[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 7th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 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
7
Coasting Arc #1 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2011/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2011743
21 A = 6765090
52 meter
Y = 5184485
76 meter E =
0008839
Z = 3862363
41 I = 51
44181
XDOT = -6457
377641 Wp = 330
13480
YDOT = 552
100990 meter/sec RA = 324
82264 deg
ZDOT = -4100
994476 TA = 163
02153
MA = 162
99194
Ha = 211
977 n
mi
Hp = 205
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6600207
38 X = -2088330
27
Y = 17009467
73 feet Y = 5161561
23 meter
Z = 12671795
97 Z = 3852404
03
XDOT = -21185
622183 XDOT = -6443
149544
YDOT = 1811
354955 feet/sec YDOT = 479
969947 meter/sec
ZDOT = -13454
706285 ZDOT = -4132
329852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2671178
64 X = 814175
25
Y = -18077160
43 feet Y = -5509918
50 meter
Z = 12630923
10 Z = 3849905
36
XDOT = 18834
848747 XDOT = 5740
861898
YDOT = -6715
140101 feet/sec YDOT = -2046
774703 meter/sec
ZDOT = -13582
342211 ZDOT = -4139
897906
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 11278
54028305
00016717 00000-0 10270-3 0 9003
2 25544 51
6402 325
2114 0016729 291
3898 68
5472 15
60312804 18149
Satellite: ISS
Catalog Number: 25544
Epoch time: 11278
54028305 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 325
2114 deg
Eccentricity:
0016729
Arg of perigee: 291
3898 deg
Mean anomaly: 68
5472 deg
Mean motion: 15
60312804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 296
Coasting Arc #2 (Orbit 1828)
---------------------------------------
Vector Time (GMT): 2011/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4855029
99 A = 6771378
05 meter
Y = -4672719
50 meter E =
0017320
Z = -545479
68 I = 51
43833
XDOT = 3684
756909 Wp = 333
27446
YDOT = 3124
003165 meter/sec RA = 319
79630 deg
ZDOT = 5976
592064 TA = 20
80271
MA = 20
73231
Ha = 212
273 n
mi
Hp = 205
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15928576
09 X = 4909570
26
Y = -15330444
57 feet Y = -4618122
68 meter
Z = -1789631
50 Z = -521761
14
XDOT = 12089
097471 XDOT = 3620
516660
YDOT = 10249
354216 feet/sec YDOT = 3164
849650 meter/sec
ZDOT = 19608
241681 ZDOT = 5994
336307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11753463
94 X = -3582455
81
Y = 18733271
75 feet Y = 5709901
23 meter
Z = -1692767
76 Z = -515955
61
XDOT = -12730
008931 XDOT = -3880
106722
YDOT = -6190
273774 feet/sec YDOT = -1886
795446 meter/sec
ZDOT = 19680
310315 ZDOT = 5998
558584
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 11279
50099525
00016717 00000-0 10270-3 0 9013
2 25544 51
6401 320
3768 0016629 295
7630 64
1809 15
60287016 18298
Satellite: ISS
Catalog Number: 25544
Epoch time: 11279
50099525 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 320
3768 deg
Eccentricity:
0016629
Arg of perigee: 295
7630 deg
Mean anomaly: 64
1809 deg
Mean motion: 15
60287016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1829
Checksum: 315
Coasting Arc #3 (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 = -5623708
12 A = 6767243
90 meter
Y = 2238877
66 meter E =
0012098
Z = -3025612
04 I = 51
40363
XDOT = 312
702835 Wp = 303
62192
YDOT = -5885
760249 meter/sec RA = 314
77758 deg
ZDOT = -4915
776202 TA = 271
27298
MA = 271
41158
Ha = 212
364 n
mi
Hp = 205
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18450485
95 X = -5633627
84
Y = 7345399
16 feet Y = 2175934
17 meter
Z = -9926548
69 Z = -3052956
33
XDOT = 1025
927936 XDOT = 402
375286
YDOT = -19310
237038 feet/sec YDOT = -5881
762492 meter/sec
ZDOT = -16127
874678 ZDOT = -4914
038722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15863478
29 X = 4835188
18
Y = -11853261
11 feet Y = -3612873
99 meter
Z = -10038025
06 Z = -3059590
04
XDOT = 3047
429759 XDOT = 928
856590
YDOT = 17787
214162 feet/sec YDOT = 5421
542876 meter/sec
ZDOT = -16120
454212 ZDOT = -4913
514444
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
52572916
00016717 00000-0 10270-3 0 9028
2 25544 51
6407 315
2204 0016470 299
5125 60
4388 15
60372397 18453
Satellite: ISS
Catalog Number: 25544
Epoch time: 11280
52572916 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 315
2204 deg
Eccentricity:
0016470
Arg of perigee: 299
5125 deg
Mean anomaly: 60
4388 deg
Mean motion: 15
60372397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1845
Checksum: 305
Coasting Arc #4 (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 = 4183240
66 A = 6759797
50 meter
Y = 1386681
44 meter E =
0011914
Z = 5133006
82 I = 51
35694
XDOT = -3883
202251 Wp = 302
49341
YDOT = 6461
533774 meter/sec RA = 309
71446 deg
ZDOT = 1427
812816 TA = 133
77219
MA = 133
67354
Ha = 212
531 n
mi
Hp = 204
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13724542
83 X = 4142488
29
Y = 4549479
80 feet Y = 1433233
69 meter
Z = 16840573
56 Z = 5153229
93
XDOT = -12740
164865 XDOT = -3962
103863
YDOT = 21199
257789 feet/sec YDOT = 6417
668417 meter/sec
ZDOT = 4684
425249 ZDOT = 1408
755814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14349015
69 X = -4373579
98
Y = -623730
24 feet Y = -190112
98 meter
Z = 16922838
70 Z = 5158081
24
XDOT = 6392
425227 XDOT = 1948
411209
YDOT = -22849
219015 feet/sec YDOT = -6964
441956 meter/sec
ZDOT = 4606
456824 ZDOT = 1404
048040
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
55043735
00016717 00000-0 10270-3 0 9035
2 25544 51
6393 310
0631 0016388 303
6144 56
3448 15
60400952 18618
Satellite: ISS
Catalog Number: 25544
Epoch time: 11281
55043735 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 310
0631 deg
Eccentricity:
0016388
Arg of perigee: 303
6144 deg
Mean anomaly: 56
3448 deg
Mean motion: 15
60400952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 287
Coasting Arc #5 (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 = -1318678
40 A = 6761654
26 meter
Y = -4686909
67 meter E =
0007012
Z = -4686539
38 I = 51
34561
XDOT = 5692
772598 Wp = 335
72762
YDOT = -4357
308526 meter/sec RA = 304
62988 deg
ZDOT = 2760
661912 TA = 321
64572
MA = 321
69556
Ha = 212
805 n
mi
Hp = 204
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4326372
72 X = -1243403
92
Y = -15377000
22 feet Y = -4701235
59 meter
Z = -15375785
37 Z = -4692762
19
XDOT = 18677
075454 XDOT = 5727
662879
YDOT = -14295
631647 feet/sec YDOT = -4293
453059 meter/sec
ZDOT = 9057
289738 ZDOT = 2788
402845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8536847
70 X = 2602031
18
Y = 13472944
21 feet Y = 4106553
40 meter
Z = -15400857
71 Z = -4694181
43
XDOT = -12657
390369 XDOT = -3857
972585
YDOT = 18484
793240 feet/sec YDOT = 5634
164979 meter/sec
ZDOT = 9170
487683 ZDOT = 2795
164646
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
51107762
00016717 00000-0 10270-3 0 9044
2 25544 51
6402 305
2286 0016505 307
2976 52
6674 15
60423058 18763
Satellite: ISS
Catalog Number: 25544
Epoch time: 11282
51107762 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 305
2286 deg
Eccentricity:
0016505
Arg of perigee: 307
2976 deg
Mean anomaly: 52
6674 deg
Mean motion: 15
60423058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1876
Checksum: 301
Coasting Arc #6 (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 = -1793552
34 A = 6769366
45 meter
Y = 6246583
00 meter E =
0005370
Z = 1905644
03 I = 51
35418
XDOT = -5250
381284 Wp = 6
06128
YDOT = 199
113705 meter/sec RA = 299
57994 deg
ZDOT = -5587
542527 TA = 152
82218
MA = 152
79406
Ha = 213
016 n
mi
Hp = 204
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5884358
08 X = -1872526
94
Y = 20494038
72 feet Y = 6226085
05 meter
Z = 6252112
96 Z = 1896738
31
XDOT = -17225
660380 XDOT = -5225
073998
YDOT = 653
260186 feet/sec YDOT = 140
541590 meter/sec
ZDOT = -18331
832438 ZDOT = -5612
987721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -683392
67 X = -208298
09
Y = -21321835
69 feet Y = -6498895
52 meter
Z = 6215505
35 Z = 1894486
03
XDOT = 14525
567760 XDOT = 4427
393053
YDOT = -5846
094807 feet/sec YDOT = -1781
889697 meter/sec
ZDOT = -18435
443899 ZDOT = -5619
123301
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
53573495
00016717 00000-0 10270-3 0 9058
2 25544 51
6386 300
0710 0016387 311
5321 48
4429 15
60488893 18926
Satellite: ISS
Catalog Number: 25544
Epoch time: 11283
53573495 = yrday
fracday
Element set: 905
Inclination: 51
6386 deg
RA of node: 300
0710 deg
Eccentricity:
0016387
Arg of perigee: 311
5321 deg
Mean anomaly: 48
4429 deg
Mean motion: 15
60488893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 318
Coasting Arc #7 (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 = 3976449
28 A = 6769327
30 meter
Y = -5141949
72 meter E =
0017248
Z = 1849464
15 I = 51
34020
XDOT = 2972
814138 Wp = 4
04234
YDOT = 4316
292500 meter/sec RA = 294
55896 deg
ZDOT = 5622
319289 TA = 16
47325
MA = 16
41727
Ha = 213
143 n
mi
Hp = 204
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13046093
43 X = 4024667
52
Y = -16869913
78 feet Y = -5097212
83 meter
Z = 6067795
75 Z = 1868899
71
XDOT = 9753
327223 XDOT = 2897
014917
YDOT = 14161
064631 feet/sec YDOT = 4349
113116 meter/sec
ZDOT = 18445
929425 ZDOT = 5636
576860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6829991
01 X = -2081781
26
Y = 20178596
04 feet Y = 6150436
07 meter
Z = 6147208
68 Z = 1873669
21
XDOT = -12244
775370 XDOT = -3732
207533
YDOT = -9768
025699 feet/sec YDOT = -2977
294233 meter/sec
ZDOT = 18503
739829 ZDOT = 5639
939900
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
56036571
00016717 00000-0 10270-3 0 9062
2 25544 51
6385 294
9132 0016428 315
3848 44
5985 15
60515990 19087
Satellite: ISS
Catalog Number: 25544
Epoch time: 11284
56036571 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 294
9132 deg
Eccentricity:
0016428
Arg of perigee: 315
3848 deg
Mean anomaly: 44
5985 deg
Mean motion: 15
60515990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 333
Coasting Arc #8 (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 = -4581318
35 A = 6761314
51 meter
Y = 1744547
77 meter E =
0015949
Z = -4663349
36 I = 51
30170
XDOT = 148
734513 Wp = 357
85542
YDOT = -7141
412480 meter/sec RA = 289
50683 deg
ZDOT = -2801
711668 TA = 244
16607
MA = 244
33065
Ha = 213
344 n
mi
Hp = 204
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15030572
03 X = -4577831
60
Y = 5723581
93 feet Y = 1693335
71 meter
Z = -15299702
61 Z = -4685597
51
XDOT = 487
974125 XDOT = 242
190605
YDOT = -23429
830972 feet/sec YDOT = -7139
226967 meter/sec
ZDOT = -9191
967415 ZDOT = -2800
761408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12093711
81 X = 3686163
36
Y = -10470759
80 feet Y = -3191487
59 meter
Z = -15390377
17 Z = -4690986
96
XDOT = 6709
977542 XDOT = 2045
201155
YDOT = 21331
169817 feet/sec YDOT = 6501
740560 meter/sec
ZDOT = -9187
708646 ZDOT = -2800
413595
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
52093191
00016717 00000-0 10270-3 0 9071
2 25544 51
6380 290
0777 0016398 318
9944 40
9978 15
60557027 19232
Satellite: ISS
Catalog Number: 25544
Epoch time: 11285
52093191 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 290
0777 deg
Eccentricity:
0016398
Arg of perigee: 318
9944 deg
Mean anomaly: 40
9978 deg
Mean motion: 15
60557027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 337
Coasting Arc #9 (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 = 3560627
28 A = 6759309
52 meter
Y = 2627450
02 meter E =
0016912
Z = 5118251
09 I = 51
28553
XDOT = -2985
009826 Wp = 338
60533
YDOT = 6914
866313 meter/sec RA = 284
41491 deg
ZDOT = -1459
189267 TA = 125
58250
MA = 125
42478
Ha = 213
516 n
mi
Hp = 203
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11681848
02 X = 3506117
92
Y = 8620242
85 feet Y = 2666962
77 meter
Z = 16792162
38 Z = 5135416
36
XDOT = -9793
339324 XDOT = -3055
022739
YDOT = 22686
569267 feet/sec YDOT = 6881
094523 meter/sec
ZDOT = -4787
366360 ZDOT = -1473
861367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13894520
76 X = -4235049
93
Y = -3920374
12 feet Y = -1194930
03 meter
Z = 16861904
90 Z = 5139508
61
XDOT = 738
749799 XDOT = 225
170939
YDOT = -23663
928914 feet/sec YDOT = -7212
765533 meter/sec
ZDOT = -4847
475958 ZDOT = -1477
510672
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
54550910
00016717 00000-0 10270-3 0 9082
2 25544 51
6373 284
9187 0016428 322
8634 37
1384 15
60600333 19390
Satellite: ISS
Catalog Number: 25544
Epoch time: 11286
54550910 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 284
9187 deg
Eccentricity:
0016428
Arg of perigee: 322
8634 deg
Mean anomaly: 37
1384 deg
Mean motion: 15
60600333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1939
Checksum: 316
Coasting Arc #10 (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 = -1421552
13 A = 6766744
34 meter
Y = -5910011
83 meter E =
0016186
Z = -2949224
24 I = 51
30438
XDOT = 4629
826864 Wp = 342
73180
YDOT = -3592
136856 meter/sec RA = 279
34558 deg
ZDOT = 4974
936718 TA = 343
26113
MA = 343
31449
Ha = 213
681 n
mi
Hp = 203
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4663884
95 X = -1341032
45
Y = -19389802
60 feet Y = -5925458
47 meter
Z = -9675932
54 Z = -2955934
33
XDOT = 15189
720683 XDOT = 4645
482875
YDOT = -11785
225906 feet/sec YDOT = -3540
275446 meter/sec
ZDOT = 16321
970861 ZDOT = 4997
467155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11504058
01 X = 3506436
88
Y = 16274202
74 feet Y = 4960377
00 meter
Z = -9702933
19 Z = -2957454
04
XDOT = -8421
166277 XDOT = -2566
771481
YDOT = 15723
062505 feet/sec YDOT = 4792
389452 meter/sec
ZDOT = 16413
893929 ZDOT = 5002
954870
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
50602463
00016717 00000-0 10270-3 0 9091
2 25544 51
6374 280
0835 0016429 326
8131 33
1993 15
60631068 19543
Satellite: ISS
Catalog Number: 25544
Epoch time: 11287
50602463 = yrday
fracday
Element set: 909
Inclination: 51
6374 deg
RA of node: 280
0835 deg
Eccentricity:
0016429
Arg of perigee: 326
8131 deg
Mean anomaly: 33
1993 deg
Mean motion: 15
60631068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 308
Coasting Arc #11 (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 = -1108760
76 A = 6770059
40 meter
Y = 6639862
34 meter E =
0006494
Z = -756459
73 I = 51
31192
XDOT = -4647
772013 Wp = 347
38812
YDOT = -1452
816093 meter/sec RA = 274
31719 deg
ZDOT = -5923
942770 TA = 200
83694
MA = 200
86342
Ha = 213
878 n
mi
Hp = 203
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3637666
54 X = -1179251
78
Y = 21784325
28 feet Y = 6627069
33 meter
Z = -2481823
26 Z = -762017
73
XDOT = -15248
595843 XDOT = -4602
402854
YDOT = -4766
456998 feet/sec YDOT = -1504
536922 meter/sec
ZDOT = -19435
507775 ZDOT = -5946
411846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5132451
02 X = -1564371
07
Y = -21478658
63 feet Y = -6546695
15 meter
Z = -2504807
80 Z = -763465
42
XDOT = 14227
886372 XDOT = 4336
659766
YDOT = -1116
620911 feet/sec YDOT = -340
346054 meter/sec
ZDOT = -19526
912569 ZDOT = -5951
802951
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
53054683
00016717 00000-0 10270-3 0 9102
2 25544 51
6371 274
9244 0016461 330
7752 29
2481 15
60691635 19707
Satellite: ISS
Catalog Number: 25544
Epoch time: 11288
53054683 = yrday
fracday
Element set: 910
Inclination: 51
6371 deg
RA of node: 274
9244 deg
Eccentricity:
0016461
Arg of perigee: 330
7752 deg
Mean anomaly: 29
2481 deg
Mean motion: 15
60691635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 313
Coasting Arc #12 (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 = 3215116
41 A = 6762948
59 meter
Y = -4320807
66 meter E =
0012641
Z = 4079108
05 I = 51
28728
XDOT = 3122
336439 Wp = 13
40287
YDOT = 5903
590852 meter/sec RA = 269
27583 deg
ZDOT = 3802
137011 TA = 37
29039
MA = 37
20270
Ha = 213
843 n
mi
Hp = 203
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10548282
17 X = 3243377
62
Y = -14175878
15 feet Y = -4284696
12 meter
Z = 13382900
42 Z = 4094796
16
XDOT = 10243
885956 XDOT = 3037
618817
YDOT = 19368
736391 feet/sec YDOT = 5938
033167 meter/sec
ZDOT = 12474
202792 ZDOT = 3817
099641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3836925
41 X = -1169494
87
Y = 17198250
74 feet Y = 5242026
82 meter
Z = 13447006
24 Z = 4098647
50
XDOT = -15881
787506 XDOT = -4840
768832
YDOT = -13319
109237 feet/sec YDOT = -4059
664496 meter/sec
ZDOT = 12534
813288 ZDOT = 3820
611090
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
55503842
00016717 00000-0 10270-3 0 9112
2 25544 51
6369 269
7659 0016468 333
8413 26
1910 15
60749791 19868
Satellite: ISS
Catalog Number: 25544
Epoch time: 11289
55503842 = yrday
fracday
Element set: 911
Inclination: 51
6369 deg
RA of node: 269
7659 deg
Eccentricity:
0016468
Arg of perigee: 333
8413 deg
Mean anomaly: 26
1910 deg
Mean motion: 15
60749791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 344
Coasting Arc #13 (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 = -4238936
57 A = 6758140
64 meter
Y = 86385
96 meter E =
0017022
Z = -5269633
57 I = 51
27271
XDOT = -526
402513 Wp = 30
82584
YDOT = -7649
324062 meter/sec RA = 264
18805 deg
ZDOT = 312
872211 TA = 242
08369
MA = 242
25615
Ha = 214
056 n
mi
Hp = 202
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13907272
22 X = -4213988
16
Y = 283418
52 feet Y = 39122
95 meter
Z = -17288824
05 Z = -5290166
06
XDOT = -1727
042365 XDOT = -442
347043
YDOT = -25096
207553 feet/sec YDOT = -7654
740630 meter/sec
ZDOT = 1026
483631 ZDOT = 310
519259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12405771
77 X = 3781279
23
Y = -6057333
99 feet Y = -1846275
40 meter
Z = -17372435
51 Z = -5295118
34
XDOT = 11678
317681 XDOT = 3559
551229
YDOT = 21139
087419 feet/sec YDOT = 6443
193845 meter/sec
ZDOT = 1017
301663 ZDOT = 310
073547
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
51547394
00016717 00000-0 10270-3 0 9121
2 25544 51
6369 264
9295 0016436 338
0294 22
0156 15
60759989 20016
Satellite: ISS
Catalog Number: 25544
Epoch time: 11290
51547394 = yrday
fracday
Element set: 912
Inclination: 51
6369 deg
RA of node: 264
9295 deg
Eccentricity:
0016436
Arg of perigee: 338
0294 deg
Mean anomaly: 22
0156 deg
Mean motion: 15
60759989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 321
Coasting Arc #14 (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 = 3810775
94 A = 6764094
18 meter
Y = 4217914
93 meter E =
0017978
Z = 3675435
04 I = 51
29736
XDOT = -2367
236656 Wp = 21
15624
YDOT = 5899
725794 meter/sec RA = 259
10495 deg
ZDOT = -4293
015102 TA = 114
75649
MA = 114
56931
Ha = 214
215 n
mi
Hp = 202
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12502545
72 X = 3745472
32
Y = 13838303
59 feet Y = 4260164
32 meter
Z = 12058513
90 Z = 3693789
30
XDOT = -7766
524461 XDOT = -2412
177648
YDOT = 19356
055754 feet/sec YDOT = 5873
002526 meter/sec
ZDOT = -14084
695216 ZDOT = -4304
624584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17218317
23 X = -5248143
09
Y = -7038389
52 feet Y = -2145301
13 meter
Z = 12133040
75 Z = 3698150
82
XDOT = -2035
239620 XDOT = -620
341036
YDOT = -19512
589063 feet/sec YDOT = -5947
437147 meter/sec
ZDOT = -14132
273331 ZDOT = -4307
516911
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
53990729
00016717 00000-0 10270-3 0 9139
2 25544 51
6368 259
7705 0016536 341
5946 18
4610 15
60827379 20177
Satellite: ISS
Catalog Number: 25544
Epoch time: 11291
53990729 = yrday
fracday
Element set: 913
Inclination: 51
6368 deg
RA of node: 259
7705 deg
Eccentricity:
0016536
Arg of perigee: 341
5946 deg
Mean anomaly: 18
4610 deg
Mean motion: 15
60827379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2017
Checksum: 330
Coasting Arc #15 (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 = -1957622
32 A = 6769784
39 meter
Y = -6462004
75 meter E =
0024693
Z = -135965
55 I = 51
32360
XDOT = 4567
321802 Wp = 9
81454
YDOT = -1506
071661 meter/sec RA = 254
06976 deg
ZDOT = 6003
045693 TA = 348
70771
MA = 348
76302
Ha = 214
214 n
mi
Hp = 202
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6422645
39 X = -1884556
91
Y = -21200802
97 feet Y = -6483487
55 meter
Z = -446081
19 Z = -145298
10
XDOT = 14984
651582 XDOT = 4554
661528
YDOT = -4941
179990 feet/sec YDOT = -1455
067679 meter/sec
ZDOT = 19695
031802 ZDOT = 6025
203258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15295739
02 X = 4662141
25
Y = 16022788
38 feet Y = 4883745
90 meter
Z = -483765
76 Z = -147451
81
XDOT = -9868
430467 XDOT = -3007
897606
YDOT = 10001
174700 feet/sec YDOT = 3048
358049 meter/sec
ZDOT = 19785
343990 ZDOT = 6030
572848
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
50028582
00016717 00000-0 10270-3 0 9147
2 25544 51
6367 254
9342 0016354 345
4424 14
6259 15
60877373 20325
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
50028582 = yrday
fracday
Element set: 914
Inclination: 51
6367 deg
RA of node: 254
9342 deg
Eccentricity:
0016354
Arg of perigee: 345
4424 deg
Mean anomaly: 14
6259 deg
Mean motion: 15
60877373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 306
Coasting Arc #16 (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 = -2903786
32 A = 6762739
36 meter
Y = 3758633
40 meter E =
0017853
Z = -4823721
79 I = 51
29514
XDOT = -3889
035249 Wp = 10
69403
YDOT = -6146
525580 meter/sec RA = 253
22107 deg
ZDOT = -2432
432957 TA = 235
24203
MA = 235
41023
Ha = 215
023 n
mi
Hp = 204
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9526858
00 X = -2922167
28
Y = 12331474
41 feet Y = 3726058
56 meter
Z = -15825858
88 Z = -4837873
28
XDOT = -12759
301997 XDOT = -3808
198110
YDOT = -20165
766337 feet/sec YDOT = -6189
563246 meter/sec
ZDOT = -7980
423087 ZDOT = -2451
129522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12153505
69 X = -3704388
53
Y = -9658423
79 feet Y = -2943887
57 meter
Z = -15883678
52 Z = -4841345
21
XDOT = 19694
314457 XDOT = 6002
827047
YDOT = -11448
180711 feet/sec YDOT = -3489
405481 meter/sec
ZDOT = -8056
260903 ZDOT = -2455
548323
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
69236402
00016717 00000-0 10270-3 0 9150
2 25544 51
6403 253
9682 0016081 330
5028 29
5219 15
59857152 20359
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
69236402 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 253
9682 deg
Eccentricity:
0016081
Arg of perigee: 330
5028 deg
Mean anomaly: 29
5219 deg
Mean motion: 15
59857152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2035
Checksum: 303
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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