[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 12th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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
172/13:49:37
923 -0
8 4
2 4
2
N/A 4
1 0
0 221
1
000/00:09:15
847 -0
4 -0
2 209
8
Coasting Arc #1 (Orbit 1712)
---------------------------------------
Vector Time (GMT): 2012/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3019309
18 A = 6777755
20 meter
Y = -4947316
44 meter E =
0021664
Z = 3502617
90 I = 51
80864
XDOT = 6169
736620 Wp = 71
64717
YDOT = 534
292471 meter/sec RA = 149
78163 deg
ZDOT = -4534
126764 TA = 67
19926
MA = 66
97056
Ha = 221
189 n
mi
Hp = 207
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9905870
02 X = 3057391
75
Y = -16231353
14 feet Y = -4913340
03 meter
Z = 11491528
55 Z = 3517377
65
XDOT = 20241
918044 XDOT = 6185
329278
YDOT = 1752
928054 feet/sec YDOT = 603
373870 meter/sec
ZDOT = -14875
743978 ZDOT = -4504
116519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14150496
97 X = -4313071
48
Y = -12646577
84 feet Y = -3854676
93 meter
Z = 11552740
74 Z = 3521275
38
XDOT = 4530
496998 XDOT = 1380
895485
YDOT = -18633
758973 feet/sec YDOT = -5679
569735 meter/sec
ZDOT = -14752
180870 ZDOT = -4496
464729
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
53959025
00016717 00000-0 10270-3 0 9008
2 25544 51
6342 150
6490 0010589 52
1046 308
1064 15
56299388 17139
Satellite: ISS
Catalog Number: 25544
Epoch time: 12163
53959025 = yrday
fracday
Element set: 900
Inclination: 51
6342 deg
RA of node: 150
6490 deg
Eccentricity:
0010589
Arg of perigee: 52
1046 deg
Mean anomaly: 308
1064 deg
Mean motion: 15
56299388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1713
Checksum: 301
Coasting Arc #2 (Orbit 1727)
---------------------------------------
Vector Time (GMT): 2012/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4711500
00 A = 6782107
46 meter
Y = 4665837
35 meter E =
0018929
Z = -1396998
08 I = 51
84884
XDOT = -4270
949389 Wp = 48
60383
YDOT = -2587
483668 meter/sec RA = 144
80524 deg
ZDOT = 5825
371561 TA = 296
19810
MA = 296
39260
Ha = 221
253 n
mi
Hp = 207
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15457677
15 X = -4756537
84
Y = 15307865
31 feet Y = 4612898
74 meter
Z = -4583327
03 Z = -1419995
39
XDOT = -14012
301145 XDOT = -4269
996635
YDOT = -8489
119645 feet/sec YDOT = -2635
239274 meter/sec
ZDOT = 19112
111420 ZDOT = 5804
625478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12524196
76 X = 3817375
17
Y = 17763275
16 feet Y = 5414246
27 meter
Z = -4678457
13 Z = -1425993
73
XDOT = -9426
998394 XDOT = -2873
349111
YDOT = 11604
407039 feet/sec YDOT = 3537
023266 meter/sec
ZDOT = 19026
875717 ZDOT = 5799
391718
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
50277831
00016717 00000-0 10270-3 0 9015
2 25544 51
6339 145
8317 0010673 56
7324 303
4851 15
56316462 17283
Satellite: ISS
Catalog Number: 25544
Epoch time: 12164
50277831 = yrday
fracday
Element set: 901
Inclination: 51
6339 deg
RA of node: 145
8317 deg
Eccentricity:
0010673
Arg of perigee: 56
7324 deg
Mean anomaly: 303
4851 deg
Mean motion: 15
56316462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1728
Checksum: 302
Coasting Arc #3 (Orbit 1743)
---------------------------------------
Vector Time (GMT): 2012/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5622053
40 A = 6782457
76 meter
Y = -3639285
04 meter E =
0015304
Z = -1076161
52 I = 51
87471
XDOT = 1817
665544 Wp = 98
18050
YDOT = 4533
195340 meter/sec RA = 139
83916 deg
ZDOT = -5908
046935 TA = 93
45472
MA = 93
27966
Ha = 221
301 n
mi
Hp = 207
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18445057
07 X = 5667558
56
Y = -11939911
55 feet Y = -3576161
21 meter
Z = -3530713
64 Z = -1048739
49
XDOT = 5963
469633 XDOT = 1795
539474
YDOT = 14872
688124 feet/sec YDOT = 4553
398489 meter/sec
ZDOT = -19383
356085 ZDOT = -5899
270023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9044171
11 X = -2756663
36
Y = -20044243
29 feet Y = -6109485
35 meter
Z = -3417431
32 Z = -1041633
07
XDOT = 14152
059329 XDOT = 4313
547684
YDOT = -3129
557443 feet/sec YDOT = -953
889109 meter/sec
ZDOT = -19347
593534 ZDOT = -5897
146509
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
53016350
00016717 00000-0 10270-3 0 9027
2 25544 51
6342 140
6911 0010673 59
3065 300
9139 15
56333497 17447
Satellite: ISS
Catalog Number: 25544
Epoch time: 12165
53016350 = yrday
fracday
Element set: 902
Inclination: 51
6342 deg
RA of node: 140
6911 deg
Eccentricity:
0010673
Arg of perigee: 59
3065 deg
Mean anomaly: 300
9139 deg
Mean motion: 15
56333497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1744
Checksum: 288
Coasting Arc #4 (Orbit 1759)
---------------------------------------
Vector Time (GMT): 2012/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5585700
14 A = 6778333
92 meter
Y = 1980164
34 meter E =
0022723
Z = 3265286
31 I = 51
88389
XDOT = 678
993126 Wp = 76
69955
YDOT = -5984
751814 meter/sec RA = 134
86825 deg
ZDOT = 4768
176430 TA = 321
13429
MA = 321
29746
Ha = 221
256 n
mi
Hp = 207
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18325787
85 X = -5623289
75
Y = 6496602
16 feet Y = 1917491
02 meter
Z = 10712881
60 Z = 3238059
94
XDOT = 2227
667736 XDOT = 722
702470
YDOT = -19635
012514 feet/sec YDOT = -5976
915055 meter/sec
ZDOT = 15643
623457 ZDOT = 4771
580448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4002782
82 X = 1220048
20
Y = 19089591
86 feet Y = 5818507
60 meter
Z = 10600537
00 Z = 3231043
68
XDOT = -17786
225419 XDOT = -5421
241508
YDOT = -5007
285557 feet/sec YDOT = -1526
220638 meter/sec
ZDOT = 15658
177507 ZDOT = 4772
612504
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 12166
55753186
00016717 00000-0 10270-3 0 9036
2 25544 51
6341 135
5523 0010439 63
5589 296
6634 15
56385059 17606
Satellite: ISS
Catalog Number: 25544
Epoch time: 12166
55753186 = yrday
fracday
Element set: 903
Inclination: 51
6341 deg
RA of node: 135
5523 deg
Eccentricity:
0010439
Arg of perigee: 63
5589 deg
Mean anomaly: 296
6634 deg
Mean motion: 15
56385059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1760
Checksum: 326
Coasting Arc #5 (Orbit 1774)
---------------------------------------
Vector Time (GMT): 2012/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4770293
62 A = 6773100
83 meter
Y = 193908
50 meter E =
0021924
Z = -4825169
40 I = 51
88728
XDOT = -2878
851950 Wp = 69
39894
YDOT = 6605
774234 meter/sec RA = 129
87714 deg
ZDOT = -2582
617781 TA = 175
21914
MA = 175
19817
Ha = 221
265 n
mi
Hp = 207
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15650569
63 X = 4791210
54
Y = 636182
75 feet Y = 247370
47 meter
Z = -15830608
26 Z = -4801944
50
XDOT = -9445
052329 XDOT = -2939
959225
YDOT = 21672
487643 feet/sec YDOT = 6573
239800 meter/sec
ZDOT = -8473
155450 ZDOT = -2596
750789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2448943
77 X = 746438
06
Y = -15568164
93 feet Y = -4745176
67 meter
Z = -15734933
47 Z = -4796007
72
XDOT = 19307
285184 XDOT = 5884
860524
YDOT = 11653
925130 feet/sec YDOT = 3552
116380 meter/sec
ZDOT = -8531
983390 ZDOT = -2600
548537
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 12167
52067836
00016717 00000-0 10270-3 0 9045
2 25544 51
6344 130
7329 0010581 66
4874 293
7390 15
56365131 17759
Satellite: ISS
Catalog Number: 25544
Epoch time: 12167
52067836 = yrday
fracday
Element set: 904
Inclination: 51
6344 deg
RA of node: 130
7329 deg
Eccentricity:
0010581
Arg of perigee: 66
4874 deg
Mean anomaly: 293
7390 deg
Mean motion: 15
56365131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1775
Checksum: 318
Coasting Arc #6 (Orbit 1790)
---------------------------------------
Vector Time (GMT): 2012/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3334165
60 A = 6770743
91 meter
Y = -2512028
90 meter E =
0012873
Z = 5320173
97 I = 51
89902
XDOT = 4478
500729 Wp = 72
65379
YDOT = -6240
147426 meter/sec RA = 124
87286 deg
ZDOT = -135
710063 TA = 18
65612
MA = 18
60897
Ha = 221
336 n
mi
Hp = 207
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10938863
53 X = -3331672
17
Y = -8241564
65 feet Y = -2549300
45 meter
Z = 17454639
02 Z = 5303982
31
XDOT = 14693
243862 XDOT = 4548
605732
YDOT = -20472
924626 feet/sec YDOT = -6189
674059 meter/sec
ZDOT = -445
242989 ZDOT = -113
784175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9286774
38 X = -2830608
83
Y = 10181090
16 feet Y = 3103196
28 meter
Z = 17388150
31 Z = 5299908
21
XDOT = -18185
951783 XDOT = -5543
078103
YDOT = -15960
754898 feet/sec YDOT = -4864
838093 meter/sec
ZDOT = -354
319441 ZDOT = -107
996566
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 12168
54801772
00016717 00000-0 10270-3 0 9054
2 25544 51
6348 125
5937 0010524 69
7492 290
4793 15
56397598 17910
Satellite: ISS
Catalog Number: 25544
Epoch time: 12168
54801772 = yrday
fracday
Element set: 905
Inclination: 51
6348 deg
RA of node: 125
5937 deg
Eccentricity:
0010524
Arg of perigee: 69
7492 deg
Mean anomaly: 290
4793 deg
Mean motion: 15
56397598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1791
Checksum: 348
Coasting Arc #7 (Orbit 1805)
---------------------------------------
Vector Time (GMT): 2012/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1624865
62 A = 6773316
14 meter
Y = 4595962
84 meter E =
0020281
Z = -4720358
38 I = 51
92471
XDOT = -5288
421297 Wp = 91
70012
YDOT = 4762
319388 meter/sec RA = 119
86978 deg
ZDOT = 2826
288603 TA = 206
20944
MA = 206
31222
Ha = 221
222 n
mi
Hp = 207
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5330923
97 X = 1596282
42
Y = 15078618
23 feet Y = 4613974
03 meter
Z = -15486740
08 Z = -4712533
50
XDOT = -17350
463573 XDOT = -5355
011022
YDOT = 15624
407442 feet/sec YDOT = 4702
808211 meter/sec
ZDOT = 9272
600402 ZDOT = 2800
436559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15468431
20 X = 4714777
83
Y = -4182766
43 feet Y = -1274907
21 meter
Z = -15454924
70 Z = -4710661
05
XDOT = 13854
640701 XDOT = 4222
894486
YDOT = 17490
228708 feet/sec YDOT = 5331
021710 meter/sec
ZDOT = 9165
615309 ZDOT = 2793
679546
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 12169
51113400
00016717 00000-0 10270-3 0 9067
2 25544 51
6352 120
7750 0010491 73
1242 287
1061 15
56405258 18061
Satellite: ISS
Catalog Number: 25544
Epoch time: 12169
51113400 = yrday
fracday
Element set: 906
Inclination: 51
6352 deg
RA of node: 120
7750 deg
Eccentricity:
0010491
Arg of perigee: 73
1242 deg
Mean anomaly: 287
1061 deg
Mean motion: 15
56405258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1806
Checksum: 272
Coasting Arc #8 (Orbit 1821)
---------------------------------------
Vector Time (GMT): 2012/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 169565
36 A = 6778628
33 meter
Y = -6040792
47 meter E =
0023245
Z = 3052039
84 I = 51
95812
XDOT = 5369
111392 Wp = 87
54030
YDOT = -2367
773348 meter/sec RA = 114
88475 deg
ZDOT = -4951
383216 TA = 57
54115
MA = 57
31661
Ha = 221
178 n
mi
Hp = 207
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 556316
80 X = 222275
98
Y = -19818872
95 feet Y = -6038602
08 meter
Z = 10013254
05 Z = 3052990
59
XDOT = 17615
194857 XDOT = 5419
242031
YDOT = -7768
285262 feet/sec YDOT = -2307
451488 meter/sec
ZDOT = -16244
695592 ZDOT = -4925
178877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19745788
20 X = -6018516
24
Y = -1763805
58 feet Y = -537607
94 meter
Z = 10017749
66 Z = 3053410
09
XDOT = -6747
220085 XDOT = -2056
552682
YDOT = -16735
372115 feet/sec YDOT = -5100
941421 meter/sec
ZDOT = -16136
468119 ZDOT = -4918
395483
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 12170
53844281
00016717 00000-0 10270-3 0 9070
2 25544 51
6361 115
6351 0010503 76
7151 283
5174 15
56449314 18227
Satellite: ISS
Catalog Number: 25544
Epoch time: 12170
53844281 = yrday
fracday
Element set: 907
Inclination: 51
6361 deg
RA of node: 115
6351 deg
Eccentricity:
0010503
Arg of perigee: 76
7151 deg
Mean anomaly: 283
5174 deg
Mean motion: 15
56449314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1822
Checksum: 291
Coasting Arc #9 (Orbit 1836)
---------------------------------------
Vector Time (GMT): 2012/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1710732
87 A = 6782287
40 meter
Y = 6511388
67 meter E =
0019476
Z = -780481
30 I = 51
98251
XDOT = -4773
128251 Wp = 60
25525
YDOT = -551
658474 meter/sec RA = 109
92052 deg
ZDOT = 5980
593508 TA = 291
33954
MA = 291
54731
Ha = 221
143 n
mi
Hp = 207
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5612640
65 X = -1779626
01
Y = 21362823
72 feet Y = 6491873
13 meter
Z = -2560634
17 Z = -788958
17
XDOT = -15659
869590 XDOT = -4795
657083
YDOT = -1809
903129 feet/sec YDOT = -605
161544 meter/sec
ZDOT = 19621
369777 ZDOT = 5957
351067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21076745
83 X = 6424192
13
Y = 6592367
92 feet Y = 2009353
74 meter
Z = -2596206
86 Z = -791323
85
XDOT = -2065
740443 XDOT = -629
637687
YDOT = 14140
148666 feet/sec YDOT = 4309
917313 meter/sec
ZDOT = 19525
619411 ZDOT = 5951
408797
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 12171
50153032
00016717 00000-0 10270-3 0 9086
2 25544 51
6362 110
8170 0010447 80
3026 279
9307 15
56460904 18374
Satellite: ISS
Catalog Number: 25544
Epoch time: 12171
50153032 = yrday
fracday
Element set: 908
Inclination: 51
6362 deg
RA of node: 110
8170 deg
Eccentricity:
0010447
Arg of perigee: 80
3026 deg
Mean anomaly: 279
9307 deg
Mean motion: 15
56460904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1837
Checksum: 284
Coasting Arc #10 (Orbit 1852)
---------------------------------------
Vector Time (GMT): 2012/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2969954
68 A = 6781200
67 meter
Y = -5842501
01 meter E =
0015835
Z = -1741094
15 I = 51
98988
XDOT = 3672
386239 Wp = 108
07125
YDOT = 3555
507836 meter/sec RA = 104
96263 deg
ZDOT = -5713
966086 TA = 90
94654
MA = 90
76511
Ha = 221
118 n
mi
Hp = 207
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9743945
80 X = 3043523
79
Y = -19168310
41 feet Y = -5808877
50 meter
Z = -5712251
14 Z = -1726488
59
XDOT = 12048
511284 XDOT = 3660
111912
YDOT = 11665
051957 feet/sec YDOT = 3596
507065 meter/sec
ZDOT = -18746
607894 ZDOT = -5696
155091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18869835
51 X = -5751525
86
Y = -10343531
04 feet Y = -3152708
26 meter
Z = -5651468
01 Z = -1722567
45
XDOT = 11265
615408 XDOT = 3433
759576
YDOT = -10434
876158 feet/sec YDOT = -3180
550253 meter/sec
ZDOT = -18673
534114 ZDOT = -5691
693198
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
52880835
00016717 00000-0 10270-3 0 9098
2 25544 51
6375 105
6767 0010425 84
0198 276
2143 15
56491230 18531
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
52880835 = yrday
fracday
Element set: 909
Inclination: 51
6375 deg
RA of node: 105
6767 deg
Eccentricity:
0010425
Arg of perigee: 84
0198 deg
Mean anomaly: 276
2143 deg
Mean motion: 15
56491230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1853
Checksum: 313
Coasting Arc #11 (Orbit 1853)
---------------------------------------
Vector Time (GMT): 2012/172/13:54:15
847
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3530364
10 A = 6773490
78 meter
Y = 2575073
87 meter E =
0020665
Z = -5193598
64 I = 51
95805
XDOT = -2949
361899 Wp = 95
27834
YDOT = 6918
635064 meter/sec RA = 104
54102 deg
ZDOT = 1428
568684 TA = 188
41045
MA = 188
44514
Ha = 221
115 n
mi
Hp = 209
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11582559
39 X = 3526535
92
Y = 8448405
10 feet Y = 2614532
06 meter
Z = -17039365
60 Z = -5176457
23
XDOT = -9676
384184 XDOT = -3033
447918
YDOT = 22698
933938 feet/sec YDOT = 6885
183083 meter/sec
ZDOT = 4686
905131 ZDOT = 1414
037799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2235439
10 X = 681361
84
Y = -14245299
92 feet Y = -4341967
41 meter
Z = -16968955
57 Z = -5172137
66
XDOT = 23593
916839 XDOT = 7191
425853
YDOT = -1796
502000 feet/sec YDOT = -547
573810 meter/sec
ZDOT = 4626
322997 ZDOT = 1410
103249
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
59301454
00016717 00000-0 10270-3 0 9102
2 25544 51
6387 105
3565 0007009 84
1331 276
0621 15
55685048 18542
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
59301454 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 105
3565 deg
Eccentricity:
0007009
Arg of perigee: 84
1331 deg
Mean anomaly: 276
0621 deg
Mean motion: 15
55685048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1854
Checksum: 298
Coasting Arc #12 (Orbit 1869)
---------------------------------------
Vector Time (GMT): 2012/173/13:54:15
847
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2546290
94 A = 6777270
42 meter
Y = -4658440
53 meter E =
0017136
Z = 4200153
30 I = 51
97750
XDOT = 3873
709834 Wp = 80
04824
YDOT = -5486
307749 meter/sec RA = 99
55413 deg
ZDOT = -3720
803750 TA = 47
98915
MA = 47
84337
Ha = 221
144 n
mi
Hp = 209
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8353972
90 X = -2514413
30
Y = -15283597
54 feet Y = -4686737
15 meter
Z = 13780030
52 Z = 4187860
33
XDOT = 12709
021765 XDOT = 3952
845631
YDOT = -17999
697339 feet/sec YDOT = -5442
546473 meter/sec
ZDOT = -12207
361385 ZDOT = -3701
794220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9550826
96 X = -2911092
06
Y = 14613021
72 feet Y = 4454049
02 meter
Z = 13729812
78 Z = 4184846
94
XDOT = -20825
682000 XDOT = -6347
667874
YDOT = -2167
225516 feet/sec YDOT = -660
570337 meter/sec
ZDOT = -12128
444871 ZDOT = -3696
749997
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
62081141
00016717 00000-0 10270-3 0 9116
2 25544 51
6385 100
2203 0007007 87
5313 272
6643 15
55713360 18701
Satellite: ISS
Catalog Number: 25544
Epoch time: 12173
62081141 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 100
2203 deg
Eccentricity:
0007007
Arg of perigee: 87
5313 deg
Mean anomaly: 272
6643 deg
Mean motion: 15
55713360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1870
Checksum: 271
Coasting Arc #13 (Orbit 1884)
---------------------------------------
Vector Time (GMT): 2012/174/13:54:15
847
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1473882
32 A = 6781994
79 meter
Y = 6128422
33 meter E =
0011449
Z = -2507151
03 I = 51
99839
XDOT = -4443
578176 Wp = 73
17222
YDOT = 3242
664943 meter/sec RA = 94
58362 deg
ZDOT = 5337
344161 TA = 258
85613
MA = 258
98488
Ha = 221
014 n
mi
Hp = 209
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4835571
92 X = 1417422
56
Y = 20106372
46 feet Y = 6144588
86 meter
Z = -8225561
11 Z = -2500127
32
XDOT = -14578
668555 XDOT = -4505
435427
YDOT = 10638
664511 feet/sec YDOT = 3192
627493 meter/sec
ZDOT = 17510
971657 ZDOT = 5315
607861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15237442
73 X = 4644372
54
Y = -13997671
39 feet Y = -4266490
24 meter
Z = -8197216
58 Z = -2498511
61
XDOT = 15392
990470 XDOT = 4691
783495
YDOT = 6599
290251 feet/sec YDOT = 2011
463669 meter/sec
ZDOT = 17421
026944 ZDOT = 5309
929012
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
58435679
00016717 00000-0 10270-3 0 9122
2 25544 51
6392 95
4048 0006922 91
2763 268
9183 15
55738772 18854
Satellite: ISS
Catalog Number: 25544
Epoch time: 12174
58435679 = yrday
fracday
Element set: 912
Inclination: 51
6392 deg
RA of node: 95
4048 deg
Eccentricity:
0006922
Arg of perigee: 91
2763 deg
Mean anomaly: 268
9183 deg
Mean motion: 15
55738772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1885
Checksum: 350
Coasting Arc #14 (Orbit 1900)
---------------------------------------
Vector Time (GMT): 2012/175/13:54:15
847
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -284556
89 A = 6784686
99 meter
Y = -6764845
56 meter E =
0018722
Z = 308045
32 I = 52
00842
XDOT = 4711
491962 Wp = 119
26805
YDOT = -485
164443 meter/sec RA = 89
62774 deg
ZDOT = -6036
169836 TA = 57
42593
MA = 57
24528
Ha = 221
034 n
mi
Hp = 209
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -933585
59 X = -210386
25
Y = -22194375
20 feet Y = -6767612
98 meter
Z = 1010647
39 Z = 306842
32
XDOT = 15457
650793 XDOT = 4745
889061
YDOT = -1591
746860 feet/sec YDOT = -432
284570 meter/sec
ZDOT = -19803
706811 ZDOT = -6013
198351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18771864
72 X = -5721664
37
Y = 11878029
84 feet Y = 3620423
50 meter
Z = 1006370
97 Z = 306741
87
XDOT = -8280
209351 XDOT = -2523
807810
YDOT = -11341
800283 feet/sec YDOT = -3456
980726 meter/sec
ZDOT = -19708
940286 ZDOT = -6007
284999
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
61212495
00016717 00000-0 10270-3 0 9137
2 25544 51
6391 90
2680 0006890 96
3296 263
8643 15
55713885 19011
Satellite: ISS
Catalog Number: 25544
Epoch time: 12175
61212495 = yrday
fracday
Element set: 913
Inclination: 51
6391 deg
RA of node: 90
2680 deg
Eccentricity:
0006890
Arg of perigee: 96
3296 deg
Mean anomaly: 263
8643 deg
Mean motion: 15
55713885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1901
Checksum: 322
Coasting Arc #15 (Orbit 1916)
---------------------------------------
Vector Time (GMT): 2012/176/13:54:15
847
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -884076
01 A = 6783070
50 meter
Y = 6445348
30 meter E =
0020091
Z = 1892693
99 I = 52
00211
XDOT = -4649
617132 Wp = 76
73441
YDOT = -2310
728884 meter/sec RA = 84
67318 deg
ZDOT = 5651
392760 TA = 304
02754
MA = 304
21817
Ha = 220
918 n
mi
Hp = 209
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2900511
86 X = -965277
71
Y = 21146155
85 feet Y = 6435007
80 meter
Z = 6209625
95 Z = 1888202
65
XDOT = -15254
649383 XDOT = -4650
885473
YDOT = -7581
131510 feet/sec YDOT = -2362
731458 meter/sec
ZDOT = 18541
314831 ZDOT = 5628
802000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19656264
15 X = 5991229
31
Y = -8333183
80 feet Y = -2539954
42 meter
Z = 6190448
96 Z = 1886848
84
XDOT = 775
604936 XDOT = 236
404384
YDOT = 15645
909400 feet/sec YDOT = 4768
873185 meter/sec
ZDOT = 18448
399572 ZDOT = 5623
072190
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
63987634
00016717 00000-0 10270-3 0 9145
2 25544 51
6389 85
1310 0006778 97
9099 262
2824 15
55764814 19173
Satellite: ISS
Catalog Number: 25544
Epoch time: 12176
63987634 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 85
1310 deg
Eccentricity:
0006778
Arg of perigee: 97
9099 deg
Mean anomaly: 262
2824 deg
Mean motion: 15
55764814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1917
Checksum: 352
Coasting Arc #16 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2012/177/13:54:15
847
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2086674
61 A = 6778396
64 meter
Y = -5206713
40 meter E =
0012329
Z = -3816247
35 I = 51
98259
XDOT = 4230
192011 Wp = 89
78490
YDOT = 4786
958026 meter/sec RA = 79
70691 deg
ZDOT = -4229
815263 TA = 135
77628
MA = 135
67767
Ha = 220
804 n
mi
Hp = 209
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6846045
32 X = 2163280
42
Y = -17082393
05 feet Y = -5182950
24 meter
Z = -12520496
54 Z = -3805924
83
XDOT = 13878
582713 XDOT = 4196
896239
YDOT = 15705
242867 feet/sec YDOT = 4834
076873 meter/sec
ZDOT = -13877
346662 ZDOT = -4209
345732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18162777
06 X = -5536014
45
Y = 3141251
68 feet Y = 957453
51 meter
Z = -12477395
16 Z = -3803110
04
XDOT = 6193
387134 XDOT = 1887
744398
YDOT = -18825
449583 feet/sec YDOT = -5737
997033 meter/sec
ZDOT = -13793
434300 ZDOT = -4204
238775
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
60337951
00016717 00000-0 10270-3 0 9155
2 25544 51
6386 80
3149 0006576 102
4769 257
7120 15
55779389 19327
Satellite: ISS
Catalog Number: 25544
Epoch time: 12177
60337951 = yrday
fracday
Element set: 915
Inclination: 51
6386 deg
RA of node: 80
3149 deg
Eccentricity:
0006576
Arg of perigee: 102
4769 deg
Mean anomaly: 257
7120 deg
Mean motion: 15
55779389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1932
Checksum: 336
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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