[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 10th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17760 45 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 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
292/16:06:53
238 -3
0 5
6 5
6
N/A -4
3 0
0 215
0
000/00:01:46
475 -2
0 0
0 204
8
Coasting Arc #1 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2011/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5623821
01 A = 6767247
33 meter
Y = 2239058
75 meter E =
0012076
Z = -3025380
23 I = 51
40384
XDOT = 312
478556 Wp = 303
94317
YDOT = -5885
538119 meter/sec RA = 314
77919 deg
ZDOT = -4915
970743 TA = 270
94826
MA = 271
08662
Ha = 212
375 n
mi
Hp = 205
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18450856
34 X = -5633743
87
Y = 7345993
29 feet Y = 2176113
97 meter
Z = -9925788
17 Z = -3052725
08
XDOT = 1025
192114 XDOT = 402
149485
YDOT = -19309
508266 feet/sec YDOT = -5881
542879 meter/sec
ZDOT = -16128
512936 ZDOT = -4914
234356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15863686
75 X = 4835251
72
Y = -11853932
06 feet Y = -3613078
49 meter
Z = -10037266
82 Z = -3059358
93
XDOT = 3047
899301 XDOT = 928
999707
YDOT = 17786
305643 feet/sec YDOT = 5421
265960 meter/sec
ZDOT = -16121
096932 ZDOT = -4913
710345
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 11280
52572994
00016717 00000-0 10270-3 0 9002
2 25544 51
6409 315
2221 0016443 299
7450 60
2069 15
60371428 18455
Satellite: ISS
Catalog Number: 25544
Epoch time: 11280
52572994 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 315
2221 deg
Eccentricity:
0016443
Arg of perigee: 299
7450 deg
Mean anomaly: 60
2069 deg
Mean motion: 15
60371428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1845
Checksum: 301
Coasting Arc #2 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2011/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4183703
65 A = 6759804
31 meter
Y = 1385881
70 meter E =
0011886
Z = 5132793
44 I = 51
35714
XDOT = -3882
654106 Wp = 302
81068
YDOT = 6461
711324 meter/sec RA = 309
71611 deg
ZDOT = 1428
761192 TA = 133
44586
MA = 133
34691
Ha = 212
544 n
mi
Hp = 204
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13726061
85 X = 4142961
23
Y = 4546855
98 feet Y = 1432439
19 meter
Z = 16839873
50 Z = 5153018
83
XDOT = -12738
366490 XDOT = -3961
562351
YDOT = 21199
840302 feet/sec YDOT = 6417
852060 meter/sec
ZDOT = 4687
536719 ZDOT = 1409
706837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14349757
60 X = -4373806
12
Y = -620788
41 feet Y = -189216
31 meter
Z = 16922147
95 Z = 5157870
69
XDOT = 6390
768533 XDOT = 1947
906249
YDOT = -22849
235093 feet/sec YDOT = -6964
446856 meter/sec
ZDOT = 4609
579057 ZDOT = 1404
999697
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 11281
55043919
00016717 00000-0 10270-3 0 9017
2 25544 51
6395 310
0647 0016362 303
8471 56
1127 15
60398850 18619
Satellite: ISS
Catalog Number: 25544
Epoch time: 11281
55043919 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 310
0647 deg
Eccentricity:
0016362
Arg of perigee: 303
8471 deg
Mean anomaly: 56
1127 deg
Mean motion: 15
60398850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 300
Coasting Arc #3 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2011/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1320270
17 A = 6761660
27 meter
Y = -4685632
63 meter E =
0007020
Z = -4687417
16 I = 51
34580
XDOT = 5692
358366 Wp = 336
33607
YDOT = -4358
938964 meter/sec RA = 304
63158 deg
ZDOT = 2758
843529 TA = 321
01740
MA = 321
06798
Ha = 212
819 n
mi
Hp = 204
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4331595
05 X = -1245005
58
Y = -15372810
48 feet Y = -4699976
41 meter
Z = -15378665
22 Z = -4693647
73
XDOT = 18675
716423 XDOT = 5727
275742
YDOT = -14300
980854 feet/sec YDOT = -4295
087978 meter/sec
ZDOT = 9051
323915 ZDOT = 2786
582515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8540603
38 X = 2603175
91
Y = 13467418
07 feet Y = 4104869
03 meter
Z = -15403769
22 Z = -4695068
86
XDOT = -12654
966805 XDOT = -3857
233882
YDOT = 18489
249929 feet/sec YDOT = 5635
523378 meter/sec
ZDOT = 9164
514030 ZDOT = 2793
343876
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 11282
51108116
00016717 00000-0 10270-3 0 9026
2 25544 51
6404 305
2303 0016481 307
5278 52
4379 15
60419779 18761
Satellite: ISS
Catalog Number: 25544
Epoch time: 11282
51108116 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 305
2303 deg
Eccentricity:
0016481
Arg of perigee: 307
5278 deg
Mean anomaly: 52
4379 deg
Mean motion: 15
60419779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1876
Checksum: 301
Coasting Arc #4 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2011/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1791143
58 A = 6769374
66 meter
Y = 6246445
12 meter E =
0005421
Z = 1908428
52 I = 51
35437
XDOT = -5251
515797 Wp = 6
68300
YDOT = 202
997416 meter/sec RA = 299
58166 deg
ZDOT = -5586
312669 TA = 152
16824
MA = 152
13923
Ha = 213
032 n
mi
Hp = 204
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5876455
32 X = -1870130
35
Y = 20493586
34 feet Y = 6225974
03 meter
Z = 6261248
44 Z = 1899534
48
XDOT = -17229
382535 XDOT = -5226
257830
YDOT = 666
002022 feet/sec YDOT = 144
412339 meter/sec
ZDOT = -18327
797471 ZDOT = -5611
763495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -690718
79 X = -210531
09
Y = -21318986
90 feet Y = -6498027
21 meter
Z = 6224688
36 Z = 1897285
01
XDOT = 14525
412005 XDOT = 4427
345579
YDOT = -5858
836984 feet/sec YDOT = -1785
773513 meter/sec
ZDOT = -18431
432079 ZDOT = -5617
900498
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 11283
53574105
00016717 00000-0 10270-3 0 9035
2 25544 51
6388 300
0728 0016365 311
7648 48
2109 15
60484495 18924
Satellite: ISS
Catalog Number: 25544
Epoch time: 11283
53574105 = yrday
fracday
Element set: 903
Inclination: 51
6388 deg
RA of node: 300
0728 deg
Eccentricity:
0016365
Arg of perigee: 311
7648 deg
Mean anomaly: 48
2109 deg
Mean motion: 15
60484495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 313
Coasting Arc #5 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2011/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3974220
15 A = 6769350
76 meter
Y = -5145252
91 meter E =
0017297
Z = 1844984
45 I = 51
34043
XDOT = 2976
747971 Wp = 4
21557
YDOT = 4311
122950 meter/sec RA = 294
56073 deg
ZDOT = 5624
255619 TA = 16
24810
MA = 16
19271
Ha = 213
160 n
mi
Hp = 204
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13038780
03 X = 4022497
26
Y = -16880751
00 feet Y = -5100540
61 meter
Z = 6053098
57 Z = 1864409
32
XDOT = 9766
233501 XDOT = 2900
996859
YDOT = 14144
104168 feet/sec YDOT = 4343
987826 meter/sec
ZDOT = 18452
282216 ZDOT = 5638
532419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6819640
02 X = -2078626
28
Y = 20186502
56 feet Y = 6152845
98 meter
Z = 6132468
18 Z = 1869176
30
XDOT = -12250
865555 XDOT = -3734
063821
YDOT = -9748
562209 feet/sec YDOT = -2971
361761 meter/sec
ZDOT = 18510
171188 ZDOT = 5641
900178
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 11284
56037516
00016717 00000-0 10270-3 0 9040
2 25544 51
6387 294
9150 0016407 315
6159 44
3681 15
60510376 19088
Satellite: ISS
Catalog Number: 25544
Epoch time: 11284
56037516 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 294
9150 deg
Eccentricity:
0016407
Arg of perigee: 315
6159 deg
Mean anomaly: 44
3681 deg
Mean motion: 15
60510376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 312
Coasting Arc #6 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2011/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4581567
95 A = 6761347
01 meter
Y = 1752526
87 meter E =
0015975
Z = -4660225
77 I = 51
30195
XDOT = 142
290393 Wp = 358
00958
YDOT = -7138
796500 meter/sec RA = 289
50874 deg
ZDOT = -2808
510280 TA = 243
93812
MA = 244
10265
Ha = 213
364 n
mi
Hp = 204
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15031390
92 X = -4578185
57
Y = 5749760
06 feet Y = 1701311
43 meter
Z = -15289454
64 Z = -4682475
40
XDOT = 466
831997 XDOT = 235
750738
YDOT = -23421
248359 feet/sec YDOT = -7136
683025 meter/sec
ZDOT = -9214
272571 ZDOT = -2807
591316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12085618
83 X = 3683696
62
Y = -10495671
65 feet Y = -3199080
72 meter
Z = -15380135
60 Z = -4687865
33
XDOT = 6724
986407 XDOT = 2049
775857
YDOT = 21316
533412 feet/sec YDOT = 6497
279384 meter/sec
ZDOT = -9210
141358 ZDOT = -2807
251086
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 11285
52094525
00016717 00000-0 10270-3 0 9051
2 25544 51
6382 290
0795 0016379 319
2263 40
7667 15
60550189 19236
Satellite: ISS
Catalog Number: 25544
Epoch time: 11285
52094525 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 290
0795 deg
Eccentricity:
0016379
Arg of perigee: 319
2263 deg
Mean anomaly: 40
7667 deg
Mean motion: 15
60550189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 321
Coasting Arc #7 (Orbit 1938)
---------------------------------------
Vector Time (GMT): 2011/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3565116
96 A = 6759322
86 meter
Y = 2616884
45 meter E =
0016907
Z = 5120498
50 I = 51
28570
XDOT = -2978
169776 Wp = 338
76011
YDOT = 6920
000634 meter/sec RA = 284
41694 deg
ZDOT = -1449
009472 TA = 125
32740
MA = 125
16922
Ha = 213
536 n
mi
Hp = 203
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11696577
97 X = 3510714
50
Y = 8585578
91 feet Y = 2656448
01 meter
Z = 16799535
75 Z = 5137685
84
XDOT = -9770
898215 XDOT = -3048
290063
YDOT = 22703
414154 feet/sec YDOT = 6886
304734 meter/sec
ZDOT = -4753
968085 ZDOT = -1463
648605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13895867
63 X = -4235460
45
Y = -3882752
27 feet Y = -1183462
89 meter
Z = 16869368
71 Z = 5141783
58
XDOT = 714
706142 XDOT = 217
842432
YDOT = -23671
630751 feet/sec YDOT = -7215
113053 meter/sec
ZDOT = -4813
943741 ZDOT = -1467
290052
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 11286
54552739
00016717 00000-0 10270-3 0 9061
2 25544 51
6375 284
9206 0016411 323
0953 36
9073 15
60592219 19398
Satellite: ISS
Catalog Number: 25544
Epoch time: 11286
54552739 = yrday
fracday
Element set: 906
Inclination: 51
6375 deg
RA of node: 284
9206 deg
Eccentricity:
0016411
Arg of perigee: 323
0953 deg
Mean anomaly: 36
9073 deg
Mean motion: 15
60592219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1939
Checksum: 323
Coasting Arc #8 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2011/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1430820
29 A = 6766745
88 meter
Y = -5902725
79 meter E =
0016150
Z = -2959419
93 I = 51
30450
XDOT = 4626
152857 Wp = 342
96238
YDOT = -3607
546717 meter/sec RA = 279
34758 deg
ZDOT = 4967
119847 TA = 342
89714
MA = 342
95150
Ha = 213
704 n
mi
Hp = 203
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4694292
29 X = -1350331
87
Y = -19365898
27 feet Y = -5918276
25 meter
Z = -9709382
98 Z = -2966175
12
XDOT = 15177
666855 XDOT = 4642
019431
YDOT = -11835
783193 feet/sec YDOT = -3555
725215 meter/sec
ZDOT = 16296
324958 ZDOT = 4989
632947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11523170
69 X = 3512262
43
Y = 16240760
49 feet Y = 4950183
80 meter
Z = -9736567
65 Z = -2967705
82
XDOT = -8393
710533 XDOT = -2558
402970
YDOT = 15764
143213 feet/sec YDOT = 4804
910851 meter/sec
ZDOT = 16388
178276 ZDOT = 4995
116739
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 11287
50604833
00016717 00000-0 10270-3 0 9072
2 25544 51
6377 280
0855 0016415 327
0440 32
9692 15
60621516 19549
Satellite: ISS
Catalog Number: 25544
Epoch time: 11287
50604833 = yrday
fracday
Element set: 907
Inclination: 51
6377 deg
RA of node: 280
0855 deg
Eccentricity:
0016415
Arg of perigee: 327
0440 deg
Mean anomaly: 32
9692 deg
Mean motion: 15
60621516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 305
Coasting Arc #9 (Orbit 1969)
---------------------------------------
Vector Time (GMT): 2011/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1097005
38 A = 6770099
74 meter
Y = 6643593
32 meter E =
0006474
Z = -741185
66 I = 51
31216
XDOT = -4651
335994 Wp = 348
27682
YDOT = -1430
928513 meter/sec RA = 274
31918 deg
ZDOT = -5926
420198 TA = 199
78094
MA = 199
80606
Ha = 213
903 n
mi
Hp = 203
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3599099
02 X = -1167613
19
Y = 21796566
02 feet Y = 6630931
11 meter
Z = -2431711
47 Z = -746686
83
XDOT = -15260
288694 XDOT = -4606
199286
YDOT = -4694
647352 feet/sec YDOT = -1482
690496 meter/sec
ZDOT = -19443
635819 ZDOT = -5948
907154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5172465
06 X = -1576567
35
Y = -21475060
70 feet Y = -6545598
50 meter
Z = -2454464
86 Z = -748120
89
XDOT = 14210
955626 XDOT = 4331
499275
YDOT = -1184
389229 feet/sec YDOT = -361
001837 meter/sec
ZDOT = -19535
114580 ZDOT = -5954
302924
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 11288
53057713
00016717 00000-0 10270-3 0 9086
2 25544 51
6373 274
9264 0016449 331
0078 29
0163 15
60681068 19706
Satellite: ISS
Catalog Number: 25544
Epoch time: 11288
53057713 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 274
9264 deg
Eccentricity:
0016449
Arg of perigee: 331
0078 deg
Mean anomaly: 29
0163 deg
Mean motion: 15
60681068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 316
Coasting Arc #10 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2011/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3205170
79 A = 6763025
89 meter
Y = -4339683
97 meter E =
0012721
Z = 4066834
52 I = 51
28763
XDOT = 3135
467548 Wp = 13
86116
YDOT = 5885
722646 meter/sec RA = 269
27812 deg
ZDOT = 3819
143923 TA = 36
62192
MA = 36
53503
Ha = 213
870 n
mi
Hp = 203
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10515652
21 X = 3233703
45
Y = -14237808
31 feet Y = -4303682
13 meter
Z = 13342632
95 Z = 4082474
98
XDOT = 10286
967020 XDOT = 3050
866137
YDOT = 19310
113668 feet/sec YDOT = 5920
312452 meter/sec
ZDOT = 12529
999747 ZDOT = 3834
170628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3782250
20 X = -1152829
86
Y = 17241783
44 feet Y = 5255295
59 meter
Z = 13406545
73 Z = 4086315
14
XDOT = -15893
983770 XDOT = -4844
486253
YDOT = -13252
194490 feet/sec YDOT = -4039
268880 meter/sec
ZDOT = 12590
872078 ZDOT = 3837
697809
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 11289
55507620
00016717 00000-0 10270-3 0 9097
2 25544 51
6371 269
7680 0016455 334
0713 25
9617 15
60737993 19869
Satellite: ISS
Catalog Number: 25544
Epoch time: 11289
55507620 = yrday
fracday
Element set: 909
Inclination: 51
6371 deg
RA of node: 269
7680 deg
Eccentricity:
0016455
Arg of perigee: 334
0713 deg
Mean anomaly: 25
9617 deg
Mean motion: 15
60737993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 340
Coasting Arc #11 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2011/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4236866
19 A = 6758173
89 meter
Y = 116240
86 meter E =
0017121
Z = -5270888
08 I = 51
27290
XDOT = -547
462711 Wp = 30
92390
YDOT = -7648
762349 meter/sec RA = 264
19065 deg
ZDOT = 286
242858 TA = 241
73027
MA = 241
90316
Ha = 214
086 n
mi
Hp = 202
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13900479
63 X = -4212245
68
Y = 381367
66 feet Y = 68999
17 meter
Z = -17292939
89 Z = -5291411
31
XDOT = -1796
137504 XDOT = -463
282595
YDOT = -25094
364661 feet/sec YDOT = -7654
413729 meter/sec
ZDOT = 939
116987 ZDOT = 283
787896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12358420
15 X = 3766846
46
Y = -6143347
32 feet Y = -1872492
26 meter
Z = -17376515
20 Z = -5296361
83
XDOT = 11733
490007 XDOT = 3576
367754
YDOT = 21112
055128 feet/sec YDOT = 6434
954403 meter/sec
ZDOT = 929
519619 ZDOT = 283
317580
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 11290
51551957
00016717 00000-0 10270-3 0 9109
2 25544 51
6371 264
9317 0016427 338
2636 21
7822 15
60746756 20010
Satellite: ISS
Catalog Number: 25544
Epoch time: 11290
51551957 = yrday
fracday
Element set: 910
Inclination: 51
6371 deg
RA of node: 264
9317 deg
Eccentricity:
0016427
Arg of perigee: 338
2636 deg
Mean anomaly: 21
7822 deg
Mean motion: 15
60746756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 303
Coasting Arc #12 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2011/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3821655
03 A = 6764073
06 meter
Y = 4190357
77 meter E =
0018061
Z = 3695530
76 I = 51
29735
XDOT = -2344
451384 Wp = 21
07192
YDOT = 5924
972664 meter/sec RA = 259
10745 deg
ZDOT = -4270
751818 TA = 114
53624
MA = 114
34786
Ha = 214
246 n
mi
Hp = 202
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12538238
28 X = 3756561
13
Y = 13747892
93 feet Y = 4232729
98 meter
Z = 12124444
76 Z = 3713938
39
XDOT = -7691
769632 XDOT = -2389
784537
YDOT = 19438
886693 feet/sec YDOT = 5898
502003 meter/sec
ZDOT = -14011
652946 ZDOT = -4282
251561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17210681
49 X = -5245815
72
Y = -6941638
02 feet Y = -2115811
27 meter
Z = 12199190
32 Z = 3718313
21
XDOT = -2131
169471 XDOT = -649
580455
YDOT = -19555
312562 feet/sec YDOT = -5960
459269 meter/sec
ZDOT = -14058
785474 ZDOT = -4285
117813
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 11291
53996217
00016717 00000-0 10270-3 0 9115
2 25544 51
6370 259
7728 0016529 341
8258 18
2305 15
60812625 20173
Satellite: ISS
Catalog Number: 25544
Epoch time: 11291
53996217 = yrday
fracday
Element set: 911
Inclination: 51
6370 deg
RA of node: 259
7728 deg
Eccentricity:
0016529
Arg of perigee: 341
8258 deg
Mean anomaly: 18
2305 deg
Mean motion: 15
60812625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2017
Checksum: 312
Coasting Arc #13 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2011/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1982750
98 A = 6769827
22 meter
Y = -6453611
73 meter E =
0024693
Z = -169372
33 I = 51
32379
XDOT = 4553
157945 Wp = 9
75729
YDOT = -1552
404499 meter/sec RA = 254
07208 deg
ZDOT = 6001
945335 TA = 348
40179
MA = 348
45857
Ha = 214
249 n
mi
Hp = 202
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6505088
51 X = -1909615
27
Y = -21173266
84 feet Y = -6475375
15 meter
Z = -555683
51 Z = -178826
79
XDOT = 14938
182234 XDOT = 4541
022172
YDOT = -5093
190614 feet/sec YDOT = -1501
555974 meter/sec
ZDOT = 19691
421702 ZDOT = 6024
035366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15356297
01 X = 4680599
33
Y = 15961317
49 feet Y = 4865009
57 meter
Z = -593864
97 Z = -181010
04
XDOT = -9762
870471 XDOT = -2975
722920
YDOT = 10111
454990 feet/sec YDOT = 3081
971481 meter/sec
ZDOT = 19781
461171 ZDOT = 6029
389365
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 11292
50035023
00016717 00000-0 10270-3 0 9123
2 25544 51
6369 254
9365 0016351 345
6815 14
3875 15
60860873 20323
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
50035023 = yrday
fracday
Element set: 912
Inclination: 51
6369 deg
RA of node: 254
9365 deg
Eccentricity:
0016351
Arg of perigee: 345
6815 deg
Mean anomaly: 14
3875 deg
Mean motion: 15
60860873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 300
Coasting Arc #14 (Orbit 2034)
---------------------------------------
Vector Time (GMT): 2011/292/16:07:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2881717
96 A = 6762845
49 meter
Y = 3793547
37 meter E =
0017845
Z = -4809824
61 I = 51
29555
XDOT = -3909
907027 Wp = 10
63187
YDOT = -6118
991576 meter/sec RA = 253
22396 deg
ZDOT = -2467
766431 TA = 234
93354
MA = 235
10104
Ha = 215
045 n
mi
Hp = 204
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9454455
27 X = -2900558
49
Y = 12446021
54 feet Y = 3761216
73 meter
Z = -15780264
46 Z = -4823870
01
XDOT = -12827
778959 XDOT = -3829
204582
YDOT = -20075
431681 feet/sec YDOT = -6162
263398 meter/sec
ZDOT = -8096
346558 ZDOT = -2486
564720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12269374
09 X = -3739705
22
Y = -9588436
03 feet Y = -2922555
30 meter
Z = -15837653
77 Z = -4827316
87
XDOT = 19610
362748 XDOT = 5977
238566
YDOT = -11509
172512 feet/sec YDOT = -3507
995782 meter/sec
ZDOT = -8172
600015 ZDOT = -2491
008484
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 11292
69243050
00016717 00000-0 10270-3 0 9135
2 25544 51
6406 253
9706 0016031 330
7230 29
3026 15
59840611 20357
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
69243050 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 253
9706 deg
Eccentricity:
0016031
Arg of perigee: 330
7230 deg
Mean anomaly: 29
3026 deg
Mean motion: 15
59840611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2035
Checksum: 276
Coasting Arc #15 (Orbit 2050)
---------------------------------------
Vector Time (GMT): 2011/293/16:07:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4447043
12 A = 6761395
67 meter
Y = 114590
95 meter E =
0017494
Z = 5098558
88 I = 51
30071
XDOT = 1606
691957 Wp = 349
79542
YDOT = 7340
294850 meter/sec RA = 248
13981 deg
ZDOT = -1550
239915 TA = 115
30011
MA = 115
11876
Ha = 215
089 n
mi
Hp = 204
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14590036
47 X = 4420663
14
Y = 375954
56 feet Y = 164173
24 meter
Z = 16727555
38 Z = 5120098
71
XDOT = 5271
299073 XDOT = 1532
022768
YDOT = 24082
332184 feet/sec YDOT = 7357
844294 meter/sec
ZDOT = -5086
088961 ZDOT = -1542
616252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -396493
14 X = -120851
11
Y = 14488299
31 feet Y = 4416033
63 meter
Z = 16815278
52 Z = 5125296
89
XDOT = -23032
760520 XDOT = -7020
385406
YDOT = 5298
066759 feet/sec YDOT = 1614
850748 meter/sec
ZDOT = -5055
392630 ZDOT = -1540
883674
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 11293
71749243
00016717 00000-0 10270-3 0 9145
2 25544 51
6401 248
8156 0016077 334
0158 26
0189 15
59900803 20512
Satellite: ISS
Catalog Number: 25544
Epoch time: 11293
71749243 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 248
8156 deg
Eccentricity:
0016077
Arg of perigee: 334
0158 deg
Mean anomaly: 26
0189 deg
Mean motion: 15
59900803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2051
Checksum: 301
Coasting Arc #16 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2011/294/16:07:46
475
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4685007
87 A = 6768418
77 meter
Y = -3767536
83 meter E =
0016028
Z = -3088788
96 I = 51
33697
XDOT = 1438
721850 Wp = 354
10785
YDOT = -5769
309222 meter/sec RA = 243
07702 deg
ZDOT = 4868
296842 TA = 330
07101
MA = 330
16256
Ha = 215
214 n
mi
Hp = 204
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15370760
73 X = -4627525
42
Y = -12360685
14 feet Y = -3819606
26 meter
Z = -10133822
04 Z = -3111409
05
XDOT = 4720
216043 XDOT = 1479
478965
YDOT = -18928
179863 feet/sec YDOT = -5752
992357 meter/sec
ZDOT = 15972
102500 ZDOT = 4875
385579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12117113
56 X = 3693296
21
Y = -15503230
23 feet Y = -4725384
57 meter
Z = -10225780
32 Z = -3116817
84
XDOT = 17867
740277 XDOT = 5446
087237
YDOT = 3439
715806 feet/sec YDOT = 1048
425378 meter/sec
ZDOT = 16001
244993 ZDOT = 4877
179474
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 11294
67846325
00016717 00000-0 10270-3 0 9151
2 25544 51
6404 243
9828 0016042 337
6989 22
3467 15
59908476 20668
Satellite: ISS
Catalog Number: 25544
Epoch time: 11294
67846325 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 243
9828 deg
Eccentricity:
0016042
Arg of perigee: 337
6989 deg
Mean anomaly: 22
3467 deg
Mean motion: 15
59908476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2066
Checksum: 343
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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