[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 28th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 1961)
---------------------------------------
Vector Time (GMT): 2012/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1551783
19 A = 6784118
61 meter
Y = -6528760
13 meter E =
0016208
Z = -969650
62 I = 51
98861
XDOT = 4838
572021 Wp = 120
48923
YDOT = -279
377674 meter/sec RA = 70
14510 deg
ZDOT = -5943
961717 TA = 69
96846
MA = 69
79404
Ha = 221
266 n
mi
Hp = 209
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5091152
20 X = -1473951
57
Y = -21419816
71 feet Y = -6545677
86 meter
Z = -3181268
42 Z = -977000
69
XDOT = 15874
580121 XDOT = 4870
210937
YDOT = -916
593420 feet/sec YDOT = -225
092296 meter/sec
ZDOT = -19501
186736 ZDOT = -5920
379284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20872509
25 X = -6361940
82
Y = 6991239
08 feet Y = 2130929
67 meter
Z = -3210884
81 Z = -978677
69
XDOT = -1853
097375 XDOT = -564
824080
YDOT = -14322
304813 feet/sec YDOT = -4365
438507 meter/sec
ZDOT = -19403
914471 ZDOT = -5914
313131
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 12179
53029381
00016717 00000-0 10270-3 0 9008
2 25544 51
6398 70
6942 0007831 94
5220 265
6828 15
55781142 19627
Satellite: ISS
Catalog Number: 25544
Epoch time: 12179
53029381 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 70
6942 deg
Eccentricity:
0007831
Arg of perigee: 94
5220 deg
Mean anomaly: 265
6828 deg
Mean motion: 15
55781142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1962
Checksum: 319
Coasting Arc #2 (Orbit 1977)
---------------------------------------
Vector Time (GMT): 2012/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 177067
76 A = 6780507
09 meter
Y = 6048813
78 meter E =
0020841
Z = 3040003
49 I = 51
96575
XDOT = -5364
286155 Wp = 88
25303
YDOT = -2351
457568 meter/sec RA = 65
18363 deg
ZDOT = 4962
617746 TA = 306
49241
MA = 306
68423
Ha = 221
237 n
mi
Hp = 209
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 580930
96 X = 94647
81
Y = 19845189
57 feet Y = 6050332
68 meter
Z = 9973764
73 Z = 3040664
16
XDOT = -17599
364025 XDOT = -5361
700371
YDOT = -7714
755801 feet/sec YDOT = -2411
430441 meter/sec
ZDOT = 16281
554286 ZDOT = 4936
564180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19674370
91 X = 5996748
25
Y = -2654586
12 feet Y = -809117
85 meter
Z = 9975836
53 Z = 3040634
97
XDOT = -5956
163786 XDOT = -1815
438722
YDOT = 16991
560340 feet/sec YDOT = 5179
027592 meter/sec
ZDOT = 16174
374974 ZDOT = 4929
949492
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 12180
55800640
00016717 00000-0 10270-3 0 9018
2 25544 51
6400 65
5572 0007863 96
3896 263
8154 15
55814060 19782
Satellite: ISS
Catalog Number: 25544
Epoch time: 12180
55800640 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 65
5572 deg
Eccentricity:
0007863
Arg of perigee: 96
3896 deg
Mean anomaly: 263
8154 deg
Mean motion: 15
55814060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1978
Checksum: 314
Coasting Arc #3 (Orbit 1992)
---------------------------------------
Vector Time (GMT): 2012/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1434606
02 A = 6775345
00 meter
Y = -4765330
74 meter E =
0017231
Z = -4613533
25 I = 51
93543
XDOT = 5353
424373 Wp = 82
56087
YDOT = 4551
666037 meter/sec RA = 60
20467 deg
ZDOT = -3044
296923 TA = 157
15138
MA = 157
07462
Ha = 221
078 n
mi
Hp = 209
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4706712
65 X = 1510197
92
Y = -15634287
20 feet Y = -4748864
80 meter
Z = -15136263
94 Z = -4606381
00
XDOT = 17563
728258 XDOT = 5316
917415
YDOT = 14933
287524 feet/sec YDOT = 4611
327641 meter/sec
ZDOT = -9987
850798 ZDOT = -3018
378138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16111924
25 X = -4910914
51
Y = -2810296
21 feet Y = -856578
28 meter
Z = -15106247
01 Z = -4604384
09
XDOT = 12411
594347 XDOT = 3783
053957
YDOT = -18175
154358 feet/sec YDOT = -5539
787048 meter/sec
ZDOT = -9881
472378 ZDOT = -3011
872781
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 12181
52147589
00016717 00000-0 10270-3 0 9023
2 25544 51
6402 60
7412 0007638 100
0707 260
1309 15
55851261 19931
Satellite: ISS
Catalog Number: 25544
Epoch time: 12181
52147589 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 60
7412 deg
Eccentricity:
0007638
Arg of perigee: 100
0707 deg
Mean anomaly: 260
1309 deg
Mean motion: 15
55851261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1993
Checksum: 288
Coasting Arc #4 (Orbit 2008)
---------------------------------------
Vector Time (GMT): 2012/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3029665
98 A = 6772386
26 meter
Y = 2918628
40 meter E =
0010503
Z = 5298918
31 I = 51
90995
XDOT = -4743
125570 Wp = 106
15362
YDOT = -6010
062871 meter/sec RA = 55
20958 deg
ZDOT = 594
609752 TA = 338
17807
MA = 338
22277
Ha = 221
162 n
mi
Hp = 209
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9939849
01 X = -3087818
54
Y = 9575552
49 feet Y = 2884422
79 meter
Z = 17384902
58 Z = 5284059
49
XDOT = -15561
435597 XDOT = -4678
455784
YDOT = -19718
054040 feet/sec YDOT = -6062
741947 meter/sec
ZDOT = 1950
819397 ZDOT = 571
723887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10904757
57 X = 3323770
11
Y = 8585808
48 feet Y = 2616954
42 meter
Z = 17323302
13 Z = 5280142
49
XDOT = -16683
587858 XDOT = -5085
157579
YDOT = 17417
223119 feet/sec YDOT = 5308
769607 meter/sec
ZDOT = 1857
117231 ZDOT = 566
049332
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 12182
54916783
00016717 00000-0 10270-3 0 9037
2 25544 51
6405 55
6044 0007688 104
0212 256
1797 15
55867869 20094
Satellite: ISS
Catalog Number: 25544
Epoch time: 12182
54916783 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 55
6044 deg
Eccentricity:
0007688
Arg of perigee: 104
0212 deg
Mean anomaly: 256
1797 deg
Mean motion: 15
55867869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2009
Checksum: 325
Coasting Arc #5 (Orbit 2023)
---------------------------------------
Vector Time (GMT): 2012/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4465665
53 A = 6773567
02 meter
Y = -820564
66 meter E =
0020342
Z = -5045014
49 I = 51
89515
XDOT = 3436
170165 Wp = 105
44052
YDOT = 6548
992727 meter/sec RA = 50
20868 deg
ZDOT = 1977
751077 TA = 183
71808
MA = 183
73322
Ha = 220
949 n
mi
Hp = 209
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14651133
62 X = 4499016
87
Y = -2692141
26 feet Y = -770439
44 meter
Z = -16551884
82 Z = -5023239
64
XDOT = 11273
524165 XDOT = 3353
075142
YDOT = 21486
196611 feet/sec YDOT = 6586
953146 meter/sec
ZDOT = 6488
684637 ZDOT = 1994
243166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5002321
32 X = -1524707
54
Y = -14136752
19 feet Y = -4308882
07 meter
Z = -16461994
13 Z = -5017615
81
XDOT = 18398
496285 XDOT = 5607
861668
YDOT = -14139
407524 feet/sec YDOT = -4309
691413 meter/sec
ZDOT = 6555
951684 ZDOT = 1998
254073
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 12183
51261899
00016717 00000-0 10270-3 0 9047
2 25544 51
6400 50
7878 0007538 107
2750 252
9229 15
55887591 20241
Satellite: ISS
Catalog Number: 25544
Epoch time: 12183
51261899 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 50
7878 deg
Eccentricity:
0007538
Arg of perigee: 107
2750 deg
Mean anomaly: 252
9229 deg
Mean motion: 15
55887591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2024
Checksum: 322
Coasting Arc #6 (Orbit 2039)
---------------------------------------
Vector Time (GMT): 2012/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5449054
90 A = 6777978
95 meter
Y = -1237517
12 meter E =
0018421
Z = 3819618
79 I = 51
89023
XDOT = -1542
805128 Wp = 93
21745
YDOT = -6237
489905 meter/sec RA = 45
21849 deg
ZDOT = -4205
433925 TA = 40
95822
MA = 40
82000
Ha = 220
931 n
mi
Hp = 209
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17877476
69 X = -5453366
46
Y = -4060095
55 feet Y = -1298476
65 meter
Z = 12531557
72 Z = 3793136
99
XDOT = -5061
696615 XDOT = -1452
512660
YDOT = -20464
205726 feet/sec YDOT = -6254
236877 meter/sec
ZDOT = -13797
355396 ZDOT = -4212
710592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -839684
60 X = -255935
87
Y = 18387638
54 feet Y = 5604552
23 meter
Z = 12422486
31 Z = 3786373
83
XDOT = -17930
452154 XDOT = -5465
201817
YDOT = 8559
013950 feet/sec YDOT = 2608
787452 meter/sec
ZDOT = -13826
647625 ZDOT = -4214
362196
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 12184
54028928
00016717 00000-0 10270-3 0 9056
2 25544 51
6401 45
6508 0007417 110
1915 250
0037 15
55934913 20402
Satellite: ISS
Catalog Number: 25544
Epoch time: 12184
54028928 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 45
6508 deg
Eccentricity:
0007417
Arg of perigee: 110
1915 deg
Mean anomaly: 250
0037 deg
Mean motion: 15
55934913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2040
Checksum: 282
Coasting Arc #7 (Orbit 2054)
---------------------------------------
Vector Time (GMT): 2012/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5805414
96 A = 6782662
60 meter
Y = 2933945
09 meter E =
0011457
Z = -1925873
09 I = 51
88212
XDOT = -746
971053 Wp = 77
28584
YDOT = 5151
140893 meter/sec RA = 40
24377 deg
ZDOT = 5626
344435 TA = 261
56197
MA = 261
69186
Ha = 220
852 n
mi
Hp = 209
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19046637
02 X = 5781530
86
Y = 9625804
11 feet Y = 2998731
64 meter
Z = -6318481
27 Z = -1897728
48
XDOT = -2450
692431 XDOT = -831
847819
YDOT = 16900
068546 feet/sec YDOT = 5142
312225 meter/sec
ZDOT = 18459
135284 ZDOT = 5622
510483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5767044
47 X = 1757795
16
Y = -20582051
68 feet Y = -6273409
35 meter
Z = -6202744
44 Z = -1890596
51
XDOT = 15577
580986 XDOT = 4748
046685
YDOT = -1162
396983 feet/sec YDOT = -354
298601 meter/sec
ZDOT = 18442
726228 ZDOT = 5621
342954
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 12185
50372219
00016717 00000-0 10270-3 0 9069
2 25544 51
6388 40
8340 0007379 114
3685 245
8240 15
55898527 20558
Satellite: ISS
Catalog Number: 25544
Epoch time: 12185
50372219 = yrday
fracday
Element set: 906
Inclination: 51
6388 deg
RA of node: 40
8340 deg
Eccentricity:
0007379
Arg of perigee: 114
3685 deg
Mean anomaly: 245
8240 deg
Mean motion: 15
55898527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 321
Coasting Arc #8 (Orbit 2070)
---------------------------------------
Vector Time (GMT): 2012/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5342346
10 A = 6784111
05 meter
Y = -4151481
09 meter E =
0018439
Z = -386397
44 I = 51
86279
XDOT = 3174
843411 Wp = 129
94419
YDOT = -3543
943377 meter/sec RA = 35
28037 deg
ZDOT = -6020
213291 TA = 54
21297
MA = 54
04171
Ha = 220
799 n
mi
Hp = 209
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17527382
21 X = -5293649
33
Y = -13620344
79 feet Y = -4210950
17 meter
Z = -1267708
15 Z = -412232
28
XDOT = 10416
152924 XDOT = 3243
480896
YDOT = -11627
110818 feet/sec YDOT = -3508
055567 meter/sec
ZDOT = -19751
355941 ZDOT = -6004
624154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9646558
55 X = -2940271
05
Y = 19984660
14 feet Y = 6091324
41 meter
Z = -1373779
70 Z = -418728
05
XDOT = -12120
965882 XDOT = -3694
470401
YDOT = -7162
213605 feet/sec YDOT = -2183
042707 meter/sec
ZDOT = -19686
647935 ZDOT = -6000
490291
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 12186
53137336
00016717 00000-0 10270-3 0 9073
2 25544 51
6385 35
6965 0007450 118
9234 241
2668 15
55900058 20715
Satellite: ISS
Catalog Number: 25544
Epoch time: 12186
53137336 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 35
6965 deg
Eccentricity:
0007450
Arg of perigee: 118
9234 deg
Mean anomaly: 241
2668 deg
Mean motion: 15
55900058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2071
Checksum: 312
Coasting Arc #9 (Orbit 2086)
---------------------------------------
Vector Time (GMT): 2012/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4103243
03 A = 6781155
62 meter
Y = 4739305
75 meter E =
0019432
Z = 2570182
54 I = 51
82719
XDOT = -5301
125120 Wp = 92
12695
YDOT = 1707
923702 meter/sec RA = 30
31097 deg
ZDOT = 5278
719936 TA = 296
72465
MA = 296
92341
Ha = 220
608 n
mi
Hp = 209
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13462083
44 X = 4037457
05
Y = 15548903
39 feet Y = 4784822
57 meter
Z = 8432357
41 Z = 2589956
40
XDOT = -17392
142781 XDOT = -5345
471828
YDOT = 5603
424220 feet/sec YDOT = 1648
394549 meter/sec
ZDOT = 17318
634961 ZDOT = 5252
860308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12110400
99 X = 3691250
22
Y = -16581965
21 feet Y = -5054183
00 meter
Z = 8513363
39 Z = 2594873
16
XDOT = 8210
528548 XDOT = 2502
569102
YDOT = 14891
683584 feet/sec YDOT = 4538
985156 meter/sec
ZDOT = 17211
779142 ZDOT = 5246
150282
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 12187
55901179
00016717 00000-0 10270-3 0 9081
2 25544 51
6376 30
5577 0007306 123
0845 237
1011 15
55959524 20878
Satellite: ISS
Catalog Number: 25544
Epoch time: 12187
55901179 = yrday
fracday
Element set: 908
Inclination: 51
6376 deg
RA of node: 30
5577 deg
Eccentricity:
0007306
Arg of perigee: 123
0845 deg
Mean anomaly: 237
1011 deg
Mean motion: 15
55959524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2087
Checksum: 313
Coasting Arc #10 (Orbit 2101)
---------------------------------------
Vector Time (GMT): 2012/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2123846
86 A = 6776045
01 meter
Y = -4773683
10 meter E =
0014165
Z = -4326082
80 I = 51
78228
XDOT = 6803
286017 Wp = 94
69921
YDOT = 153
083233 meter/sec RA = 25
32463 deg
ZDOT = -3519
975151 TA = 139
56639
MA = 139
46103
Ha = 220
624 n
mi
Hp = 209
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6968001
51 X = -2049293
96
Y = -15661689
97 feet Y = -4797015
93 meter
Z = -14193185
04 Z = -4336219
62
XDOT = 22320
492182 XDOT = 6818
167502
YDOT = 502
241577 feet/sec YDOT = 229
245404 meter/sec
ZDOT = -11548
474904 ZDOT = -3486
889534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13520205
78 X = -4120958
72
Y = 10482025
18 feet Y = 3194921
28 meter
Z = -14234439
33 Z = -4338657
11
XDOT = -4191
758202 XDOT = -1277
647900
YDOT = -20855
021922 feet/sec YDOT = -6356
610682 meter/sec
ZDOT = -11412
033434 ZDOT = -3478
387791
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 12188
52241571
00016717 00000-0 10270-3 0 9093
2 25544 51
6366 25
7404 0007371 125
7070 234
4770 15
55952972 21023
Satellite: ISS
Catalog Number: 25544
Epoch time: 12188
52241571 = yrday
fracday
Element set: 909
Inclination: 51
6366 deg
RA of node: 25
7404 deg
Eccentricity:
0007371
Arg of perigee: 125
7070 deg
Mean anomaly: 234
4770 deg
Mean motion: 15
55952972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2102
Checksum: 300
Coasting Arc #11 (Orbit 2117)
---------------------------------------
Vector Time (GMT): 2012/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -242438
08 A = 6772496
61 meter
Y = 4299779
00 meter E =
0011150
Z = 5220203
78 I = 51
74238
XDOT = -7381
277440 Wp = 126
59029
YDOT = -1789
149726 meter/sec RA = 20
31916 deg
ZDOT = 1122
725316 TA = 312
62985
MA = 312
72380
Ha = 220
653 n
mi
Hp = 209
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -795400
54 X = -315859
23
Y = 14106886
49 feet Y = 4296656
90 meter
Z = 17126652
82 Z = 5218848
11
XDOT = -24216
789500 XDOT = -7366
176064
YDOT = -5869
913798 feet/sec YDOT = -1871
607416 meter/sec
ZDOT = 3683
482008 ZDOT = 1086
904498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13857588
19 X = 4223792
88
Y = -2795126
32 feet Y = -851954
50 meter
Z = 17120562
60 Z = 5218347
48
XDOT = 423
325823 XDOT = 129
029711
YDOT = 23921
005652 feet/sec YDOT = 7291
122523 meter/sec
ZDOT = 3535
953596 ZDOT = 1077
758656
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 12189
55003657
00016717 00000-0 10270-3 0 9100
2 25544 51
6369 20
6021 0007391 129
1877 230
9934 15
55927901 21184
Satellite: ISS
Catalog Number: 25544
Epoch time: 12189
55003657 = yrday
fracday
Element set: 910
Inclination: 51
6369 deg
RA of node: 20
6021 deg
Eccentricity:
0007391
Arg of perigee: 129
1877 deg
Mean anomaly: 230
9934 deg
Mean motion: 15
55927901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2118
Checksum: 308
Coasting Arc #12 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2012/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2718806
15 A = 6772760
67 meter
Y = -3475531
44 meter E =
0020354
Z = -5155992
00 I = 51
71415
XDOT = 6834
051888 Wp = 112
31826
YDOT = 3104
428115 meter/sec RA = 15
30406 deg
ZDOT = 1508
265302 TA = 172
23296
MA = 172
20139
Ha = 220
520 n
mi
Hp = 209
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8919967
69 X = 2782514
50
Y = -11402662
21 feet Y = -3444771
44 meter
Z = -16915984
27 Z = -5142629
87
XDOT = 22421
430078 XDOT = 6791
502899
YDOT = 10185
131611 feet/sec YDOT = 3180
612697 meter/sec
ZDOT = 4948
376976 ZDOT = 1541
361280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13452878
50 X = -4100437
37
Y = -5521009
84 feet Y = -1682803
80 meter
Z = -16860473
40 Z = -5139072
29
XDOT = 3199
865866 XDOT = 975
319116
YDOT = -23352
391033 feet/sec YDOT = -7117
808787 meter/sec
ZDOT = 5084
508740 ZDOT = 1549
758264
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 12190
51341911
00016717 00000-0 10270-3 0 9117
2 25544 51
6364 15
7842 0007439 133
2334 226
9442 15
55985063 21331
Satellite: ISS
Catalog Number: 25544
Epoch time: 12190
51341911 = yrday
fracday
Element set: 911
Inclination: 51
6364 deg
RA of node: 15
7842 deg
Eccentricity:
0007439
Arg of perigee: 133
2334 deg
Mean anomaly: 226
9442 deg
Mean motion: 15
55985063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 292
Coasting Arc #13 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2012/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4844987
13 A = 6776940
23 meter
Y = 2391128
99 meter E =
0015725
Z = 4075419
86 I = 51
69886
XDOT = -5256
811425 Wp = 101
03083
YDOT = -4054
382372 meter/sec RA = 10
29754 deg
ZDOT = -3861
013112 TA = 28
85188
MA = 28
76502
Ha = 220
507 n
mi
Hp = 209
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15895627
07 X = -4891162
41
Y = 7844911
38 feet Y = 2336690
85 meter
Z = 13370800
05 Z = 4051771
38
XDOT = -17246
756645 XDOT = -5192
328049
YDOT = -13301
779436 feet/sec YDOT = -4112
806458 meter/sec
ZDOT = -12667
365852 ZDOT = -3886
393895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12179803
58 X = 3712404
13
Y = 12979669
79 feet Y = 3956203
35 meter
Z = 13272996
86 Z = 4045609
44
XDOT = -6746
265888 XDOT = -2056
261843
YDOT = 19423
377207 feet/sec YDOT = 5920
245373 meter/sec
ZDOT = -12771
562880 ZDOT = -3892
772366
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 12191
54101767
00016717 00000-0 10270-3 0 9125
2 25544 51
6367 10
6465 0007314 137
6484 222
5235 15
55993100 21495
Satellite: ISS
Catalog Number: 25544
Epoch time: 12191
54101767 = yrday
fracday
Element set: 912
Inclination: 51
6367 deg
RA of node: 10
6465 deg
Eccentricity:
0007314
Arg of perigee: 137
6484 deg
Mean anomaly: 222
5235 deg
Mean motion: 15
55993100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 294
Coasting Arc #14 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2012/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6289888
49 A = 6781774
11 meter
Y = -1197466
14 meter E =
0008990
Z = -2245102
68 I = 51
68511
XDOT = 2813
960796 Wp = 97
77101
YDOT = 4589
083469 meter/sec RA = 5
30629 deg
ZDOT = 5453
457326 TA = 237
28569
MA = 237
37239
Ha = 220
386 n
mi
Hp = 209
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20636117
08 X = 6313717
44
Y = -3928694
69 feet Y = -1126995
29 meter
Z = -7365822
45 Z = -2214489
12
XDOT = 9232
154841 XDOT = 2735
944104
YDOT = 15056
048128 feet/sec YDOT = 4620
114267 meter/sec
ZDOT = 17891
920362 ZDOT = 5466
938200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10130933
98 X = -3087908
68
Y = -18452479
42 feet Y = -5624315
73 meter
Z = -7239439
91 Z = -2206581
29
XDOT = 10153
151894 XDOT = 3094
680697
YDOT = -12592
533839 feet/sec YDOT = -3838
204314 meter/sec
ZDOT = 17946
976335 ZDOT = 5470
238387
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 12192
50438257
00016717 00000-0 10270-3 0 9130
2 25544 51
6367 5
8291 0007474 140
6691 219
5007 15
56015633 21646
Satellite: ISS
Catalog Number: 25544
Epoch time: 12192
50438257 = yrday
fracday
Element set: 913
Inclination: 51
6367 deg
RA of node: 5
8291 deg
Eccentricity:
0007474
Arg of perigee: 140
6691 deg
Mean anomaly: 219
5007 deg
Mean motion: 15
56015633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 300
Coasting Arc #15 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2012/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6773233
09 A = 6783684
10 meter
Y = -91307
57 meter E =
0019072
Z = -66429
80 I = 51
66173
XDOT = 113
297200 Wp = 137
95361
YDOT = -4760
687270 meter/sec RA =
32797 deg
ZDOT = -6020
525146 TA = 42
76274
MA = 42
61451
Ha = 220
119 n
mi
Hp = 209
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22221893
35 X = -6771385
97
Y = -299565
52 feet Y = -167039
73 meter
Z = -217945
52 Z = -99329
22
XDOT = 371
709973 XDOT = 195
769967
YDOT = -15619
052722 feet/sec YDOT = -4758
958624 meter/sec
ZDOT = -19752
379088 ZDOT = -6019
774872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6949481
40 X = 2118201
93
Y = 21107568
79 feet Y = 6433586
97 meter
Z = -353598
39 Z = -107776
79
XDOT = -13390
718229 XDOT = -4081
490916
YDOT = 4112
231153 feet/sec YDOT = 1253
408055 meter/sec
ZDOT = -19748
727335 ZDOT = -6019
412092
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 12193
53195947
00016717 00000-0 10270-3 0 9141
2 25544 51
6368
6911 0007201 143
4781 216
6865 15
56072373 21800
Satellite: ISS
Catalog Number: 25544
Epoch time: 12193
53195947 = yrday
fracday
Element set: 914
Inclination: 51
6368 deg
RA of node:
6911 deg
Eccentricity:
0007201
Arg of perigee: 143
4781 deg
Mean anomaly: 216
6865 deg
Mean motion: 15
56072373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2180
Checksum: 305
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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