Date:
September 11th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17760 45 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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
258/09:08:12
987 -0
5 3
8 3
8
N/A 3
2 0
0 195
7
000/00:10:25
973 -2
0 -0
1 188
1
Coasting Arc #1 (Orbit 3969)
---------------------------------------
Vector Time (GMT): 2010/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2911286
60 A = 6732680
31 meter
Y = 4780555
19 meter E =
0008827
Z = -3739690
13 I = 51
79820
XDOT = -6372
085071 Wp = 34
69255
YDOT = -541
056359 meter/sec RA = 153
06288 deg
ZDOT = 4280
941984 TA = 280
32079
MA = 280
42029
Ha = 195
333 n
mi
Hp = 186
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9551465
23 X = -2946360
45
Y = 15684236
20 feet Y = 4747803
02 meter
Z = -12269324
57 Z = -3753918
82
XDOT = -20905
790915 XDOT = -6386
357425
YDOT = -1775
119289 feet/sec YDOT = -612
392277 meter/sec
ZDOT = 14045
085250 ZDOT = 4249
951641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12383106
82 X = 3774370
96
Y = -13508690
13 feet Y = -4117448
75 meter
Z = -12326233
61 Z = -3757036
00
XDOT = 19242
464291 XDOT = 5865
103116
YDOT = 4972
586434 feet/sec YDOT = 1515
644345 meter/sec
ZDOT = 13920
921162 ZDOT = 4243
096770
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 10253
50801119
00016717 00000-0 10270-3 0 9003
2 25544 51
6468 154
0654 0008739 354
0972 6
0085 15
71672731 39702
Satellite: ISS
Catalog Number: 25544
Epoch time: 10253
50801119 = yrday
fracday
Element set: 900
Inclination: 51
6468 deg
RA of node: 154
0654 deg
Eccentricity:
0008739
Arg of perigee: 354
0972 deg
Mean anomaly: 6
0085 deg
Mean motion: 15
71672731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3970
Checksum: 299
Coasting Arc #2 (Orbit 3985)
---------------------------------------
Vector Time (GMT): 2010/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5893769
44 A = 6734446
57 meter
Y = -726494
82 meter E =
0008741
Z = -3188522
04 I = 51
83052
XDOT = -1913
565982 Wp = 27
43585
YDOT = 5668
477598 meter/sec RA = 148
00797 deg
ZDOT = -4826
283454 TA = 189
55669
MA = 189
57333
Ha = 195
418 n
mi
Hp = 186
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19336513
92 X = 5916944
58
Y = -2383513
18 feet Y = -660457
77 meter
Z = -10461030
33 Z = -3159833
57
XDOT = -6278
103614 XDOT = -1953
364336
YDOT = 18597
367448 feet/sec YDOT = 5646
856126 meter/sec
ZDOT = -15834
263299 ZDOT = -4835
676652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19510286
05 X = -5946735
19
Y = -1149750
86 feet Y = -350444
06 meter
Z = -10346104
22 Z = -3153492
57
XDOT = 9349
299846 XDOT = 2849
666593
YDOT = -15755
837659 feet/sec YDOT = -4802
379318 meter/sec
ZDOT = -15871
793208 ZDOT = -4837
722570
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 10254
52534344
00016717 00000-0 10270-3 0 9010
2 25544 51
6467 148
8594 0008723 356
9814 3
1293 15
71692153 39860
Satellite: ISS
Catalog Number: 25544
Epoch time: 10254
52534344 = yrday
fracday
Element set: 901
Inclination: 51
6467 deg
RA of node: 148
8594 deg
Eccentricity:
0008723
Arg of perigee: 356
9814 deg
Mean anomaly: 3
1293 deg
Mean motion: 15
71692153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3986
Checksum: 324
Coasting Arc #3 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2010/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 415472
15 A = 6729249
65 meter
Y = -4871898
98 meter E =
0014519
Z = 4622712
10 I = 51
83858
XDOT = 6758
092498 Wp = 31
33808
YDOT = -2224
812733 meter/sec RA = 142
85702 deg
ZDOT = -2935
879647 TA = 87
76571
MA = 87
59946
Ha = 195
438 n
mi
Hp = 186
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1363097
59 X = 447463
27
Y = -15983920
53 feet Y = -4867073
85 meter
Z = 15166378
30 Z = 4624808
39
XDOT = 22172
219481 XDOT = 6796
730563
YDOT = -7299
254372 feet/sec YDOT = -2149
023773 meter/sec
ZDOT = -9632
151072 ZDOT = -2902
954646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3864613
17 X = -1177934
09
Y = 15561366
88 feet Y = 4743104
63 meter
Z = 15174696
27 Z = 4625247
42
XDOT = -21987
474005 XDOT = -6701
782077
YDOT = 3855
657344 feet/sec YDOT = 1175
204359 meter/sec
ZDOT = -9500
264371 ZDOT = -2895
680580
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 10255
54265279
00016717 00000-0 10270-3 0 9022
2 25544 51
6462 143
6529 0008858
6761 359
4412 15
71770870 40022
Satellite: ISS
Catalog Number: 25544
Epoch time: 10255
54265279 = yrday
fracday
Element set: 902
Inclination: 51
6462 deg
RA of node: 143
6529 deg
Eccentricity:
0008858
Arg of perigee:
6761 deg
Mean anomaly: 359
4412 deg
Mean motion: 15
71770870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4002
Checksum: 308
Coasting Arc #4 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2010/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5649189
41 A = 6737075
21 meter
Y = 3117899
38 meter E =
0019868
Z = 1893964
32 I = 51
88807
XDOT = -935
367592 Wp = 43
54535
YDOT = -5145
407345 meter/sec RA = 137
79296 deg
ZDOT = 5659
741219 TA = 337
42940
MA = 337
51667
Ha = 195
655 n
mi
Hp = 186
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18534086
00 X = -5692835
06
Y = 10229328
69 feet Y = 3054482
77 meter
Z = 6213793
70 Z = 1866414
31
XDOT = -3068
791311 XDOT = -905
255338
YDOT = -16881
257694 feet/sec YDOT = -5155
698677 meter/sec
ZDOT = 18568
704786 ZDOT = 5655
270450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19866690
56 X = 6055367
28
Y = -7404412
89 feet Y = -2256865
05 meter
Z = 6103443
09 Z = 1860329
45
XDOT = 136
665493 XDOT = 41
655642
YDOT = 15715
343540 feet/sec YDOT = 4790
036711 meter/sec
ZDOT = 18550
711267 ZDOT = 5654
256794
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 10256
55994203
00016717 00000-0 10270-3 0 9031
2 25544 51
6463 138
4461 0008886 4
5459 355
5782 15
71756520 40188
Satellite: ISS
Catalog Number: 25544
Epoch time: 10256
55994203 = yrday
fracday
Element set: 903
Inclination: 51
6463 deg
RA of node: 138
4461 deg
Eccentricity:
0008886
Arg of perigee: 4
5459 deg
Mean anomaly: 355
5782 deg
Mean motion: 15
71756520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4018
Checksum: 323
Coasting Arc #5 (Orbit 4032)
---------------------------------------
Vector Time (GMT): 2010/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1940273
06 A = 6726923
14 meter
Y = 3870232
03 meter E =
0016241
Z = -5160214
00 I = 51
87624
XDOT = -5868
729395 Wp = 67
64485
YDOT = 4769
814990 meter/sec RA = 132
66296 deg
ZDOT = 1380
222953 TA = 215
49369
MA = 215
60185
Ha = 195
590 n
mi
Hp = 186
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6365725
27 X = 1921918
66
Y = 12697611
65 feet Y = 3891826
62 meter
Z = -16929835
96 Z = -5150832
78
XDOT = -19254
361531 XDOT = -5928
335056
YDOT = 15648
999311 feet/sec YDOT = 4703
854088 meter/sec
ZDOT = 4528
290527 ZDOT = 1351
567730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4771768
39 X = -1454435
00
Y = -13425923
58 feet Y = -4092221
51 meter
Z = -16892186
00 Z = -5148738
29
XDOT = 20161
723399 XDOT = 6145
293292
YDOT = -12679
557122 feet/sec YDOT = -3864
729011 meter/sec
ZDOT = 4413
517955 ZDOT = 1345
240273
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 10257
51362827
00016717 00000-0 10270-3 0 9040
2 25544 51
6462 133
5649 0008834 7
2840 352
8449 15
71817057 40338
Satellite: ISS
Catalog Number: 25544
Epoch time: 10257
51362827 = yrday
fracday
Element set: 904
Inclination: 51
6462 deg
RA of node: 133
5649 deg
Eccentricity:
0008834
Arg of perigee: 7
2840 deg
Mean anomaly: 352
8449 deg
Mean motion: 15
71817057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4033
Checksum: 312
Coasting Arc #6 (Orbit 4046)
---------------------------------------
Vector Time (GMT): 2010/258/09:13:25
973
Vector Time (MET): N/A
Weight (LBS) : 826418
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4470110
45 A = 6729743
15 meter
Y = 659444
45 meter E =
0015519
Z = -5000458
69 I = 51
89581
XDOT = -3240
189114 Wp = 50
23758
YDOT = 6671
904487 meter/sec RA = 128
18014 deg
ZDOT = -2011
079137 TA = 200
30694
MA = 200
36873
Ha = 195
667 n
mi
Hp = 188
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14665716
69 X = 4486695
50
Y = 2163531
67 feet Y = 709524
56 meter
Z = -16405704
35 Z = -4978702
63
XDOT = -10630
541713 XDOT = -3304
785305
YDOT = 21889
450417 feet/sec YDOT = 6635
309542 meter/sec
ZDOT = -6598
028665 ZDOT = -2026
976973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8229163
83 X = -2508249
14
Y = -12445831
94 feet Y = -3793489
57 meter
Z = -16318498
11 Z = -4973878
22
XDOT = 22468
774448 XDOT = 6848
482452
YDOT = -6097
643400 feet/sec YDOT = -1858
561708 meter/sec
ZDOT = -6661
660534 ZDOT = -2030
474131
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 10258
40372629
00016717 00000-0 10270-3 0 9051
2 25544 51
6457 129
0090 0006656 355
4195 4
6905 15
71103602 40471
Satellite: ISS
Catalog Number: 25544
Epoch time: 10258
40372629 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 129
0090 deg
Eccentricity:
0006656
Arg of perigee: 355
4195 deg
Mean anomaly: 4
6905 deg
Mean motion: 15
71103602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4047
Checksum: 296
Coasting Arc #7 (Orbit 4062)
---------------------------------------
Vector Time (GMT): 2010/259/09:13:25
973
Vector Time (MET): N/A
Weight (LBS) : 826418
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1480445
25 A = 6737447
31 meter
Y = -6028171
17 meter E =
0013715
Z = 2613707
40 I = 51
93952
XDOT = 5529
938386 Wp = 74
89166
YDOT = -937
125453 meter/sec RA = 123
04817 deg
ZDOT = -5267
274696 TA = 75
57859
MA = 75
42642
Ha = 195
724 n
mi
Hp = 187
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4857103
84 X = 1535046
47
Y = -19777464
48 feet Y = -6011310
60 meter
Z = 8575155
51 Z = 2621032
13
XDOT = 18142
842475 XDOT = 5565
593865
YDOT = -3074
558574 feet/sec YDOT = -875
087116 meter/sec
ZDOT = -17281
084960 ZDOT = -5240
323736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17777689
91 X = -5418639
88
Y = 9909094
49 feet Y = 3020292
00 meter
Z = 8604442
98 Z = 2622634
22
XDOT = -13928
913497 XDOT = -4245
532834
YDOT = -10002
788767 feet/sec YDOT = -3048
850016 meter/sec
ZDOT = -17173
066802 ZDOT = -5234
350761
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 10259
42143497
00016717 00000-0 10270-3 0 9064
2 25544 51
6456 123
8056 0006622 358
7513 1
3631 15
71106561 40632
Satellite: ISS
Catalog Number: 25544
Epoch time: 10259
42143497 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 123
8056 deg
Eccentricity:
0006622
Arg of perigee: 358
7513 deg
Mean anomaly: 1
3631 deg
Mean motion: 15
71106561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4063
Checksum: 290
Coasting Arc #8 (Orbit 4078)
---------------------------------------
Vector Time (GMT): 2010/260/09:13:25
973
Vector Time (MET): N/A
Weight (LBS) : 826418
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4833941
30 A = 6733232
79 meter
Y = 2307550
73 meter E =
0011583
Z = 4067521
69 I = 51
94168
XDOT = 94
958926 Wp = 68
06305
YDOT = -6652
056838 meter/sec RA = 118
00290 deg
ZDOT = 3882
112819 TA = 342
11755
MA = 342
15827
Ha = 195
930 n
mi
Hp = 187
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15859387
47 X = -4879144
64
Y = 7570704
50 feet Y = 2253242
09 meter
Z = 13344887
45 Z = 4043928
69
XDOT = 311
545034 XDOT = 150
477913
YDOT = -21824
333459 feet/sec YDOT = -6650
684397 meter/sec
ZDOT = 12736
590612 ZDOT = 3882
709205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16493847
53 X = 5027324
73
Y = 6269237
98 feet Y = 1910863
74 meter
Z = 13250336
11 Z = 4038702
45
XDOT = -15463
190313 XDOT = -4713
180407
YDOT = 13726
484906 feet/sec YDOT = 4183
832599 meter/sec
ZDOT = 12738
905386 ZDOT = 3882
818362
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 10260
43912165
00016717 00000-0 10270-3 0 9074
2 25544 51
6461 118
6019 0006725 2
3728 357
7465 15
71144424 40793
Satellite: ISS
Catalog Number: 25544
Epoch time: 10260
43912165 = yrday
fracday
Element set: 907
Inclination: 51
6461 deg
RA of node: 118
6019 deg
Eccentricity:
0006725
Arg of perigee: 2
3728 deg
Mean anomaly: 357
7465 deg
Mean motion: 15
71144424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4079
Checksum: 301
Coasting Arc #9 (Orbit 4093)
---------------------------------------
Vector Time (GMT): 2010/261/09:13:25
973
Vector Time (MET): N/A
Weight (LBS) : 826418
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1243302
79 A = 6733077
59 meter
Y = 5228318
43 meter E =
0008714
Z = -4059562
12 I = 51
95533
XDOT = -5099
450079 Wp = 59
95208
YDOT = 4234
610319 meter/sec RA = 112
86035 deg
ZDOT = 3902
439235 TA = 250
10827
MA = 250
20219
Ha = 195
850 n
mi
Hp = 187
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4079077
41 X = 1204466
84
Y = 17153275
68 feet Y = 5242004
44 meter
Z = -13318773
37 Z = -4053616
80
XDOT = -16730
479262 XDOT = -5165
380470
YDOT = 13893
078475 feet/sec YDOT = 4177
216769 meter/sec
ZDOT = 12803
278331 ZDOT = 3877
505940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9250466
12 X = 2819542
07
Y = -15031249
42 feet Y = -4581524
82 meter
Z = -13294881
74 Z = -4052279
95
XDOT = 20603
180634 XDOT = 6279
849457
YDOT = 1474
018714 feet/sec YDOT = 449
280904 meter/sec
ZDOT = 12703
366769 ZDOT = 3871
986191
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 10261
39318281
00016717 00000-0 10270-3 0 9080
2 25544 51
6466 113
7236 0006789 4
7375 355
3850 15
71186739 40943
Satellite: ISS
Catalog Number: 25544
Epoch time: 10261
39318281 = yrday
fracday
Element set: 908
Inclination: 51
6466 deg
RA of node: 113
7236 deg
Eccentricity:
0006789
Arg of perigee: 4
7375 deg
Mean anomaly: 355
3850 deg
Mean motion: 15
71186739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4094
Checksum: 327
Coasting Arc #10 (Orbit 4109)
---------------------------------------
Vector Time (GMT): 2010/262/09:13:25
973
Vector Time (MET): N/A
Weight (LBS) : 826418
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3775906
40 A = 6737104
63 meter
Y = -4898646
01 meter E =
0006177
Z = -2680737
58 I = 51
97964
XDOT = 2705
036108 Wp = 52
37357
YDOT = 4943
891599 meter/sec RA = 107
81676 deg
ZDOT = -5228
575083 TA = 157
94463
MA = 157
91804
Ha = 195
837 n
mi
Hp = 187
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12388144
35 X = 3843425
77
Y = -16071673
25 feet Y = -4856044
22 meter
Z = -8795070
82 Z = -2662230
02
XDOT = 8874
790381 XDOT = 2674
950852
YDOT = 16220
116795 feet/sec YDOT = 4973
972360 meter/sec
ZDOT = -17154
117725 ZDOT = -5215
507529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20125689
53 X = -6134310
17
Y = 2832001
38 feet Y = 863194
02 meter
Z = -8720920
87 Z = -2658136
68
XDOT = 5094
374555 XDOT = 1552
765364
YDOT = -16414
227347 feet/sec YDOT = -5003
056495 meter/sec
ZDOT = -17101
675918 ZDOT = -5212
590820
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 10262
41082763
00016717 00000-0 10270-3 0 9098
2 25544 51
6467 108
5196 0006698 7
3556 352
7703 15
71196534 41101
Satellite: ISS
Catalog Number: 25544
Epoch time: 10262
41082763 = yrday
fracday
Element set: 909
Inclination: 51
6467 deg
RA of node: 108
5196 deg
Eccentricity:
0006698
Arg of perigee: 7
3556 deg
Mean anomaly: 352
7703 deg
Mean motion: 15
71196534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4110
Checksum: 313
Coasting Arc #11 (Orbit 4125)
---------------------------------------
Vector Time (GMT): 2010/263/09:13:25
973
Vector Time (MET): N/A
Weight (LBS) : 826418
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3265513
81 A = 6729290
93 meter
Y = -3162073
68 meter E =
0012030
Z = 4959719
42 I = 51
96228
XDOT = 3206
726503 Wp = 32
32342
YDOT = -6667
436430 meter/sec RA = 102
68612 deg
ZDOT = -2127
201711 TA = 78
28276
MA = 78
14780
Ha = 195
890 n
mi
Hp = 187
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10713627
97 X = -3254005
52
Y = -10374257
48 feet Y = -3198525
84 meter
Z = 16272045
34 Z = 4943883
86
XDOT = 10520
756244 XDOT = 3291
378187
YDOT = -21874
791437 feet/sec YDOT = -6631
103759 meter/sec
ZDOT = -6979
008237 ZDOT = -2111
417321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 762158
25 X = 232305
83
Y = 14962932
77 feet Y = 4560701
91 meter
Z = 16208524
30 Z = 4940358
21
XDOT = -21592
392287 XDOT = -6581
361169
YDOT = 8635
209106 feet/sec YDOT = 2632
011736 meter/sec
ZDOT = -6915
788224 ZDOT = -2107
932251
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 10263
42844876
00016717 00000-0 10270-3 0 9103
2 25544 51
6465 103
3153 0006883 10
5319 349
5986 15
71296549 41265
Satellite: ISS
Catalog Number: 25544
Epoch time: 10263
42844876 = yrday
fracday
Element set: 910
Inclination: 51
6465 deg
RA of node: 103
3153 deg
Eccentricity:
0006883
Arg of perigee: 10
5319 deg
Mean anomaly: 349
5986 deg
Mean motion: 15
71296549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4126
Checksum: 322
Coasting Arc #12 (Orbit 4141)
---------------------------------------
Vector Time (GMT): 2010/264/09:13:25
973
Vector Time (MET): N/A
Weight (LBS) : 826418
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1640199
21 A = 6739484
60 meter
Y = 6450401
64 meter E =
0019403
Z = 985913
56 I = 52
00168
XDOT = -4426
713023 Wp = 41
94371
YDOT = -2045
167639 meter/sec RA = 97
62124 deg
ZDOT = 5963
413190 TA = 328
77271
MA = 328
88784
Ha = 195
943 n
mi
Hp = 186
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5381231
01 X = -1716996
27
Y = 21162735
04 feet Y = 6431630
65 meter
Z = 3234624
55 Z = 977758
31
XDOT = -14523
336688 XDOT = -4432
483721
YDOT = -6709
867581 feet/sec YDOT = -2094
701475 meter/sec
ZDOT = 19565
003903 ZDOT = 5941
894438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18232517
27 X = 5557271
26
Y = -12025157
18 feet Y = -3665267
91 meter
Z = 3201984
75 Z = 975964
95
XDOT = 5440
915229 XDOT = 1658
390962
YDOT = 13482
766357 feet/sec YDOT = 4109
547186 meter/sec
ZDOT = 19478
707915 ZDOT = 5937
110172
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 10264
44604986
00016717 00000-0 10270-3 0 9113
2 25544 51
6461 98
1106 0006901 14
3026 345
8330 15
71294220 41422
Satellite: ISS
Catalog Number: 25544
Epoch time: 10264
44604986 = yrday
fracday
Element set: 911
Inclination: 51
6461 deg
RA of node: 98
1106 deg
Eccentricity:
0006901
Arg of perigee: 14
3026 deg
Mean anomaly: 345
8330 deg
Mean motion: 15
71294220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4142
Checksum: 279
Coasting Arc #13 (Orbit 4156)
---------------------------------------
Vector Time (GMT): 2010/265/09:13:25
973
Vector Time (MET): N/A
Weight (LBS) : 826418
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4141104
35 A = 6727703
40 meter
Y = 324178
37 meter E =
0018222
Z = -5306745
74 I = 51
96470
XDOT = -440
428813 Wp = 69
54729
YDOT = 7670
470082 meter/sec RA = 92
51932 deg
ZDOT = 131
459926 TA = 201
65870
MA = 201
73586
Ha = 195
947 n
mi
Hp = 186
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13586300
36 X = 4162950
84
Y = 1063577
32 feet Y = 370608
26 meter
Z = -17410583
13 Z = -5286575
17
XDOT = -1444
976420 XDOT = -526
807301
YDOT = 25165
584257 feet/sec YDOT = 7665
061988 meter/sec
ZDOT = 431
298971 ZDOT = 129
109674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9583991
21 X = -2921200
52
Y = -9832369
35 feet Y = -2996906
18 meter
Z = -17329708
15 Z = -5282095
04
XDOT = 16977
473022 XDOT = 5174
733777
YDOT = -17254
080509 feet/sec YDOT = -5259
043739 meter/sec
ZDOT = 421
937039 ZDOT = 128
606410
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 10265
40002929
00016717 00000-0 10270-3 0 9120
2 25544 51
6455 93
2309 0006938 17
2142 342
9254 15
71339498 41573
Satellite: ISS
Catalog Number: 25544
Epoch time: 10265
40002929 = yrday
fracday
Element set: 912
Inclination: 51
6455 deg
RA of node: 93
2309 deg
Eccentricity:
0006938
Arg of perigee: 17
2142 deg
Mean anomaly: 342
9254 deg
Mean motion: 15
71339498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4157
Checksum: 307
Coasting Arc #14 (Orbit 4172)
---------------------------------------
Vector Time (GMT): 2010/266/09:13:25
973
Vector Time (MET): N/A
Weight (LBS) : 826418
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -876073
78 A = 6739556
25 meter
Y = -6639035
61 meter E =
0013307
Z = 738163
45 I = 52
00469
XDOT = 4635
796523 Wp = 97
50096
YDOT = -1289
157322 meter/sec RA = 87
42245 deg
ZDOT = -6002
763834 TA = 74
50718
MA = 74
36027
Ha = 196
010 n
mi
Hp = 186
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2874257
80 X = -805355
64
Y = -21781612
90 feet Y = -6648436
91 meter
Z = 2421796
10 Z = 734079
97
XDOT = 15209
306179 XDOT = 4679
028138
YDOT = -4229
518772 feet/sec YDOT = -1237
076007 meter/sec
ZDOT = -19694
107068 ZDOT = -5980
137815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11887285
90 X = -3623244
74
Y = 18478952
88 feet Y = 5632384
84 meter
Z = 2405379
24 Z = 733159
59
XDOT = -13076
248442 XDOT = -3985
640525
YDOT = -5821
343557 feet/sec YDOT = -1774
345516 meter/sec
ZDOT = -19603
398753 ZDOT = -5975
115940
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 10266
41758653
00016717 00000-0 10270-3 0 9135
2 25544 51
6455 88
0264 0006856 21
6301 338
5149 15
71328190 41739
Satellite: ISS
Catalog Number: 25544
Epoch time: 10266
41758653 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 88
0264 deg
Eccentricity:
0006856
Arg of perigee: 21
6301 deg
Mean anomaly: 338
5149 deg
Mean motion: 15
71328190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4173
Checksum: 308
Coasting Arc #15 (Orbit 4188)
---------------------------------------
Vector Time (GMT): 2010/267/09:13:25
973
Vector Time (MET): N/A
Weight (LBS) : 826418
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3650350
95 A = 6728666
26 meter
Y = 2518200
34 meter E =
0008029
Z = 5053353
58 I = 51
96546
XDOT = -2384
896542 Wp = 65
85555
YDOT = -7096
066969 meter/sec RA = 82
35192 deg
ZDOT = 1814
338129 TA = 6
74946
MA = 6
73865
Ha = 196
189 n
mi
Hp = 186
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11976217
02 X = -3702787
20
Y = 8261812
15 feet Y = 2477087
28 meter
Z = 16579244
02 Z = 5035492
33
XDOT = -7824
463719 XDOT = -2314
183591
YDOT = -23281
059611 feet/sec YDOT = -7122
340743 meter/sec
ZDOT = 5952
552918 ZDOT = 1802
924690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14576360
85 X = 4442874
79
Y = 1259372
54 feet Y = 383856
75 meter
Z = 16507644
64 Z = 5031530
09
XDOT = -8580
274040 XDOT = -2615
267527
YDOT = 21927
673502 feet/sec YDOT = 6683
554883 meter/sec
ZDOT = 5906
755595 ZDOT = 1800
379105
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 10267
43511909
00016717 00000-0 10270-3 0 9140
2 25544 51
6451 82
8206 0007018 24
5826 335
5669 15
71369833 41898
Satellite: ISS
Catalog Number: 25544
Epoch time: 10267
43511909 = yrday
fracday
Element set: 914
Inclination: 51
6451 deg
RA of node: 82
8206 deg
Eccentricity:
0007018
Arg of perigee: 24
5826 deg
Mean anomaly: 335
5669 deg
Mean motion: 15
71369833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4189
Checksum: 322
Coasting Arc #16 (Orbit 4203)
---------------------------------------
Vector Time (GMT): 2010/268/09:13:25
973
Vector Time (MET): N/A
Weight (LBS) : 826418
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3148245
35 A = 6737099
29 meter
Y = 5452828
99 meter E =
0012448
Z = -2385368
70 I = 51
98831
XDOT = -3367
265727 Wp = 34
94092
YDOT = 4304
413785 meter/sec RA = 77
22377 deg
ZDOT = 5419
286690 TA = 298
33770
MA = 298
46320
Ha = 196
053 n
mi
Hp = 186
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10328888
93 X = 3098624
69
Y = 17889858
90 feet Y = 5487756
89 meter
Z = -7826012
78 Z = -2370195
34
XDOT = -11047
459733 XDOT = -3441
474533
YDOT = 14122
092470 feet/sec YDOT = 4266
344593 meter/sec
ZDOT = 17779
811975 ZDOT = 5402
747596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2958201
40 X = 901659
79
Y = -20467799
62 feet Y = -6238585
32 meter
Z = -7765159
20 Z = -2366820
52
XDOT = 16015
392994 XDOT = 4881
491785
YDOT = -4375
689294 feet/sec YDOT = -1333
710097 meter/sec
ZDOT = 17713
515548 ZDOT = 5399
079539
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 10268
38903360
00016717 00000-0 10270-3 0 9152
2 25544 51
6443 77
9402 0006977 26
2405 333
9109 15
71418163 42047
Satellite: ISS
Catalog Number: 25544
Epoch time: 10268
38903360 = yrday
fracday
Element set: 915
Inclination: 51
6443 deg
RA of node: 77
9402 deg
Eccentricity:
0006977
Arg of perigee: 26
2405 deg
Mean anomaly: 333
9109 deg
Mean motion: 15
71418163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4204
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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