Date:
September 29th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 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 3956)
---------------------------------------
Vector Time (GMT): 2010/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2379683
88 A = 6729363
93 meter
Y = 4019834
31 meter E =
0010274
Z = 4834464
21 I = 51
94093
XDOT = -4578
491733 Wp = 79
74718
YDOT = -5682
736145 meter/sec RA = 66
50183 deg
ZDOT = 2468
864077 TA = 346
22197
MA = 346
24999
Ha = 196
182 n
mi
Hp = 185
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7807361
80 X = -2447942
92
Y = 13188432
78 feet Y = 3992841
87 meter
Z = 15861103
06 Z = 4822737
47
XDOT = -15021
298338 XDOT = -4526
599555
YDOT = -18644
147458 feet/sec YDOT = -5733
645305 meter/sec
ZDOT = 8099
947758 ZDOT = 2446
747732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6627176
58 X = 2019963
42
Y = -13872979
22 feet Y = -4228484
07 meter
Z = 15814083
15 Z = 4820132
54
XDOT = 15742
524186 XDOT = 4798
321372
YDOT = 16662
303521 feet/sec YDOT = 5078
670113 meter/sec
ZDOT = 8011
279141 ZDOT = 2441
837882
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 10270
55193638
00016717 00000-0 10270-3 0 9007
2 25544 51
6421 66
8894 0006758 37
2724 322
8905 15
71441902 39570
Satellite: ISS
Catalog Number: 25544
Epoch time: 10270
55193638 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 66
8894 deg
Eccentricity:
0006758
Arg of perigee: 37
2724 deg
Mean anomaly: 322
8905 deg
Mean motion: 15
71441902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3957
Checksum: 321
Coasting Arc #2 (Orbit 3971)
---------------------------------------
Vector Time (GMT): 2010/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4695131
15 A = 6735802
83 meter
Y = 3859061
43 meter E =
0011233
Z = -2902306
58 I = 51
95108
XDOT = -1471
815446 Wp = 50
66660
YDOT = 5592
199055 meter/sec RA = 61
36524 deg
ZDOT = 5074
631855 TA = 276
15667
MA = 276
28464
Ha = 196
195 n
mi
Hp = 185
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15403973
58 X = 4665728
57
Y = 12660962
71 feet Y = 3911400
70 meter
Z = -9522003
22 Z = -2879568
82
XDOT = -4828
790834 XDOT = -1558
891117
YDOT = 18347
109761 feet/sec YDOT = 5575
253660 meter/sec
ZDOT = 16649
054641 ZDOT = 5067
269931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16770744
19 X = -5111722
83
Y = -10865182
27 feet Y = -3311707
56 meter
Z = -9430847
13 Z = -2874522
20
XDOT = 2066
850978 XDOT = 629
976178
YDOT = -17558
468658 feet/sec YDOT = -5351
821247 meter/sec
ZDOT = 16619
522827 ZDOT = 5065
630558
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 10271
50582767
00016717 00000-0 10270-3 0 9019
2 25544 51
6436 62
0100 0006821 42
0127 318
1557 15
71468332 39720
Satellite: ISS
Catalog Number: 25544
Epoch time: 10271
50582767 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 62
0100 deg
Eccentricity:
0006821
Arg of perigee: 42
0127 deg
Mean anomaly: 318
1557 deg
Mean motion: 15
71468332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3972
Checksum: 283
Coasting Arc #3 (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 = 83425
30 A = 6732504
11 meter
Y = -5459692
23 meter E =
0013362
Z = -3953563
70 I = 51
92526
XDOT = 5805
350896 Wp = 58
44913
YDOT = 3009
296113 meter/sec RA = 56
31924 deg
ZDOT = -4036
332810 TA = 169
70943
MA = 169
68205
Ha = 196
132 n
mi
Hp = 185
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 273705
05 X = 163676
35
Y = -17912376
07 feet Y = -5458310
71 meter
Z = -12971009
52 Z = -3952963
34
XDOT = 19046
426823 XDOT = 5790
876968
YDOT = 9873
018742 feet/sec YDOT = 3074
133999 meter/sec
ZDOT = -13242
561714 ZDOT = -4008
165262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1947699
78 X = 593658
89
Y = 17810042
90 feet Y = 5428501
08 meter
Z = -12968579
57 Z = -3952823
05
XDOT = -18933
402624 XDOT = -5770
901120
YDOT = -7482
455486 feet/sec YDOT = -2280
652432 meter/sec
ZDOT = -13129
634533 ZDOT = -4001
912606
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
52328539
00016717 00000-0 10270-3 0 9028
2 25544 51
6439 56
8050 0006897 44
9467 315
2252 15
71513985 39881
Satellite: ISS
Catalog Number: 25544
Epoch time: 10272
52328539 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 56
8050 deg
Eccentricity:
0006897
Arg of perigee: 44
9467 deg
Mean anomaly: 315
2252 deg
Mean motion: 15
71513985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3988
Checksum: 333
Coasting Arc #4 (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 = -5178561
75 A = 6732099
73 meter
Y = -1329876
08 meter E =
0017059
Z = 4082438
01 I = 51
90587
XDOT = -1375
858428 Wp = 65
88568
YDOT = -6524
789014 meter/sec RA = 51
17084 deg
ZDOT = -3851
374040 TA = 63
65924
MA = 63
48415
Ha = 196
252 n
mi
Hp = 185
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16990032
00 X = -5183137
89
Y = -4363110
51 feet Y = -1387811
37 meter
Z = 13393825
48 Z = 4057269
22
XDOT = -4513
971221 XDOT = -1284
085308
YDOT = -21406
788104 feet/sec YDOT = -6539
661642 meter/sec
ZDOT = -12635
741600 ZDOT = -3857
834964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17521754
85 X = 5340630
88
Y = 1838215
90 feet Y = 560288
21 meter
Z = 13292913
57 Z = 4051680
06
XDOT = 7633
983914 XDOT = 2326
838297
YDOT = 19258
187860 feet/sec YDOT = 5869
895660 meter/sec
ZDOT = -12661
612603 ZDOT = -3859
259521
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
54071741
00016717 00000-0 10270-3 0 9032
2 25544 51
6438 51
5990 0006865 49
1117 311
0639 15
71527360 40044
Satellite: ISS
Catalog Number: 25544
Epoch time: 10273
54071741 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 51
5990 deg
Eccentricity:
0006865
Arg of perigee: 49
1117 deg
Mean anomaly: 311
0639 deg
Mean motion: 15
71527360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 290
Coasting Arc #5 (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 = 2481072
58 A = 6735756
80 meter
Y = 5636734
34 meter E =
0019939
Z = 2702117
79 I = 51
90061
XDOT = -5676
517435 Wp = 69
77966
YDOT = -10
201396 meter/sec RA = 46
12078 deg
ZDOT = 5209
368667 TA = 320
92164
MA = 321
06550
Ha = 196
021 n
mi
Hp = 185
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8140001
90 X = 2404730
69
Y = 18493222
91 feet Y = 5664052
41 meter
Z = 8865215
86 Z = 2713985
32
XDOT = -18623
744864 XDOT = -5701
287794
YDOT = -33
469147 feet/sec YDOT = -73
817975 meter/sec
ZDOT = 17091
104550 ZDOT = 5181
731810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10979551
81 X = -3346567
39
Y = -16937030
41 feet Y = -5162406
87 meter
Z = 8912767
24 Z = 2716611
45
XDOT = 17247
201113 XDOT = 5256
946899
YDOT = -2203
766505 feet/sec YDOT = -671
708031 meter/sec
ZDOT = 16980
286133 ZDOT = 5175
591213
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
55811985
00016717 00000-0 10270-3 0 9047
2 25544 51
6451 46
3937 0006813 52
4224 307
7556 15
71621421 40202
Satellite: ISS
Catalog Number: 25544
Epoch time: 10274
55811985 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 46
3937 deg
Eccentricity:
0006813
Arg of perigee: 52
4224 deg
Mean anomaly: 307
7556 deg
Mean motion: 15
71621421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 293
Coasting Arc #6 (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 = 4457023
33 A = 6728619
58 meter
Y = -1229224
83 meter E =
0017377
Z = -4903265
79 I = 51
85478
XDOT = 4181
576497 Wp = 88
25224
YDOT = 6023
587769 meter/sec RA = 40
98043 deg
ZDOT = 2298
424973 TA = 204
06029
MA = 204
14157
Ha = 196
094 n
mi
Hp = 185
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14622779
96 X = 4494256
75
Y = -4032889
86 feet Y = -1179175
75 meter
Z = -16086830
03 Z = -4881523
01
XDOT = 13719
082995 XDOT = 4102
743470
YDOT = 19762
427065 feet/sec YDOT = 6069
907991 meter/sec
ZDOT = 7540
764348 ZDOT = 2318
547385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13757398
02 X = -4193254
92
Y = 6604668
10 feet Y = 2013102
84 meter
Z = -15999636
05 Z = -4876689
07
XDOT = -16511
468023 XDOT = -5032
695454
YDOT = -15990
291084 feet/sec YDOT = -4873
840722 meter/sec
ZDOT = 7621
412501 ZDOT = 2323
006530
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
51191258
00016717 00000-0 10270-3 0 9059
2 25544 51
6451 41
5142 0006933 55
0354 305
1458 15
71639815 40358
Satellite: ISS
Catalog Number: 25544
Epoch time: 10275
51191258 = yrday
fracday
Element set: 905
Inclination: 51
6451 deg
RA of node: 41
5142 deg
Eccentricity:
0006933
Arg of perigee: 55
0354 deg
Mean anomaly: 305
1458 deg
Mean motion: 15
71639815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 291
Coasting Arc #7 (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 = -4685784
79 A = 6737989
99 meter
Y = -4661351
49 meter E =
0011779
Z = -1308546
59 I = 51
86350
XDOT = 4231
462234 Wp = 106
06995
YDOT = -2620
505289 meter/sec RA = 35
90786 deg
ZDOT = -5864
244389 TA = 88
22528
MA = 88
09037
Ha = 196
043 n
mi
Hp = 185
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15373309
68 X = -4626955
74
Y = -15293147
94 feet Y = -4713421
91 meter
Z = -4293131
87 Z = -1331166
97
XDOT = 13882
750112 XDOT = 4288
938218
YDOT = -8597
458297 feet/sec YDOT = -2572
865566 meter/sec
ZDOT = -19239
646947 ZDOT = -5843
548118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18047745
45 X = 5500952
81
Y = 11987958
36 feet Y = 3653929
71 meter
Z = -4383804
81 Z = -1336183
71
XDOT = -11165
453615 XDOT = -3403
230262
YDOT = 9858
978333 feet/sec YDOT = 3005
016596 meter/sec
ZDOT = -19156
639707 ZDOT = -5838
943783
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
52926330
00016717 00000-0 10270-3 0 9069
2 25544 51
6454 36
3071 0006993 58
1689 302
0153 15
71685693 40516
Satellite: ISS
Catalog Number: 25544
Epoch time: 10276
52926330 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 36
3071 deg
Eccentricity:
0006993
Arg of perigee: 58
1689 deg
Mean anomaly: 302
0153 deg
Mean motion: 15
71685693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 309
Coasting Arc #8 (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 = -2729189
66 A = 6726699
42 meter
Y = 3184598
60 meter E =
0010021
Z = 5252064
39 I = 51
80162
XDOT = -6323
539027 Wp = 60
96496
YDOT = -4353
920861 meter/sec RA = 30
78577 deg
ZDOT = -640
282702 TA = 35
13864
MA = 35
07259
Ha = 196
112 n
mi
Hp = 184
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8954034
32 X = -2790111
26
Y = 10448158
15 feet Y = 3153739
02 meter
Z = 17231182
39 Z = 5238657
67
XDOT = -20746
519119 XDOT = -6271
272308
YDOT = -14284
517262 feet/sec YDOT = -4424
342294 meter/sec
ZDOT = -2100
665034 ZDOT = -670
875202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6624366
60 X = 2019106
94
Y = -12137009
22 feet Y = -3699360
41 meter
Z = 17177402
60 Z = 5235672
31
XDOT = 22414
196664 XDOT = 6831
847143
YDOT = 9060
556837 feet/sec YDOT = 2761
657724 meter/sec
ZDOT = -2223
303974 ZDOT = -677
663051
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
54658596
00016717 00000-0 10270-3 0 9079
2 25544 51
6464 31
1011 0007025 60
7392 299
4471 15
71736535 40672
Satellite: ISS
Catalog Number: 25544
Epoch time: 10277
54658596 = yrday
fracday
Element set: 907
Inclination: 51
6464 deg
RA of node: 31
1011 deg
Eccentricity:
0007025
Arg of perigee: 60
7392 deg
Mean anomaly: 299
4471 deg
Mean motion: 15
71736535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4067
Checksum: 315
Coasting Arc #9 (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 = 6127351
17 A = 6738582
72 meter
Y = 2779317
29 meter E =
0018787
Z = -191877
63 I = 51
81568
XDOT = -1820
477206 Wp = 50
99943
YDOT = 4403
069980 meter/sec RA = 25
68386 deg
ZDOT = 6048
534804 TA = 306
92218
MA = 307
09414
Ha = 196
081 n
mi
Hp = 184
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20102858
16 X = 6096749
04
Y = 9118495
05 feet Y = 2847665
89 meter
Z = -629519
78 Z = -162185
38
XDOT = -5972
694246 XDOT = -1898
960759
YDOT = 14445
767652 feet/sec YDOT = 4382
274152 meter/sec
ZDOT = 19844
274291 ZDOT = 6039
499737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21662905
89 X = -6602853
71
Y = -4257471
80 feet Y = -1297677
40 meter
Z = -510485
78 Z = -155596
06
XDOT = 2299
586903 XDOT = 700
914088
YDOT = -13879
250473 feet/sec YDOT = -4230
395544 meter/sec
ZDOT = 19808
016102 ZDOT = 6037
483308
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
50030109
00016717 00000-0 10270-3 0 9081
2 25544 51
6470 26
2207 0007121 63
8396 296
3497 15
71747883 40825
Satellite: ISS
Catalog Number: 25544
Epoch time: 10278
50030109 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 26
2207 deg
Eccentricity:
0007121
Arg of perigee: 63
8396 deg
Mean anomaly: 296
3497 deg
Mean motion: 15
71747883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4082
Checksum: 310
Coasting Arc #10 (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 = 382724
54 A = 6726714
91 meter
Y = -4250615
49 meter E =
0021387
Z = -5218038
97 I = 51
74870
XDOT = 7369
812148 Wp = 77
06563
YDOT = 1912
397344 meter/sec RA = 20
58615 deg
ZDOT = -1016
091369 TA = 183
23009
MA = 183
24392
Ha = 195
969 n
mi
Hp = 184
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1255657
95 X = 455575
90
Y = -13945588
87 feet Y = -4245928
90 meter
Z = -17119550
44 Z = -5216002
23
XDOT = 24179
173713 XDOT = 7352
815675
YDOT = 6274
269500 feet/sec YDOT = 1994
715863 meter/sec
ZDOT = -3333
633102 ZDOT = -980
329859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2120262
30 X = 646255
95
Y = 13850676
97 feet Y = 4221686
34 meter
Z = -17111352
03 Z = -5215540
10
XDOT = -23988
391523 XDOT = -7311
661736
YDOT = -274
023825 feet/sec YDOT = -83
522462 meter/sec
ZDOT = -3190
267279 ZDOT = -972
393466
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
51756940
00016717 00000-0 10270-3 0 9092
2 25544 51
6474 21
0149 0007018 67
0987 293
0915 15
71794530 40981
Satellite: ISS
Catalog Number: 25544
Epoch time: 10279
51756940 = yrday
fracday
Element set: 909
Inclination: 51
6474 deg
RA of node: 21
0149 deg
Eccentricity:
0007018
Arg of perigee: 67
0987 deg
Mean anomaly: 293
0915 deg
Mean motion: 15
71794530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4098
Checksum: 327
Coasting Arc #11 (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 = -6526432
17 A = 6737355
54 meter
Y = -529635
55 meter E =
0019663
Z = 1558633
64 I = 51
75573
XDOT = -987
365768 Wp = 102
22844
YDOT = -4995
297111 meter/sec RA = 15
45309 deg
ZDOT = -5774
900774 TA = 60
62323
MA = 60
42703
Ha = 196
007 n
mi
Hp = 184
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21412179
03 X = -6527596
33
Y = -1737649
46 feet Y = -602624
39 meter
Z = 5113627
44 Z = 1526924
86
XDOT = -3239
389001 XDOT = -903
380081
YDOT = -16388
770050 feet/sec YDOT = -5005
869445 meter/sec
ZDOT = -18946
524848 ZDOT = -5779
492959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21144308
24 X = 6444785
15
Y = -3962699
40 feet Y = -1207830
78 meter
Z = 4986508
29 Z = 1519887
73
XDOT = 7038
056714 XDOT = 2145
199686
YDOT = 13448
257280 feet/sec YDOT = 4099
028819 meter/sec
ZDOT = -18964
892624 ZDOT = -5780
499272
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
53481010
00016717 00000-0 10270-3 0 9101
2 25544 51
6471 15
8088 0007143 71
5541 288
6397 15
71832313 41141
Satellite: ISS
Catalog Number: 25544
Epoch time: 10280
53481010 = yrday
fracday
Element set: 910
Inclination: 51
6471 deg
RA of node: 15
8088 deg
Eccentricity:
0007143
Arg of perigee: 71
5541 deg
Mean anomaly: 288
6397 deg
Mean motion: 15
71832313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4114
Checksum: 286
Coasting Arc #12 (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 = 2099439
99 A = 6728095
94 meter
Y = 4226486
03 meter E =
0013136
Z = 4784902
27 I = 51
69666
XDOT = -7240
213727 Wp = 96
84793
YDOT = 713
406475 meter/sec RA = 10
37409 deg
ZDOT = 2539
125964 TA = 328
28403
MA = 328
36310
Ha = 195
815 n
mi
Hp = 184
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6887926
49 X = 2028777
87
Y = 13866423
99 feet Y = 4249568
53 meter
Z = 15698498
26 Z = 4794929
59
XDOT = -23753
982043 XDOT = -7259
987960
YDOT = 2340
572426 feet/sec YDOT = 632
331701 meter/sec
ZDOT = 8330
465761 ZDOT = 2503
904094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10400176
90 X = -3169973
92
Y = -11414689
68 feet Y = -3479197
42 meter
Z = 15738655
38 Z = 4797142
16
XDOT = 21367
302152 XDOT = 6512
753696
YDOT = -8143
129825 feet/sec YDOT = -2482
025971 meter/sec
ZDOT = 8189
258157 ZDOT = 2496
085886
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
55202002
00016717 00000-0 10270-3 0 9117
2 25544 51
6478 10
6020 0007106 74
2863 285
9083 15
71917474 41305
Satellite: ISS
Catalog Number: 25544
Epoch time: 10281
55202002 = yrday
fracday
Element set: 911
Inclination: 51
6478 deg
RA of node: 10
6020 deg
Eccentricity:
0007106
Arg of perigee: 74
2863 deg
Mean anomaly: 285
9083 deg
Mean motion: 15
71917474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4130
Checksum: 276
Coasting Arc #13 (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 = 5874805
02 A = 6734740
78 meter
Y = -1702729
06 meter E =
0011729
Z = -2822297
25 I = 51
68840
XDOT = 3715
570089 Wp = 69
31163
YDOT = 4390
532749 meter/sec RA = 5
21684 deg
ZDOT = 5106
445637 TA = 258
41538
MA = 258
54707
Ha = 195
909 n
mi
Hp = 184
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19274294
68 X = 5907119
17
Y = -5586381
43 feet Y = -1636852
94 meter
Z = -9259505
40 Z = -2793678
15
XDOT = 12190
190581 XDOT = 3641
391378
YDOT = 14404
635004 feet/sec YDOT = 4431
668017 meter/sec
ZDOT = 16753
430567 ZDOT = 5124
315893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16808867
32 X = -5123342
76
Y = 11058023
51 feet Y = 3370485
57 meter
Z = -9144759
62 Z = -2787322
73
XDOT = -15006
509860 XDOT = -4573
984205
YDOT = -8954
820817 feet/sec YDOT = -2729
429385 meter/sec
ZDOT = 16825
019076 ZDOT = 5128
265814
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
50563069
00016717 00000-0 10270-3 0 9127
2 25544 51
6474 5
7218 0007116 76
1980 283
9974 15
71915291 41455
Satellite: ISS
Catalog Number: 25544
Epoch time: 10282
50563069 = yrday
fracday
Element set: 912
Inclination: 51
6474 deg
RA of node: 5
7218 deg
Eccentricity:
0007116
Arg of perigee: 76
1980 deg
Mean anomaly: 283
9974 deg
Mean motion: 15
71915291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4145
Checksum: 316
Coasting Arc #14 (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 = -4249931
09 A = 6730632
87 meter
Y = -3252742
19 meter E =
0014825
Z = -4096578
47 I = 51
64404
XDOT = 5961
712882 Wp = 74
78458
YDOT = -3000
017161 meter/sec RA =
14758 deg
ZDOT = -3810
453627 TA = 156
03103
MA = 155
96195
Ha = 195
822 n
mi
Hp = 184
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13943343
47 X = -4193341
55
Y = -10671726
34 feet Y = -3299951
19 meter
Z = -13440218
08 Z = -4117087
56
XDOT = 19559
425467 XDOT = 6013
327467
YDOT = -9842
575988 feet/sec YDOT = -2933
061235 meter/sec
ZDOT = -12501
488278 ZDOT = -3781
365477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16503492
45 X = 5030264
50
Y = 5807036
14 feet Y = 1769984
61 meter
Z = -13522392
56 Z = -4121625
25
XDOT = -15152
155523 XDOT = -4618
377003
YDOT = 14280
427087 feet/sec YDOT = 4352
674176 meter/sec
ZDOT = -12384
845804 ZDOT = -3774
901001
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
52278686
00016717 00000-0 10270-3 0 9139
2 25544 51
6465
5147 0007175 80
4541 279
7432 15
71961685 41613
Satellite: ISS
Catalog Number: 25544
Epoch time: 10283
52278686 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node:
5147 deg
Eccentricity:
0007175
Arg of perigee: 80
4541 deg
Mean anomaly: 279
7432 deg
Mean motion: 15
71961685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4161
Checksum: 316
Coasting Arc #15 (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 = -4378970
20 A = 6731554
16 meter
Y = 3405826
07 meter E =
0018795
Z = 3799118
33 I = 51
61766
XDOT = -5829
567269 Wp = 82
08645
YDOT = -2810
743596 meter/sec RA = 354
97571 deg
ZDOT = -4179
439805 TA = 51
79209
MA = 51
62300
Ha = 195
799 n
mi
Hp = 184
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14366700
13 X = -4435185
12
Y = 11173970
06 feet Y = 3356543
54 meter
Z = 12464299
00 Z = 3777708
27
XDOT = -19125
876868 XDOT = -5777
400368
YDOT = -9221
599724 feet/sec YDOT = -2875
641700 meter/sec
ZDOT = -13712
072852 ZDOT = -4207
633657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9965026
71 X = 3037340
14
Y = -15300039
27 feet Y = -4663451
97 meter
Z = 12378427
62 Z = 3772944
74
XDOT = 19901
539367 XDOT = 6065
989199
YDOT = 1723
161066 feet/sec YDOT = 525
219493 meter/sec
ZDOT = -13825
056146 ZDOT = -4213
877113
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
53991295
00016717 00000-0 10270-3 0 9140
2 25544 51
6469 355
3071 0007224 82
3761 277
8221 15
72048019 41774
Satellite: ISS
Catalog Number: 25544
Epoch time: 10284
53991295 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 355
3071 deg
Eccentricity:
0007224
Arg of perigee: 82
3761 deg
Mean anomaly: 277
8221 deg
Mean motion: 15
72048019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4177
Checksum: 318
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list