937901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19673769
54 X = -5996564
96
Y = -256506
95 feet Y = -78183
32 meter
Z = -10073718
24 Z = -3070469
32
XDOT = 8439
783817 XDOT = 2572
446108
YDOT = -16040
220467 feet/sec YDOT = -4889
059198 meter/sec
ZDOT = -16109
848110 ZDOT = -4910
281704
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 10358
76219767
00016717 00000-0 10270-3 0 9021
2 25544 51
6477 335
0302 0004874 61
9057 298
2597 15
72115504 13455
Satellite: ISS
Catalog Number: 25544
Epoch time: 10358
76219767 = yrday
fracday
Element set: 902
Inclination: 51
6477 deg
RA of node: 335
0302 deg
Eccentricity:
0004874
Arg of perigee: 61
9057 deg
Mean anomaly: 298
2597 deg
Mean motion: 15
72115504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 320
Coasting Arc #4 (Orbit 1360)
---------------------------------------
Vector Time (GMT): 2010/359/17:40:45
857
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -912088
62 A = 6728097
06 meter
Y = 4803951
82 meter E =
0013243
Z = 4613915
83 I = 51
46480
XDOT = -6992
180746 Wp = 63
88595
YDOT = 1455
438009 meter/sec RA = 329
47157 deg
ZDOT = -2885
477752 TA = 54
78857
MA = 54
66465
Ha = 194
619 n
mi
Hp = 184
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2992416
73 X = -988152
85
Y = 15760996
77 feet Y = 4793326
65 meter
Z = 15137519
11 Z = 4609300
55
XDOT = -22940
225545 XDOT = -6993
919068
YDOT = 4775
059085 feet/sec YDOT = 1377
237730 meter/sec
ZDOT = -9466
790524 ZDOT = -2919
449528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3484489
16 X = -1062072
30
Y = 15677657
75 feet Y = 4778550
08 meter
Z = 15118777
89 Z = 4608203
50
XDOT = -21854
759804 XDOT = -6661
330788
YDOT = 4442
200564 feet/sec YDOT = 1353
982732 meter/sec
ZDOT = -9603
507094 ZDOT = -2927
148962
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 10359
77923261
00016717 00000-0 10270-3 0 9035
2 25544 51
6476 329
8223 0004952 64
1742 295
9931 15
72191209 13610
Satellite: ISS
Catalog Number: 25544
Epoch time: 10359
77923261 = yrday
fracday
Element set: 903
Inclination: 51
6476 deg
RA of node: 329
8223 deg
Eccentricity:
0004952
Arg of perigee: 64
1742 deg
Mean anomaly: 295
9931 deg
Mean motion: 15
72191209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1361
Checksum: 319
Coasting Arc #5 (Orbit 1376)
---------------------------------------
Vector Time (GMT): 2010/360/17:40:45
857
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5984362
90 A = 6735648
67 meter
Y = -2352159
35 meter E =
0019075
Z = 1975682
21 I = 51
46447
XDOT = 230
131723 Wp = 68
02410
YDOT = 5303
757609 meter/sec RA = 324
37760 deg
ZDOT = 5581
425109 TA = 314
02977
MA = 314
18677
Ha = 194
622 n
mi
Hp = 184
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19633736
56 X = 6000622
98
Y = -7717058
22 feet Y = -2285147
80 meter
Z = 6481897
02 Z = 2004793
40
XDOT = 755
025339 XDOT = 143
693645
YDOT = 17400
779556 feet/sec YDOT = 5305
847434 meter/sec
ZDOT = 18311
762170 ZDOT = 5582
333452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19658628
45 X = 5991949
95
Y = -7552612
28 feet Y = -2302036
22 meter
Z = 6599088
04 Z = 2011402
03
XDOT = -50
432403 XDOT = -15
371796
YDOT = 15972
788401 feet/sec YDOT = 4868
505905 meter/sec
ZDOT = 18315
228614 ZDOT = 5582
481682
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 10360
79625377
00016717 00000-0 10270-3 0 9047
2 25544 51
6476 324
6140 0004985 68
0310 292
1382 15
72167334 13779
Satellite: ISS
Catalog Number: 25544
Epoch time: 10360
79625377 = yrday
fracday
Element set: 904
Inclination: 51
6476 deg
RA of node: 324
6140 deg
Eccentricity:
0004985
Arg of perigee: 68
0310 deg
Mean anomaly: 292
1382 deg
Mean motion: 15
72167334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1377
Checksum: 310
Coasting Arc #6 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2010/361/17:40:45
857
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1247346
56 A = 6726132
50 meter
Y = -4263703
70 meter E =
0017907
Z = -5066031
38 I = 51
40838
XDOT = 6452
843122 Wp = 94
28784
YDOT = -3835
929760 meter/sec RA = 319
20940 deg
ZDOT = 1643
291091 TA = 191
56951
MA = 191
61072
Ha = 194
570 n
mi
Hp = 184
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4092344
35 X = -1174966
53
Y = -13988529
21 feet Y = -4277247
28 meter
Z = -16620837
88 Z = -5071915
42
XDOT = 21170
745150 XDOT = 6487
274827
YDOT = -12585
071392 feet/sec YDOT = -3763
577761 meter/sec
ZDOT = 5391
374972 ZDOT = 1674
722319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4116697
60 X = -1254769
43
Y = -13953371
47 feet Y = -4252987
63 meter
Z = -16644359
67 Z = -5073200
83
XDOT = 20008
707720 XDOT = 6098
654113
YDOT = -12470
961884 feet/sec YDOT = -3801
149182 meter/sec
ZDOT = 5517
945808 ZDOT = 1681
869882
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 10361
74969443
00016717 00000-0 10270-3 0 9059
2 25544 51
6473 319
7312 0004866 71
6246 288
5445 15
72214382 13920
Satellite: ISS
Catalog Number: 25544
Epoch time: 10361
74969443 = yrday
fracday
Element set: 905
Inclination: 51
6473 deg
RA of node: 319
7312 deg
Eccentricity:
0004866
Arg of perigee: 71
6246 deg
Mean anomaly: 288
5445 deg
Mean motion: 15
72214382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 323
Coasting Arc #7 (Orbit 1407)
---------------------------------------
Vector Time (GMT): 2010/362/17:40:45
857
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5132849
09 A = 6736956
12 meter
Y = 4264341
06 meter E =
0012852
Z = -901459
45 I = 51
42216
XDOT = -2485
562376 Wp = 121
53338
YDOT = -4230
538824 meter/sec RA = 314
09455 deg
ZDOT = -5928
504326 TA = 68
32677
MA = 68
18996
Ha = 194
582 n
mi
Hp = 184
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16840056
07 X = -5175773
13
Y = 13990620
28 feet Y = 4206702
51 meter
Z = -2957544
12 Z = -926498
81
XDOT = -8154
732206 XDOT = -2409
271340
YDOT = -13879
720552 feet/sec YDOT = -4257
906889 meter/sec
ZDOT = -19450
473512 ZDOT = -5940
394192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16452167
15 X = -5014620
55
Y = 14423741
23 feet Y = 4396356
33 meter
Z = -3058414
05 Z = -932204
60
XDOT = -7345
558462 XDOT = -2238
926219
YDOT = -12466
800929 feet/sec YDOT = -3799
880923 meter/sec
ZDOT = -19498
156665 ZDOT = -5943
038151
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 10362
76668398
00016717 00000-0 10270-3 0 9068
2 25544 51
6471 314
5231 0004779 77
4149 282
7547 15
72188387 14082
Satellite: ISS
Catalog Number: 25544
Epoch time: 10362
76668398 = yrday
fracday
Element set: 906
Inclination: 51
6471 deg
RA of node: 314
5231 deg
Eccentricity:
0004779
Arg of perigee: 77
4149 deg
Mean anomaly: 282
7547 deg
Mean motion: 15
72188387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1408
Checksum: 344
Coasting Arc #8 (Orbit 1423)
---------------------------------------
Vector Time (GMT): 2010/363/17:40:45
857
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2989343
39 A = 6725109
68 meter
Y = 2963480
67 meter E =
0007425
Z = 5238762
12 I = 51
36222
XDOT = -5069
045702 Wp = 76
25222
YDOT = 5789
198787 meter/sec RA = 308
94215 deg
ZDOT = -380
162952 TA = 17
38244
MA = 17
35703
Ha = 194
425 n
mi
Hp = 184
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9807557
04 X = 2930533
98
Y = 9722705
60 feet Y = 2996580
00 meter
Z = 17187539
78 Z = 5253141
82
XDOT = -16630
727368 XDOT = -5131
558094
YDOT = 18993
434342 feet/sec YDOT = 5732
164174 meter/sec
ZDOT = -1247
253779 ZDOT = -404
939759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10116209
11 X = 3083420
54
Y = 9294796
84 feet Y = 2833054
08 meter
Z = 17245282
48 Z = 5256362
10
XDOT = -15108
625643 XDOT = -4605
109096
YDOT = 18956
519641 feet/sec YDOT = 5777
947187 meter/sec
ZDOT = -1347
118739 ZDOT = -410
601792
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 10363
78365546
00016717 00000-0 10270-3 0 9071
2 25544 51
6468 309
3141 0004824 79
4384 280
7322 15
72259059 14246
Satellite: ISS
Catalog Number: 25544
Epoch time: 10363
78365546 = yrday
fracday
Element set: 907
Inclination: 51
6468 deg
RA of node: 309
3141 deg
Eccentricity:
0004824
Arg of perigee: 79
4384 deg
Mean anomaly: 280
7322 deg
Mean motion: 15
72259059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1424
Checksum: 321
Coasting Arc #9 (Orbit 1438)
---------------------------------------
Vector Time (GMT): 2010/364/17:40:45
857
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3585383
48 A = 6737052
48 meter
Y = -5692028
92 meter E =
0015808
Z = -234379
57 I = 51
38349
XDOT = 4174
062239 Wp = 54
21039
YDOT = 2393
794647 meter/sec RA = 303
80137 deg
ZDOT = 6009
592899 TA = 303
23542
MA = 303
38684
Ha = 194
477 n
mi
Hp = 184
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11763069
16 X = 3649904
92
Y = -18674635
57 feet Y = -5651574
22 meter
Z = -768961
83 Z = -216805
66
XDOT = 13694
429917 XDOT = 4117
790562
YDOT = 7853
656979 feet/sec YDOT = 2440
156199 meter/sec
ZDOT = 19716
512136 ZDOT = 6029
734141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10617874
15 X = 3236328
04
Y = -19351396
68 feet Y = -5898305
71 meter
Z = -698073
86 Z = -212772
91
XDOT = 12615
228081 XDOT = 3845
121519
YDOT = 6245
736326 feet/sec YDOT = 1903
700432 meter/sec
ZDOT = 19797
452408 ZDOT = 6034
263494
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 10364
73705266
00016717 00000-0 10270-3 0 9085
2 25544 51
6459 304
4303 0004771 82
5161 277
6543 15
72280493 14393
Satellite: ISS
Catalog Number: 25544
Epoch time: 10364
73705266 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 304
4303 deg
Eccentricity:
0004771
Arg of perigee: 82
5161 deg
Mean anomaly: 277
6543 deg
Mean motion: 15
72280493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1439
Checksum: 312
Coasting Arc #10 (Orbit 1454)
---------------------------------------
Vector Time (GMT): 2010/365/17:40:45
857
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4122840
79 A = 6725176
96 meter
Y = -1144207
26 meter E =
0019408
Z = -5205436
57 I = 51
32665
XDOT = 3038
139167 Wp = 83
90694
YDOT = -7004
120258 meter/sec RA = 298
66723 deg
ZDOT = -867
457187 TA = 177
78309
MA = 177
77447
Ha = 194
432 n
mi
Hp = 184
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13526380
54 X = -4084452
56
Y = -3753960
81 feet Y = -1190096
00 meter
Z = -17078203
96 Z = -5225372
24
XDOT = 9967
648185 XDOT = 3120
448699
YDOT = -22979
397171 feet/sec YDOT = -6969
685621 meter/sec
ZDOT = -2845
988145 ZDOT = -852
498923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13675148
08 X = -4168185
13
Y = -2702060
49 feet Y = -823588
04 meter
Z = -17158363
46 Z = -5229869
18
XDOT = 7974
840433 XDOT = 2430
731364
YDOT = -22687
541342 feet/sec YDOT = -6915
162601 meter/sec
ZDOT = -2785
576548 ZDOT = -849
043732
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 10365
75399389
00016717 00000-0 10270-3 0 9094
2 25544 51
6448 299
2205 0004748 86
3053 273
8652 15
72306204 14555
Satellite: ISS
Catalog Number: 25544
Epoch time: 10365
75399389 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 299
2205 deg
Eccentricity:
0004748
Arg of perigee: 86
3053 deg
Mean anomaly: 273
8652 deg
Mean motion: 15
72306204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 333
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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