[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 1st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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 1525)
---------------------------------------
Vector Time (GMT): 2012/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5510154
01 A = 6783593
74 meter
Y = 3881202
66 meter E =
0008486
Z = -787800
61 I = 51
47938
XDOT = -3328
697364 Wp = 76
68175
YDOT = 3532
698930 meter/sec RA = 209
82103 deg
ZDOT = -5929
779673 TA = 111
85178
MA = 111
76150
Ha = 220
631 n
mi
Hp = 210
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18077933
11 X = 5470171
09
Y = 12733604
53 feet Y = 3942597
10 meter
Z = -2584647
66 Z = -761129
09
XDOT = -10920
923111 XDOT = -3339
147449
YDOT = 11590
219585 feet/sec YDOT = 3495
417301 meter/sec
ZDOT = -19454
657720 ZDOT = -5945
975702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18667410
74 X = 5689826
79
Y = -11875924
11 feet Y = -3619781
67 meter
Z = -2475268
93 Z = -754461
97
XDOT = 5732
257080 XDOT = 1747
191958
YDOT = 13042
059124 feet/sec YDOT = 3975
219621 meter/sec
ZDOT = -19521
554619 ZDOT = -5950
169848
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 12151
53069913
00016717 00000-0 10270-3 0 9003
2 25544 51
6376 210
6986 0010126 9
0438 351
0896 15
56017199 15266
Satellite: ISS
Catalog Number: 25544
Epoch time: 12151
53069913 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 210
6986 deg
Eccentricity:
0010126
Arg of perigee: 9
0438 deg
Mean anomaly: 351
0896 deg
Mean motion: 15
56017199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1526
Checksum: 303
Coasting Arc #2 (Orbit 1541)
---------------------------------------
Vector Time (GMT): 2012/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4121354
94 A = 6780226
00 meter
Y = -4488236
74 meter E =
0019398
Z = 2945048
02 I = 51
49458
XDOT = 5548
564816 Wp = 52
97450
YDOT = -1810
789585 meter/sec RA = 204
82606 deg
ZDOT = 4993
897114 TA = 340
81026
MA = 340
88322
Ha = 220
792 n
mi
Hp = 209
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13521505
70 X = -4085166
85
Y = -14725186
14 feet Y = -4534122
16 meter
Z = 9662231
04 Z = 2925113
92
XDOT = 18203
952807 XDOT = 5544
141439
YDOT = -5940
910711 feet/sec YDOT = -1748
767195 meter/sec
ZDOT = 16384
176884 ZDOT = 5020
841346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18666250
72 X = -5689473
22
Y = 7266638
35 feet Y = 2214871
37 meter
Z = 9580604
54 Z = 2920168
26
XDOT = 1609
834880 XDOT = 490
677671
YDOT = -17661
542528 feet/sec YDOT = -5383
238162 meter/sec
ZDOT = 16495
148079 ZDOT = 5027
721134
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 12152
55828454
00016717 00000-0 10270-3 0 9010
2 25544 51
6373 205
5606 0010173 13
1445 346
9972 15
56013989 15420
Satellite: ISS
Catalog Number: 25544
Epoch time: 12152
55828454 = yrday
fracday
Element set: 901
Inclination: 51
6373 deg
RA of node: 205
5606 deg
Eccentricity:
0010173
Arg of perigee: 13
1445 deg
Mean anomaly: 346
9972 deg
Mean motion: 15
56013989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1542
Checksum: 304
Coasting Arc #3 (Orbit 1556)
---------------------------------------
Vector Time (GMT): 2012/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2033784
19 A = 6775034
57 meter
Y = 4591733
76 meter E =
0017932
Z = -4564981
68 I = 51
50566
XDOT = -7018
179969 Wp = 43
13276
YDOT = 59
160111 meter/sec RA = 199
81552 deg
ZDOT = -3061
546033 TA = 196
11792
MA = 196
17504
Ha = 220
830 n
mi
Hp = 209
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6672520
32 X = 2004463
39
Y = 15064743
31 feet Y = 4614313
29 meter
Z = -14976974
01 Z = -4555172
24
XDOT = -23025
524833 XDOT = -7003
447325
YDOT = 194
094851 feet/sec YDOT = -19
238851 meter/sec
ZDOT = -10044
442365 ZDOT = -3095
604874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16477179
83 X = 5022244
41
Y = -1080465
07 feet Y = -329325
75 meter
Z = -14936998
00 Z = -4552796
99
XDOT = -7912
731806 XDOT = -2411
800655
YDOT = 20385
674419 feet/sec YDOT = 6213
553563 meter/sec
ZDOT = -10184
548004 ZDOT = -3104
250232
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 12153
52163581
00016717 00000-0 10270-3 0 9022
2 25544 51
6376 200
7438 0010174 16
6407 343
5078 15
56028981 15574
Satellite: ISS
Catalog Number: 25544
Epoch time: 12153
52163581 = yrday
fracday
Element set: 902
Inclination: 51
6376 deg
RA of node: 200
7438 deg
Eccentricity:
0010174
Arg of perigee: 16
6407 deg
Mean anomaly: 343
5078 deg
Mean motion: 15
56028981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1557
Checksum: 300
Coasting Arc #4 (Orbit 1572)
---------------------------------------
Vector Time (GMT): 2012/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 488401
40 A = 6771815
43 meter
Y = -4208494
92 meter E =
0010508
Z = 5276689
59 I = 51
52352
XDOT = 7502
615575 Wp = 36
53105
YDOT = 1537
440903 meter/sec RA = 194
79028 deg
ZDOT = 539
504677 TA = 48
36404
MA = 48
27409
Ha = 220
863 n
mi
Hp = 209
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1602366
79 X = 509791
91
Y = -13807398
02 feet Y = -4202914
38 meter
Z = 17311973
73 Z = 5279113
70
XDOT = 24614
880495 XDOT = 7482
245140
YDOT = 5044
097450 feet/sec YDOT = 1621
225828 meter/sec
ZDOT = 1770
028468 ZDOT = 575
903435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12520734
19 X = -3816319
78
Y = -6007130
94 feet Y = -1830973
51 meter
Z = 17322293
36 Z = 5279835
02
XDOT = 12508
208309 XDOT = 3812
501893
YDOT = -20608
537224 feet/sec YDOT = -6281
482146 meter/sec
ZDOT = 1919
645467 ZDOT = 585
107938
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 12154
54919848
00016717 00000-0 10270-3 0 9031
2 25544 51
6367 195
6059 0010285 20
4882 339
6682 15
56066791 15734
Satellite: ISS
Catalog Number: 25544
Epoch time: 12154
54919848 = yrday
fracday
Element set: 903
Inclination: 51
6367 deg
RA of node: 195
6059 deg
Eccentricity:
0010285
Arg of perigee: 20
4882 deg
Mean anomaly: 339
6682 deg
Mean motion: 15
56066791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1573
Checksum: 339
Coasting Arc #5 (Orbit 1587)
---------------------------------------
Vector Time (GMT): 2012/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2981286
64 A = 6773124
63 meter
Y = 3501895
49 meter E =
0017596
Z = -4984654
20 I = 51
55800
XDOT = -6801
772061 Wp = 69
81624
YDOT = -2846
124873 meter/sec RA = 189
76336 deg
ZDOT = 2080
494105 TA = 220
40519
MA = 220
53602
Ha = 221
002 n
mi
Hp = 209
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9781124
14 X = -2996009
27
Y = 11489158
44 feet Y = 3468475
35 meter
Z = -16353852
37 Z = -4999172
61
XDOT = -22315
525133 XDOT = -6779
547309
YDOT = -9337
680029 feet/sec YDOT = -2922
062551 meter/sec
ZDOT = 6825
768062 ZDOT = 2047
504435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7832119
07 X = 2387229
89
Y = 12820377
23 feet Y = 3907650
98 meter
Z = -16413880
62 Z = -5002950
81
XDOT = -15000
096550 XDOT = -4572
029428
YDOT = 17679
434400 feet/sec YDOT = 5388
691605 meter/sec
ZDOT = 6690
266950 ZDOT = 2039
193366
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 12155
51252961
00016717 00000-0 10270-3 0 9046
2 25544 51
6371 190
7888 0010383 23
7097 336
4533 15
56053364 15886
Satellite: ISS
Catalog Number: 25544
Epoch time: 12155
51252961 = yrday
fracday
Element set: 904
Inclination: 51
6371 deg
RA of node: 190
7888 deg
Eccentricity:
0010383
Arg of perigee: 23
7097 deg
Mean anomaly: 336
4533 deg
Mean motion: 15
56053364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1588
Checksum: 316
Coasting Arc #6 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2012/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5113275
69 A = 6777724
99 meter
Y = -2498336
73 meter E =
0019545
Z = 3675895
29 I = 51
60277
XDOT = 5019
390768 Wp = 58
32182
YDOT = 3861
168291 meter/sec RA = 184
75014 deg
ZDOT = -4330
849729 TA = 77
86547
MA = 77
64657
Ha = 221
003 n
mi
Hp = 209
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16775838
88 X = 5122975
72
Y = -8196642
81 feet Y = -2441103
31 meter
Z = 12060023
92 Z = 3700758
73
XDOT = 16467
817479 XDOT = 4996
879836
YDOT = 12667
874970 feet/sec YDOT = 3917
173103 meter/sec
ZDOT = -14208
824571 ZDOT = -4306
519523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2803275
32 X = -854438
32
Y = -18392169
11 feet Y = -5605933
14 meter
Z = 12162551
67 Z = 3707145
75
XDOT = 15711
482419 XDOT = 4788
859841
YDOT = -11782
948928 feet/sec YDOT = -3591
442833 meter/sec
ZDOT = -14109
024225 ZDOT = -4300
430584
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 12156
54007046
00016717 00000-0 10270-3 0 9053
2 25544 51
6357 185
6502 0010482 27
8673 332
3040 15
56114304 16040
Satellite: ISS
Catalog Number: 25544
Epoch time: 12156
54007046 = yrday
fracday
Element set: 905
Inclination: 51
6357 deg
RA of node: 185
6502 deg
Eccentricity:
0010482
Arg of perigee: 27
8673 deg
Mean anomaly: 332
3040 deg
Mean motion: 15
56114304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1604
Checksum: 277
Coasting Arc #7 (Orbit 1618)
---------------------------------------
Vector Time (GMT): 2012/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6418822
51 A = 6782227
71 meter
Y = 1361570
82 meter E =
0017992
Z = -1686701
63 I = 51
64921
XDOT = -2444
834934 Wp = 35
03529
YDOT = -4507
404094 meter/sec RA = 179
75852 deg
ZDOT = 5709
945638 TA = 306
45529
MA = 306
62099
Ha = 221
026 n
mi
Hp = 208
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21059128
98 X = -6425377
17
Y = 4467095
87 feet Y = 1289755
23 meter
Z = -5533797
98 Z = -1717899
78
XDOT = -8021
111989 XDOT = -2421
988238
YDOT = -14788
071173 feet/sec YDOT = -4534
617015 meter/sec
ZDOT = 18733
417448 ZDOT = 5698
123394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1683366
22 X = -513090
03
Y = 21428233
25 feet Y = 6531325
50 meter
Z = -5662320
79 Z = -1725875
38
XDOT = -14924
987332 XDOT = -4549
136139
YDOT = 3727
230985 feet/sec YDOT = 1136
060004 meter/sec
ZDOT = 18685
137408 ZDOT = 5695
229882
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 12157
50338112
00016717 00000-0 10270-3 0 9062
2 25544 51
6364 180
8332 0010423 32
0106 328
1679 15
56136781 16190
Satellite: ISS
Catalog Number: 25544
Epoch time: 12157
50338112 = yrday
fracday
Element set: 906
Inclination: 51
6364 deg
RA of node: 180
8332 deg
Eccentricity:
0010423
Arg of perigee: 32
0106 deg
Mean anomaly: 328
1679 deg
Mean motion: 15
56136781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1619
Checksum: 286
Coasting Arc #8 (Orbit 1634)
---------------------------------------
Vector Time (GMT): 2012/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6748219
30 A = 6783356
19 meter
Y = -60801
95 meter E =
0013015
Z = -700319
19 I = 51
68220
XDOT = -565
711341 Wp = 88
51170
YDOT = 4782
693400 meter/sec RA = 174
77976 deg
ZDOT = -5961
839129 TA = 99
04805
MA = 98
90074
Ha = 221
226 n
mi
Hp = 208
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22139827
08 X = 6751799
64
Y = -199481
45 feet Y = 14680
95 meter
Z = -2297635
13 Z = -667528
01
XDOT = -1856
008335 XDOT = -590
189135
YDOT = 15691
251312 feet/sec YDOT = 4776
231402 meter/sec
ZDOT = -19559
839661 ZDOT = -5964
645979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5727994
76 X = 1745892
80
Y = -21401025
99 feet Y = -6523032
72 meter
Z = -2162643
28 Z = -659173
67
XDOT = 13094
608514 XDOT = 3991
236675
YDOT = 5448
949286 feet/sec YDOT = 1660
839742 meter/sec
ZDOT = -19571
796381 ZDOT = -5965
483537
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 12158
53090079
00016717 00000-0 10270-3 0 9074
2 25544 51
6355 175
6938 0010501 35
5987 324
5866 15
56118900 16355
Satellite: ISS
Catalog Number: 25544
Epoch time: 12158
53090079 = yrday
fracday
Element set: 907
Inclination: 51
6355 deg
RA of node: 175
6938 deg
Eccentricity:
0010501
Arg of perigee: 35
5987 deg
Mean anomaly: 324
5866 deg
Mean motion: 15
56118900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1635
Checksum: 323
Coasting Arc #9 (Orbit 1650)
---------------------------------------
Vector Time (GMT): 2012/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5985103
97 A = 6780020
71 meter
Y = -1249613
65 meter E =
0022337
Z = 2899551
06 I = 51
70096
XDOT = 3429
320898 Wp = 62
81523
YDOT = -4667
186820 meter/sec RA = 169
79885 deg
ZDOT = 5047
402651 TA = 330
27772
MA = 330
40444
Ha = 221
360 n
mi
Hp = 208
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19636167
88 X = -5984771
00
Y = -4099782
32 feet Y = -1316541
36 meter
Z = 9512962
81 Z = 2870476
46
XDOT = 11251
052814 XDOT = 3456
736439
YDOT = -15312
292717 feet/sec YDOT = -4628
685497 meter/sec
ZDOT = 16559
719983 ZDOT = 5064
127952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8904164
96 X = -2713989
48
Y = 18037858
67 feet Y = 5497939
32 meter
Z = 9393362
90 Z = 2863097
01
XDOT = -10712
721485 XDOT = -3265
237509
YDOT = -13982
164381 feet/sec YDOT = -4261
763703 meter/sec
ZDOT = 16628
972274 ZDOT = 5068
510749
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 12159
55840928
00016717 00000-0 10270-3 0 9084
2 25544 51
6352 170
5553 0010588 38
9032 321
2882 15
56133635 16514
Satellite: ISS
Catalog Number: 25544
Epoch time: 12159
55840928 = yrday
fracday
Element set: 908
Inclination: 51
6352 deg
RA of node: 170
5553 deg
Eccentricity:
0010588
Arg of perigee: 38
9032 deg
Mean anomaly: 321
2882 deg
Mean motion: 15
56133635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1651
Checksum: 312
Coasting Arc #10 (Orbit 1665)
---------------------------------------
Vector Time (GMT): 2012/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4313973
79 A = 6774717
38 meter
Y = 2566098
07 meter E =
0019796
Z = -4569812
35 I = 51
71333
XDOT = -5697
325924 Wp = 55
90362
YDOT = 4074
582343 meter/sec RA = 164
80180 deg
ZDOT = -3089
113098 TA = 183
15317
MA = 183
16566
Ha = 221
303 n
mi
Hp = 208
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14153457
32 X = 4307157
52
Y = 8418956
91 feet Y = 2614302
06 meter
Z = -14992822
66 Z = -4548871
61
XDOT = -18692
014186 XDOT = -5727
459171
YDOT = 13368
052305 feet/sec YDOT = 4010
703227 meter/sec
ZDOT = -10134
885491 ZDOT = -3116
862965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11516773
77 X = 3510312
64
Y = -11880019
11 feet Y = -3621029
83 meter
Z = -14906810
15 Z = -4543595
73
XDOT = 7771
911036 XDOT = 2368
878484
YDOT = 20400
269951 feet/sec YDOT = 6218
002281 meter/sec
ZDOT = -10249
491776 ZDOT = -3124
045093
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 12160
52168768
00016717 00000-0 10270-3 0 9099
2 25544 51
6353 165
7375 0010558 42
3684 317
8283 15
56151448 16666
Satellite: ISS
Catalog Number: 25544
Epoch time: 12160
52168768 = yrday
fracday
Element set: 909
Inclination: 51
6353 deg
RA of node: 165
7375 deg
Eccentricity:
0010558
Arg of perigee: 42
3684 deg
Mean anomaly: 317
8283 deg
Mean motion: 15
56151448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1666
Checksum: 329
Coasting Arc #11 (Orbit 1681)
---------------------------------------
Vector Time (GMT): 2012/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1992803
09 A = 6771511
34 meter
Y = -3713824
96 meter E =
0011948
Z = 5290690
82 I = 51
73146
XDOT = 7036
603293 Wp = 58
71737
YDOT = -3033
084048 meter/sec RA = 159
78919 deg
ZDOT = 526
528219 TA = 26
30369
MA = 26
24307
Ha = 221
391 n
mi
Hp = 208
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6538067
89 X = -1976827
09
Y = -12184465
11 feet Y = -3736020
97 meter
Z = 17357909
50 Z = 5281048
32
XDOT = 23085
968808 XDOT = 7067
439137
YDOT = -9951
063148 feet/sec YDOT = -2954
224036 meter/sec
ZDOT = 1727
454786 ZDOT = 560
786133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13335451
52 X = -4064645
62
Y = 3839198
22 feet Y = 1170187
62 meter
Z = 17318511
31 Z = 5278682
25
XDOT = -4422
038190 XDOT = -1347
837240
YDOT = -23712
955400 feet/sec YDOT = -7227
708806 meter/sec
ZDOT = 1868
787333 ZDOT = 569
606379
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 12161
54917390
00016717 00000-0 10270-3 0 9107
2 25544 51
6347 160
5983 0010579 45
7498 314
4522 15
56168870 16824
Satellite: ISS
Catalog Number: 25544
Epoch time: 12161
54917390 = yrday
fracday
Element set: 910
Inclination: 51
6347 deg
RA of node: 160
5983 deg
Eccentricity:
0010579
Arg of perigee: 45
7498 deg
Mean anomaly: 314
4522 deg
Mean motion: 15
56168870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1682
Checksum: 325
Coasting Arc #12 (Orbit 1696)
---------------------------------------
Vector Time (GMT): 2012/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -505378
07 A = 6772890
55 meter
Y = 4577583
30 meter E =
0020455
Z = -4982367
55 I = 51
76447
XDOT = -7193
090413 Wp = 80
21327
YDOT = 1523
993643 meter/sec RA = 154
77621 deg
ZDOT = 2140
667847 TA = 210
57423
MA = 210
69362
Ha = 221
396 n
mi
Hp = 208
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1658064
54 X = -532324
83
Y = 15018317
93 feet Y = 4571781
65 meter
Z = -16346350
24 Z = -4984887
67
XDOT = -23599
377997 XDOT = -7219
996268
YDOT = 4999
979145 feet/sec YDOT = 1443
405412 meter/sec
ZDOT = 7023
188474 ZDOT = 2105
659010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14400532
19 X = 4389282
21
Y = 4535605
18 feet Y = 1382452
46 meter
Z = -16357113
91 Z = -4985648
32
XDOT = 492
970637 XDOT = 150
257450
YDOT = 23114
133805 feet/sec YDOT = 7045
187984 meter/sec
ZDOT = 6878
875793 ZDOT = 2096
681342
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 12162
51243159
00016717 00000-0 10270-3 0 9111
2 25544 51
6349 155
7814 0010599 48
8655 311
3412 15
56162860 16979
Satellite: ISS
Catalog Number: 25544
Epoch time: 12162
51243159 = yrday
fracday
Element set: 911
Inclination: 51
6349 deg
RA of node: 155
7814 deg
Eccentricity:
0010599
Arg of perigee: 48
8655 deg
Mean anomaly: 311
3412 deg
Mean motion: 15
56162860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1697
Checksum: 314
Coasting Arc #13 (Orbit 1712)
---------------------------------------
Vector Time (GMT): 2012/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2856447
86 A = 6777625
59 meter
Y = -4959604
38 meter E =
0021528
Z = 3619574
30 I = 51
80748
XDOT = 6268
086318 Wp = 70
24830
YDOT = 367
632314 meter/sec RA = 149
77632 deg
ZDOT = -4414
417150 TA = 66
90175
MA = 66
67497
Ha = 221
313 n
mi
Hp = 208
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9371548
09 X = 2894111
78
Y = -16271667
91 feet Y = -4927451
54 meter
Z = 11875243
75 Z = 3633541
85
XDOT = 20564
587658 XDOT = 6284
953772
YDOT = 1206
142764 feet/sec YDOT = 437
820638 meter/sec
ZDOT = -14482
995899 ZDOT = -4383
926044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14288565
56 X = -4355154
78
Y = -12126428
91 feet Y = -3696135
53 meter
Z = 11933194
05 Z = 3637237
55
XDOT = 4089
709825 XDOT = 1246
543555
YDOT = -19038
840246 feet/sec YDOT = -5803
038507 meter/sec
ZDOT = -14357
438078 ZDOT = -4376
147126
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 12163
53989439
00016717 00000-0 10270-3 0 9123
2 25544 51
6343 150
6417 0010601 52
0119 308
1990 15
56222178 17135
Satellite: ISS
Catalog Number: 25544
Epoch time: 12163
53989439 = yrday
fracday
Element set: 912
Inclination: 51
6343 deg
RA of node: 150
6417 deg
Eccentricity:
0010601
Arg of perigee: 52
0119 deg
Mean anomaly: 308
1990 deg
Mean motion: 15
56222178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1713
Checksum: 292
Coasting Arc #14 (Orbit 1727)
---------------------------------------
Vector Time (GMT): 2012/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4578236
76 A = 6782124
61 meter
Y = 4742524
29 meter E =
0018438
Z = -1573636
21 I = 51
84811
XDOT = -4452
603364 Wp = 48
87371
YDOT = -2403
211486 meter/sec RA = 144
79916 deg
ZDOT = 5767
106727 TA = 293
95193
MA = 294
14491
Ha = 221
392 n
mi
Hp = 207
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15020461
82 X = -4623283
97
Y = 15559462
90 feet Y = 4691075
88 meter
Z = -5162848
45 Z = -1595986
15
XDOT = -14608
278752 XDOT = -4453
414639
YDOT = -7884
552118 feet/sec YDOT = -2453
008317 meter/sec
ZDOT = 18920
953829 ZDOT = 5745
473906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12845644
60 X = 3915352
47
Y = 17370584
50 feet Y = 5294554
15 meter
Z = -5255318
46 Z = -1601821
07
XDOT = -8958
578767 XDOT = -2730
574808
YDOT = 12268
143157 feet/sec YDOT = 3739
330034 meter/sec
ZDOT = 18832
049692 ZDOT = 5740
008746
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 12164
50313097
00016717 00000-0 10270-3 0 9133
2 25544 51
6340 145
8248 0010701 56
5207 303
6968 15
56232269 17281
Satellite: ISS
Catalog Number: 25544
Epoch time: 12164
50313097 = yrday
fracday
Element set: 913
Inclination: 51
6340 deg
RA of node: 145
8248 deg
Eccentricity:
0010701
Arg of perigee: 56
5207 deg
Mean anomaly: 303
6968 deg
Mean motion: 15
56232269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1728
Checksum: 298
Coasting Arc #15 (Orbit 1743)
---------------------------------------
Vector Time (GMT): 2012/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5553761
35 A = 6782868
41 meter
Y = -3796026
52 meter E =
0015831
Z = -868298
94 I = 51
87526
XDOT = 2068
640449 Wp = 98
99068
YDOT = 4366
200264 meter/sec RA = 139
83330 deg
ZDOT = -5951
629441 TA = 90
37456
MA = 90
19315
Ha = 221
440 n
mi
Hp = 207
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18221001
80 X = 5600014
55
Y = -12454155
26 feet Y = -3733662
22 meter
Z = -2848749
80 Z = -841206
88
XDOT = 6786
878114 XDOT = 2048
574814
YDOT = 14324
804015 feet/sec YDOT = 4389
221494 meter/sec
ZDOT = -19526
343311 ZDOT = -5941
628309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9586717
59 X = -2922031
52
Y = -19895501
13 feet Y = -6064148
74 meter
Z = -2736813
13 Z = -834180
64
XDOT = 13744
445695 XDOT = 4189
307048
YDOT = -3986
928265 feet/sec YDOT = -1215
215735 meter/sec
ZDOT = -19485
523025 ZDOT = -5939
187418
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 12165
53057083
00016717 00000-0 10270-3 0 9148
2 25544 51
6343 140
6845 0010697 59
1347 301
0858 15
56249117 17446
Satellite: ISS
Catalog Number: 25544
Epoch time: 12165
53057083 = yrday
fracday
Element set: 914
Inclination: 51
6343 deg
RA of node: 140
6845 deg
Eccentricity:
0010697
Arg of perigee: 59
1347 deg
Mean anomaly: 301
0858 deg
Mean motion: 15
56249117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1744
Checksum: 308
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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