[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 21st 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 1854)
---------------------------------------
Vector Time (GMT): 2012/172/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3726927
45 A = 6780758
70 meter
Y = 4722789
31 meter E =
0020969
Z = 3105226
43 I = 51
98427
XDOT = -2599
087295 Wp = 78
41426
YDOT = -5297
557014 meter/sec RA = 104
48212 deg
ZDOT = 4913
865891 TA = 317
18864
MA = 317
35175
Ha = 221
526 n
mi
Hp = 209
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12227452
26 X = -3794546
07
Y = 15494715
60 feet Y = 4680733
91 meter
Z = 10187750
74 Z = 3086957
81
XDOT = -8527
189289 XDOT = -2563
526093
YDOT = -17380
436398 feet/sec YDOT = -5326
423607 meter/sec
ZDOT = 16121
607255 ZDOT = 4901
325190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19721733
28 X = 6011184
30
Y = 1479271
12 feet Y = 450881
84 meter
Z = 10111976
01 Z = 3082130
29
XDOT = -9439
251839 XDOT = -2877
083961
YDOT = 15452
471385 feet/sec YDOT = 4709
913278 meter/sec
ZDOT = 16070
430701 ZDOT = 4898
267278
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 12172
65717222
00016717 00000-0 10270-3 0 9002
2 25544 51
6403 105
0406 0008143 68
5796 291
6226 15
55689366 18555
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
65717222 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 105
0406 deg
Eccentricity:
0008143
Arg of perigee: 68
5796 deg
Mean anomaly: 291
6226 deg
Mean motion: 15
55689366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1855
Checksum: 311
Coasting Arc #2 (Orbit 1869)
---------------------------------------
Vector Time (GMT): 2012/173/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4132666
61 A = 6775690
30 meter
Y = -2745075
99 meter E =
0018208
Z = -4632497
44 I = 51
97500
XDOT = 1229
113904 Wp = 70
71129
YDOT = 6929
960723 meter/sec RA = 99
50611 deg
ZDOT = -3013
775176 TA = 169
32773
MA = 169
28904
Ha = 221
363 n
mi
Hp = 209
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13558617
47 X = 4185558
91
Y = -9006154
81 feet Y = -2698565
49 meter
Z = -15198482
43 Z = -4612293
24
XDOT = 4032
525931 XDOT = 1166
170441
YDOT = 22736
091610 feet/sec YDOT = 6943
353969 meter/sec
ZDOT = -9887
713831 ZDOT = -3007
956048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15220080
16 X = -4639080
43
Y = -5985763
87 feet Y = -1824460
83 meter
Z = -15114912
87 Z = -4607025
44
XDOT = 15807
158428 XDOT = 4818
021889
YDOT = -15315
581462 feet/sec YDOT = -4668
189229 meter/sec
ZDOT = -9864
411794 ZDOT = -3006
672715
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 12173
62072157
00016717 00000-0 10270-3 0 9012
2 25544 51
6409 100
2254 0008013 71
5507 288
6517 15
55731112 18702
Satellite: ISS
Catalog Number: 25544
Epoch time: 12173
62072157 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 100
2254 deg
Eccentricity:
0008013
Arg of perigee: 71
5507 deg
Mean anomaly: 288
6517 deg
Mean motion: 15
55731112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1870
Checksum: 278
Coasting Arc #3 (Orbit 1885)
---------------------------------------
Vector Time (GMT): 2012/174/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4187703
44 A = 6772739
05 meter
Y = 346172
36 meter E =
0010379
Z = 5302655
31 I = 51
96939
XDOT = 131
276534 Wp = 85
59431
YDOT = -7654
731323 meter/sec RA = 94
51537 deg
ZDOT = 603
162755 TA = 358
68175
MA = 358
68448
Ha = 221
486 n
mi
Hp = 209
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13739184
51 X = -4217022
03
Y = 1135736
08 feet Y = 299178
20 meter
Z = 17397163
10 Z = 5282240
66
XDOT = 430
697290 XDOT = 213
933548
YDOT = -25113
947910 feet/sec YDOT = -7652
801230 meter/sec
ZDOT = 1978
880429 ZDOT = 604
000191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9075941
91 X = 2766347
09
Y = 10516897
65 feet Y = 3205550
40 meter
Z = 17312957
97 Z = 5276989
59
XDOT = -19771
569065 XDOT = -6026
374251
YDOT = 13796
742722 feet/sec YDOT = 4205
247182 meter/sec
ZDOT = 1983
100784 ZDOT = 604
449119
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 12174
64849751
00016717 00000-0 10270-3 0 9028
2 25544 51
6408 95
0891 0007966 75
6216 284
5821 15
55751037 18865
Satellite: ISS
Catalog Number: 25544
Epoch time: 12174
64849751 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 95
0891 deg
Eccentricity:
0007966
Arg of perigee: 75
6216 deg
Mean anomaly: 284
5821 deg
Mean motion: 15
55751037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1886
Checksum: 337
Coasting Arc #4 (Orbit 1900)
---------------------------------------
Vector Time (GMT): 2012/175/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3981559
72 A = 6773820
65 meter
Y = 2126842
91 meter E =
0020380
Z = -5068528
43 I = 51
97427
XDOT = -1442
406540 Wp = 94
53870
YDOT = 7268
897143 meter/sec RA = 89
52088 deg
ZDOT = 1922
151226 TA = 194
01872
MA = 194
07537
Ha = 221
308 n
mi
Hp = 209
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13062859
97 X = 3982102
53
Y = 6977831
07 feet Y = 2171370
82 meter
Z = -16629030
29 Z = -5049184
81
XDOT = -4732
304920 XDOT = -1532
918916
YDOT = 23848
087741 feet/sec YDOT = 7252
260947 meter/sec
ZDOT = 6306
270427 ZDOT = 1914
925169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2372305
17 X = -723078
62
Y = -14708492
45 feet Y = -4483148
50 meter
Z = -16549486
50 Z = -5044283
49
XDOT = 20829
070641 XDOT = 6348
700731
YDOT = -10401
917418 feet/sec YDOT = -3170
504429 meter/sec
ZDOT = 6275
740507 ZDOT = 1912
845706
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 12175
61202771
00016717 00000-0 10270-3 0 9032
2 25544 51
6407 90
2734 0007891 78
4457 281
7582 15
55760809 19010
Satellite: ISS
Catalog Number: 25544
Epoch time: 12175
61202771 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 90
2734 deg
Eccentricity:
0007891
Arg of perigee: 78
4457 deg
Mean anomaly: 281
7582 deg
Mean motion: 15
55760809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1901
Checksum: 316
Coasting Arc #5 (Orbit 1916)
---------------------------------------
Vector Time (GMT): 2012/176/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3467145
75 A = 6778101
75 meter
Y = -4322943
93 meter E =
0019162
Z = 3889084
80 I = 51
98770
XDOT = 2682
338939 Wp = 81
26786
YDOT = -5887
909936 meter/sec RA = 84
53688 deg
ZDOT = -4133
295115 TA = 51
92009
MA = 51
74740
Ha = 221
323 n
mi
Hp = 209
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11375150
11 X = -3437440
16
Y = -14182886
91 feet Y = -4361550
01 meter
Z = 12759464
56 Z = 3872313
41
XDOT = 8800
324602 XDOT = 2768
057838
YDOT = -19317
289817 feet/sec YDOT = -5857
434655 meter/sec
ZDOT = -13560
679510 ZDOT = -4120
056938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4102650
22 X = -1250487
79
Y = 17761344
97 feet Y = 5413657
95 meter
Z = 12690750
30 Z = 3868140
69
XDOT = -19390
532999 XDOT = -5910
234458
YDOT = 5218
364455 feet/sec YDOT = 1590
557486 meter/sec
ZDOT = -13505
492409 ZDOT = -4116
474086
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 12176
63978171
00016717 00000-0 10270-3 0 9040
2 25544 51
6406 85
1368 0007889 81
3272 278
8775 15
55802151 19175
Satellite: ISS
Catalog Number: 25544
Epoch time: 12176
63978171 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 85
1368 deg
Eccentricity:
0007889
Arg of perigee: 81
3272 deg
Mean anomaly: 278
8775 deg
Mean motion: 15
55802151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1917
Checksum: 339
Coasting Arc #6 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2012/177/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2715195
34 A = 6782759
58 meter
Y = 5864166
64 meter E =
0013331
Z = -2058881
22 I = 51
99858
XDOT = -3753
186308 Wp = 64
56742
YDOT = 3684
367433 meter/sec RA = 79
56944 deg
ZDOT = 5577
952760 TA = 272
77402
MA = 272
92660
Ha = 221
273 n
mi
Hp = 209
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8908121
20 X = 2659420
75
Y = 19239391
87 feet Y = 5894217
97 meter
Z = -6754859
65 Z = -2045825
94
XDOT = -12313
603372 XDOT = -3821
202996
YDOT = 12087
819661 feet/sec YDOT = 3642
016168 meter/sec
ZDOT = 18300
369949 ZDOT = 5559
555174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9300822
73 X = 2834890
77
Y = -19071439
12 feet Y = -5812974
64 meter
Z = -6701631
02 Z = -2042657
14
XDOT = 15825
528312 XDOT = 4823
621029
YDOT = 1353
031353 feet/sec YDOT = 412
403957 meter/sec
ZDOT = 18224
127874 ZDOT = 5554
714176
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 12177
60329191
00016717 00000-0 10270-3 0 9051
2 25544 51
6400 80
3208 0007777 84
9836 275
2205 15
55777740 19321
Satellite: ISS
Catalog Number: 25544
Epoch time: 12177
60329191 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 80
3208 deg
Eccentricity:
0007777
Arg of perigee: 84
9836 deg
Mean anomaly: 275
2205 deg
Mean motion: 15
55777740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1932
Checksum: 316
Coasting Arc #7 (Orbit 1947)
---------------------------------------
Vector Time (GMT): 2012/178/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1640975
83 A = 6784560
07 meter
Y = -6574357
43 meter E =
0017971
Z = -207424
93 I = 51
99780
XDOT = 4626
268587 Wp = 118
03846
YDOT = -976
935907 meter/sec RA = 74
61465 deg
ZDOT = -6040
422577 TA = 64
18686
MA = 64
00158
Ha = 221
279 n
mi
Hp = 209
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5383778
97 X = -1566330
44
Y = -21569414
13 feet Y = -6592290
45 meter
Z = -680527
98 Z = -215215
97
XDOT = 15178
046546 XDOT = 4666
192007
YDOT = -3205
170297 feet/sec YDOT = -924
978348 meter/sec
ZDOT = -19817
659374 ZDOT = -6017
851521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13052083
85 X = -3978275
16
Y = 17995111
27 feet Y = 5484909
91 meter
Z = -711967
62 Z = -217007
73
XDOT = -10984
925426 XDOT = -3348
205270
YDOT = -8697
611864 feet/sec YDOT = -2651
032096 meter/sec
ZDOT = -19724
485264 ZDOT = -6012
023109
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 12178
63102593
00016717 00000-0 10270-3 0 9061
2 25544 51
6398 75
1838 0007774 90
3437 269
8607 15
55763441 19488
Satellite: ISS
Catalog Number: 25544
Epoch time: 12178
63102593 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 75
1838 deg
Eccentricity:
0007774
Arg of perigee: 90
3437 deg
Mean anomaly: 269
8607 deg
Mean motion: 15
55763441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1948
Checksum: 343
Coasting Arc #8 (Orbit 1963)
---------------------------------------
Vector Time (GMT): 2012/179/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 366037
15 A = 6781992
60 meter
Y = 6332281
57 meter E =
0021156
Z = 2376661
68 I = 51
98022
XDOT = -5158
256398 Wp = 80
24983
YDOT = -1746
191049 meter/sec RA = 69
65672 deg
ZDOT = 5409
619232 TA = 306
19838
MA = 306
39383
Ha = 221
129 n
mi
Hp = 209
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1200909
28 X = 283655
77
Y = 20775201
99 feet Y = 6335913
97 meter
Z = 7797446
44 Z = 2378240
38
XDOT = -16923
413378 XDOT = -5164
625519
YDOT = -5728
973257 feet/sec YDOT = -1803
910001 meter/sec
ZDOT = 17748
094593 ZDOT = 5384
544960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14915992
10 X = 4546394
39
Y = -14507698
24 feet Y = -4421946
42 meter
Z = 7803284
15 Z = 2378441
01
XDOT = 5800
827315 XDOT = 1768
092166
YDOT = 15520
545777 feet/sec YDOT = 4730
662353 meter/sec
ZDOT = 17644
885635 ZDOT = 5378
161142
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
65874659
00016717 00000-0 10270-3 0 9074
2 25544 51
6393 70
0461 0007624 92
9594 267
2432 15
55828943 19640
Satellite: ISS
Catalog Number: 25544
Epoch time: 12179
65874659 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 70
0461 deg
Eccentricity:
0007624
Arg of perigee: 92
9594 deg
Mean anomaly: 267
2432 deg
Mean motion: 15
55828943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1964
Checksum: 348
Coasting Arc #9 (Orbit 1978)
---------------------------------------
Vector Time (GMT): 2012/180/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1143073
66 A = 6777043
11 meter
Y = -5225533
00 meter E =
0014976
Z = -4175220
95 I = 51
95132
XDOT = 5223
350073 Wp = 83
15253
YDOT = 4145
465378 meter/sec RA = 64
68443 deg
ZDOT = -3768
093693 TA = 148
23143
MA = 148
14100
Ha = 221
126 n
mi
Hp = 209
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3750241
66 X = 1221704
06
Y = -17144137
14 feet Y = -5212310
32 meter
Z = -13698231
46 Z = -4169477
53
XDOT = 17136
975305 XDOT = 5194
911050
YDOT = 13600
608195 feet/sec YDOT = 4203
717536 meter/sec
ZDOT = -12362
512115 ZDOT = -3742
787372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15304522
72 X = -4664818
53
Y = 8626763
95 feet Y = 2629437
65 meter
Z = -13673983
47 Z = -4167830
16
XDOT = -786
479931 XDOT = -239
719083
YDOT = -20774
771455 feet/sec YDOT = -6332
150340 meter/sec
ZDOT = -12258
608393 ZDOT = -3736
423838
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
62222694
00016717 00000-0 10270-3 0 9080
2 25544 51
6384 65
2298 0007623 96
5542 263
6480 15
55823101 19796
Satellite: ISS
Catalog Number: 25544
Epoch time: 12180
62222694 = yrday
fracday
Element set: 908
Inclination: 51
6384 deg
RA of node: 65
2298 deg
Eccentricity:
0007623
Arg of perigee: 96
5542 deg
Mean anomaly: 263
6480 deg
Mean motion: 15
55823101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1979
Checksum: 320
Coasting Arc #10 (Orbit 1994)
---------------------------------------
Vector Time (GMT): 2012/181/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2662954
78 A = 6773129
21 meter
Y = 3464413
95 meter E =
0011988
Z = 5166199
53 I = 51
92454
XDOT = -4751
772701 Wp = 108
97437
YDOT = -5851
068477 meter/sec RA = 59
69411 deg
ZDOT = 1467
775070 TA = 326
93583
MA = 327
01072
Ha = 221
255 n
mi
Hp = 209
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8736728
29 X = -2726593
01
Y = 11366187
51 feet Y = 3434278
60 meter
Z = 16949473
51 Z = 5153108
85
XDOT = -15589
805448 XDOT = -4693
121847
YDOT = -19196
418888 feet/sec YDOT = -5903
878013 meter/sec
ZDOT = 4815
535005 ZDOT = 1444
832693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14342387
47 X = 4371559
70
Y = -1287026
41 feet Y = -392285
65 meter
Z = 16895111
03 Z = 5149629
84
XDOT = -3481
433643 XDOT = -1061
140974
YDOT = 23468
722765 feet/sec YDOT = 7153
266699 meter/sec
ZDOT = 4721
573999 ZDOT = 1439
135755
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
64992959
00016717 00000-0 10270-3 0 9092
2 25544 51
6388 60
0925 0007702 100
0463 260
1560 15
55812957 19957
Satellite: ISS
Catalog Number: 25544
Epoch time: 12181
64992959 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 60
0925 deg
Eccentricity:
0007702
Arg of perigee: 100
0463 deg
Mean anomaly: 260
1560 deg
Mean motion: 15
55812957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1995
Checksum: 323
Coasting Arc #11 (Orbit 2009)
---------------------------------------
Vector Time (GMT): 2012/182/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4087671
82 A = 6772742
77 meter
Y = -1347145
54 meter E =
0021845
Z = -5248504
69 I = 51
90636
XDOT = 3629
606853 Wp = 100
37470
YDOT = 6645
749471 meter/sec RA = 54
69328 deg
ZDOT = 1121
185086 TA = 180
35021
MA = 180
35174
Ha = 221
042 n
mi
Hp = 209
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13410996
79 X = 4127928
20
Y = -4419768
82 feet Y = -1301208
71 meter
Z = -17219503
58 Z = -5228549
33
XDOT = 11908
158965 XDOT = 3549
576478
YDOT = 21803
639997 feet/sec YDOT = 6685
890326 meter/sec
ZDOT = 3678
428760 ZDOT = 1138
624308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12567191
86 X = -3830480
08
Y = -6654870
16 feet Y = -2028404
43 meter
Z = -17137061
78 Z = -5223376
43
XDOT = 6949
195734 XDOT = 2118
114860
YDOT = -22777
527674 feet/sec YDOT = -6942
590435 meter/sec
ZDOT = 3749
598258 ZDOT = 1142
877549
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
61338895
00016717 00000-0 10270-3 0 9105
2 25544 51
6378 55
2754 0007660 104
1130 256
0875 15
55865786 20101
Satellite: ISS
Catalog Number: 25544
Epoch time: 12182
61338895 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 55
2754 deg
Eccentricity:
0007660
Arg of perigee: 104
1130 deg
Mean anomaly: 256
0875 deg
Mean motion: 15
55865786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2010
Checksum: 310
Coasting Arc #12 (Orbit 2025)
---------------------------------------
Vector Time (GMT): 2012/183/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5139068
47 A = 6776369
18 meter
Y = -813463
02 meter E =
0016482
Z = 4327635
75 I = 51
90070
XDOT = -1935
929252 Wp = 87
46844
YDOT = -6546
461251 meter/sec RA = 49
69927 deg
ZDOT = -3517
231152 TA = 38
18131
MA = 38
06468
Ha = 221
069 n
mi
Hp = 209
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16860460
86 X = -5150612
86
Y = -2668841
93 feet Y = -870996
59 meter
Z = 14198280
01 Z = 4302642
22
XDOT = -6351
473923 XDOT = -1845
495606
YDOT = -21477
891245 feet/sec YDOT = -6567
603735 meter/sec
ZDOT = -11539
472283 ZDOT = -3526
417318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10089438
56 X = 3075260
87
Y = 13874967
54 feet Y = 4229090
11 meter
Z = 14095301
29 Z = 4296247
83
XDOT = -9744
881599 XDOT = -2970
239911
YDOT = 18887
640833 feet/sec YDOT = 5756
952926 meter/sec
ZDOT = -11576
609855 ZDOT = -3528
550684
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
64106927
00016717 00000-0 10270-3 0 9119
2 25544 51
6383 50
1386 0007493 108
0846 252
1124 15
55882954 20260
Satellite: ISS
Catalog Number: 25544
Epoch time: 12183
64106927 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 50
1386 deg
Eccentricity:
0007493
Arg of perigee: 108
0846 deg
Mean anomaly: 252
1124 deg
Mean motion: 15
55882954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2026
Checksum: 303
Coasting Arc #13 (Orbit 2040)
---------------------------------------
Vector Time (GMT): 2012/184/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5647389
68 A = 6781302
66 meter
Y = 2672702
10 meter E =
0011139
Z = -2645440
45 I = 51
89585
XDOT = -198
422281 Wp = 88
68693
YDOT = 5587
137022 meter/sec RA = 44
71955 deg
ZDOT = 5240
398125 TA = 241
61053
MA = 241
72287
Ha = 220
978 n
mi
Hp = 209
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18528181
37 X = 5629934
11
Y = 8768707
69 feet Y = 2735757
60 meter
Z = -8679266
56 Z = -2618047
78
XDOT = -650
991737 XDOT = -286
340532
YDOT = 18330
502042 feet/sec YDOT = 5584
425595 meter/sec
ZDOT = 17192
907234 ZDOT = 5239
221688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7260179
83 X = -2212902
81
Y = -19220210
77 feet Y = -5858320
24 meter
Z = -8566603
44 Z = -2611100
73
XDOT = 11886
204865 XDOT = 3622
915243
YDOT = -12121
876712 feet/sec YDOT = -3694
748022 meter/sec
ZDOT = 17187
412153 ZDOT = 5238
723224
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
60451130
00016717 00000-0 10270-3 0 9126
2 25544 51
6373 45
3216 0007663 112
0214 248
1754 15
55893340 20412
Satellite: ISS
Catalog Number: 25544
Epoch time: 12184
60451130 = yrday
fracday
Element set: 912
Inclination: 51
6373 deg
RA of node: 45
3216 deg
Eccentricity:
0007663
Arg of perigee: 112
0214 deg
Mean anomaly: 248
1754 deg
Mean motion: 15
55893340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2041
Checksum: 272
Coasting Arc #14 (Orbit 2056)
---------------------------------------
Vector Time (GMT): 2012/185/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5401032
42 A = 6783976
62 meter
Y = -4069853
75 meter E =
0020073
Z = 414390
15 I = 51
88315
XDOT = 2552
204640 Wp = 124
27464
YDOT = -4019
845013 meter/sec RA = 39
75478 deg
ZDOT = -6019
248949 TA = 51
26680
MA = 51
08753
Ha = 220
785 n
mi
Hp = 209
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17719922
64 X = -5357134
05
Y = -13352538
55 feet Y = -4130006
06 meter
Z = 1359547
75 Z = 388258
42
XDOT = 8373
374803 XDOT = 2626
205458
YDOT = -13188
467892 feet/sec YDOT = -3990
889854 meter/sec
ZDOT = -19748
192089 ZDOT = -6006
671577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3836606
58 X = 1169397
69
Y = 21859703
78 feet Y = 6662837
71 meter
Z = 1252243
99 Z = 381683
97
XDOT = -13617
236653 XDOT = -4150
533732
YDOT = 3558
298711 feet/sec YDOT = 1084
569447 meter/sec
ZDOT = -19695
853212 ZDOT = -6003
296059
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
63217034
00016717 00000-0 10270-3 0 9134
2 25544 51
6374 40
1840 0007482 114
0811 246
1126 15
55951874 20578
Satellite: ISS
Catalog Number: 25544
Epoch time: 12185
63217034 = yrday
fracday
Element set: 913
Inclination: 51
6374 deg
RA of node: 40
1840 deg
Eccentricity:
0007482
Arg of perigee: 114
0811 deg
Mean anomaly: 246
1126 deg
Mean motion: 15
55951874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2057
Checksum: 286
Coasting Arc #15 (Orbit 2072)
---------------------------------------
Vector Time (GMT): 2012/186/14:22:55
734
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4400641
62 A = 6782650
49 meter
Y = 4814868
67 meter E =
0019598
Z = 1837681
19 I = 51
85364
XDOT = -4719
632352 Wp = 84
39259
YDOT = 2134
219191 meter/sec RA = 34
79001 deg
ZDOT = 5660
254687 TA = 295
77758
MA = 295
97968
Ha = 220
854 n
mi
Hp = 209
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14437800
59 X = 4337546
82
Y = 15796813
22 feet Y = 4863726
30 meter
Z = 6029137
75 Z = 1858906
46
XDOT = -15484
358111 XDOT = -4770
642623
YDOT = 7002
031465 feet/sec YDOT = 2081
155222 meter/sec
ZDOT = 18570
389393 ZDOT = 5637
203750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -104156
99 X = -31747
05
Y = -21375736
64 feet Y = -6515324
53 meter
Z = 6116120
54 Z = 1864193
54
XDOT = 14711
793904 XDOT = 4484
154782
YDOT = 5260
650072 feet/sec YDOT = 1603
446142 meter/sec
ZDOT = 18475
069313 ZDOT = 5631
201127
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
65982149
00016717 00000-0 10270-3 0 9144
2 25544 51
6366 35
0457 0007696 119
6596 240
5324 15
55921722 20739
Satellite: ISS
Catalog Number: 25544
Epoch time: 12186
65982149 = yrday
fracday
Element set: 914
Inclination: 51
6366 deg
RA of node: 35
0457 deg
Eccentricity:
0007696
Arg of perigee: 119
6596 deg
Mean anomaly: 240
5324 deg
Mean motion: 15
55921722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2073
Checksum: 327
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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