[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 23rd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 30138 95 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 284 ET - UTC (sec) : 67 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 3779)
---------------------------------------
Vector Time (GMT): 2012/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213457
64 A = 6788551
09 meter
Y = -2152756
20 meter E =
0012203
Z = 4862627
36 I = 51
46580
XDOT = 5310
168829 Wp = 176
31137
YDOT = 4978
103657 meter/sec RA = 207
86870 deg
ZDOT = -2408
965248 TA = 297
30910
MA = 297
43330
Ha = 229
715 n
mi
Hp = 217
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13823679
93 X = 4213595
28
Y = -7062848
43 feet Y = -2105637
69 meter
Z = 15953501
84 Z = 4883096
78
XDOT = 17421
813743 XDOT = 5265
810292
YDOT = 16332
361079 feet/sec YDOT = 5037
237147 meter/sec
ZDOT = -7903
429291 ZDOT = -2383
276415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8239058
73 X = -2511265
10
Y = 13052984
19 feet Y = 3978549
58 meter
Z = 16038381
80 Z = 4888498
77
XDOT = -22391
082742 XDOT = -6824
802020
YDOT = -4598
755555 feet/sec YDOT = -1401
700693 meter/sec
ZDOT = -7797
591513 ZDOT = -2376
705893
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 12296
54415434
00016717 00000-0 10270-3 0 9007
2 25544 51
6477 208
7175 0016455 197
7679 162
2898 15
50921750 37808
Satellite: ISS
Catalog Number: 25544
Epoch time: 12296
54415434 = yrday
fracday
Element set: 900
Inclination: 51
6477 deg
RA of node: 208
7175 deg
Eccentricity:
0016455
Arg of perigee: 197
7679 deg
Mean anomaly: 162
2898 deg
Mean motion: 15
50921750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3780
Checksum: 339
Coasting Arc #2 (Orbit 3794)
---------------------------------------
Vector Time (GMT): 2012/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4637492
59 A = 6789648
32 meter
Y = 1979125
79 meter E =
0019087
Z = -4559734
00 I = 51
49802
XDOT = -5094
949272 Wp = 170
10005
YDOT = -4809
210466 meter/sec RA = 202
89235 deg
ZDOT = 3077
947313 TA = 130
91035
MA = 130
74490
Ha = 229
512 n
mi
Hp = 218
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15214870
69 X = -4637128
53
Y = 6493194
86 feet Y = 1927268
20 meter
Z = -14959757
22 Z = -4582262
19
XDOT = -16715
712836 XDOT = -5055
745128
YDOT = -15778
249561 feet/sec YDOT = -4865
965975 meter/sec
ZDOT = 10098
252340 ZDOT = 3053
291567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9502273
29 X = 2896292
90
Y = -13437179
25 feet Y = -4095652
24 meter
Z = -15053146
58 Z = -4588199
08
XDOT = 21568
886393 XDOT = 6574
196573
YDOT = 3993
659217 feet/sec YDOT = 1217
267329 meter/sec
ZDOT = 9996
659522 ZDOT = 3046
981822
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 12297
51066594
00016717 00000-0 10270-3 0 9015
2 25544 51
6485 203
9217 0016465 201
3791 158
6674 15
50975141 37959
Satellite: ISS
Catalog Number: 25544
Epoch time: 12297
51066594 = yrday
fracday
Element set: 901
Inclination: 51
6485 deg
RA of node: 203
9217 deg
Eccentricity:
0016465
Arg of perigee: 201
3791 deg
Mean anomaly: 158
6674 deg
Mean motion: 15
50975141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3795
Checksum: 328
Coasting Arc #3 (Orbit 3810)
---------------------------------------
Vector Time (GMT): 2012/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5002360
24 A = 6790827
33 meter
Y = -1874512
51 meter E =
0012519
Z = 4181959
44 I = 51
53084
XDOT = 4835
231670 Wp = 167
53816
YDOT = 4658
208753 meter/sec RA = 197
92086 deg
ZDOT = -3705
695191 TA = 320
52678
MA = 320
61792
Ha = 229
166 n
mi
Hp = 218
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16411943
06 X = 5002634
39
Y = -6149975
41 feet Y = -1818571
13 meter
Z = 13720339
38 Z = 4206261
78
XDOT = 15863
620964 XDOT = 4800
784883
YDOT = 15282
837115 feet/sec YDOT = 4712
086447 meter/sec
ZDOT = -12157
792620 ZDOT = -3682
289607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10470175
14 X = -3191309
38
Y = 13956192
53 feet Y = 4253847
48 meter
Z = 13821067
54 Z = 4212661
39
XDOT = -20634
065368 XDOT = -6289
263124
YDOT = -3567
365781 feet/sec YDOT = -1087
333090 meter/sec
ZDOT = -12061
347904 ZDOT = -3676
298841
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 12298
54157240
00016717 00000-0 10270-3 0 9029
2 25544 51
6484 198
8077 0016463 205
2186 154
8163 15
51032896 38115
Satellite: ISS
Catalog Number: 25544
Epoch time: 12298
54157240 = yrday
fracday
Element set: 902
Inclination: 51
6484 deg
RA of node: 198
8077 deg
Eccentricity:
0016463
Arg of perigee: 205
2186 deg
Mean anomaly: 154
8163 deg
Mean motion: 15
51032896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3811
Checksum: 318
Coasting Arc #4 (Orbit 3825)
---------------------------------------
Vector Time (GMT): 2012/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5412332
44 A = 6792244
81 meter
Y = 1777005
46 meter E =
0015779
Z = -3710908
37 I = 51
56625
XDOT = -4440
200542 Wp = 188
91296
YDOT = -4518
136921 meter/sec RA = 192
95087 deg
ZDOT = 4294
738939 TA = 126
91561
MA = 126
77094
Ha = 228
942 n
mi
Hp = 218
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17756996
19 X = -5413773
99
Y = 5830070
41 feet Y = 1716473
00 meter
Z = -12174896
22 Z = -3737205
28
XDOT = -14567
587079 XDOT = -4410
210971
YDOT = -14823
283862 feet/sec YDOT = -4567
621972 meter/sec
ZDOT = 14090
350850 ZDOT = 4273
241551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11534812
58 X = 3515810
88
Y = -14614485
80 feet Y = -4454495
27 meter
Z = -12283877
09 Z = -3744125
74
XDOT = 19332
628903 XDOT = 5892
585290
YDOT = 3441
437951 feet/sec YDOT = 1048
950288 meter/sec
ZDOT = 14001
781658 ZDOT = 4267
743049
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 12299
50800919
00016717 00000-0 10270-3 0 9035
2 25544 51
6492 194
0116 0016489 209
1202 150
9031 15
51098969 38266
Satellite: ISS
Catalog Number: 25544
Epoch time: 12299
50800919 = yrday
fracday
Element set: 903
Inclination: 51
6492 deg
RA of node: 194
0116 deg
Eccentricity:
0016489
Arg of perigee: 209
1202 deg
Mean anomaly: 150
9031 deg
Mean motion: 15
51098969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3826
Checksum: 315
Coasting Arc #5 (Orbit 3841)
---------------------------------------
Vector Time (GMT): 2012/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5739850
16 A = 6793669
05 meter
Y = -1734465
91 meter E =
0015165
Z = 3173362
18 I = 51
60107
XDOT = 3999
027386 Wp = 165
65185
YDOT = 4422
825247 meter/sec RA = 187
98590 deg
ZDOT = -4825
316956 TA = 337
70280
MA = 337
76867
Ha = 228
600 n
mi
Hp = 218
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18831529
38 X = 5743402
94
Y = -5690504
96 feet Y = -1670259
18 meter
Z = 10411293
25 Z = 3201255
42
XDOT = 13120
168588 XDOT = 3972
713955
YDOT = 14510
581518 feet/sec YDOT = 4467
397328 meter/sec
ZDOT = -15831
092375 ZDOT = -4805
953793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12255522
54 X = -3735483
27
Y = 15309808
40 feet Y = 4666429
60 meter
Z = 10526884
95 Z = 3208594
53
XDOT = -17990
929863 XDOT = -5483
635422
YDOT = -3592
306857 feet/sec YDOT = -1094
935130 meter/sec
ZDOT = -15751
341319 ZDOT = -4801
008834
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 12300
53883711
00016717 00000-0 10270-3 0 9043
2 25544 51
6490 188
8971 0016485 212
7751 147
2379 15
51140781 38421
Satellite: ISS
Catalog Number: 25544
Epoch time: 12300
53883711 = yrday
fracday
Element set: 904
Inclination: 51
6490 deg
RA of node: 188
8971 deg
Eccentricity:
0016485
Arg of perigee: 212
7751 deg
Mean anomaly: 147
2379 deg
Mean motion: 15
51140781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3842
Checksum: 318
Coasting Arc #6 (Orbit 3856)
---------------------------------------
Vector Time (GMT): 2012/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6072357
80 A = 6794984
08 meter
Y = 1696317
59 meter E =
0011626
Z = -2544631
73 I = 51
63678
XDOT = -3435
315892 Wp = 211
01869
YDOT = -4359
568877 meter/sec RA = 183
02298 deg
ZDOT = 5271
125737 TA = 120
47049
MA = 120
35562
Ha = 228
325 n
mi
Hp = 218
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19922433
73 X = -6078513
53
Y = 5565346
44 feet Y = 1628378
07 meter
Z = -8348529
31 Z = -2574146
72
XDOT = -11270
721432 XDOT = -3411
917477
YDOT = -14303
047497 feet/sec YDOT = -4397
853475 meter/sec
ZDOT = 17293
719609 ZDOT = 5254
493939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12961902
22 X = 3950787
80
Y = -16056411
82 feet Y = -4893994
32 meter
Z = -8470839
29 Z = -2581911
82
XDOT = 16391
008325 XDOT = 4995
979338
YDOT = 4109
544819 feet/sec YDOT = 1252
589261 meter/sec
ZDOT = 17225
263847 ZDOT = 5250
260420
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 12301
50519946
00016717 00000-0 10270-3 0 9058
2 25544 51
6494 184
1007 0016516 217
0275 142
9738 15
51219827 38573
Satellite: ISS
Catalog Number: 25544
Epoch time: 12301
50519946 = yrday
fracday
Element set: 905
Inclination: 51
6494 deg
RA of node: 184
1007 deg
Eccentricity:
0016516
Arg of perigee: 217
0275 deg
Mean anomaly: 142
9738 deg
Mean motion: 15
51219827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3857
Checksum: 315
Coasting Arc #7 (Orbit 3872)
---------------------------------------
Vector Time (GMT): 2012/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6300512
27 A = 6796199
55 meter
Y = -1688289
64 meter E =
0018180
Z = 1865193
01 I = 51
67104
XDOT = 2834
505143 Wp = 173
79150
YDOT = 4363
650192 meter/sec RA = 178
06488 deg
ZDOT = -5637
524695 TA = 345
69243
MA = 345
74384
Ha = 228
032 n
mi
Hp = 218
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20670972
00 X = 6309861
88
Y = -5539008
01 feet Y = -1617780
97 meter
Z = 6119399
64 Z = 1895824
22
XDOT = 9299
557556 XDOT = 2812
885747
YDOT = 14316
437639 feet/sec YDOT = 4395
226133 meter/sec
ZDOT = -18495
815930 ZDOT = -5623
807262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13312604
69 X = -4057681
91
Y = 16708516
81 feet Y = 5092755
92 meter
Z = 6246340
32 Z = 1903884
53
XDOT = -14855
657598 XDOT = -4528
004436
YDOT = -4957
941706 feet/sec YDOT = -1511
180632 meter/sec
ZDOT = -18439
421654 ZDOT = -5620
335720
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 12302
53594911
00016717 00000-0 10270-3 0 9068
2 25544 51
6490 178
9857 0016550 220
4534 139
5388 15
51243106 38735
Satellite: ISS
Catalog Number: 25544
Epoch time: 12302
53594911 = yrday
fracday
Element set: 906
Inclination: 51
6490 deg
RA of node: 178
9857 deg
Eccentricity:
0016550
Arg of perigee: 220
4534 deg
Mean anomaly: 139
5388 deg
Mean motion: 15
51243106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3873
Checksum: 317
Coasting Arc #8 (Orbit 3887)
---------------------------------------
Vector Time (GMT): 2012/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6496868
72 A = 6796874
23 meter
Y = 1668337
75 meter E =
0007399
Z = -1110272
65 I = 51
70415
XDOT = -2143
213751 Wp = 233
90745
YDOT = -4414
609548 meter/sec RA = 173
10834 deg
ZDOT = 5875
985480 TA = 114
08301
MA = 114
00559
Ha = 227
663 n
mi
Hp = 218
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21315186
08 X = -6509647
95
Y = 5473549
06 feet Y = 1595614
20 meter
Z = -3642626
79 Z = -1141866
13
XDOT = -7031
541178 XDOT = -2122
234367
YDOT = -14483
627125 feet/sec YDOT = -4438
458690 meter/sec
ZDOT = 19278
167584 ZDOT = 5865
624753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13586625
59 X = 4141203
48
Y = -17283791
84 feet Y = -5268099
75 meter
Z = -3773562
22 Z = -1150181
77
XDOT = 13217
277560 XDOT = 4028
626200
YDOT = 6168
356974 feet/sec YDOT = 1880
115206 meter/sec
ZDOT = 19235
672824 ZDOT = 5863
033077
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 12303
50223740
00016717 00000-0 10270-3 0 9076
2 25544 51
6485 174
1886 0016560 224
9268 135
0544 15
51342389 38887
Satellite: ISS
Catalog Number: 25544
Epoch time: 12303
50223740 = yrday
fracday
Element set: 907
Inclination: 51
6485 deg
RA of node: 174
1886 deg
Eccentricity:
0016560
Arg of perigee: 224
9268 deg
Mean anomaly: 135
0544 deg
Mean motion: 15
51342389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3888
Checksum: 317
Coasting Arc #9 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2012/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6573745
76 A = 6797372
87 meter
Y = -1644430
75 meter E =
0019637
Z = 329847
01 I = 51
73532
XDOT = 1435
258496 Wp = 188
68180
YDOT = 4544
663282 meter/sec RA = 168
15594 deg
ZDOT = -6012
653293 TA = 347
76803
MA = 347
81564
Ha = 227
444 n
mi
Hp = 218
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21567407
34 X = 6590043
18
Y = -5395114
00 feet Y = -1570827
88 meter
Z = 1082175
23 Z = 361822
51
XDOT = 4708
853332 XDOT = 1413
541377
YDOT = 14910
312606 feet/sec YDOT = 4560
591599 meter/sec
ZDOT = -19726
552797 ZDOT = -6005
733590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13545885
75 X = -4128785
98
Y = 17620013
87 feet Y = 5370580
23 meter
Z = 1214705
07 Z = 370242
11
XDOT = -11760
663877 XDOT = -3584
650350
YDOT = -7696
567673 feet/sec YDOT = -2345
913827 meter/sec
ZDOT = -19698
316842 ZDOT = -6004
046973
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 12304
53290855
00016717 00000-0 10270-3 0 9082
2 25544 51
6480 169
0729 0016668 228
3862 131
5862 15
51348389 39047
Satellite: ISS
Catalog Number: 25544
Epoch time: 12304
53290855 = yrday
fracday
Element set: 908
Inclination: 51
6480 deg
RA of node: 169
0729 deg
Eccentricity:
0016668
Arg of perigee: 228
3862 deg
Mean anomaly: 131
5862 deg
Mean motion: 15
51348389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 333
Coasting Arc #10 (Orbit 3919)
---------------------------------------
Vector Time (GMT): 2012/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6593198
05 A = 6796971
73 meter
Y = 1581623
40 meter E =
0003860
Z = 496340
32 I = 51
76376
XDOT = -684
489235 Wp = 242
51790
YDOT = -4721
814820 meter/sec RA = 163
20368 deg
ZDOT = 5987
927619 TA = 122
81540
MA = 122
77822
Ha = 226
967 n
mi
Hp = 218
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21631227
19 X = -6612805
24
Y = 5189053
15 feet Y = 1507784
52 meter
Z = 1628413
12 Z = 464262
33
XDOT = -2245
699591 XDOT = -660
726835
YDOT = -15491
518439 feet/sec YDOT = -4729
336231 meter/sec
ZDOT = 19645
431820 ZDOT = 5984
660119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13433596
00 X = 4094560
06
Y = -17742325
81 feet Y = -5407860
91 meter
Z = 1495448
11 Z = 455812
58
XDOT = 10363
862201 XDOT = 3158
905199
YDOT = 9491
499374 feet/sec YDOT = 2893
009009 meter/sec
ZDOT = 19632
336741 ZDOT = 5983
936239
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 12305
56353573
00016717 00000-0 10270-3 0 9094
2 25544 51
6470 163
9549 0016656 232
9839 126
9789 15
51470466 39207
Satellite: ISS
Catalog Number: 25544
Epoch time: 12305
56353573 = yrday
fracday
Element set: 909
Inclination: 51
6470 deg
RA of node: 163
9549 deg
Eccentricity:
0016656
Arg of perigee: 232
9839 deg
Mean anomaly: 126
9789 deg
Mean motion: 15
51470466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3920
Checksum: 345
Coasting Arc #11 (Orbit 3934)
---------------------------------------
Vector Time (GMT): 2012/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6490253
35 A = 6796375
81 meter
Y = -1476442
72 meter E =
0018383
Z = -1312454
14 I = 51
78991
XDOT = -53
633070 Wp = 207
87293
YDOT = 4972
614323 meter/sec RA = 158
25439 deg
ZDOT = -5842
019243 TA = 346
38023
MA = 346
42977
Ha = 226
766 n
mi
Hp = 218
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21293482
13 X = 6512656
64
Y = -4843972
18 feet Y = -1403739
40 meter
Z = -4305951
91 Z = -1280869
56
XDOT = -175
961517 XDOT = -80
853965
YDOT = 16314
351455 feet/sec YDOT = 4971
862336 meter/sec
ZDOT = -19166
729799 ZDOT = -5842
345941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13105007
81 X = -3994406
38
Y = 17499875
10 feet Y = 5333961
93 meter
Z = -4175022
33 Z = -1272546
81
XDOT = -9245
724176 XDOT = -2818
096729
YDOT = -11510
737928 feet/sec YDOT = -3508
472920 meter/sec
ZDOT = -19168
545981 ZDOT = -5842
572815
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 12306
52971551
00016717 00000-0 10270-3 0 9105
2 25544 51
6464 159
1584 0016744 236
6133 123
3417 15
51474826 39351
Satellite: ISS
Catalog Number: 25544
Epoch time: 12306
52971551 = yrday
fracday
Element set: 910
Inclination: 51
6464 deg
RA of node: 159
1584 deg
Eccentricity:
0016744
Arg of perigee: 236
6133 deg
Mean anomaly: 123
3417 deg
Mean motion: 15
51474826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3935
Checksum: 310
Coasting Arc #12 (Orbit 3950)
---------------------------------------
Vector Time (GMT): 2012/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6321653
54 A = 6794860
51 meter
Y = 1301687
14 meter E =
0003719
Z = 2132312
41 I = 51
81312
XDOT = 780
003758 Wp = 205
67375
YDOT = -5250
138272 meter/sec RA = 153
30345 deg
ZDOT = 5517
802060 TA = 177
84850
MA = 177
84690
Ha = 226
250 n
mi
Hp = 218
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20740333
14 X = -6346097
96
Y = 4270627
09 feet Y = 1230857
77 meter
Z = 6995775
61 Z = 2101542
02
XDOT = 2559
067447 XDOT = 811
849079
YDOT = -17224
863097 feet/sec YDOT = -5241
237750 meter/sec
ZDOT = 18103
025130 ZDOT = 5521
668700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12777937
43 X = 3894715
33
Y = -16937900
18 feet Y = -5162671
97 meter
Z = 6868216
89 Z = 2093432
51
XDOT = 8307
574952 XDOT = 2532
148845
YDOT = 13614
127965 feet/sec YDOT = 4149
586204 meter/sec
ZDOT = 18119
534190 ZDOT = 5522
834021
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 12307
56026469
00016717 00000-0 10270-3 0 9110
2 25544 51
6456 154
0394 0016762 240
8460 119
1014 15
51591292 39516
Satellite: ISS
Catalog Number: 25544
Epoch time: 12307
56026469 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 154
0394 deg
Eccentricity:
0016762
Arg of perigee: 240
8460 deg
Mean anomaly: 119
1014 deg
Mean motion: 15
51591292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 300
Coasting Arc #13 (Orbit 3965)
---------------------------------------
Vector Time (GMT): 2012/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6043588
74 A = 6793173
54 meter
Y = -1049963
11 meter E =
0014351
Z = -2897129
81 I = 51
83365
XDOT = -1461
810414 Wp = 230
09861
YDOT = 5574
568101 meter/sec RA = 148
35385 deg
ZDOT = -5062
121202 TA = 342
80205
MA = 342
85062
Ha = 226
006 n
mi
Hp = 218
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19828047
05 X = 6068954
36
Y = -3444760
85 feet Y = -982238
08 meter
Z = -9505019
05 Z = -2867708
13
XDOT = -4795
965926 XDOT = -1499
446617
YDOT = 18289
265423 feet/sec YDOT = 5558
010827 meter/sec
ZDOT = -16608
009193 ZDOT = -5069
314131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12377913
19 X = -3772787
94
Y = 15940789
84 feet Y = 4858752
74 meter
Z = -9383053
80 Z = -2859954
80
XDOT = -7685
949163 XDOT = -2342
677305
YDOT = -15776
617062 feet/sec YDOT = -4808
712880 meter/sec
ZDOT = -16638
334250 ZDOT = -5071
364279
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 12308
52637017
00016717 00000-0 10270-3 0 9125
2 25544 51
6448 149
2420 0016687 244
6965 115
2458 15
51618949 39665
Satellite: ISS
Catalog Number: 25544
Epoch time: 12308
52637017 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 149
2420 deg
Eccentricity:
0016687
Arg of perigee: 244
6965 deg
Mean anomaly: 115
2458 deg
Mean motion: 15
51618949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3966
Checksum: 334
Coasting Arc #14 (Orbit 3981)
---------------------------------------
Vector Time (GMT): 2012/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5711329
38 A = 6791005
30 meter
Y = 704365
99 meter E =
0007636
Z = 3615328
32 I = 51
85242
XDOT = 2082
415102 Wp = 208
23069
YDOT = -5883
713165 meter/sec RA = 143
40147 deg
ZDOT = 4433
290681 TA = 194
33628
MA = 194
35796
Ha = 225
532 n
mi
Hp = 218
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18737957
30 X = -5736344
02
Y = 2310912
06 feet Y = 640358
46 meter
Z = 11861313
38 Z = 3587521
70
XDOT = 6832
070544 XDOT = 2126
516939
YDOT = -19303
520881 feet/sec YDOT = -5860
179733 meter/sec
ZDOT = 14544
916934 ZDOT = 4443
514232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12097317
03 X = 3687262
23
Y = -14588597
97 feet Y = -4446604
66 meter
Z = 11746056
50 Z = 3580198
02
XDOT = 7275
859289 XDOT = 2217
681911
YDOT = 17786
073557 feet/sec YDOT = 5421
195220 meter/sec
ZDOT = 14587
834890 ZDOT = 4446
372074
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 12309
55684140
00016717 00000-0 10270-3 0 9139
2 25544 51
6447 144
1228 0016765 248
7272 111
2089 15
51694612 39822
Satellite: ISS
Catalog Number: 25544
Epoch time: 12309
55684140 = yrday
fracday
Element set: 913
Inclination: 51
6447 deg
RA of node: 144
1228 deg
Eccentricity:
0016765
Arg of perigee: 248
7272 deg
Mean anomaly: 111
2089 deg
Mean motion: 15
51694612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3982
Checksum: 315
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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