[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 27th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7104 18 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 1930)
---------------------------------------
Vector Time (GMT): 2012/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3478080
19 A = 6779935
41 meter
Y = -4759209
70 meter E =
0020557
Z = 3332080
19 I = 51
98871
XDOT = 2802
840493 Wp = 89
78543
YDOT = -5369
092894 meter/sec RA = 80
06014 deg
ZDOT = -4717
933693 TA = 51
56394
MA = 51
37960
Ha = 221
411 n
mi
Hp = 209
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11411024
25 X = -3440789
63
Y = -15614205
06 feet Y = -4797895
55 meter
Z = 10932021
61 Z = 3315274
07
XDOT = 9195
670910 XDOT = 2885
588996
YDOT = -17615
134168 feet/sec YDOT = -5337
286689 meter/sec
ZDOT = -15478
785081 ZDOT = -4704
117198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14942797
36 X = -4554564
64
Y = 12338046
89 feet Y = 3760636
69 meter
Z = 10863212
07 Z = 3311107
04
XDOT = -17211
345161 XDOT = -5246
018005
YDOT = -7194
116276 feet/sec YDOT = -2192
766641 meter/sec
ZDOT = -15421
260085 ZDOT = -4700
400074
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
53906674
00016717 00000-0 10270-3 0 9005
2 25544 51
6392 80
6456 0007952 87
1425 273
0638 15
55758287 19313
Satellite: ISS
Catalog Number: 25544
Epoch time: 12177
53906674 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 80
6456 deg
Eccentricity:
0007952
Arg of perigee: 87
1425 deg
Mean anomaly: 273
0638 deg
Mean motion: 15
55758287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1931
Checksum: 332
Coasting Arc #2 (Orbit 1945)
---------------------------------------
Vector Time (GMT): 2012/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925141
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2699022
92 A = 6783744
49 meter
Y = 6075465
63 meter E =
0014939
Z = -1338392
49 I = 51
99632
XDOT = -3927
583523 Wp = 62
16579
YDOT = 3021
508828 meter/sec RA = 75
09769 deg
ZDOT = 5851
795566 TA = 283
32893
MA = 283
49547
Ha = 221
268 n
mi
Hp = 209
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8855062
09 X = 2637386
82
Y = 19932630
03 feet Y = 6105303
27 meter
Z = -4391051
47 Z = -1325429
96
XDOT = -12885
772712 XDOT = -3989
505386
YDOT = 9913
086705 feet/sec YDOT = 2977
241416 meter/sec
ZDOT = 19198
804349 ZDOT = 5832
565438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19226190
49 X = 5860142
86
Y = -10321653
03 feet Y = -3146039
84 meter
Z = -4338234
15 Z = -1322293
77
XDOT = 10089
873428 XDOT = 3075
393421
YDOT = 10837
378065 feet/sec YDOT = 3303
232834 meter/sec
ZDOT = 19119
193484 ZDOT = 5827
530174
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
50257344
00016717 00000-0 10270-3 0 9017
2 25544 51
6399 75
8297 0007826 90
2812 269
9239 15
55793380 19464
Satellite: ISS
Catalog Number: 25544
Epoch time: 12178
50257344 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 75
8297 deg
Eccentricity:
0007826
Arg of perigee: 90
2812 deg
Mean anomaly: 269
9239 deg
Mean motion: 15
55793380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1946
Checksum: 345
Coasting Arc #3 (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 = -1557233
38 A = 6784167
77 meter
Y = -6528409
44 meter E =
0016179
Z = -963196
77 I = 51
98907
XDOT = 4836
383294 Wp = 120
77536
YDOT = -288
531150 meter/sec RA = 70
14348 deg
ZDOT = -5945
353074 TA = 69
61190
MA = 69
43819
Ha = 221
261 n
mi
Hp = 209
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5109033
41 X = -1479436
63
Y = -21418666
13 feet Y = -6545388
31 meter
Z = -3160094
39 Z = -970573
40
XDOT = 15867
399260 XDOT = 4868
131488
YDOT = -946
624507 feet/sec YDOT = -234
269636 meter/sec
ZDOT = -19505
751555 ZDOT = -5921
781009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20869730
50 X = -6361093
86
Y = 7009070
74 feet Y = 2136364
76 meter
Z = -3189820
33 Z = -972257
24
XDOT = -1881
056994 XDOT = -573
346172
YDOT = -14312
663427 feet/sec YDOT = -4362
499813 meter/sec
ZDOT = -19408
521073 ZDOT = -5915
717223
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
53030638
00016717 00000-0 10270-3 0 9027
2 25544 51
6403 70
6925 0007754 94
8916 265
3123 15
55766061 19622
Satellite: ISS
Catalog Number: 25544
Epoch time: 12179
53030638 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 70
6925 deg
Eccentricity:
0007754
Arg of perigee: 94
8916 deg
Mean anomaly: 265
3123 deg
Mean motion: 15
55766061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1962
Checksum: 313
Coasting Arc #4 (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 = 187875
51 A = 6780583
94 meter
Y = 6053533
92 meter E =
0020770
Z = 3030230
84 I = 51
96627
XDOT = -5363
786935 Wp = 88
24452
YDOT = -2335
892082 meter/sec RA = 65
18220 deg
ZDOT = 4970
343642 TA = 306
37223
MA = 306
56369
Ha = 221
236 n
mi
Hp = 209
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 616389
47 X = 105449
45
Y = 19860675
59 feet Y = 6055173
65 meter
Z = 9941702
24 Z = 3030944
01
XDOT = -17597
726166 XDOT = -5361
412776
YDOT = -7663
687934 feet/sec YDOT = -2395
860557 meter/sec
ZDOT = 16306
901711 ZDOT = 4944
291988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19685924
64 X = 6000269
83
Y = -2691699
92 feet Y = -820430
13 meter
Z = 9943989
98 Z = 3030928
14
XDOT = -5908
257494 XDOT = -1800
836884
YDOT = 16983
742714 feet/sec YDOT = 5176
644779 meter/sec
ZDOT = 16199
728609 ZDOT = 4937
677280
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
55802992
00016717 00000-0 10270-3 0 9032
2 25544 51
6405 65
5556 0007787 96
7213 263
4827 15
55796276 19782
Satellite: ISS
Catalog Number: 25544
Epoch time: 12180
55802992 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 65
5556 deg
Eccentricity:
0007787
Arg of perigee: 96
7213 deg
Mean anomaly: 263
4827 deg
Mean motion: 15
55796276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1978
Checksum: 348
Coasting Arc #5 (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 = 1418077
56 A = 6775441
05 meter
Y = -4779243
71 meter E =
0017092
Z = -4604223
48 I = 51
93599
XDOT = 5359
086609 Wp = 82
64220
YDOT = 4532
990021 meter/sec RA = 60
20355 deg
ZDOT = -3062
320341 TA = 156
87212
MA = 156
79510
Ha = 221
083 n
mi
Hp = 209
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4652485
42 X = 1493781
04
Y = -15679933
45 feet Y = -4762961
98 meter
Z = -15105720
09 Z = -4597151
26
XDOT = 17582
305147 XDOT = 5322
875623
YDOT = 14872
014506 feet/sec YDOT = 4592
716601 meter/sec
ZDOT = -10046
982747 ZDOT = -3036
373333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16150421
43 X = -4922648
45
Y = -2750612
90 feet Y = -838386
81 meter
Z = -15076031
62 Z = -4595174
44
XDOT = 12352
785434 XDOT = 3765
129000
YDOT = -18183
489492 feet/sec YDOT = -5542
327597 meter/sec
ZDOT = -9940
485893 ZDOT = -3029
860100
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
52151140
00016717 00000-0 10270-3 0 9043
2 25544 51
6407 60
7397 0007565 100
4086 259
7921 15
55830483 19938
Satellite: ISS
Catalog Number: 25544
Epoch time: 12181
52151140 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 60
7397 deg
Eccentricity:
0007565
Arg of perigee: 100
4086 deg
Mean anomaly: 259
7921 deg
Mean motion: 15
55830483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1993
Checksum: 305
Coasting Arc #6 (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 = -3009289
64 A = 6772466
21 meter
Y = 2944407
72 meter E =
0010475
Z = 5296438
09 I = 51
91043
XDOT = -4759
764779 Wp = 106
65829
YDOT = -5993
793931 meter/sec RA = 55
20883 deg
ZDOT = 623
770617 TA = 337
39480
MA = 337
44091
Ha = 221
173 n
mi
Hp = 209
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9872997
50 X = -3067719
94
Y = 9660130
32 feet Y = 2910428
42 meter
Z = 17376765
39 Z = 5281677
59
XDOT = -15616
026177 XDOT = -4695
417336
YDOT = -19664
678250 feet/sec YDOT = -6046
660883 meter/sec
ZDOT = 2046
491526 ZDOT = 600
803139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10978990
61 X = 3346396
34
Y = 8507588
42 feet Y = 2593112
95 meter
Z = 17315567
48 Z = 5277784
97
XDOT = -16628
623613 XDOT = -5068
404477
YDOT = 17458
853703 feet/sec YDOT = 5321
458609 meter/sec
ZDOT = 1952
450990 ZDOT = 595
107062
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
54921781
00016717 00000-0 10270-3 0 9053
2 25544 51
6410 55
6032 0007621 104
3361 255
8633 15
55844205 20096
Satellite: ISS
Catalog Number: 25544
Epoch time: 12182
54921781 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 55
6032 deg
Eccentricity:
0007621
Arg of perigee: 104
3361 deg
Mean anomaly: 255
8633 deg
Mean motion: 15
55844205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2009
Checksum: 283
Coasting Arc #7 (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 = 4446169
17 A = 6773594
83 meter
Y = -857549
42 meter E =
0020350
Z = -5056121
97 I = 51
89544
XDOT = 3468
288484 Wp = 105
39699
YDOT = 6542
900883 meter/sec RA = 50
20818 deg
ZDOT = 1941
411666 TA = 183
39675
MA = 183
41058
Ha = 220
964 n
mi
Hp = 209
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14587169
18 X = 4479989
49
Y = -2813482
35 feet Y = -807639
60 meter
Z = -16588326
67 Z = -5034440
69
XDOT = 11378
899227 XDOT = 3385
435723
YDOT = 21466
210245 feet/sec YDOT = 6581
221830 meter/sec
ZDOT = 6369
460846 ZDOT = 1958
060372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5111999
07 X = -1558137
32
Y = -14054545
52 feet Y = -4283825
47 meter
Z = -16498817
69 Z = -5028839
63
XDOT = 18367
896797 XDOT = 5598
534944
YDOT = -14232
987176 feet/sec YDOT = -4338
214491 meter/sec
ZDOT = 6437
374456 ZDOT = 1962
111734
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
51268443
00016717 00000-0 10270-3 0 9061
2 25544 51
6404 50
7867 0007473 107
5879 252
6091 15
55861686 20247
Satellite: ISS
Catalog Number: 25544
Epoch time: 12183
51268443 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 50
7867 deg
Eccentricity:
0007473
Arg of perigee: 107
5879 deg
Mean anomaly: 252
6091 deg
Mean motion: 15
55861686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2024
Checksum: 322
Coasting Arc #8 (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 = -5437882
44 A = 6777963
64 meter
Y = -1192637
20 meter E =
0018243
Z = 3849778
84 I = 51
89035
XDOT = -1593
080425 Wp = 92
97080
YDOT = -6248
576191 meter/sec RA = 45
21801 deg
ZDOT = -4169
973053 TA = 40
73779
MA = 40
60151
Ha = 220
952 n
mi
Hp = 209
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17840821
64 X = -5442843
20
Y = -3912851
72 feet Y = -1253475
42 meter
Z = 12630508
02 Z = 3823349
75
XDOT = -5226
641815 XDOT = -1502
832511
YDOT = -20500
578056 feet/sec YDOT = -6265
885628 meter/sec
ZDOT = -13681
013952 ZDOT = -4177
494064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -701065
66 X = -213684
81
Y = 18326261
92 feet Y = 5585844
63 meter
Z = 12521648
82 Z = 3816598
56
XDOT = -17941
603382 XDOT = -5468
600711
YDOT = 8718
370935 feet/sec YDOT = 2657
359461 meter/sec
ZDOT = -13711
312605 ZDOT = -4179
208082
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
54037286
00016717 00000-0 10270-3 0 9075
2 25544 51
6406 45
6499 0007353 110
5051 249
6892 15
55906436 20402
Satellite: ISS
Catalog Number: 25544
Epoch time: 12184
54037286 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 45
6499 deg
Eccentricity:
0007353
Arg of perigee: 110
5051 deg
Mean anomaly: 249
6892 deg
Mean motion: 15
55906436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2040
Checksum: 311
Coasting Arc #9 (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 = 5811820
03 A = 6782672
93 meter
Y = 2888275
60 meter E =
0011297
Z = -1975504
46 I = 51
88230
XDOT = -681
268996 Wp = 77
94968
YDOT = 5183
967909 meter/sec RA = 40
24317 deg
ZDOT = 5604
254982 TA = 260
32630
MA = 260
45393
Ha = 220
877 n
mi
Hp = 209
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19067651
02 X = 5788687
23
Y = 9475969
81 feet Y = 2953137
98 meter
Z = -6481313
85 Z = -1947326
92
XDOT = -2235
134500 XDOT = -766
410419
YDOT = 17007
768731 feet/sec YDOT = 5175
872486 meter/sec
ZDOT = 18386
663328 ZDOT = 5600
739568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5615767
22 X = 1711685
85
Y = -20574769
32 feet Y = -6271189
69 meter
Z = -6365435
92 Z = -1940184
87
XDOT = 15642
163203 XDOT = 4767
731344
YDOT = -1384
067518 feet/sec YDOT = -421
863780 meter/sec
ZDOT = 18371
564208 ZDOT = 5599
652771
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
50382450
00016717 00000-0 10270-3 0 9089
2 25544 51
6393 40
8332 0007320 114
6802 245
5114 15
55867211 20558
Satellite: ISS
Catalog Number: 25544
Epoch time: 12185
50382450 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 40
8332 deg
Eccentricity:
0007320
Arg of perigee: 114
6802 deg
Mean anomaly: 245
5114 deg
Mean motion: 15
55867211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 281
Coasting Arc #10 (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 = -5375974
35 A = 6784229
89 meter
Y = -4113331
65 meter E =
0018553
Z = -322082
30 I = 51
86333
XDOT = 3101
388571 Wp = 129
84263
YDOT = -3600
488603 meter/sec RA = 35
27983 deg
ZDOT = -6025
079125 TA = 53
62164
MA = 53
45062
Ha = 220
832 n
mi
Hp = 209
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17637711
13 X = -5328014
10
Y = -13495182
58 feet Y = -4173180
91 meter
Z = -1056700
45 Z = -348082
28
XDOT = 10175
159355 XDOT = 3170
687452
YDOT = -11812
626651 feet/sec YDOT = -3565
418512 meter/sec
ZDOT = -19767
319965 ZDOT = -6009
845226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9500771
61 X = -2895835
19
Y = 20067564
07 feet Y = 6116593
53 meter
Z = -1163457
55 Z = -354621
86
XDOT = -12245
835565 XDOT = -3732
530680
YDOT = -6898
424158 feet/sec YDOT = -2102
639683 meter/sec
ZDOT = -19704
070537 ZDOT = -6005
800700
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
53149742
00016717 00000-0 10270-3 0 9099
2 25544 51
6390 35
6959 0007399 119
1891 241
0003 15
55866474 20712
Satellite: ISS
Catalog Number: 25544
Epoch time: 12186
53149742 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 35
6959 deg
Eccentricity:
0007399
Arg of perigee: 119
1891 deg
Mean anomaly: 241
0003 deg
Mean motion: 15
55866474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2071
Checksum: 325
Coasting Arc #11 (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 = 4169915
41 A = 6781405
71 meter
Y = 4717291
36 meter E =
0019364
Z = 2503291
71 I = 51
82812
XDOT = -5234
001969 Wp = 91
44043
YDOT = 1784
518160 meter/sec RA = 30
31096 deg
ZDOT = 5319
917512 TA = 296
59111
MA = 296
78940
Ha = 220
646 n
mi
Hp = 209
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13680824
82 X = 4104695
57
Y = 15476677
70 feet Y = 4763556
93 meter
Z = 8212899
32 Z = 2523390
84
XDOT = -17171
922471 XDOT = -5279
410286
YDOT = 5854
718372 feet/sec YDOT = 1725
733678 meter/sec
ZDOT = 17453
797613 ZDOT = 5294
381392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11990220
93 X = 3654619
34
Y = -16779978
41 feet Y = -5114537
42 meter
Z = 8295249
38 Z = 2528392
01
XDOT = 8391
209897 XDOT = 2557
640777
YDOT = 14629
867126 feet/sec YDOT = 4459
183500 meter/sec
ZDOT = 17348
267187 ZDOT = 5287
751839
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
55915939
00016717 00000-0 10270-3 0 9103
2 25544 51
6381 30
5574 0007261 123
4001 236
7848 15
55923306 20871
Satellite: ISS
Catalog Number: 25544
Epoch time: 12187
55915939 = yrday
fracday
Element set: 910
Inclination: 51
6381 deg
RA of node: 30
5574 deg
Eccentricity:
0007261
Arg of perigee: 123
4001 deg
Mean anomaly: 236
7848 deg
Mean motion: 15
55923306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2087
Checksum: 308
Coasting Arc #12 (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 = -2224120
25 A = 6776348
45 meter
Y = -4775302
63 meter E =
0013863
Z = -4273551
02 I = 51
78339
XDOT = 6762
293449 Wp = 95
31928
YDOT = 63
152516 meter/sec RA = 25
32563 deg
ZDOT = -3601
219435 TA = 137
98943
MA = 137
88303
Ha = 220
665 n
mi
Hp = 209
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7296982
46 X = -2149796
98
Y = -15667003
38 feet Y = -4799758
07 meter
Z = -14020836
68 Z = -4284175
52
XDOT = 22186
002128 XDOT = 6778
578263
YDOT = 207
193294 feet/sec YDOT = 138
864138 meter/sec
ZDOT = -11815
024394 ZDOT = -3568
329557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13445127
96 X = -4098075
00
Y = 10803442
69 feet Y = 3292889
33 meter
Z = -14064102
15 Z = -4286738
34
XDOT = -4422
241052 XDOT = -1347
899073
YDOT = -20659
898188 feet/sec YDOT = -6297
136968 meter/sec
ZDOT = -11679
379785 ZDOT = -3559
874959
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
52258712
00016717 00000-0 10270-3 0 9111
2 25544 51
6371 25
7403 0007324 125
9722 234
2112 15
55913684 21027
Satellite: ISS
Catalog Number: 25544
Epoch time: 12188
52258712 = yrday
fracday
Element set: 911
Inclination: 51
6371 deg
RA of node: 25
7403 deg
Eccentricity:
0007324
Arg of perigee: 125
9722 deg
Mean anomaly: 234
2112 deg
Mean motion: 15
55913684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2102
Checksum: 282
Coasting Arc #13 (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 = -116577
28 A = 6772707
04 meter
Y = 4329536
04 meter E =
0011350
Z = 5200246
95 I = 51
74314
XDOT = -7385
087982 Wp = 126
98769
YDOT = -1694
816960 meter/sec RA = 20
32115 deg
ZDOT = 1236
950636 TA = 311
12330
MA = 311
22121
Ha = 220
698 n
mi
Hp = 209
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -382471
40 X = -190243
59
Y = 14204514
57 feet Y = 4327820
02 meter
Z = 17061177
66 Z = 5199502
11
XDOT = -24229
291281 XDOT = -7371
596044
YDOT = -5560
423096 feet/sec YDOT = -1777
326271 meter/sec
ZDOT = 4058
236996 ZDOT = 1201
107407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13844512
60 X = 4219807
44
Y = -3219618
79 feet Y = -981339
81 meter
Z = 17057603
21 Z = 5199157
46
XDOT = 695
105852 XDOT = 211
868264
YDOT = 23855
852530 feet/sec YDOT = 7271
263851 meter/sec
ZDOT = 3910
605200 ZDOT = 1191
952465
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
55023517
00016717 00000-0 10270-3 0 9129
2 25544 51
6374 20
6022 0007345 129
4200 230
7605 15
55885223 21186
Satellite: ISS
Catalog Number: 25544
Epoch time: 12189
55023517 = yrday
fracday
Element set: 912
Inclination: 51
6374 deg
RA of node: 20
6022 deg
Eccentricity:
0007345
Arg of perigee: 129
4200 deg
Mean anomaly: 230
7605 deg
Mean motion: 15
55885223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2118
Checksum: 279
Coasting Arc #14 (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 = 2585113
86 A = 6772765
75 meter
Y = -3535143
05 meter E =
0020458
Z = -5184223
91 I = 51
71420
XDOT = 6899
695948 Wp = 111
65272
YDOT = 3017
609749 meter/sec RA = 15
30652 deg
ZDOT = 1379
826253 TA = 171
63834
MA = 171
60420
Ha = 220
574 n
mi
Hp = 209
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8481344
68 X = 2649635
88
Y = -11598238
34 feet Y = -3505873
52 meter
Z = -17008608
62 Z = -5171509
27
XDOT = 22636
797729 XDOT = 6858
736820
YDOT = 9900
294453 feet/sec YDOT = 3094
537304 meter/sec
ZDOT = 4526
989020 ZDOT = 1413
244978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13519815
72 X = -4120839
83
Y = -5045973
95 feet Y = -1538012
86 meter
Z = -16955761
17 Z = -5168116
00
XDOT = 2900
515705 XDOT = 884
077187
YDOT = -23478
255350 feet/sec YDOT = -7156
172231 meter/sec
ZDOT = 4664
461922 ZDOT = 1421
727994
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
51364485
00016717 00000-0 10270-3 0 9130
2 25544 51
6368 15
7845 0007401 133
4944 226
6826 15
55939877 21331
Satellite: ISS
Catalog Number: 25544
Epoch time: 12190
51364485 = yrday
fracday
Element set: 913
Inclination: 51
6368 deg
RA of node: 15
7845 deg
Eccentricity:
0007401
Arg of perigee: 133
4944 deg
Mean anomaly: 226
6826 deg
Mean motion: 15
55939877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 325
Coasting Arc #15 (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 = -4727626
10 A = 6776787
17 meter
Y = 2479811
42 meter E =
0015284
Z = 4159453
55 I = 51
69833
XDOT = -5392
345459 Wp = 100
41134
YDOT = -3985
331313 meter/sec RA = 10
29967 deg
ZDOT = -3743
961850 TA = 28
03577
MA = 27
95353
Ha = 220
571 n
mi
Hp = 209
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15510584
30 X = -4775209
97
Y = 8135864
23 feet Y = 2426677
80 meter
Z = 13646501
13 Z = 4136371
79
XDOT = -17691
422110 XDOT = -5329
192755
YDOT = -13075
233965 feet/sec YDOT = -4045
278473 meter/sec
ZDOT = -12283
339404 ZDOT = -3770
004272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12345782
64 X = 3762994
55
Y = 12527924
24 feet Y = 3818511
31 meter
Z = 13551024
72 Z = 4130352
33
XDOT = -6431
689905 XDOT = -1960
379083
YDOT = 19772
349960 feet/sec YDOT = 6026
612268 meter/sec
ZDOT = -12390
273031 ZDOT = -3776
555220
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
54127423
00016717 00000-0 10270-3 0 9144
2 25544 51
6372 10
6471 0007287 137
8990 222
2724 15
55943995 21498
Satellite: ISS
Catalog Number: 25544
Epoch time: 12191
54127423 = yrday
fracday
Element set: 914
Inclination: 51
6372 deg
RA of node: 10
6471 deg
Eccentricity:
0007287
Arg of perigee: 137
8990 deg
Mean anomaly: 222
2724 deg
Mean motion: 15
55943995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 316
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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