[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 3rd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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 3178)
---------------------------------------
Vector Time (GMT): 2012/001/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1348038
23 A = 6768166
42 meter
Y = 5100674
67 meter E =
0016988
Z = -4221680
97 I = 51
32012
XDOT = -5213
574052 Wp = 219
94281
YDOT = -4353
191257 meter/sec RA = 244
96613 deg
ZDOT = -3599
575759 TA = 13
22020
MA = 13
17574
Ha = 218
077 n
mi
Hp = 204
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4422697
60 X = -1384466
84
Y = 16734496
96 feet Y = 5085396
63 meter
Z = -13850659
34 Z = -4228317
88
XDOT = -17104
901746 XDOT = -5147
022403
YDOT = -14282
123548 feet/sec YDOT = -4411
120342 meter/sec
ZDOT = -11809
631755 ZDOT = -3624
741629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17214077
82 X = 5246850
92
Y = 1586506
05 feet Y = 483567
04 meter
Z = -13878145
78 Z = -4230058
83
XDOT = -11236
794930 XDOT = -3424
975095
YDOT = 17856
113759 feet/sec YDOT = 5442
543474 meter/sec
ZDOT = -11912
187237 ZDOT = -3630
834670
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 12001
18002196
00016717 00000-0 10270-3 0 9008
2 25544 51
6417 245
7366 0024414 229
5237 130
3790 15
58783768 31795
Satellite: ISS
Catalog Number: 25544
Epoch time: 12001
18002196 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 245
7366 deg
Eccentricity:
0024414
Arg of perigee: 229
5237 deg
Mean anomaly: 130
3790 deg
Mean motion: 15
58783768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3179
Checksum: 307
Coasting Arc #2 (Orbit 3194)
---------------------------------------
Vector Time (GMT): 2012/002/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3569441
96 A = 6763690
70 meter
Y = -2282813
89 meter E =
0022724
Z = 5287369
61 I = 51
31995
XDOT = 3948
931475 Wp = 229
16979
YDOT = 6565
643665 meter/sec RA = 239
90113 deg
ZDOT = 154
680157 TA = 219
26604
MA = 219
43107
Ha = 217
749 n
mi
Hp = 204
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11710767
59 X = 3569018
67
Y = -7489546
88 feet Y = -2242900
89 meter
Z = 17347013
17 Z = 5304708
65
XDOT = 12955
811925 XDOT = 3874
468243
YDOT = 21540
825674 feet/sec YDOT = 6609
386687 meter/sec
ZDOT = 507
480829 ZDOT = 173
683460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9435138
95 X = -2875830
35
Y = -10086825
14 feet Y = -3074464
30 meter
Z = 17418047
17 Z = 5309020
78
XDOT = 18155
117135 XDOT = 5533
679703
YDOT = -15892
656024 feet/sec YDOT = -4844
081556 meter/sec
ZDOT = 584
701936 ZDOT = 178
217150
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 12002
20575695
00016717 00000-0 10270-3 0 9012
2 25544 51
6422 240
5871 0024382 233
5431 126
3477 15
58838962 31952
Satellite: ISS
Catalog Number: 25544
Epoch time: 12002
20575695 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 240
5871 deg
Eccentricity:
0024382
Arg of perigee: 233
5431 deg
Mean anomaly: 126
3477 deg
Mean motion: 15
58838962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3195
Checksum: 308
Coasting Arc #3 (Orbit 3209)
---------------------------------------
Vector Time (GMT): 2012/003/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5053009
80 A = 6767363
01 meter
Y = -1117967
37 meter E =
0020126
Z = -4359850
58 I = 51
34840
XDOT = -1443
790261 Wp = 216
20708
YDOT = -6739
183915 meter/sec RA = 234
83367 deg
ZDOT = 3377
456491 TA = 88
20453
MA = 87
97403
Ha = 217
337 n
mi
Hp = 204
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16578116
13 X = -5018953
68
Y = -3667871
96 feet Y = -1174282
48 meter
Z = -14303971
71 Z = -4384315
30
XDOT = -4736
844689 XDOT = -1384
731022
YDOT = -22110
183449 feet/sec YDOT = -6754
999303 meter/sec
ZDOT = 11080
894000 ZDOT = 3370
585547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -383539
12 X = -116902
72
Y = 16889975
46 feet Y = 5148064
52 meter
Z = -14403904
07 Z = -4390309
96
XDOT = -19517
286105 XDOT = -5948
868805
YDOT = 9049
693632 feet/sec YDOT = 2758
346619 meter/sec
ZDOT = 11053
271132 ZDOT = 3369
037041
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 12003
16736755
00016717 00000-0 10270-3 0 9025
2 25544 51
6418 235
7584 0024145 237
1170 122
7662 15
58869592 32108
Satellite: ISS
Catalog Number: 25544
Epoch time: 12003
16736755 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 235
7584 deg
Eccentricity:
0024145
Arg of perigee: 237
1170 deg
Mean anomaly: 122
7662 deg
Mean motion: 15
58869592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3210
Checksum: 307
Coasting Arc #4 (Orbit 3225)
---------------------------------------
Vector Time (GMT): 2012/004/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5213032
19 A = 6773992
62 meter
Y = 3903454
64 meter E =
0019114
Z = 1831128
79 I = 51
38959
XDOT = -1725
247394 Wp = 206
03676
YDOT = 4928
290071 meter/sec RA = 229
80124 deg
ZDOT = -5633
303006 TA = 313
69627
MA = 313
85448
Ha = 216
992 n
mi
Hp = 204
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17103123
98 X = 5160100
30
Y = 12806609
72 feet Y = 3961453
85 meter
Z = 6007640
40 Z = 1856325
32
XDOT = -5660
260480 XDOT = -1752
862905
YDOT = 16168
930680 feet/sec YDOT = 4908
843396 meter/sec
ZDOT = -18481
965244 ZDOT = -5641
750837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8902105
98 X = 2713361
90
Y = -19391585
10 feet Y = -5910555
14 meter
Z = 6110383
14 Z = 1862444
78
XDOT = 15562
082812 XDOT = 4743
322841
YDOT = 1349
156201 feet/sec YDOT = 411
222810 meter/sec
ZDOT = -18516
839880 ZDOT = -5643
932795
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 12004
19306564
00016717 00000-0 10270-3 0 9031
2 25544 51
6421 230
6091 0024119 241
2992 118
5739 15
58907068 32264
Satellite: ISS
Catalog Number: 25544
Epoch time: 12004
19306564 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 230
6091 deg
Eccentricity:
0024119
Arg of perigee: 241
2992 deg
Mean anomaly: 118
5739 deg
Mean motion: 15
58907068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3226
Checksum: 299
Coasting Arc #5 (Orbit 3241)
---------------------------------------
Vector Time (GMT): 2012/005/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3816267
05 A = 6774679
68 meter
Y = -5412817
81 meter E =
0010104
Z = 1444468
06 I = 51
41123
XDOT = 4720
749921 Wp = 251
16419
YDOT = -1797
450227 meter/sec RA = 224
79178 deg
ZDOT = 5766
543539 TA = 124
65620
MA = 124
56091
Ha = 216
808 n
mi
Hp = 204
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12520561
19 X = -3762473
12
Y = -17758588
60 feet Y = -5455193
02 meter
Z = 4739068
45 Z = 1426058
88
XDOT = 15488
024674 XDOT = 4712
485906
YDOT = -5897
146415 feet/sec YDOT = -1744
706713 meter/sec
ZDOT = 18919
106100 ZDOT = 5789
456502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14420021
30 X = -4395222
49
Y = 16275724
86 feet Y = 4960840
94 meter
Z = 4664167
39 Z = 1421638
22
XDOT = -8066
841639 XDOT = -2458
773332
YDOT = -12567
075320 feet/sec YDOT = -3830
444557 meter/sec
ZDOT = 19012
912670 ZDOT = 5795
135782
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 12005
21874680
00016717 00000-0 10270-3 0 9045
2 25544 51
6413 225
4584 0023899 245
2629 114
6039 15
58881224 32422
Satellite: ISS
Catalog Number: 25544
Epoch time: 12005
21874680 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 225
4584 deg
Eccentricity:
0023899
Arg of perigee: 245
2629 deg
Mean anomaly: 114
6039 deg
Mean motion: 15
58881224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3242
Checksum: 311
Coasting Arc #6 (Orbit 3256)
---------------------------------------
Vector Time (GMT): 2012/006/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1114524
31 A = 6768038
29 meter
Y = 5223994
17 meter E =
0016316
Z = -4138937
35 I = 51
41266
XDOT = -6535
318342 Wp = 248
04189
YDOT = -1565
945331 meter/sec RA = 219
76612 deg
ZDOT = -3730
498241 TA = 343
54864
MA = 343
60152
Ha = 216
512 n
mi
Hp = 204
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3656575
81 X = 1076131
72
Y = 17139088
48 feet Y = 5236243
29 meter
Z = -13579190
78 Z = -4133615
69
XDOT = -21441
333144 XDOT = -6499
200016
YDOT = -5137
615914 feet/sec YDOT = -1638
824888 meter/sec
ZDOT = -12239
167457 ZDOT = -3762
158938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15697775
17 X = 4784681
87
Y = -7828135
50 feet Y = -2386015
70 meter
Z = -13557782
72 Z = -4132412
17
XDOT = -311
498581 XDOT = -94
944768
YDOT = 20829
724764 feet/sec YDOT = 6348
900108 meter/sec
ZDOT = -12368
528262 ZDOT = -3769
927414
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 12006
18030201
00016717 00000-0 10270-3 0 9056
2 25544 51
6421 220
6305 0023979 248
7136 111
1459 15
58950495 32570
Satellite: ISS
Catalog Number: 25544
Epoch time: 12006
18030201 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 220
6305 deg
Eccentricity:
0023979
Arg of perigee: 248
7136 deg
Mean anomaly: 111
1459 deg
Mean motion: 15
58950495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3257
Checksum: 290
Coasting Arc #7 (Orbit 3272)
---------------------------------------
Vector Time (GMT): 2012/007/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2167000
11 A = 6763324
89 meter
Y = -3635581
29 meter E =
0021738
Z = 5293235
19 I = 51
41963
XDOT = 6406
472849 Wp = 249
40061
YDOT = 4193
665051 meter/sec RA = 214
70683 deg
ZDOT = 250
949551 TA = 198
15898
MA = 198
23673
Ha = 216
241 n
mi
Hp = 204
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7109580
40 X = 2181779
64
Y = -11927760
15 feet Y = -3611266
59 meter
Z = 17366257
18 Z = 5303797
77
XDOT = 21018
611710 XDOT = 6357
883257
YDOT = 13758
743607 feet/sec YDOT = 4265
034455 meter/sec
ZDOT = 823
325298 ZDOT = 281
954248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13344910
94 X = -4067528
85
Y = -3635961
55 feet Y = -1108241
08 meter
Z = 17409699
02 Z = 5306476
26
XDOT = 7509
714129 XDOT = 2288
960866
YDOT = -22910
181471 feet/sec YDOT = -6983
023312 meter/sec
ZDOT = 949
845386 ZDOT = 289
512874
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 12007
20594355
00016717 00000-0 10270-3 0 9066
2 25544 51
6406 215
4799 0023870 252
6607 107
1937 15
58972112 32733
Satellite: ISS
Catalog Number: 25544
Epoch time: 12007
20594355 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 215
4799 deg
Eccentricity:
0023870
Arg of perigee: 252
6607 deg
Mean anomaly: 107
1937 deg
Mean motion: 15
58972112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3273
Checksum: 313
Coasting Arc #8 (Orbit 3287)
---------------------------------------
Vector Time (GMT): 2012/008/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5007923
33 A = 6766883
65 meter
Y = 1173237
94 meter E =
0017096
Z = -4389442
23 I = 51
45820
XDOT = -4228
340692 Wp = 239
45978
YDOT = -5471
187074 meter/sec RA = 209
64562 deg
ZDOT = 3343
512786 TA = 64
44702
MA = 64
27037
Ha = 215
965 n
mi
Hp = 204
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16430194
64 X = -4999347
80
Y = 3849205
85 feet Y = 1117284
76 meter
Z = -14401057
19 Z = -4413749
29
XDOT = -13872
508831 XDOT = -4183
088399
YDOT = -17950
088825 feet/sec YDOT = -5518
218367 meter/sec
ZDOT = 10969
530137 ZDOT = 3323
081139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8247162
14 X = 2513735
02
Y = 14624508
62 feet Y = 4457550
23 meter
Z = -14500558
41 Z = -4419770
20
XDOT = -12291
414431 XDOT = -3746
423119
YDOT = 17784
434558 feet/sec YDOT = 5420
695653 meter/sec
ZDOT = 10886
320516 ZDOT = 3318
150493
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 12008
16746430
00016717 00000-0 10270-3 0 9076
2 25544 51
6413 210
6510 0023947 256
6361 103
2125 15
58991306 32883
Satellite: ISS
Catalog Number: 25544
Epoch time: 12008
16746430 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 210
6510 deg
Eccentricity:
0023947
Arg of perigee: 256
6361 deg
Mean anomaly: 103
2125 deg
Mean motion: 15
58991306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3288
Checksum: 293
Coasting Arc #9 (Orbit 3303)
---------------------------------------
Vector Time (GMT): 2012/009/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6382251
73 A = 6773600
57 meter
Y = 1324145
95 meter E =
0014308
Z = 1829611
14 I = 51
50652
XDOT = 531
846591 Wp = 228
57337
YDOT = 5177
821663 meter/sec RA = 204
61940 deg
ZDOT = -5640
453064 TA = 291
22726
MA = 291
38003
Ha = 215
762 n
mi
Hp = 204
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20939146
11 X = 6358082
81
Y = 4344310
87 feet Y = 1395380
87 meter
Z = 6002661
21 Z = 1860556
84
XDOT = 1744
903513 XDOT = 501
307293
YDOT = 16987
603881 feet/sec YDOT = 5183
598968 meter/sec
ZDOT = -18505
423437 ZDOT = -5637
943017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2013890
71 X = -613833
89
Y = -21253948
61 feet Y = -6478203
54 meter
Z = 6129170
50 Z = 1868171
17
XDOT = 14133
230700 XDOT = 4307
808717
YDOT = -6637
789882 feet/sec YDOT = -2023
198356 meter/sec
ZDOT = -18495
492744 ZDOT = -5637
426188
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 12009
19306781
00016717 00000-0 10270-3 0 9082
2 25544 51
6397 205
5004 0023825 260
5378 99
3084 15
59038602 33042
Satellite: ISS
Catalog Number: 25544
Epoch time: 12009
19306781 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 205
5004 deg
Eccentricity:
0023825
Arg of perigee: 260
5378 deg
Mean anomaly: 99
3084 deg
Mean motion: 15
59038602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3304
Checksum: 308
Coasting Arc #10 (Orbit 3319)
---------------------------------------
Vector Time (GMT): 2012/010/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5718830
58 A = 6774060
05 meter
Y = -3304594
50 meter E =
0012377
Z = 1501393
40 I = 51
53636
XDOT = 3574
254014 Wp = 290
58446
YDOT = -3586
463591 meter/sec RA = 199
61781 deg
ZDOT = 5763
235970 TA = 85
86013
MA = 85
71869
Ha = 215
735 n
mi
Hp = 204
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18762567
51 X = -5688746
21
Y = -10841845
46 feet Y = -3368377
90 meter
Z = 4925831
35 Z = 1473684
82
XDOT = 11726
555163 XDOT = 3586
096898
YDOT = -11766
612831 feet/sec YDOT = -3546
428395 meter/sec
ZDOT = 18908
254495 ZDOT = 5780
627680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4451836
13 X = -1356919
65
Y = 21233527
36 feet Y = 6471979
14 meter
Z = 4812674
69 Z = 1466903
25
XDOT = -13247
648701 XDOT = -4037
883324
YDOT = -7046
818544 feet/sec YDOT = -2147
870292 meter/sec
ZDOT = 18979
641657 ZDOT = 5784
994777
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 12010
21865049
00016717 00000-0 10270-3 0 9095
2 25544 51
6397 200
3489 0023944 264
4832 95
3592 15
59077045 33204
Satellite: ISS
Catalog Number: 25544
Epoch time: 12010
21865049 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 200
3489 deg
Eccentricity:
0023944
Arg of perigee: 264
4832 deg
Mean anomaly: 95
3592 deg
Mean motion: 15
59077045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3320
Checksum: 313
Coasting Arc #11 (Orbit 3334)
---------------------------------------
Vector Time (GMT): 2012/011/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3130481
67 A = 6767460
46 meter
Y = 4266792
31 meter E =
0016543
Z = -4205395
75 I = 51
54268
XDOT = -6643
091860 Wp = 277
32385
YDOT = 1263
987718 meter/sec RA = 194
59867 deg
ZDOT = -3648
294641 TA = 315
28371
MA = 315
41697
Ha = 215
697 n
mi
Hp = 204
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10270609
17 X = 3102965
37
Y = 13998662
45 feet Y = 4301645
72 meter
Z = -13797230
15 Z = -4190254
84
XDOT = -21794
920802 XDOT = -6639
010031
YDOT = 4146
941333 feet/sec YDOT = 1189
723652 meter/sec
ZDOT = -11969
470608 ZDOT = -3680
555888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9832715
68 X = 2997011
74
Y = -14368858
74 feet Y = -4379628
14 meter
Z = -13735542
35 Z = -4186593
31
XDOT = 9986
741137 XDOT = 3043
958699
YDOT = 18447
411257 feet/sec YDOT = 5622
770951 meter/sec
ZDOT = -12101
562173 ZDOT = -3688
556150
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 12011
18011743
00016717 00000-0 10270-3 0 9108
2 25544 51
6392 195
5196 0023904 268
3875 91
4542 15
59086137 33355
Satellite: ISS
Catalog Number: 25544
Epoch time: 12011
18011743 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 195
5196 deg
Eccentricity:
0023904
Arg of perigee: 268
3875 deg
Mean anomaly: 91
4542 deg
Mean motion: 15
59086137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3335
Checksum: 307
Coasting Arc #12 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2012/012/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 613130
97 A = 6762907
07 meter
Y = -4169454
69 meter E =
0021489
Z = 5307836
51 I = 51
55719
XDOT = 7564
233122 Wp = 272
31034
YDOT = 1209
629736 meter/sec RA = 189
54588 deg
ZDOT = 77
539822 TA = 176
95576
MA = 176
94266
Ha = 215
608 n
mi
Hp = 204
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2011584
54 X = 633925
27
Y = -13679313
29 feet Y = -4162482
26 meter
Z = 17414161
77 Z = 5310865
34
XDOT = 24817
037801 XDOT = 7549
767947
YDOT = 3968
601497 feet/sec YDOT = 1294
136759 meter/sec
ZDOT = 254
395741 ZDOT = 114
250786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13499655
60 X = -4114695
03
Y = 2913509
60 feet Y = 888037
72 meter
Z = 17426814
84 Z = 5311693
16
XDOT = -4593
588715 XDOT = -1400
125840
YDOT = -23682
128497 feet/sec YDOT = -7218
312766 meter/sec
ZDOT = 404
558038 ZDOT = 123
309290
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 12012
20566242
00016717 00000-0 10270-3 0 9112
2 25544 51
6389 190
3676 0023913 272
4626 87
3792 15
59108526 33513
Satellite: ISS
Catalog Number: 25544
Epoch time: 12012
20566242 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 190
3676 deg
Eccentricity:
0023913
Arg of perigee: 272
4626 deg
Mean anomaly: 87
3792 deg
Mean motion: 15
59108526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 309
Coasting Arc #13 (Orbit 3365)
---------------------------------------
Vector Time (GMT): 2012/013/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4224450
02 A = 6766873
37 meter
Y = 3075424
58 meter E =
0015724
Z = -4286164
81 I = 51
60126
XDOT = -5984
289549 Wp = 269
07035
YDOT = -3279
564326 meter/sec RA = 184
49463 deg
ZDOT = 3533
531710 TA = 36
90855
MA = 36
80045
Ha = 215
550 n
mi
Hp = 204
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13859744
16 X = -4237705
17
Y = 10089975
67 feet Y = 3028110
19 meter
Z = -14062220
52 Z = -4306718
79
XDOT = -19633
495895 XDOT = -5964
336871
YDOT = -10759
725478 feet/sec YDOT = -3346
372867 meter/sec
ZDOT = 11592
951803 ZDOT = 3504
509129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14370982
62 X = 4380275
50
Y = 9219362
62 feet Y = 2810061
73 meter
Z = -14146532
25 Z = -4311863
03
XDOT = -2273
320164 XDOT = -692
907986
YDOT = 21207
493022 feet/sec YDOT = 6464
043873 meter/sec
ZDOT = 11474
367270 ZDOT = 3497
387144
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 12013
16709157
00016717 00000-0 10270-3 0 9123
2 25544 51
6391 185
5384 0023944 276
3558 83
4870 15
59129971 33666
Satellite: ISS
Catalog Number: 25544
Epoch time: 12013
16709157 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 185
5384 deg
Eccentricity:
0023944
Arg of perigee: 276
3558 deg
Mean anomaly: 83
4870 deg
Mean motion: 15
59129971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3366
Checksum: 333
Coasting Arc #14 (Orbit 3381)
---------------------------------------
Vector Time (GMT): 2012/014/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6449171
97 A = 6773469
18 meter
Y = -1322714
98 meter E =
0011262
Z = 1598018
16 I = 51
65440
XDOT = 2339
814293 Wp = 261
00141
YDOT = 4518
663563 meter/sec RA = 179
47978 deg
ZDOT = -5738
887839 TA = 261
49508
MA = 261
62274
Ha = 215
638 n
mi
Hp = 204
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21158700
69 X = 6455720
80
Y = -4339616
07 feet Y = -1250559
78 meter
Z = 5242841
72 Z = 1629363
45
XDOT = 7676
556080 XDOT = 2316
989680
YDOT = 14825
011690 feet/sec YDOT = 4544
701289 meter/sec
ZDOT = -18828
372175 ZDOT = -5727
576623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11963457
52 X = -3646461
85
Y = -17945358
83 feet Y = -5469745
37 meter
Z = 5371224
48 Z = 1637149
22
XDOT = 9499
043552 XDOT = 2895
308475
YDOT = -11919
657125 feet/sec YDOT = -3633
111492 meter/sec
ZDOT = -18782
347015 ZDOT = -5724
859370
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 12014
19259616
00016717 00000-0 10270-3 0 9138
2 25544 51
6391 180
3869 0024011 280
6464 79
1987 15
59202727 33827
Satellite: ISS
Catalog Number: 25544
Epoch time: 12014
19259616 = yrday
fracday
Element set: 913
Inclination: 51
6391 deg
RA of node: 180
3869 deg
Eccentricity:
0024011
Arg of perigee: 280
6464 deg
Mean anomaly: 79
1987 deg
Mean motion: 15
59202727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3382
Checksum: 319
Coasting Arc #15 (Orbit 3397)
---------------------------------------
Vector Time (GMT): 2012/015/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6479451
10 A = 6773156
27 meter
Y = -793574
85 meter E =
0015750
Z = 1787206
71 I = 51
68400
XDOT = 2131
130591 Wp = 317
89150
YDOT = -4710
817851 meter/sec RA = 174
48820 deg
ZDOT = 5674
900431 TA = 61
77572
MA = 61
61679
Ha = 215
735 n
mi
Hp = 204
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21258041
67 X = -6478777
40
Y = -2603592
04 feet Y = -866028
33 meter
Z = 5863539
07 Z = 1755731
70
XDOT = 6991
898265 XDOT = 2156
082344
YDOT = -15455
439144 feet/sec YDOT = -4686
846835 meter/sec
ZDOT = 18618
439733 ZDOT = 5685
313799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5948244
29 X = 1813024
86
Y = 20610561
24 feet Y = 6282099
07 meter
Z = 5734742
59 Z = 1747949
54
XDOT = -15411
033676 XDOT = -4697
283064
YDOT = -707
109452 feet/sec YDOT = -215
526961 meter/sec
ZDOT = 18661
353409 ZDOT = 5687
980519
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 12015
21807881
00016717 00000-0 10270-3 0 9146
2 25544 51
6390 175
2352 0024003 283
9211 75
9274 15
59257004 33981
Satellite: ISS
Catalog Number: 25544
Epoch time: 12015
21807881 = yrday
fracday
Element set: 914
Inclination: 51
6390 deg
RA of node: 175
2352 deg
Eccentricity:
0024003
Arg of perigee: 283
9211 deg
Mean anomaly: 75
9274 deg
Mean motion: 15
59257004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3398
Checksum: 301
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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