[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 21st 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 109 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 101 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
299/12:43:09
828 -5
8 7
3 7
3
N/A -4
4 -0
0 218
2
000/00:02:19
656 -0
3 0
0 204
8
Coasting Arc #1 (Orbit 2035)
---------------------------------------
Vector Time (GMT): 2011/292/17:21:47
765
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2222465
51 A = 6772844
56 meter
Y = 6395952
69 meter E =
0008040
Z = 311159
95 I = 51
33034
XDOT = -4438
607112 Wp = 5
21443
YDOT = 1833
959268 meter/sec RA = 252
94629 deg
ZDOT = -5974
498308 TA = 171
41485
MA = 171
40109
Ha = 216
034 n
mi
Hp = 204
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7291553
52 X = 2149267
96
Y = 20984096
75 feet Y = 6420396
40 meter
Z = 1020865
98 Z = 321778
79
XDOT = -14562
359292 XDOT = -4429
761603
YDOT = 6016
926731 feet/sec YDOT = 1784
373309 meter/sec
ZDOT = -19601
372402 ZDOT = -5996
039840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17823945
95 X = -5432738
73
Y = 13255811
09 feet Y = 4040371
22 meter
Z = 1063794
93 Z = 324244
69
XDOT = -9112
653229 XDOT = -2777
536704
YDOT = -10667
849583 feet/sec YDOT = -3251
560553 meter/sec
ZDOT = -19689
192998 ZDOT = -6001
266026
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
75613047
00016717 00000-0 10270-3 0 9005
2 25544 51
6419 253
6552 0018653 331
8740 28
1406 15
59797036 20369
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
75613047 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 253
6552 deg
Eccentricity:
0018653
Arg of perigee: 331
8740 deg
Mean anomaly: 28
1406 deg
Mean motion: 15
59797036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2036
Checksum: 308
Coasting Arc #2 (Orbit 2051)
---------------------------------------
Vector Time (GMT): 2011/293/17:21:47
765
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 241587
49 A = 6768628
33 meter
Y = -5999850
86 meter E =
0019108
Z = 3097287
48 I = 51
32627
XDOT = 5300
358472 Wp = 16
10214
YDOT = 2716
999836 meter/sec RA = 247
92161 deg
ZDOT = 4860
621419 TA = 19
85475
MA = 19
78048
Ha = 216
186 n
mi
Hp = 203
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 792609
87 X = 293614
86
Y = -19684550
07 feet Y = -5996858
24 meter
Z = 10161704
32 Z = 3098587
77
XDOT = 17389
627534 XDOT = 5245
970293
YDOT = 8914
041456 feet/sec YDOT = 2775
967818 meter/sec
ZDOT = 15946
920666 ZDOT = 4886
238531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18900993
32 X = 5761022
77
Y = -5545147
65 feet Y = -1690161
01 meter
Z = 10167288
99 Z = 3098989
68
XDOT = -3378
676465 XDOT = -1029
820586
YDOT = 17848
739862 feet/sec YDOT = 5440
295910 meter/sec
ZDOT = 16051
125047 ZDOT = 4892
382914
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
78118733
00016717 00000-0 10270-3 0 9012
2 25544 51
6416 248
4998 0018859 336
0765 23
9512 15
59852748 20525
Satellite: ISS
Catalog Number: 25544
Epoch time: 11293
78118733 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 248
4998 deg
Eccentricity:
0018859
Arg of perigee: 336
0765 deg
Mean anomaly: 23
9512 deg
Mean motion: 15
59852748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2052
Checksum: 341
Coasting Arc #3 (Orbit 2066)
---------------------------------------
Vector Time (GMT): 2011/294/17:21:47
765
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2842562
80 A = 6761314
24 meter
Y = 3416865
61 meter E =
0021468
Z = -5105611
88 I = 51
31437
XDOT = -4473
545720 Wp = 18
19788
YDOT = -6037
900033 meter/sec RA = 242
85920 deg
ZDOT = -1531
826888 TA = 236
87302
MA = 237
07923
Ha = 216
239 n
mi
Hp = 203
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9325993
43 X = -2855757
24
Y = 11210188
99 feet Y = 3385004
22 meter
Z = -16750695
13 Z = -5119453
43
XDOT = -14676
987271 XDOT = -4398
254844
YDOT = -19809
383312 feet/sec YDOT = -6087
505088 meter/sec
ZDOT = -5025
678765 ZDOT = -1553
376280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13642540
30 X = -4158246
28
Y = -4962489
16 feet Y = -1512566
70 meter
Z = -16807232
78 Z = -5122844
55
XDOT = 13435
362910 XDOT = 4095
098615
YDOT = -19415
337028 feet/sec YDOT = -5917
794726 meter/sec
ZDOT = -5113
170653 ZDOT = -1558
494415
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
74214919
00016717 00000-0 10270-3 0 9023
2 25544 51
6410 243
6674 0018851 339
1880 20
8506 15
59936537 20675
Satellite: ISS
Catalog Number: 25544
Epoch time: 11294
74214919 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 243
6674 deg
Eccentricity:
0018851
Arg of perigee: 339
1880 deg
Mean anomaly: 20
8506 deg
Mean motion: 15
59936537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2067
Checksum: 322
Coasting Arc #4 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2011/295/17:21:47
765
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4768599
62 A = 6762424
30 meter
Y = 380680
91 meter E =
0021541
Z = 4787795
63 I = 51
33396
XDOT = 2000
458797 Wp = 1
91134
YDOT = 6961
993224 meter/sec RA = 237
77580 deg
ZDOT = -2524
492401 TA = 113
13061
MA = 112
90348
Ha = 216
275 n
mi
Hp = 202
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15645011
89 X = 4740729
86
Y = 1248953
13 feet Y = 433850
88 meter
Z = 15707990
92 Z = 4810894
01
XDOT = 6563
185031 XDOT = 1934
723398
YDOT = 22841
185118 feet/sec YDOT = 6983
995826 meter/sec
ZDOT = -8282
455385 ZDOT = -2514
934315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4261842
56 X = 1299009
61
Y = 15006625
90 feet Y = 4574019
57 meter
Z = 15802061
15 Z = 4816468
24
XDOT = -17996
610450 XDOT = -5485
366865
YDOT = 13865
627150 feet/sec YDOT = 4226
243155 meter/sec
ZDOT = -8243
836953 ZDOT = -2512
721503
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 11295
76714616
00016717 00000-0 10270-3 0 9036
2 25544 51
6413 238
5119 0018824 342
6857 17
3654 15
60000562 20833
Satellite: ISS
Catalog Number: 25544
Epoch time: 11295
76714616 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 238
5119 deg
Eccentricity:
0018824
Arg of perigee: 342
6857 deg
Mean anomaly: 17
3654 deg
Mean motion: 15
60000562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 303
Coasting Arc #5 (Orbit 2097)
---------------------------------------
Vector Time (GMT): 2011/296/17:21:47
765
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5139413
68 A = 6770046
69 meter
Y = -3747747
02 meter E =
0022409
Z = -2277699
83 I = 51
37571
XDOT = 1441
282678 Wp = 359
18998
YDOT = -5258
296416 meter/sec RA = 232
72509 deg
ZDOT = 5421
285511 TA = 335
24623
MA = 335
35359
Ha = 216
404 n
mi
Hp = 202
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16861593
44 X = -5086058
84
Y = -12295757
94 feet Y = -3804920
98 meter
Z = -7472768
47 Z = -2302537
52
XDOT = 4728
617709 XDOT = 1473
638844
YDOT = -17251
628660 feet/sec YDOT = -5241
997692 meter/sec
ZDOT = 17786
369786 ZDOT = 5428
366448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5300251
53 X = 1615516
66
Y = -20146624
07 feet Y = -6140691
02 meter
Z = -7573779
63 Z = -2308488
03
XDOT = 16277
229562 XDOT = 4961
299570
YDOT = -2389
147213 feet/sec YDOT = -728
212071 meter/sec
ZDOT = 17815
446297 ZDOT = 5430
148031
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 11296
72805459
00016717 00000-0 10270-3 0 9040
2 25544 51
6405 233
6783 0018823 346
1383 13
9254 15
59995748 20980
Satellite: ISS
Catalog Number: 25544
Epoch time: 11296
72805459 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 233
6783 deg
Eccentricity:
0018823
Arg of perigee: 346
1383 deg
Mean anomaly: 13
9254 deg
Mean motion: 15
59995748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2098
Checksum: 344
Coasting Arc #6 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2011/297/17:21:47
765
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3636239
65 A = 6771476
56 meter
Y = 5566549
73 meter E =
0011472
Z = -1322597
15 I = 51
39983
XDOT = -4712
420250 Wp = 11
07607
YDOT = 1699
722411 meter/sec RA = 227
70925 deg
ZDOT = -5799
484811 TA = 183
37992
MA = 183
38768
Ha = 216
548 n
mi
Hp = 202
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11929920
10 X = 3580148
20
Y = 18262958
43 feet Y = 5606898
64 meter
Z = -4339229
51 Z = -1305068
70
XDOT = -15460
696358 XDOT = -4702
903220
YDOT = 5576
517096 feet/sec YDOT = 1647
077923 meter/sec
ZDOT = -19027
181137 ZDOT = -5822
355243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12322234
83 X = -3755817
18
Y = 18017593
95 feet Y = 5491762
64 meter
Z = -4268066
75 Z = -1300906
74
XDOT = -9693
080306 XDOT = -2954
450877
YDOT = -11160
508822 feet/sec YDOT = -3401
723089 meter/sec
ZDOT = -19120
422155 ZDOT = -5827
904673
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 11297
75299311
00016717 00000-0 10270-3 0 9059
2 25544 51
6403 228
5232 0018618 349
9351 10
1429 15
60036424 21149
Satellite: ISS
Catalog Number: 25544
Epoch time: 11297
75299311 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 228
5232 deg
Eccentricity:
0018618
Arg of perigee: 349
9351 deg
Mean anomaly: 10
1429 deg
Mean motion: 15
60036424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 292
Coasting Arc #7 (Orbit 2129)
---------------------------------------
Vector Time (GMT): 2011/298/17:21:47
765
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -545680
92 A = 6764167
52 meter
Y = -5176507
58 meter E =
0017204
Z = 4303819
56 I = 51
39650
XDOT = 6490
702904 Wp = 25
21554
YDOT = 2202
425102 meter/sec RA = 222
67228 deg
ZDOT = 3482
145536 TA = 29
41166
MA = 29
31496
Ha = 216
664 n
mi
Hp = 202
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1790291
74 X = -508663
34
Y = -16983292
59 feet Y = -5182402
43 meter
Z = 14120142
91 Z = 4301258
87
XDOT = 21294
957034 XDOT = 6448
676483
YDOT = 7225
804139 feet/sec YDOT = 2274
773395 meter/sec
ZDOT = 11424
361995 ZDOT = 3513
575910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14840083
07 X = 4523257
32
Y = -8467433
99 feet Y = -2580873
88 meter
Z = 14109936
34 Z = 4300708
60
XDOT = 1182
629571 XDOT = 360
465493
YDOT = 21267
504322 feet/sec YDOT = 6482
335317 meter/sec
ZDOT = 11552
310111 ZDOT = 3521
144122
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 11298
77790090
00016717 00000-0 10270-3 0 9063
2 25544 51
6399 223
3661 0018718 353
9155 6
1770 15
60074124 21301
Satellite: ISS
Catalog Number: 25544
Epoch time: 11298
77790090 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 223
3661 deg
Eccentricity:
0018718
Arg of perigee: 353
9155 deg
Mean anomaly: 6
1770 deg
Mean motion: 15
60074124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2130
Checksum: 308
Coasting Arc #8 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2011/299/12:44:19
656
Vector Time (MET): N/A
Weight (LBS) : 870759
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2775647
20 A = 6763813
44 meter
Y = 3185685
70 meter E =
0019765
Z = -5288473
63 I = 51
40309
XDOT = -5908
068006 Wp = 24
96906
YDOT = -4889
157313 meter/sec RA = 218
57423 deg
ZDOT = 173
517783 TA = 246
58551
MA = 246
79347
Ha = 218
248 n
mi
Hp = 204
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9106454
07 X = -2785372
71
Y = 10451724
73 feet Y = 3154592
06 meter
Z = -17350635
28 Z = -5301981
89
XDOT = -19383
425216 XDOT = -5853
800319
YDOT = -16040
542366 feet/sec YDOT = -4954
921515 meter/sec
ZDOT = 569
284064 ZDOT = 144
947668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -985124
21 X = -300265
86
Y = -13757831
96 feet Y = -4193387
18 meter
Z = -17405809
09 Z = -5305290
61
XDOT = 24054
172435 XDOT = 7331
711758
YDOT = -2221
892439 feet/sec YDOT = -677
232816 meter/sec
ZDOT = 453
100300 ZDOT = 138
104971
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 11299
54656439
00016717 00000-0 10270-3 0 9078
2 25544 51
6416 219
5010 0019415 339
9494 20
0896 15
58791079 21420
Satellite: ISS
Catalog Number: 25544
Epoch time: 11299
54656439 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 219
5010 deg
Eccentricity:
0019415
Arg of perigee: 339
9494 deg
Mean anomaly: 20
0896 deg
Mean motion: 15
58791079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 332
Coasting Arc #9 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2011/300/12:44:19
656
Vector Time (MET): N/A
Weight (LBS) : 870759
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5283672
90 A = 6768065
90 meter
Y = -523339
49 meter E =
0021820
Z = 4207519
23 I = 51
44164
XDOT = 3485
360108 Wp = 11
33107
YDOT = 5782
084415 meter/sec RA = 213
51607 deg
ZDOT = -3633
405577 TA = 116
08491
MA = 115
86018
Ha = 218
377 n
mi
Hp = 204
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17334884
84 X = 5268692
34
Y = -1716993
07 feet Y = -464337
90 meter
Z = 13804196
95 Z = 4233151
65
XDOT = 11434
908492 XDOT = 3438
095579
YDOT = 18970
093226 feet/sec YDOT = 5820
795508 meter/sec
ZDOT = -11920
621971 ZDOT = -3616
588142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10791718
86 X = -3289315
91
Y = 13567982
84 feet Y = 4135521
17 meter
Z = 13908659
07 Z = 4239359
28
XDOT = -20633
838539 XDOT = -6289
193987
YDOT = -4180
983503 feet/sec YDOT = -1274
363772 meter/sec
ZDOT = -11852
356258 ZDOT = -3612
598187
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 11300
57231196
00016717 00000-0 10270-3 0 9084
2 25544 51
6411 214
3514 0019411 343
6764 16
3764 15
58826015 21583
Satellite: ISS
Catalog Number: 25544
Epoch time: 11300
57231196 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 214
3514 deg
Eccentricity:
0019411
Arg of perigee: 343
6764 deg
Mean anomaly: 16
3764 deg
Mean motion: 15
58826015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 291
Coasting Arc #10 (Orbit 2172)
---------------------------------------
Vector Time (GMT): 2011/301/12:44:19
656
Vector Time (MET): N/A
Weight (LBS) : 870759
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6267972
14 A = 6774482
17 meter
Y = -1978964
76 meter E =
0025211
Z = -1571932
27 I = 51
48979
XDOT = 177
754633 Wp = 1
50446
YDOT = -5105
966602 meter/sec RA = 208
49253 deg
ZDOT = 5746
098692 TA = 341
20340
MA = 341
29632
Ha = 218
419 n
mi
Hp = 204
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20564213
06 X = -6237740
75
Y = -6492666
52 feet Y = -2048888
01 meter
Z = -5157258
12 Z = -1602309
43
XDOT = 583
184490 XDOT = 206
923133
YDOT = -16751
858929 feet/sec YDOT = -5103
815801 meter/sec
ZDOT = 18852
029831 ZDOT = 5747
033053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18787650
19 X = 5726475
78
Y = -10524951
69 feet Y = -3208005
27 meter
Z = -5280954
54 Z = -1609634
94
XDOT = 11123
305702 XDOT = 3390
383578
YDOT = 10437
674964 feet/sec YDOT = 3181
403329 meter/sec
ZDOT = 18856
066890 ZDOT = 5747
329188
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 11301
53392381
00016717 00000-0 10270-3 0 9096
2 25544 51
6416 209
5231 0019411 346
9873 13
0778 15
58869249 21739
Satellite: ISS
Catalog Number: 25544
Epoch time: 11301
53392381 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 209
5231 deg
Eccentricity:
0019411
Arg of perigee: 346
9873 deg
Mean anomaly: 13
0778 deg
Mean motion: 15
58869249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2173
Checksum: 319
Coasting Arc #11 (Orbit 2188)
---------------------------------------
Vector Time (GMT): 2011/302/12:44:19
656
Vector Time (MET): N/A
Weight (LBS) : 870759
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5362426
74 A = 6774356
68 meter
Y = 3794734
01 meter E =
0012943
Z = -1689052
27 I = 51
51633
XDOT = -4038
172117 Wp = 7
37719
YDOT = 3172
626450 meter/sec RA = 203
49099 deg
ZDOT = -5684
892632 TA = 191
17165
MA = 191
20041
Ha = 218
604 n
mi
Hp = 204
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17593263
59 X = 5327800
01
Y = 12449914
73 feet Y = 3854506
39 meter
Z = -5541510
06 Z = -1663085
08
XDOT = -13248
596186 XDOT = -4045
732175
YDOT = 10408
879429 feet/sec YDOT = 3127
427009 meter/sec
ZDOT = -18651
222547 ZDOT = -5704
528758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21063443
46 X = -6420137
57
Y = 4691959
67 feet Y = 1430109
31 meter
Z = -5435853
08 Z = -1656848
02
XDOT = 1457
924668 XDOT = 444
375439
YDOT = -15186
113979 feet/sec YDOT = -4628
727541 meter/sec
ZDOT = -18731
393297 ZDOT = -5709
328677
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 11302
55961590
00016717 00000-0 10270-3 0 9105
2 25544 51
6413 204
3731 0019296 350
4991 9
5797 15
58885834 21892
Satellite: ISS
Catalog Number: 25544
Epoch time: 11302
55961590 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 204
3731 deg
Eccentricity:
0019296
Arg of perigee: 350
4991 deg
Mean anomaly: 9
5797 deg
Mean motion: 15
58885834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2189
Checksum: 331
Coasting Arc #12 (Orbit 2204)
---------------------------------------
Vector Time (GMT): 2011/303/12:44:19
656
Vector Time (MET): N/A
Weight (LBS) : 870759
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2628201
88 A = 6767476
96 meter
Y = -4490368
89 meter E =
0017956
Z = 4311029
19 I = 51
52166
XDOT = 6817
227021 Wp = 24
94624
YDOT = -648
607476 meter/sec RA = 198
46920 deg
ZDOT = 3491
188210 TA = 29
64118
MA = 29
53954
Ha = 218
763 n
mi
Hp = 203
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8622709
58 X = -2598736
88
Y = -14732181
39 feet Y = -4519594
42 meter
Z = 14143796
55 Z = 4298332
63
XDOT = 22366
230383 XDOT = 6807
013377
YDOT = -2127
977285 feet/sec YDOT = -572
430275 meter/sec
ZDOT = 11454
029559 ZDOT = 3524
281983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16818735
77 X = 5126350
66
Y = 3158152
57 feet Y = 962604
90 meter
Z = 14092248
55 Z = 4295317
36
XDOT = -12862
840144 XDOT = -3920
593676
YDOT = 16945
991613 feet/sec YDOT = 5165
138244 meter/sec
ZDOT = 11588
951490 ZDOT = 3532
312414
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 11303
58527943
00016717 00000-0 10270-3 0 9110
2 25544 51
6411 199
2221 0019406 354
6785 5
4161 15
58939437 22054
Satellite: ISS
Catalog Number: 25544
Epoch time: 11303
58527943 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 199
2221 deg
Eccentricity:
0019406
Arg of perigee: 354
6785 deg
Mean anomaly: 5
4161 deg
Mean motion: 15
58939437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2205
Checksum: 308
Coasting Arc #13 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2011/304/12:44:19
656
Vector Time (MET): N/A
Weight (LBS) : 870759
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1010743
31 A = 6763174
93 meter
Y = 4089767
08 meter E =
0024031
Z = -5303042
46 I = 51
53679
XDOT = -7449
049236 Wp = 36
46986
YDOT = -1811
153700 meter/sec RA = 193
41629 deg
ZDOT = 42
000792 TA = 233
81975
MA = 234
04225
Ha = 218
750 n
mi
Hp = 203
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3316086
97 X = -1030639
25
Y = 13417870
99 feet Y = 4078353
19 meter
Z = -17398433
27 Z = -5308000
95
XDOT = -24439
137912 XDOT = -7428
446957
YDOT = -5942
105314 feet/sec YDOT = -1894
338339 meter/sec
ZDOT = 137
797874 ZDOT = 5
862906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8168062
65 X = -2489625
50
Y = -11117922
99 feet Y = -3388742
93 meter
Z = -17418832
22 Z = -5309260
06
XDOT = 19512
115928 XDOT = 5947
292935
YDOT = -14222
635788 feet/sec YDOT = -4335
059388 meter/sec
ZDOT = -9
441103 ZDOT = -2
877648
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 11304
54681226
00016717 00000-0 10270-3 0 9123
2 25544 51
6407 194
3935 0019425 357
7530 2
3535 15
59011613 22206
Satellite: ISS
Catalog Number: 25544
Epoch time: 11304
54681226 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 194
3935 deg
Eccentricity:
0019425
Arg of perigee: 357
7530 deg
Mean anomaly: 2
3535 deg
Mean motion: 15
59011613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 283
Coasting Arc #14 (Orbit 2235)
---------------------------------------
Vector Time (GMT): 2011/305/12:44:19
656
Vector Time (MET): N/A
Weight (LBS) : 870759
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4516400
49 A = 6767237
09 meter
Y = -2734261
54 meter E =
0024468
Z = 4239115
37 I = 51
58093
XDOT = 5659
760138 Wp = 24
28145
YDOT = 3719
460285 meter/sec RA = 188
36452 deg
ZDOT = -3601
628310 TA = 102
67423
MA = 102
40057
Ha = 218
771 n
mi
Hp = 203
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14817586
90 X = 4526046
83
Y = -8970674
36 feet Y = -2683702
48 meter
Z = 13907858
81 Z = 4261079
64
XDOT = 18568
766858 XDOT = 5635
243963
YDOT = 12202
953691 feet/sec YDOT = 3782
614136 meter/sec
ZDOT = -11816
365847 ZDOT = -3574
192482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2376063
04 X = -724224
01
Y = 17084665
75 feet Y = 5207406
12 meter
Z = 13997533
27 Z = 4266448
14
XDOT = -19997
236385 XDOT = -6095
157650
YDOT = 6886
707411 feet/sec YDOT = 2099
068419 meter/sec
ZDOT = -11704
672552 ZDOT = -3567
584194
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 11305
57242048
00016717 00000-0 10270-3 0 9133
2 25544 51
6408 189
2423 0019502 1
2585 358
8616 15
59075779 22368
Satellite: ISS
Catalog Number: 25544
Epoch time: 11305
57242048 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 189
2423 deg
Eccentricity:
0019502
Arg of perigee: 1
2585 deg
Mean anomaly: 358
8616 deg
Mean motion: 15
59075779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2236
Checksum: 315
Coasting Arc #15 (Orbit 2250)
---------------------------------------
Vector Time (GMT): 2011/306/12:44:19
656
Vector Time (MET): N/A
Weight (LBS) : 870759
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6519907
81 A = 6773921
80 meter
Y = 856282
56 meter E =
0026527
Z = -1560916
59 I = 51
63297
XDOT = -1984
098917 Wp = 14
53780
YDOT = -4686
235417 meter/sec RA = 183
34906 deg
ZDOT = 5763
027819 TA = 328
33088
MA = 328
49021
Ha = 218
872 n
mi
Hp = 202
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21390773
66 X = -6521415
64
Y = 2809325
99 feet Y = 783364
51 meter
Z = -5121117
41 Z = -1592594
22
XDOT = -6509
510881 XDOT = -1959
545010
YDOT = -15374
788113 feet/sec YDOT = -4708
285478 meter/sec
ZDOT = 18907
571585 ZDOT = 5753
448683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11022661
53 X = 3359707
23
Y = -18509953
43 feet Y = -5641833
80 meter
Z = -5250324
83 Z = -1600299
01
XDOT = 14822
948494 XDOT = 4518
034701
YDOT = 3516
953607 feet/sec YDOT = 1071
967459 meter/sec
ZDOT = 18868
719904 ZDOT = 5751
185827
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 11306
53390475
00016717 00000-0 10270-3 0 9149
2 25544 51
6405 184
4129 0019472 4
6573 355
4760 15
59066736 22518
Satellite: ISS
Catalog Number: 25544
Epoch time: 11306
53390475 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 184
4129 deg
Eccentricity:
0019472
Arg of perigee: 4
6573 deg
Mean anomaly: 355
4760 deg
Mean motion: 15
59066736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2251
Checksum: 311
Coasting Arc #16 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2011/307/12:44:19
656
Vector Time (MET): N/A
Weight (LBS) : 870759
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6429853
33 A = 6773635
54 meter
Y = 1225119
93 meter E =
0015083
Z = -1781708
91 I = 51
66204
XDOT = -2433
457475 Wp = 29
84724
YDOT = 4549
126299 meter/sec RA = 178
35651 deg
ZDOT = -5661
733906 TA = 169
71627
MA = 169
68538
Ha = 218
971 n
mi
Hp = 202
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21095319
33 X = 6424331
21
Y = 4019422
33 feet Y = 1296991
56 meter
Z = -5845501
68 Z = -1750485
87
XDOT = -7983
784367 XDOT = -2456
641926
YDOT = 14924
955050 feet/sec YDOT = 4521
784105 meter/sec
ZDOT = -18575
242475 ZDOT = -5673
612178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15996843
07 X = -4875837
77
Y = 14378491
89 feet Y = 4382564
33 meter
Z = -5718227
52 Z = -1742915
75
XDOT = -6058
376239 XDOT = -1846
593077
YDOT = -14136
369157 feet/sec YDOT = -4308
765319 meter/sec
ZDOT = -18623
883524 ZDOT = -5676
559698
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 11307
55946107
00016717 00000-0 10270-3 0 9152
2 25544 51
6401 179
2618 0019277 8
2859 351
8611 15
59091496 22672
Satellite: ISS
Catalog Number: 25544
Epoch time: 11307
55946107 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 179
2618 deg
Eccentricity:
0019277
Arg of perigee: 8
2859 deg
Mean anomaly: 351
8611 deg
Mean motion: 15
59091496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2267
Checksum: 328
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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