Date:
September 30th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 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
There are no maneuvers
Coasting Arc #1 (Orbit 3987)
---------------------------------------
Vector Time (GMT): 2010/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 80407
78 A = 6732535
66 meter
Y = -5461306
85 meter E =
0013304
Z = -3951385
01 I = 51
92529
XDOT = 5805
361386 Wp = 58
40138
YDOT = 3005
610900 meter/sec RA = 56
32044 deg
ZDOT = -4039
110418 TA = 169
72196
MA = 169
69473
Ha = 196
128 n
mi
Hp = 185
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 263805
07 X = 160666
53
Y = -17917673
40 feet Y = -5459959
04 meter
Z = -12963861
59 Z = -3950799
29
XDOT = 19046
461241 XDOT = 5790
942160
YDOT = 9860
928151 feet/sec YDOT = 3070
449209 meter/sec
ZDOT = -13251
674599 ZDOT = -4010
942686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1958238
85 X = 596871
20
Y = 17814022
27 feet Y = 5429713
99 meter
Z = -12961490
33 Z = -3950662
25
XDOT = -18931
650791 XDOT = -5770
367161
YDOT = -7471
221470 feet/sec YDOT = -2277
228304 meter/sec
ZDOT = -13138
746663 ZDOT = -4004
689983
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 10272
52329161
00016717 00000-0 10270-3 0 9008
2 25544 51
6439 56
8062 0006855 44
7496 315
4218 15
71505514 39881
Satellite: ISS
Catalog Number: 25544
Epoch time: 10272
52329161 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 56
8062 deg
Eccentricity:
0006855
Arg of perigee: 44
7496 deg
Mean anomaly: 315
4218 deg
Mean motion: 15
71505514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3988
Checksum: 313
Coasting Arc #2 (Orbit 4003)
---------------------------------------
Vector Time (GMT): 2010/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5177169
32 A = 6732111
10 meter
Y = -1323368
54 meter E =
0017003
Z = 4086374
88 I = 51
90583
XDOT = -1382
569935 Wp = 65
77946
YDOT = -6526
540769 meter/sec RA = 51
17211 deg
ZDOT = -3845
931056 TA = 63
69882
MA = 63
52424
Ha = 196
249 n
mi
Hp = 185
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16985463
65 X = -5181837
46
Y = -4341760
29 feet Y = -1381288
76 meter
Z = 13406741
72 Z = 4061212
63
XDOT = -4535
990599 XDOT = -1290
803168
YDOT = -21412
535330 feet/sec YDOT = -6541
488484 meter/sec
ZDOT = -12617
884042 ZDOT = -3852
424601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17514210
97 X = 5338331
50
Y = 1817743
61 feet Y = 554048
25 meter
Z = 13305856
00 Z = 4055624
91
XDOT = 7655
215917 XDOT = 2333
309811
YDOT = 19261
211461 feet/sec YDOT = 5870
817253 meter/sec
ZDOT = -12643
885834 ZDOT = -3853
856402
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 10273
54072923
00016717 00000-0 10270-3 0 9013
2 25544 51
6438 51
6003 0006825 48
8883 311
2867 15
71518538 40044
Satellite: ISS
Catalog Number: 25544
Epoch time: 10273
54072923 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 51
6003 deg
Eccentricity:
0006825
Arg of perigee: 48
8883 deg
Mean anomaly: 311
2867 deg
Mean motion: 15
71518538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 301
Coasting Arc #3 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2010/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2489416
39 A = 6735800
67 meter
Y = 5636829
07 meter E =
0019908
Z = 2694371
78 I = 51
90068
XDOT = -5671
630055 Wp = 69
64976
YDOT =
705695 meter/sec RA = 46
12207 deg
ZDOT = 5214
643301 TA = 320
95375
MA = 321
09730
Ha = 196
019 n
mi
Hp = 185
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8167376
61 X = 2413110
45
Y = 18493533
68 feet Y = 5664240
64 meter
Z = 8839802
43 Z = 2706279
93
XDOT = -18607
710153 XDOT = -5696
548366
YDOT = 2
315273 feet/sec YDOT = -62
857057 meter/sec
ZDOT = 17108
409780 ZDOT = 5187
029828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11006762
69 X = -3354861
27
Y = -16932872
11 feet Y = -5161139
42 meter
Z = 8887516
70 Z = 2708915
09
XDOT = 17225
979742 XDOT = 5250
478625
YDOT = -2234
509565 feet/sec YDOT = -681
078515 meter/sec
ZDOT = 16997
685057 ZDOT = 5180
894405
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 10274
55813741
00016717 00000-0 10270-3 0 9027
2 25544 51
6451 46
3950 0006777 52
1637 308
0138 15
71612422 40202
Satellite: ISS
Catalog Number: 25544
Epoch time: 10274
55813741 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 46
3950 deg
Eccentricity:
0006777
Arg of perigee: 52
1637 deg
Mean anomaly: 308
0138 deg
Mean motion: 15
71612422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 283
Coasting Arc #4 (Orbit 4034)
---------------------------------------
Vector Time (GMT): 2010/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4448693
32 A = 6728625
82 meter
Y = -1241137
94 meter E =
0017366
Z = -4907835
12 I = 51
85472
XDOT = 4192
998290 Wp = 88
19536
YDOT = 6020
494958 meter/sec RA = 40
98191 deg
ZDOT = 2285
675380 TA = 203
98670
MA = 204
06770
Ha = 196
094 n
mi
Hp = 185
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14595450
54 X = 4486082
77
Y = -4071974
86 feet Y = -1191181
14 meter
Z = -16101821
25 Z = -4886132
42
XDOT = 13756
556070 XDOT = 4114
260934
YDOT = 19752
280046 feet/sec YDOT = 6066
943439 meter/sec
ZDOT = 7498
934974 ZDOT = 2305
853512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13723597
09 X = -4182952
39
Y = 6638241
73 feet Y = 2023336
08 meter
Z = -16014787
94 Z = -4881307
36
XDOT = -16544
312378 XDOT = -5042
706413
YDOT = -15976
014598 feet/sec YDOT = -4869
489249 meter/sec
ZDOT = 7579
806579 ZDOT = 2310
325045
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 10275
51193566
00016717 00000-0 10270-3 0 9031
2 25544 51
6451 41
5156 0006902 54
7478 305
4329 15
71630838 40358
Satellite: ISS
Catalog Number: 25544
Epoch time: 10275
51193566 = yrday
fracday
Element set: 903
Inclination: 51
6451 deg
RA of node: 41
5156 deg
Eccentricity:
0006902
Arg of perigee: 54
7478 deg
Mean anomaly: 305
4329 deg
Mean motion: 15
71630838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 303
Coasting Arc #5 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2010/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4696328
41 A = 6738033
67 meter
Y = -4654867
96 meter E =
0011769
Z = -1293790
55 I = 51
86356
XDOT = 4216
135315 Wp = 106
15884
YDOT = -2635
668075 meter/sec RA = 35
90920 deg
ZDOT = -5868
506435 TA = 87
97179
MA = 87
83702
Ha = 196
044 n
mi
Hp = 185
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15407901
60 X = -4637642
76
Y = -15271876
52 feet Y = -4707057
09 meter
Z = -4244719
65 Z = -1316462
50
XDOT = 13832
464943 XDOT = 4273
802695
YDOT = -8647
204970 feet/sec YDOT = -2588
198677 meter/sec
ZDOT = -19253
630037 ZDOT = -5847
884156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18077777
18 X = 5510106
48
Y = 11960260
83 feet Y = 3645487
50 meter
Z = -4335599
43 Z = -1321490
71
XDOT = -11108
494080 XDOT = -3385
868996
YDOT = 9895
729271 feet/sec YDOT = 3016
218282 meter/sec
ZDOT = -19170
919393 ZDOT = -5843
296231
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 10276
52929241
00016717 00000-0 10270-3 0 9041
2 25544 51
6454 36
3085 0006965 57
8422 302
3415 15
71676327 40519
Satellite: ISS
Catalog Number: 25544
Epoch time: 10276
52929241 = yrday
fracday
Element set: 904
Inclination: 51
6454 deg
RA of node: 36
3085 deg
Eccentricity:
0006965
Arg of perigee: 57
8422 deg
Mean anomaly: 302
3415 deg
Mean motion: 15
71676327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 304
Coasting Arc #6 (Orbit 4066)
---------------------------------------
Vector Time (GMT): 2010/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2710126
69 A = 6726716
69 meter
Y = 3197723
92 meter E =
0009961
Z = 5254016
66 I = 51
80159
XDOT = -6334
178444 Wp = 60
86344
YDOT = -4341
388324 meter/sec RA = 30
78748 deg
ZDOT = -619
388077 TA = 35
04110
MA = 34
97560
Ha = 196
114 n
mi
Hp = 184
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8891491
77 X = -2771205
96
Y = 10491220
21 feet Y = 3167076
63 meter
Z = 17237587
47 Z = 5240702
17
XDOT = -20781
425342 XDOT = -6282
152578
YDOT = -14243
400013 feet/sec YDOT = -4411
930078 meter/sec
ZDOT = -2032
113112 ZDOT = -650
032849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6554129
04 X = 1997698
53
Y = -12165779
43 feet Y = -3708129
57 meter
Z = 17184177
39 Z = 5237737
27
XDOT = 22437
848740 XDOT = 6839
056296
YDOT = 9017
984681 feet/sec YDOT = 2748
681731 meter/sec
ZDOT = -2154
961742 ZDOT = -656
832339
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 10277
54662124
00016717 00000-0 10270-3 0 9059
2 25544 51
6464 31
1026 0007000 60
3778 299
8081 15
71727255 40675
Satellite: ISS
Catalog Number: 25544
Epoch time: 10277
54662124 = yrday
fracday
Element set: 905
Inclination: 51
6464 deg
RA of node: 31
1026 deg
Eccentricity:
0007000
Arg of perigee: 60
3778 deg
Mean anomaly: 299
8081 deg
Mean motion: 15
71727255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4067
Checksum: 298
Coasting Arc #7 (Orbit 4081)
---------------------------------------
Vector Time (GMT): 2010/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6133718
47 A = 6738607
95 meter
Y = 2763768
77 meter E =
0018729
Z = -213412
19 I = 51
81568
XDOT = -1791
988606 Wp = 50
74509
YDOT = 4415
961058 meter/sec RA = 25
68526 deg
ZDOT = 6047
596510 TA = 306
94315
MA = 307
11453
Ha = 196
086 n
mi
Hp = 184
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20123748
27 X = 6103394
35
Y = 9067482
83 feet Y = 2832190
12 meter
Z = -700171
24 Z = -183688
33
XDOT = -5879
227711 XDOT = -1870
613869
YDOT = 14488
061215 feet/sec YDOT = 4395
483014 meter/sec
ZDOT = 19841
195898 ZDOT = 6038
699496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21671930
21 X = -6605604
33
Y = -4202927
19 feet Y = -1281052
21 meter
Z = -581010
38 Z = -177091
96
XDOT = 2202
867089 XDOT = 671
433889
YDOT = -13898
287575 feet/sec YDOT = -4236
198053 meter/sec
ZDOT = 19805
491154 ZDOT = 6036
713704
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 10278
50034230
00016717 00000-0 10270-3 0 9068
2 25544 51
6470 26
2222 0007102 63
4504 296
7385 15
71737926 40825
Satellite: ISS
Catalog Number: 25544
Epoch time: 10278
50034230 = yrday
fracday
Element set: 906
Inclination: 51
6470 deg
RA of node: 26
2222 deg
Eccentricity:
0007102
Arg of perigee: 63
4504 deg
Mean anomaly: 296
7385 deg
Mean motion: 15
71737926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4082
Checksum: 287
Coasting Arc #8 (Orbit 4097)
---------------------------------------
Vector Time (GMT): 2010/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 352437
47 A = 6726762
73 meter
Y = -4258452
40 meter E =
0021338
Z = -5213800
12 I = 51
74877
XDOT = 7371
732809 Wp = 76
78980
YDOT = 1889
843189 meter/sec RA = 20
58807 deg
ZDOT = -1044
052534 TA = 183
23640
MA = 183
25023
Ha = 195
976 n
mi
Hp = 184
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1156290
90 X = 425358
11
Y = -13971300
53 feet Y = -4254104
11 meter
Z = -17105643
42 Z = -5211910
33
XDOT = 24185
475095 XDOT = 7355
124231
YDOT = 6200
272930 feet/sec YDOT = 1972
185352 meter/sec
ZDOT = -3425
369207 ZDOT = -1008
280748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2222979
21 X = 677564
06
Y = 13851096
50 feet Y = 4221814
21 meter
Z = -17098034
20 Z = -5211480
82
XDOT = -23976
765670 XDOT = -7308
118176
YDOT = -208
108755 feet/sec YDOT = -63
431549 meter/sec
ZDOT = -3281
962010 ZDOT = -1000
342021
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 10279
51761708
00016717 00000-0 10270-3 0 9078
2 25544 51
6474 21
0164 0007002 66
6848 293
5050 15
71784186 40983
Satellite: ISS
Catalog Number: 25544
Epoch time: 10279
51761708 = yrday
fracday
Element set: 907
Inclination: 51
6474 deg
RA of node: 21
0164 deg
Eccentricity:
0007002
Arg of perigee: 66
6848 deg
Mean anomaly: 293
5050 deg
Mean motion: 15
71784186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4098
Checksum: 315
Coasting Arc #9 (Orbit 4113)
---------------------------------------
Vector Time (GMT): 2010/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6521768
38 A = 6737349
35 meter
Y = -506422
33 meter E =
0019657
Z = 1585655
76 I = 51
75561
XDOT = -1027
177584 Wp = 101
87865
YDOT = -4998
456908 meter/sec RA = 15
45463 deg
ZDOT = -5765
202844 TA = 60
66625
MA = 60
47002
Ha = 196
017 n
mi
Hp = 184
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21396877
89 X = -6523323
73
Y = -1661490
59 feet Y = -579361
20 meter
Z = 5202282
68 Z = 1553968
68
XDOT = -3370
005196 XDOT = -943
200717
YDOT = -16399
136837 feet/sec YDOT = -5009
474490 meter/sec
ZDOT = -18914
707495 ZDOT = -5769
988460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21110024
02 X = 6434335
32
Y = -4032294
58 feet Y = -1229043
39 meter
Z = 5075250
34 Z = 1546936
30
XDOT = 7161
906195 XDOT = 2182
949008
YDOT = 13426
358687 feet/sec YDOT = 4092
354128 meter/sec
ZDOT = -18933
850728 ZDOT = -5771
037702
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 10280
53486442
00016717 00000-0 10270-3 0 9082
2 25544 51
6471 15
8104 0007133 71
1163 289
0772 15
71821887 41141
Satellite: ISS
Catalog Number: 25544
Epoch time: 10280
53486442 = yrday
fracday
Element set: 908
Inclination: 51
6471 deg
RA of node: 15
8104 deg
Eccentricity:
0007133
Arg of perigee: 71
1163 deg
Mean anomaly: 289
0772 deg
Mean motion: 15
71821887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4114
Checksum: 297
Coasting Arc #10 (Orbit 4129)
---------------------------------------
Vector Time (GMT): 2010/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2137280
60 A = 6728181
86 meter
Y = 4222742
60 meter E =
0013201
Z = 4771516
22 I = 51
69685
XDOT = -7225
643534 Wp = 96
61002
YDOT = 742
277309 meter/sec RA = 10
37613 deg
ZDOT = 2572
090937 TA = 328
17699
MA = 328
25669
Ha = 195
827 n
mi
Hp = 184
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7012075
47 X = 2066722
56
Y = 13854142
39 feet Y = 4246248
84 meter
Z = 15654580
78 Z = 4781727
63
XDOT = -23706
179575 XDOT = -7245
901831
YDOT = 2435
293007 feet/sec YDOT = 661
362763 meter/sec
ZDOT = 8438
618560 ZDOT = 2536
938673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10516190
91 X = -3205334
99
Y = -11368118
91 feet Y = -3465002
64 meter
Z = 15695475
92 Z = 4783981
06
XDOT = 21298
938933 XDOT = 6491
916587
YDOT = -8212
434375 feet/sec YDOT = -2503
149997 meter/sec
ZDOT = 8297
689710 ZDOT = 2529
135824
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 10281
55208117
00016717 00000-0 10270-3 0 9097
2 25544 51
6477 10
6036 0007100 73
8195 286
3748 15
71906688 41306
Satellite: ISS
Catalog Number: 25544
Epoch time: 10281
55208117 = yrday
fracday
Element set: 909
Inclination: 51
6477 deg
RA of node: 10
6036 deg
Eccentricity:
0007100
Arg of perigee: 73
8195 deg
Mean anomaly: 286
3748 deg
Mean motion: 15
71906688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4130
Checksum: 307
Coasting Arc #11 (Orbit 4144)
---------------------------------------
Vector Time (GMT): 2010/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5852959
67 A = 6734697
22 meter
Y = -1728234
23 meter E =
0011710
Z = -2852128
36 I = 51
68815
XDOT = 3760
228197 Wp = 69
59220
YDOT = 4377
554400 meter/sec RA = 5
21861 deg
ZDOT = 5084
740131 TA = 257
75166
MA = 257
88282
Ha = 195
923 n
mi
Hp = 184
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19202623
59 X = 5885705
57
Y = -5670059
80 feet Y = -1662599
98 meter
Z = -9357376
52 Z = -2823614
34
XDOT = 12336
706684 XDOT = 3686
296737
YDOT = 14362
055117 feet/sec YDOT = 4419
190442 meter/sec
ZDOT = 16682
218276 ZDOT = 5102
827943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16716193
12 X = -5095095
66
Y = 11116910
97 feet Y = 3388434
46 meter
Z = -9243051
68 Z = -2817282
15
XDOT = -15129
961392 XDOT = -4611
612232
YDOT = -8877
409073 feet/sec YDOT = -2705
834286 meter/sec
ZDOT = 16754
679059 ZDOT = 5106
826177
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 10282
50569843
00016717 00000-0 10270-3 0 9101
2 25544 51
6474 5
7234 0007115 75
7307 284
4645 15
71905099 41456
Satellite: ISS
Catalog Number: 25544
Epoch time: 10282
50569843 = yrday
fracday
Element set: 910
Inclination: 51
6474 deg
RA of node: 5
7234 deg
Eccentricity:
0007115
Arg of perigee: 75
7307 deg
Mean anomaly: 284
4645 deg
Mean motion: 15
71905099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4145
Checksum: 311
Coasting Arc #12 (Orbit 4160)
---------------------------------------
Vector Time (GMT): 2010/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4288368
64 A = 6730751
97 meter
Y = -3233372
74 meter E =
0014710
Z = -4071821
86 I = 51
64433
XDOT = 5925
836365 Wp = 74
69995
YDOT = -3027
123713 meter/sec RA =
14966 deg
ZDOT = -3844
902473 TA = 155
69225
MA = 155
62279
Ha = 195
839 n
mi
Hp = 184
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14069450
91 X = -4232113
10
Y = -10608178
28 feet Y = -3281013
44 meter
Z = -13358995
59 Z = -4092518
49
XDOT = 19441
720356 XDOT = 5977
924076
YDOT = -9931
508246 feet/sec YDOT = -2960
566336 meter/sec
ZDOT = -12614
509427 ZDOT = -3815
987465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16603890
32 X = 5060865
77
Y = 5707119
62 feet Y = 1739530
06 meter
Z = -13441922
13 Z = -4097097
87
XDOT = -15020
482857 XDOT = -4578
243175
YDOT = 14321
029087 feet/sec YDOT = 4365
049666 meter/sec
ZDOT = -12498
560689 ZDOT = -3809
561298
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 10283
52286186
00016717 00000-0 10270-3 0 9111
2 25544 51
6465
5164 0007179 79
9434 280
2538 15
71950444 41615
Satellite: ISS
Catalog Number: 25544
Epoch time: 10283
52286186 = yrday
fracday
Element set: 911
Inclination: 51
6465 deg
RA of node:
5164 deg
Eccentricity:
0007179
Arg of perigee: 79
9434 deg
Mean anomaly: 280
2538 deg
Mean motion: 15
71950444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4161
Checksum: 310
Coasting Arc #13 (Orbit 4176)
---------------------------------------
Vector Time (GMT): 2010/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4337609
82 A = 6731488
74 meter
Y = 3425561
93 meter E =
0018715
Z = 3828680
82 I = 51
61733
XDOT = -5869
977896 Wp = 81
52161
YDOT = -2779
124782 meter/sec RA = 354
97781 deg
ZDOT = -4143
834498 TA = 51
89090
MA = 51
72230
Ha = 195
819 n
mi
Hp = 184
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14231003
35 X = -4394192
12
Y = 11238720
24 feet Y = 3376739
86 meter
Z = 12561288
77 Z = 3807470
79
XDOT = -19258
457664 XDOT = -5818
334526
YDOT = -9117
863457 feet/sec YDOT = -2844
477709 meter/sec
ZDOT = -13595
257541 ZDOT = -4172
225941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9816131
55 X = 2991956
90
Y = -15316781
15 feet Y = -4668554
89 meter
Z = 12476219
02 Z = 3802751
56
XDOT = 19992
085716 XDOT = 6093
587726
YDOT = 1592
236484 feet/sec YDOT = 485
313680 meter/sec
ZDOT = -13709
033337 ZDOT = -4178
513361
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 10284
53999544
00016717 00000-0 10270-3 0 9123
2 25544 51
6469 355
3089 0007230 81
8469 278
3513 15
72036507 41778
Satellite: ISS
Catalog Number: 25544
Epoch time: 10284
53999544 = yrday
fracday
Element set: 912
Inclination: 51
6469 deg
RA of node: 355
3089 deg
Eccentricity:
0007230
Arg of perigee: 81
8469 deg
Mean anomaly: 278
3513 deg
Mean motion: 15
72036507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4177
Checksum: 335
Coasting Arc #14 (Orbit 4192)
---------------------------------------
Vector Time (GMT): 2010/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5772525
86 A = 6733396
17 meter
Y = 1480751
19 meter E =
0020293
Z = 3115087
71 I = 51
59359
XDOT = -3817
499893 Wp = 85
52099
YDOT = 4596
139426 meter/sec RA = 349
90589 deg
ZDOT = 4863
844141 TA = 310
71835
MA = 310
89443
Ha = 195
663 n
mi
Hp = 184
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18938733
14 X = 5740406
02
Y = 4858107
56 feet Y = 1545123
47 meter
Z = 10220104
02 Z = 3143053
06
XDOT = -12524
605947 XDOT = -3892
239106
YDOT = 15079
197592 feet/sec YDOT = 4553
031998 meter/sec
ZDOT = 15957
493902 ZDOT = 4845
116845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19395067
93 X = -5911616
70
Y = 1950526
47 feet Y = 594520
47 meter
Z = 10332189
26 Z = 3149251
29
XDOT = 6786
099571 XDOT = 2068
403149
YDOT = -17092
426295 feet/sec YDOT = -5209
771535 meter/sec
ZDOT = 15882
358478 ZDOT = 4840
942864
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 10285
55710141
00016717 00000-0 10270-3 0 9131
2 25544 51
6463 350
1016 0007295 86
1628 274
0369 15
72061689 41930
Satellite: ISS
Catalog Number: 25544
Epoch time: 10285
55710141 = yrday
fracday
Element set: 913
Inclination: 51
6463 deg
RA of node: 350
1016 deg
Eccentricity:
0007295
Arg of perigee: 86
1628 deg
Mean anomaly: 274
0369 deg
Mean motion: 15
72061689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4193
Checksum: 305
Coasting Arc #15 (Orbit 4207)
---------------------------------------
Vector Time (GMT): 2010/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2251362
50 A = 6728518
46 meter
Y = -4392192
69 meter E =
0017409
Z = -4589346
15 I = 51
54700
XDOT = 7065
810562 Wp = 100
58801
YDOT = 520
152208 meter/sec RA = 344
73339 deg
ZDOT = 2974
825139 TA = 199
00671
MA = 199
07176
Ha = 195
722 n
mi
Hp = 184
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7386359
92 X = 2322603
98
Y = -14410080
99 feet Y = -4366618
31 meter
Z = -15056909
94 Z = -4578235
80
XDOT = 23181
793183 XDOT = 7045
017630
YDOT = 1706
536117 feet/sec YDOT = 599
050117 meter/sec
ZDOT = 9759
924997 ZDOT = 3009
100759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1769431
70 X = -539322
78
Y = 16137499
96 feet Y = 4918709
99 meter
Z = -15012311
30 Z = -4575752
48
XDOT = -21003
606780 XDOT = -6401
899346
YDOT = 6884
625513 feet/sec YDOT = 2098
433856 meter/sec
ZDOT = 9897
320677 ZDOT = 3016
703342
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 10286
51061255
00016717 00000-0 10270-3 0 9144
2 25544 51
6457 345
2194 0007427 88
3512 271
8501 15
72105258 42089
Satellite: ISS
Catalog Number: 25544
Epoch time: 10286
51061255 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 345
2194 deg
Eccentricity:
0007427
Arg of perigee: 88
3512 deg
Mean anomaly: 271
8501 deg
Mean motion: 15
72105258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4208
Checksum: 297
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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