[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 14th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 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
There are no maneuvers
Coasting Arc #1 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2011/192/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2950327
36 A = 6768515
04 meter
Y = 5228575
47 meter E =
0009464
Z = 3111971
87 I = 51
85329
XDOT = -5901
639535 Wp = 28
65106
YDOT = 415
543008 meter/sec RA = 36
54083 deg
ZDOT = 4898
886024 TA = 7
16462
MA = 7
15111
Ha = 212
541 n
mi
Hp = 207
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9679551
71 X = 2876523
87
Y = 17154119
01 feet Y = 5261154
63 meter
Z = 10209881
47 Z = 3126126
09
XDOT = -19362
334434 XDOT = -5929
645301
YDOT = 1363
330079 feet/sec YDOT = 349
389846 meter/sec
ZDOT = 16072
460708 ZDOT = 4870
148130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13459470
37 X = -4102446
57
Y = -14339800
03 feet Y = -4370771
05 meter
Z = 10267034
26 Z = 3129392
04
XDOT = 17514
536546 XDOT = 5338
430739
YDOT = -5019
913359 feet/sec YDOT = -1530
069592 meter/sec
ZDOT = 15955
704029 ZDOT = 4863
298588
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 11192
79489591
00016717 00000-0 10270-3 0 9003
2 25544 51
6403 36
7975 0011031 311
1165 48
9038 15
59866231 4756
Satellite: ISS
Catalog Number: 25544
Epoch time: 11192
79489591 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 36
7975 deg
Eccentricity:
0011031
Arg of perigee: 311
1165 deg
Mean anomaly: 48
9038 deg
Mean motion: 15
59866231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 313
Coasting Arc #2 (Orbit 489)
---------------------------------------
Vector Time (GMT): 2011/193/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 603607
32 A = 6761533
70 meter
Y = -4367596
64 meter E =
0012019
Z = -5133392
44 I = 51
80469
XDOT = 6960
350937 Wp = 26
94315
YDOT = 2818
409017 meter/sec RA = 31
51526 deg
ZDOT = -1570
504772 TA = 227
90729
MA = 228
00955
Ha = 212
849 n
mi
Hp = 207
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1980338
98 X = 677338
54
Y = -14329385
30 feet Y = -4360433
56 meter
Z = -16841838
71 Z = -5130281
84
XDOT = 22835
797038 XDOT = 6935
946761
YDOT = 9246
748743 feet/sec YDOT = 2896
107724 meter/sec
ZDOT = -5152
574712 ZDOT = -1536
750591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1671693
82 X = 509532
28
Y = 14383796
84 feet Y = 4384181
28 meter
Z = -16828915
15 Z = -5129453
34
XDOT = -23425
879869 XDOT = -7140
208184
YDOT = -3180
372737 feet/sec YDOT = -969
377610 meter/sec
ZDOT = -5015
650682 ZDOT = -1528
770328
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 11193
75589138
00016717 00000-0 10270-3 0 9019
2 25544 51
6403 31
9661 0011190 315
1106 44
9144 15
59846621 4902
Satellite: ISS
Catalog Number: 25544
Epoch time: 11193
75589138 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 31
9661 deg
Eccentricity:
0011190
Arg of perigee: 315
1106 deg
Mean anomaly: 44
9144 deg
Mean motion: 15
59846621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 490
Checksum: 295
Coasting Arc #3 (Orbit 505)
---------------------------------------
Vector Time (GMT): 2011/194/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4189478
00 A = 6762809
85 meter
Y = 2177822
57 meter E =
0012094
Z = 4847160
44 I = 51
78275
XDOT = -5398
243095 Wp = 354
98294
YDOT = -4860
617874 meter/sec RA = 26
46615 deg
ZDOT = -2470
611996 TA = 119
27236
MA = 119
15142
Ha = 213
102 n
mi
Hp = 206
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13745006
55 X = -4237065
66
Y = 7145087
17 feet Y = 2130706
36 meter
Z = 15902757
37 Z = 4826693
11
XDOT = -17710
771308 XDOT = -5331
487946
YDOT = -15946
909037 feet/sec YDOT = -4920
610635 meter/sec
ZDOT = -8105
682401 ZDOT = -2496
674894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11356978
19 X = 3461606
95
Y = -10660138
60 feet Y = -3249210
24 meter
Z = 15819470
88 Z = 4821774
72
XDOT = 20573
827028 XDOT = 6270
902478
YDOT = 9678
042109 feet/sec YDOT = 2949
867235 meter/sec
ZDOT = -8211
230568 ZDOT = -2502
783077
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 11194
78094446
00016717 00000-0 10270-3 0 9027
2 25544 51
6404 26
8112 0011134 319
7684 40
2647 15
59856980 5060
Satellite: ISS
Catalog Number: 25544
Epoch time: 11194
78094446 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 26
8112 deg
Eccentricity:
0011134
Arg of perigee: 319
7684 deg
Mean anomaly: 40
2647 deg
Mean motion: 15
59856980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 506
Checksum: 311
Coasting Arc #4 (Orbit 520)
---------------------------------------
Vector Time (GMT): 2011/195/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6311075
25 A = 6770413
61 meter
Y = 463737
61 meter E =
0013407
Z = -2382179
10 I = 51
78075
XDOT = 1650
942089 Wp = 347
73152
YDOT = 5213
841022 meter/sec RA = 21
44633 deg
ZDOT = 5396
043815 TA = 345
62545
MA = 345
66356
Ha = 213
397 n
mi
Hp = 206
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20705627
45 X = 6316992
53
Y = 1521448
86 feet Y = 534345
36 meter
Z = -7815548
22 Z = -2351506
12
XDOT = 5416
476669 XDOT = 1566
304783
YDOT = 17105
777632 feet/sec YDOT = 5231
828764 meter/sec
ZDOT = 17703
555822 ZDOT = 5403
859171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20300986
31 X = -6187740
63
Y = 4565022
69 feet Y = 1391418
92 meter
Z = -7690977
25 Z = -2344209
87
XDOT = -9711
663286 XDOT = -2960
114970
YDOT = -13350
005456 feet/sec YDOT = -4069
081663 meter/sec
ZDOT = 17734
956367 ZDOT = 5405
614701
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 11195
74192255
00016717 00000-0 10270-3 0 9032
2 25544 51
6406 21
9789 0011387 323
1471 36
8901 15
59844780 5217
Satellite: ISS
Catalog Number: 25544
Epoch time: 11195
74192255 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 21
9789 deg
Eccentricity:
0011387
Arg of perigee: 323
1471 deg
Mean anomaly: 36
8901 deg
Mean motion: 15
59844780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 521
Checksum: 313
Coasting Arc #5 (Orbit 536)
---------------------------------------
Vector Time (GMT): 2011/196/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6074862
36 A = 6772010
42 meter
Y = -2757196
66 meter E =
0002217
Z = -1171410
05 I = 51
75774
XDOT = 2932
615297 Wp = 345
96697
YDOT = -3962
846977 meter/sec RA = 16
45744 deg
ZDOT = -5876
420936 TA = 206
75371
MA = 206
76515
Ha = 213
376 n
mi
Hp = 206
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19930650
79 X = -6037889
00
Y = -9045920
80 feet Y = -2824922
57 meter
Z = -3843208
83 Z = -1200831
60
XDOT = 9621
441263 XDOT = 3005
256548
YDOT = -13001
466460 feet/sec YDOT = -3929
645701 meter/sec
ZDOT = -19279
596248 ZDOT = -5861
998756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21721799
51 X = 6620804
49
Y = 2508273
84 feet Y = 764521
87 meter
Z = -3962545
47 Z = -1207783
86
XDOT = -5099
770576 XDOT = -1554
410072
YDOT = 13777
315523 feet/sec YDOT = 4199
325771 meter/sec
ZDOT = -19220
745599 ZDOT = -5858
483258
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 11196
76695842
00016717 00000-0 10270-3 0 9046
2 25544 51
6401 16
8244 0011237 326
9472 33
0980 15
59887915 5377
Satellite: ISS
Catalog Number: 25544
Epoch time: 11196
76695842 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 16
8244 deg
Eccentricity:
0011237
Arg of perigee: 326
9472 deg
Mean anomaly: 33
0980 deg
Mean motion: 15
59887915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 537
Checksum: 327
Coasting Arc #6 (Orbit 552)
---------------------------------------
Vector Time (GMT): 2011/197/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3409824
04 A = 6764956
74 meter
Y = 4064876
00 meter E =
0008250
Z = 4188608
36 I = 51
70581
XDOT = -6522
959314 Wp = 30
31531
YDOT = 1661
291570 meter/sec RA = 11
44739 deg
ZDOT = 3701
733970 TA = 21
82429
MA = 21
78916
Ha = 213
463 n
mi
Hp = 205
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11187086
76 X = 3343769
40
Y = 13336207
34 feet Y = 4102636
90 meter
Z = 13742153
43 Z = 4205012
91
XDOT = -21400
785150 XDOT = -6559
033296
YDOT = 5450
431659 feet/sec YDOT = 1588
145728 meter/sec
ZDOT = 12144
796488 ZDOT = 3669
958806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14815593
56 X = -4515792
92
Y = -9037417
98 feet Y = -2754605
00 meter
Z = 13808525
66 Z = 4208838
62
XDOT = 17904
428065 XDOT = 5457
269674
YDOT = -11011
797669 feet/sec YDOT = -3356
395930 meter/sec
ZDOT = 12015
606747 ZDOT = 3662
356936
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 11197
79198446
00016717 00000-0 10270-3 0 9059
2 25544 51
6407 11
6689 0011300 330
8561 29
1963 15
59922911 5534
Satellite: ISS
Catalog Number: 25544
Epoch time: 11197
79198446 = yrday
fracday
Element set: 905
Inclination: 51
6407 deg
RA of node: 11
6689 deg
Eccentricity:
0011300
Arg of perigee: 330
8561 deg
Mean anomaly: 29
1963 deg
Mean motion: 15
59922911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 553
Checksum: 317
Coasting Arc #7 (Orbit 567)
---------------------------------------
Vector Time (GMT): 2011/198/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 628691
46 A = 6760595
71 meter
Y = -4152358
65 meter E =
0014106
Z = -5306272
10 I = 51
66071
XDOT = 7607
707090 Wp = 44
56834
YDOT = 972
610499 meter/sec RA = 6
39726 deg
ZDOT = 150
332669 TA = 226
80439
MA = 226
92231
Ha = 213
756 n
mi
Hp = 205
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2062636
02 X = 700853
50
Y = -13623223
93 feet Y = -4144924
25 meter
Z = -17409029
20 Z = -5303043
11
XDOT = 24959
668931 XDOT = 7595
535479
YDOT = 3190
979327 feet/sec YDOT = 1057
616442 meter/sec
ZDOT = 493
217419 ZDOT = 187
260545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2581037
91 X = 786700
35
Y = 13551786
38 feet Y = 4130584
49 meter
Z = -17395640
97 Z = -5302191
37
XDOT = -23571
461464 XDOT = -7184
581454
YDOT = 5272
508700 feet/sec YDOT = 1607
060652 meter/sec
ZDOT = 643
162627 ZDOT = 196
035969
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 11198
75294022
00016717 00000-0 10270-3 0 9064
2 25544 51
6404 6
8374 0011475 334
6035 25
4555 15
59905191 5682
Satellite: ISS
Catalog Number: 25544
Epoch time: 11198
75294022 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 6
8374 deg
Eccentricity:
0011475
Arg of perigee: 334
6035 deg
Mean anomaly: 25
4555 deg
Mean motion: 15
59905191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 568
Checksum: 310
Coasting Arc #8 (Orbit 583)
---------------------------------------
Vector Time (GMT): 2011/199/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4521266
41 A = 6765726
31 meter
Y = 3059824
41 meter E =
0014405
Z = 4000391
47 I = 51
64846
XDOT = -5715
092700 Wp = 26
76461
YDOT = -3259
074183 meter/sec RA = 1
34576 deg
ZDOT = -3948
301935 TA = 104
32371
MA = 104
16372
Ha = 213
929 n
mi
Hp = 205
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14833551
20 X = -4574578
68
Y = 10038793
99 feet Y = 3008966
46 meter
Z = 13124643
92 Z = 3978298
38
XDOT = -18750
304135 XDOT = -5659
044629
YDOT = -10692
500601 feet/sec YDOT = -3322
670139 meter/sec
ZDOT = -12953
746506 ZDOT = -3975
929365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10373288
96 X = 3161778
47
Y = -14681938
80 feet Y = -4475054
95 meter
Z = 13034701
89 Z = 3972977
13
XDOT = 20182
152862 XDOT = 6151
520192
YDOT = 2606
368795 feet/sec YDOT = 794
421209 meter/sec
ZDOT = -13065
759567 ZDOT = -3982
443516
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 11199
77795014
00016717 00000-0 10270-3 0 9075
2 25544 51
6408 1
6822 0011557 338
8483 21
2193 15
59950642 5842
Satellite: ISS
Catalog Number: 25544
Epoch time: 11199
77795014 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 1
6822 deg
Eccentricity:
0011557
Arg of perigee: 338
8483 deg
Mean anomaly: 21
2193 deg
Mean motion: 15
59950642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 584
Checksum: 321
Coasting Arc #9 (Orbit 598)
---------------------------------------
Vector Time (GMT): 2011/200/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6606493
91 A = 6772318
70 meter
Y = -1125331
83 meter E =
0019333
Z = -885202
32 I = 51
63956
XDOT = 1577
186886 Wp = 8
34056
YDOT = 4612
047446 meter/sec RA = 356
33399 deg
ZDOT = 5942
707896 TA = 342
04590
MA = 342
11410
Ha = 214
225 n
mi
Hp = 205
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21674848
79 X = 6622886
65
Y = -3692033
55 feet Y = -1051362
27 meter
Z = -2904207
08 Z = -853068
83
XDOT = 5174
497658 XDOT = 1496
628800
YDOT = 15131
389258 feet/sec YDOT = 4629
233688 meter/sec
ZDOT = 19497
073148 ZDOT = 5950
174363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18770838
58 X = -5721351
60
Y = 11481606
89 feet Y = 3499593
78 meter
Z = -2773611
85 Z = -845396
89
XDOT = -9476
467424 XDOT = -2888
427271
YDOT = -10804
525484 feet/sec YDOT = -3293
219368 meter/sec
ZDOT = 19527
103773 ZDOT = 5951
861230
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 11200
73888970
00016717 00000-0 10270-3 0 9089
2 25544 51
6405 356
8499 0011748 342
6697 17
4056 15
59894984 5993
Satellite: ISS
Catalog Number: 25544
Epoch time: 11200
73888970 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 356
8499 deg
Eccentricity:
0011748
Arg of perigee: 342
6697 deg
Mean anomaly: 17
4056 deg
Mean motion: 15
59894984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 599
Checksum: 366
Coasting Arc #10 (Orbit 614)
---------------------------------------
Vector Time (GMT): 2011/201/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6117065
35 A = 6769363
73 meter
Y = -1196213
52 meter E =
0008649
Z = -2654962
27 I = 51
59974
XDOT = 3170
967093 Wp = 8
85828
YDOT = -4654
597493 meter/sec RA = 351
33326 deg
ZDOT = -5202
672755 TA = 201
14520
MA = 201
18098
Ha = 214
228 n
mi
Hp = 204
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20069112
05 X = -6090337
30
Y = -3924585
03 feet Y = -1264468
65 meter
Z = -8710506
13 Z = -2684613
67
XDOT = 10403
435344 XDOT = 3248
053287
YDOT = -15270
989151 feet/sec YDOT = -4618
706464 meter/sec
ZDOT = -17069
136336 ZDOT = -5187
081489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19974871
98 X = 6088340
98
Y = -4130964
17 feet Y = -1259117
88 meter
Z = -8830864
48 Z = -2691647
49
XDOT = -4074
866117 XDOT = -1242
019192
YDOT = 16691
751246 feet/sec YDOT = 5087
645780 meter/sec
ZDOT = -17005
510384 ZDOT = -5183
279565
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 11201
76388366
00016717 00000-0 10270-3 0 9098
2 25544 51
6399 351
6951 0011601 346
9145 13
1709 15
59951379 6153
Satellite: ISS
Catalog Number: 25544
Epoch time: 11201
76388366 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 351
6951 deg
Eccentricity:
0011601
Arg of perigee: 346
9145 deg
Mean anomaly: 13
1709 deg
Mean motion: 15
59951379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 615
Checksum: 325
Coasting Arc #11 (Orbit 630)
---------------------------------------
Vector Time (GMT): 2011/202/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3209293
39 A = 6761740
60 meter
Y = 3275172
87 meter E =
0008732
Z = 4964216
48 I = 51
54514
XDOT = -6606
224246 Wp = 19
73990
YDOT = 3318
390905 meter/sec RA = 346
29364 deg
ZDOT = 2088
488394 TA = 49
98458
MA = 49
90798
Ha = 214
281 n
mi
Hp = 204
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10529177
78 X = 3148316
27
Y = 10745317
80 feet Y = 3310719
86 meter
Z = 16286799
46 Z = 4979659
15
XDOT = -21673
964063 XDOT = -6652
985522
YDOT = 10887
109267 feet/sec YDOT = 3244
254483 meter/sec
ZDOT = 6851
996043 ZDOT = 2056
282387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13877026
96 X = -4229717
82
Y = -5631469
59 feet Y = -1716471
93 meter
Z = 16349310
36 Z = 4983269
80
XDOT = 15075
523000 XDOT = 4595
019410
YDOT = -17702
945437 feet/sec YDOT = -5395
857769 meter/sec
ZDOT = 6720
977928 ZDOT = 2048
554072
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 11202
78886700
00016717 00000-0 10270-3 0 9108
2 25544 51
6403 346
5400 0011698 350
3492 9
7437 15
59979563 6313
Satellite: ISS
Catalog Number: 25544
Epoch time: 11202
78886700 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 346
5400 deg
Eccentricity:
0011698
Arg of perigee: 350
3492 deg
Mean anomaly: 9
7437 deg
Mean motion: 15
59979563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 631
Checksum: 315
Coasting Arc #12 (Orbit 645)
---------------------------------------
Vector Time (GMT): 2011/203/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 820979
30 A = 6761743
96 meter
Y = -4480825
99 meter E =
0014084
Z = -5003999
75 I = 51
51531
XDOT = 7364
785624 Wp = 52
46469
YDOT = -844
062930 meter/sec RA = 341
22531 deg
ZDOT = 1976
335260 TA = 236
68161
MA = 236
81655
Ha = 214
559 n
mi
Hp = 204
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2693501
64 X = 895332
04
Y = -14700872
66 feet Y = -4471229
18 meter
Z = -16417322
02 Z = -4999831
22
XDOT = 24162
682495 XDOT = 7364
076145
YDOT = -2769
235335 feet/sec YDOT = -761
709531 meter/sec
ZDOT = 6484
039568 ZDOT = 2012
111257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3619309
65 X = 1103165
58
Y = 14520200
53 feet Y = 4425757
12 meter
Z = -16400105
02 Z = -4998752
01
XDOT = -19689
273565 XDOT = -6001
290583
YDOT = 12350
116014 feet/sec YDOT = 3764
315361 meter/sec
ZDOT = 6629
393393 ZDOT = 2020
639106
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 11203
74978265
00016717 00000-0 10270-3 0 9114
2 25544 51
6399 341
7073 0011861 354
4611 5
6412 15
59967143 6465
Satellite: ISS
Catalog Number: 25544
Epoch time: 11203
74978265 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 341
7073 deg
Eccentricity:
0011861
Arg of perigee: 354
4611 deg
Mean anomaly: 5
6412 deg
Mean motion: 15
59967143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 646
Checksum: 313
Coasting Arc #13 (Orbit 661)
---------------------------------------
Vector Time (GMT): 2011/204/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4446340
79 A = 6769161
38 meter
Y = 4323102
65 meter E =
0015853
Z = 2715707
34 I = 51
51261
XDOT = -5260
923937 Wp = 54
07296
YDOT = -2155
361543 meter/sec RA = 336
18059 deg
ZDOT = -5152
241157 TA = 95
09861
MA = 94
91765
Ha = 214
665 n
mi
Hp = 204
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14587732
25 X = -4507544
40
Y = 14183407
64 feet Y = 4273038
51 meter
Z = 8909800
99 Z = 2693958
92
XDOT = -17260
249138 XDOT = -5211
402815
YDOT = -7071
396140 feet/sec YDOT = -2213
915048 meter/sec
ZDOT = -16903
678337 ZDOT = -5177
678423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7029843
52 X = 2142696
31
Y = -19134348
94 feet Y = -5832149
56 meter
Z = 8821197
71 Z = 2688701
06
XDOT = 17131
881722 XDOT = 5221
797549
YDOT = -1592
388105 feet/sec YDOT = -485
359894 meter/sec
ZDOT = -17006
847990 ZDOT = -5183
687267
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 11204
77474879
00016717 00000-0 10270-3 0 9121
2 25544 51
6401 336
5519 0011983 358
2815 1
8297 15
60024863 6621
Satellite: ISS
Catalog Number: 25544
Epoch time: 11204
77474879 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 336
5519 deg
Eccentricity:
0011983
Arg of perigee: 358
2815 deg
Mean anomaly: 1
8297 deg
Mean motion: 15
60024863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 662
Checksum: 316
Coasting Arc #14 (Orbit 677)
---------------------------------------
Vector Time (GMT): 2011/205/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6158512
93 A = 6772140
37 meter
Y = -2664256
20 meter E =
0023107
Z = 798870
56 I = 51
49451
XDOT = 1258
445249 Wp = 29
36234
YDOT = 4707
967347 meter/sec RA = 331
17089 deg
ZDOT = 5946
879430 TA = 339
32663
MA = 339
41996
Ha = 214
916 n
mi
Hp = 203
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20205094
90 X = 6183966
70
Y = -8740998
05 feet Y = -2595245
73 meter
Z = 2620966
40 Z = 828849
92
XDOT = 4128
757380 XDOT = 1176
817694
YDOT = 15446
087096 feet/sec YDOT = 4721
583024 meter/sec
ZDOT = 19510
759285 ZDOT = 5952
795126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14102518
63 X = -4298447
68
Y = 16885375
13 feet Y = 5146662
34 meter
Z = 2742890
19 Z = 836032
93
XDOT = -9297
415009 XDOT = -2833
852095
YDOT = -10965
296688 feet/sec YDOT = -3342
222431 meter/sec
ZDOT = 19534
482974 ZDOT = 5954
110411
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 11205
79970990
00016717 00000-0 10270-3 0 9130
2 25544 51
6398 331
3967 0012170 3
0610 357
0618 15
59961479 6784
Satellite: ISS
Catalog Number: 25544
Epoch time: 11205
79970990 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 331
3967 deg
Eccentricity:
0012170
Arg of perigee: 3
0610 deg
Mean anomaly: 357
0618 deg
Mean motion: 15
59961479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 678
Checksum: 328
Coasting Arc #15 (Orbit 692)
---------------------------------------
Vector Time (GMT): 2011/206/17:41:39
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5488074
47 A = 6765406
89 meter
Y = -129979
30 meter E =
0016198
Z = -3971770
49 I = 51
44773
XDOT = 3012
594385 Wp = 29
32424
YDOT = -5825
805965 meter/sec RA = 326
14627 deg
ZDOT = -3965
074618 TA = 199
22674
MA = 199
28793
Ha = 214
918 n
mi
Hp = 203
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18005493
67 X = -5466919
18
Y = -426441
28 feet Y = -191231
54 meter
Z = -13030743
09 Z = -3998379
92
XDOT = 9883
839845 XDOT = 3096
777195
YDOT = -19113
536630 feet/sec YDOT = -5791
646140 meter/sec
ZDOT = -13008
774993 ZDOT = -3950
235789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16069818
86 X = 4898080
79
Y = -7956928
17 feet Y = -2425271
71 meter
Z = -13138802
67 Z = -4004707
05
XDOT = -512
760586 XDOT = -156
289427
YDOT = 20382
449265 feet/sec YDOT = 6212
570536 meter/sec
ZDOT = -12948
139095 ZDOT = -3946
592796
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 11206
76059821
00016717 00000-0 10270-3 0 9140
2 25544 51
6407 326
5635 0012015 6
6465 353
4848 15
60028077 6930
Satellite: ISS
Catalog Number: 25544
Epoch time: 11206
76059821 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 326
5635 deg
Eccentricity:
0012015
Arg of perigee: 6
6465 deg
Mean anomaly: 353
4848 deg
Mean motion: 15
60028077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 693
Checksum: 304
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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