[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 4th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10979 19 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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 3701)
---------------------------------------
Vector Time (GMT): 2012/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3667057
92 A = 6764650
21 meter
Y = 2247285
80 meter E =
0018467
Z = 5214974
97 I = 51
96161
XDOT = -2635
417598 Wp = 11
62583
YDOT = -7110
375691 meter/sec RA = 76
94051 deg
ZDOT = 1227
785041 TA = 66
76277
MA = 66
56842
Ha = 219
888 n
mi
Hp = 203
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12031029
93 X = -3717247
70
Y = 7372984
89 feet Y = 2205997
67 meter
Z = 17109497
92 Z = 5197039
06
XDOT = -8646
383194 XDOT = -2561
676280
YDOT = -23328
004235 feet/sec YDOT = -7139
434290 meter/sec
ZDOT = 4028
166145 ZDOT = 1215
161362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13619608
08 X = -4151256
54
Y = -4016221
84 feet Y = -1224144
42 meter
Z = 17035778
37 Z = 5192505
25
XDOT = 11131
879492 XDOT = 3392
996869
YDOT = -21116
585630 feet/sec YDOT = -6436
335300 meter/sec
ZDOT = 3976
966266 ZDOT = 1212
179318
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 12034
55019472
00016717 00000-0 10270-3 0 9000
2 25544 51
6407 77
4144 0020358 1
3772 358
7436 15
58661152 37028
Satellite: ISS
Catalog Number: 25544
Epoch time: 12034
55019472 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 77
4144 deg
Eccentricity:
0020358
Arg of perigee: 1
3772 deg
Mean anomaly: 358
7436 deg
Mean motion: 15
58661152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3702
Checksum: 292
Coasting Arc #2 (Orbit 3716)
---------------------------------------
Vector Time (GMT): 2012/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4470246
89 A = 6766011
83 meter
Y = 1302198
87 meter E =
0021464
Z = -4914404
46 I = 51
95903
XDOT = 441
595210 Wp = 38
06095
YDOT = 7287
467865 meter/sec RA = 71
91611 deg
ZDOT = 2354
583594 TA = 254
75811
MA = 254
99552
Ha = 220
038 n
mi
Hp = 203
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14666164
35 X = 4479225
76
Y = 4272306
00 feet Y = 1352238
30 meter
Z = -16123374
20 Z = -4892666
81
XDOT = 1448
803182 XDOT = 348
634676
YDOT = 23909
015304 feet/sec YDOT = 7291
886198 meter/sec
ZDOT = 7725
011792 ZDOT = 2356
503266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7009313
80 X = 2136438
85
Y = 13677775
36 feet Y = 4168985
93 meter
Z = -16034342
90 Z = -4887267
72
XDOT = -15451
097658 XDOT = -4709
494566
YDOT = 16897
902741 feet/sec YDOT = 5150
480755 meter/sec
ZDOT = 7732
301048 ZDOT = 2356
805359
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 12035
51191994
00016717 00000-0 10270-3 0 9018
2 25544 51
6416 72
5874 0020468 4
9178 355
2174 15
58656749 37178
Satellite: ISS
Catalog Number: 25544
Epoch time: 12035
51191994 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 72
5874 deg
Eccentricity:
0020468
Arg of perigee: 4
9178 deg
Mean anomaly: 355
2174 deg
Mean motion: 15
58656749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3717
Checksum: 330
Coasting Arc #3 (Orbit 3732)
---------------------------------------
Vector Time (GMT): 2012/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4279558
50 A = 6772736
16 meter
Y = -4443199
80 meter E =
0024256
Z = 2805988
85 I = 51
97057
XDOT = 2104
812043 Wp = 42
44820
YDOT = -5294
300381 meter/sec RA = 66
91394 deg
ZDOT = -5129
971998 TA = 105
84124
MA = 105
57371
Ha = 220
044 n
mi
Hp = 202
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14040546
26 X = -4243186
20
Y = -14577427
16 feet Y = -4490853
15 meter
Z = 9206000
16 Z = 2785287
71
XDOT = 6905
551323 XDOT = 2188
777150
YDOT = -17369
751907 feet/sec YDOT = -5270
293483 meter/sec
ZDOT = -16830
616791 ZDOT = -5119
543354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 603545
30 X = 183960
61
Y = -20268776
27 feet Y = -6177923
01 meter
Z = 9121469
31 Z = 2780223
84
XDOT = 15853
820029 XDOT = 4832
244345
YDOT = -7147
121373 feet/sec YDOT = -2178
442595 meter/sec
ZDOT = -16787
425129 ZDOT = -5116
807179
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 12036
53774461
00016717 00000-0 10270-3 0 9028
2 25544 51
6405 67
4376 0020524 9
0384 351
1137 15
58717680 37338
Satellite: ISS
Catalog Number: 25544
Epoch time: 12036
53774461 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 67
4376 deg
Eccentricity:
0020524
Arg of perigee: 9
0384 deg
Mean anomaly: 351
1137 deg
Mean motion: 15
58717680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3733
Checksum: 300
Coasting Arc #4 (Orbit 3748)
---------------------------------------
Vector Time (GMT): 2012/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2984581
37 A = 6776036
27 meter
Y = 6055034
40 meter E =
0031771
Z = 274009
07 I = 51
96900
XDOT = -4367
040814 Wp = 25
89243
YDOT = 1868
149002 meter/sec RA = 61
94157 deg
ZDOT = 6050
572517 TA = 337
05897
MA = 337
20057
Ha = 220
203 n
mi
Hp = 202
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9791933
63 X = 2915319
90
Y = 19865598
44 feet Y = 6088022
57 meter
Z = 898979
90 Z = 288339
41
XDOT = -14327
561725 XDOT = -4416
997755
YDOT = 6129
097775 feet/sec YDOT = 1819
034726 meter/sec
ZDOT = 19850
959703 ZDOT = 6029
236887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7039064
84 X = -2145506
96
Y = 20996841
63 feet Y = 6399837
33 meter
Z = 957255
42 Z = 291771
45
XDOT = -13044
271274 XDOT = -3975
893884
YDOT = -5306
928413 feet/sec YDOT = -1617
551780 meter/sec
ZDOT = 19763
314324 ZDOT = 6023
858206
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 12037
56355610
00016717 00000-0 10270-3 0 9034
2 25544 51
6409 62
2885 0020593 12
9097 347
2581 15
58706756 37498
Satellite: ISS
Catalog Number: 25544
Epoch time: 12037
56355610 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 62
2885 deg
Eccentricity:
0020593
Arg of perigee: 12
9097 deg
Mean anomaly: 347
2581 deg
Mean motion: 15
58706756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3749
Checksum: 326
Coasting Arc #5 (Orbit 3763)
---------------------------------------
Vector Time (GMT): 2012/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -738219
26 A = 6771300
47 meter
Y = -5881009
26 meter E =
0021949
Z = -3304200
45 I = 51
93799
XDOT = 5690
939333 Wp = 28
28723
YDOT = 1949
568289 meter/sec RA = 56
96365 deg
ZDOT = -4735
461607 TA = 189
91449
MA = 189
95786
Ha = 220
230 n
mi
Hp = 202
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2421979
20 X = -656351
17
Y = -19294649
80 feet Y = -5888806
81 meter
Z = -10840552
65 Z = -3307587
59
XDOT = 18671
060804 XDOT = 5691
719050
YDOT = 6396
221419 feet/sec YDOT = 2013
212125 meter/sec
ZDOT = -15536
291362 ZDOT = -4707
814231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11647380
47 X = 3550121
57
Y = -15562681
37 feet Y = -4743505
28 meter
Z = -10853964
84 Z = -3308288
48
XDOT = 7990
530972 XDOT = 2435
513840
YDOT = 16750
456193 feet/sec YDOT = 5105
539047 meter/sec
ZDOT = -15423
070906 ZDOT = -4700
952012
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 12038
52523870
00016717 00000-0 10270-3 0 9047
2 25544 51
6405 57
4601 0020526 16
5619 343
6203 15
58742510 37648
Satellite: ISS
Catalog Number: 25544
Epoch time: 12038
52523870 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 57
4601 deg
Eccentricity:
0020526
Arg of perigee: 16
5619 deg
Mean anomaly: 343
6203 deg
Mean motion: 15
58742510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3764
Checksum: 289
Coasting Arc #6 (Orbit 3779)
---------------------------------------
Vector Time (GMT): 2012/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1972743
38 A = 6764806
53 meter
Y = 3966493
71 meter E =
0019893
Z = 5098688
28 I = 51
89781
XDOT = -5603
399780 Wp = 34
42564
YDOT = -4976
179932 meter/sec RA = 51
95088 deg
ZDOT = 1715
943704 TA = 39
16875
MA = 39
02494
Ha = 220
429 n
mi
Hp = 202
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6472255
18 X = -2041718
49
Y = 13013430
82 feet Y = 3944047
87 meter
Z = 16727979
94 Z = 5088937
32
XDOT = -18383
857545 XDOT = -5555
674123
YDOT = -16326
049647 feet/sec YDOT = -5038
573670 meter/sec
ZDOT = 5629
736563 ZDOT = 1688
839548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13664724
56 X = -4165008
05
Y = 5085447
50 feet Y = 1550044
40 meter
Z = 16687669
34 Z = 5086401
61
XDOT = -2055
444418 XDOT = -626
499459
YDOT = -23495
468350 feet/sec YDOT = -7161
418753 meter/sec
ZDOT = 5518
991714 ZDOT = 1682
188674
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 12039
55101961
00016717 00000-0 10270-3 0 9055
2 25544 51
6393 52
3093 0020581 20
5198 339
6779 15
58760295 37802
Satellite: ISS
Catalog Number: 25544
Epoch time: 12039
55101961 = yrday
fracday
Element set: 905
Inclination: 51
6393 deg
RA of node: 52
3093 deg
Eccentricity:
0020581
Arg of perigee: 20
5198 deg
Mean anomaly: 339
6779 deg
Mean motion: 15
58760295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3780
Checksum: 321
Coasting Arc #7 (Orbit 3794)
---------------------------------------
Vector Time (GMT): 2012/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4363911
42 A = 6765133
12 meter
Y = -1140952
82 meter E =
0026031
Z = -5055252
10 I = 51
87976
XDOT = 3859
268835 Wp = 52
80560
YDOT = 6336
730021 meter/sec RA = 46
92031 deg
ZDOT = 1923
424079 TA = 235
67220
MA = 235
91882
Ha = 220
478 n
mi
Hp = 202
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14317294
69 X = 4400902
14
Y = -3743283
51 feet Y = -1091946
37 meter
Z = -16585472
77 Z = -5033963
00
XDOT = 12661
643161 XDOT = 3778
780083
YDOT = 20789
796658 feet/sec YDOT = 6379
436834 meter/sec
ZDOT = 6310
446454 ZDOT = 1941
975866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13243361
16 X = 4036576
48
Y = 6819223
53 feet Y = 2078499
33 meter
Z = -16498078
11 Z = -5028614
21
XDOT = -3950
878946 XDOT = -1204
227903
YDOT = 22946
358401 feet/sec YDOT = 6994
050041 meter/sec
ZDOT = 6386
004121 ZDOT = 1946
454056
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 12040
51267474
00016717 00000-0 10270-3 0 9066
2 25544 51
6399 47
4821 0020592 23
6966 336
5132 15
58762003 37955
Satellite: ISS
Catalog Number: 25544
Epoch time: 12040
51267474 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 47
4821 deg
Eccentricity:
0020592
Arg of perigee: 23
6966 deg
Mean anomaly: 336
5132 deg
Mean motion: 15
58762003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3795
Checksum: 315
Coasting Arc #8 (Orbit 3810)
---------------------------------------
Vector Time (GMT): 2012/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5723915
45 A = 6771680
01 meter
Y = -1869057
54 meter E =
0028254
Z = 3099534
06 I = 51
88004
XDOT = -767
083063 Wp = 52
48478
YDOT = -5853
543066 meter/sec RA = 41
90659 deg
ZDOT = -4898
997722 TA = 91
94099
MA = 91
61740
Ha = 220
490 n
mi
Hp = 201
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18779250
17 X = -5717646
41
Y = -6132078
54 feet Y = -1933030
61 meter
Z = 10169075
00 Z = 3071743
44
XDOT = -2516
676717 XDOT = -677
772791
YDOT = -19204
537618 feet/sec YDOT = -5861
622061 meter/sec
ZDOT = -16072
827171 ZDOT = -4902
506745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10250779
35 X = -3124437
54
Y = -16955404
83 feet Y = -5168007
39 meter
Z = 10055271
27 Z = 3064846
68
XDOT = 9486
338769 XDOT = 2891
436057
YDOT = -15368
437887 feet/sec YDOT = -4684
299868 meter/sec
ZDOT = -16086
733649 ZDOT = -4903
236416
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 12041
53842440
00016717 00000-0 10270-3 0 9072
2 25544 51
6392 42
3307 0020707 27
4356 332
7888 15
58837787 38111
Satellite: ISS
Catalog Number: 25544
Epoch time: 12041
53842440 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 42
3307 deg
Eccentricity:
0020707
Arg of perigee: 27
4356 deg
Mean anomaly: 332
7888 deg
Mean motion: 15
58837787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3811
Checksum: 317
Coasting Arc #9 (Orbit 3825)
---------------------------------------
Vector Time (GMT): 2012/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5429526
21 A = 6775580
33 meter
Y = 4023369
71 meter E =
0032395
Z = -58136
44 I = 51
87047
XDOT = -2797
148948 Wp = 36
28916
YDOT = 3837
079506 meter/sec RA = 36
92597 deg
ZDOT = 6048
781924 TA = 323
08423
MA = 323
30677
Ha = 220
433 n
mi
Hp = 201
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17813406
20 X = 5384414
96
Y = 13200031
85 feet Y = 4083833
78 meter
Z = -190736
35 Z = -31870
29
XDOT = -9176
997860 XDOT = -2869
231236
YDOT = 12588
843522 feet/sec YDOT = 3805
397449 meter/sec
ZDOT = 19845
085052 ZDOT = 6035
018351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5225139
35 X = 1592622
47
Y = 21547288
22 feet Y = 6567613
45 meter
Z = -83369
90 Z = -25411
15
XDOT = -13632
654146 XDOT = -4155
232984
YDOT = 3332
049656 feet/sec YDOT = 1015
608735 meter/sec
ZDOT = 19788
329066 ZDOT = 6031
482699
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 12042
50005166
00016717 00000-0 10270-3 0 9087
2 25544 51
6395 37
5037 0020510 31
5497 328
6883 15
58874755 38265
Satellite: ISS
Catalog Number: 25544
Epoch time: 12042
50005166 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 37
5037 deg
Eccentricity:
0020510
Arg of perigee: 31
5497 deg
Mean anomaly: 328
6883 deg
Mean motion: 15
58874755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3826
Checksum: 316
Coasting Arc #10 (Orbit 3841)
---------------------------------------
Vector Time (GMT): 2012/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3424833
98 A = 6771549
30 meter
Y = -4985810
32 meter E =
0022618
Z = -3077403
01 I = 51
83167
XDOT = 5789
768862 Wp = 45
47633
YDOT = -945
740271 meter/sec RA = 31
94211 deg
ZDOT = -4918
003162 TA = 169
74697
MA = 169
70076
Ha = 220
603 n
mi
Hp = 201
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11236331
95 X = -3353877
95
Y = -16357645
41 feet Y = -5023712
36 meter
Z = -10096466
56 Z = -3093867
88
XDOT = 18995
304665 XDOT = 5823
804288
YDOT = -3102
822412 feet/sec YDOT = -880
805478 meter/sec
ZDOT = -16135
180977 ZDOT = -4889
794327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1556886
46 X = 474538
99
Y = -19749546
99 feet Y = -6019661
92 meter
Z = -10163555
21 Z = -3097851
63
XDOT = 15376
819657 XDOT = 4686
854631
YDOT = 9444
711383 feet/sec YDOT = 2878
748029 meter/sec
ZDOT = -16019
438162 ZDOT = -4882
724752
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 12043
52577132
00016717 00000-0 10270-3 0 9098
2 25544 51
6391 32
3523 0020718 35
0986 325
1530 15
58852682 38420
Satellite: ISS
Catalog Number: 25544
Epoch time: 12043
52577132 = yrday
fracday
Element set: 909
Inclination: 51
6391 deg
RA of node: 32
3523 deg
Eccentricity:
0020718
Arg of perigee: 35
0986 deg
Mean anomaly: 325
1530 deg
Mean motion: 15
58852682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3842
Checksum: 302
Coasting Arc #11 (Orbit 3857)
---------------------------------------
Vector Time (GMT): 2012/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 182833
19 A = 6764759
23 meter
Y = 4518953
07 meter E =
0021817
Z = 5011759
93 I = 51
78272
XDOT = -7185
675265 Wp = 53
00818
YDOT = -1899
339844 meter/sec RA = 26
92482 deg
ZDOT = 1981
646021 TA = 17
88879
MA = 17
81212
Ha = 220
638 n
mi
Hp = 200
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 599846
44 X = 107942
02
Y = 14825961
51 feet Y = 4520579
06 meter
Z = 16442781
91 Z = 5012466
05
XDOT = -23575
050083 XDOT = -7173
528701
YDOT = -6231
429935 feet/sec YDOT = -1979
626510 meter/sec
ZDOT = 6501
463322 ZDOT = 1946
768262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8704989
08 X = -2653280
67
Y = 12012894
75 feet Y = 3661530
32 meter
Z = 16445289
67 Z = 5012524
29
XDOT = -13943
359574 XDOT = -4249
935998
YDOT = -18777
522348 feet/sec YDOT = -5723
388812 meter/sec
ZDOT = 6358
623188 ZDOT = 1938
108348
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 12044
55147375
00016717 00000-0 10270-3 0 9106
2 25544 51
6391 27
2023 0020657 38
4048 321
8573 15
58882279 38588
Satellite: ISS
Catalog Number: 25544
Epoch time: 12044
55147375 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 27
2023 deg
Eccentricity:
0020657
Arg of perigee: 38
4048 deg
Mean anomaly: 321
8573 deg
Mean motion: 15
58882279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3858
Checksum: 318
Coasting Arc #12 (Orbit 3872)
---------------------------------------
Vector Time (GMT): 2012/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3268371
49 A = 6764547
95 meter
Y = -3027747
60 meter E =
0029586
Z = -5110038
34 I = 51
75438
XDOT = 6317
531843 Wp = 64
88478
YDOT = 3982
466969 meter/sec RA = 21
88432 deg
ZDOT = 1700
969135 TA = 221
42856
MA = 221
65327
Ha = 220
715 n
mi
Hp = 200
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10723003
59 X = 3326808
59
Y = -9933555
12 feet Y = -2990871
98 meter
Z = -16765217
66 Z = -5094018
94
XDOT = 20726
810507 XDOT = 6264
266734
YDOT = 13065
836514 feet/sec YDOT = 4052
815705 meter/sec
ZDOT = 5580
607398 ZDOT = 1731
529637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14620454
44 X = 4456314
51
Y = -1451690
96 feet Y = -442475
41 meter
Z = -16699273
98 Z = -5089938
71
XDOT = 8606
663786 XDOT = 2623
311122
YDOT = 21803
019077 feet/sec YDOT = 6645
560215 meter/sec
ZDOT = 5705
561298 ZDOT = 1739
055084
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 12045
51305516
00016717 00000-0 10270-3 0 9117
2 25544 51
6393 22
3742 0020708 42
0817 318
1924 15
58880110 38734
Satellite: ISS
Catalog Number: 25544
Epoch time: 12045
51305516 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 22
3742 deg
Eccentricity:
0020708
Arg of perigee: 42
0817 deg
Mean anomaly: 318
1924 deg
Mean motion: 15
58880110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3873
Checksum: 285
Coasting Arc #13 (Orbit 3888)
---------------------------------------
Vector Time (GMT): 2012/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5888745
64 A = 6771065
80 meter
Y = 867580
96 meter E =
0030820
Z = 3219463
07 I = 51
74800
XDOT = -3374
399094 Wp = 63
22076
YDOT = -4964
813347 meter/sec RA = 16
85974 deg
ZDOT = -4785
351025 TA = 79
49157
MA = 79
14447
Ha = 220
729 n
mi
Hp = 200
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19320031
63 X = -5913648
63
Y = 2846394
23 feet Y = 801590
13 meter
Z = 10562542
89 Z = 3190795
75
XDOT = -11070
863170 XDOT = -3295
384950
YDOT = -16288
757700 feet/sec YDOT = -5002
106157 meter/sec
ZDOT = -15699
970555 ZDOT = -4801
551549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17372821
86 X = -5295236
10
Y = -9056567
54 feet Y = -2760441
79 meter
Z = 10444928
90 Z = 3183614
33
XDOT = -2
937906 XDOT = -
895474
YDOT = -18364
226430 feet/sec YDOT = -5597
416216 meter/sec
ZDOT = -15765
957821 ZDOT = -4805
463944
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 12046
53872478
00016717 00000-0 10270-3 0 9127
2 25544 51
6392 17
2231 0020720 45
5902 314
6945 15
58939476 38897
Satellite: ISS
Catalog Number: 25544
Epoch time: 12046
53872478 = yrday
fracday
Element set: 912
Inclination: 51
6392 deg
RA of node: 17
2231 deg
Eccentricity:
0020720
Arg of perigee: 45
5902 deg
Mean anomaly: 314
6945 deg
Mean motion: 15
58939476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3889
Checksum: 328
Coasting Arc #14 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2012/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6641971
55 A = 6775300
56 meter
Y = 1249150
33 meter E =
0032526
Z = -181959
10 I = 51
73323
XDOT = -739
153778 Wp = 47
24701
YDOT = 4706
634740 meter/sec RA = 11
86806 deg
ZDOT = 6031
909672 TA = 310
78857
MA = 311
07031
Ha = 220
695 n
mi
Hp = 200
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21791245
24 X = 6628393
55
Y = 4098262
24 feet Y = 1323349
03 meter
Z = -596978
67 Z = -149726
30
XDOT = -2425
045205 XDOT = -821
030465
YDOT = 15441
715027 feet/sec YDOT = 4697
911236 meter/sec
ZDOT = 19789
729896 ZDOT = 6028
120120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15529083
17 X = 4733264
55
Y = 15831674
60 feet Y = 4825494
42 meter
Z = -464931
39 Z = -141711
09
XDOT = -9769
108347 XDOT = -2977
624224
YDOT = 10076
264569 feet/sec YDOT = 3071
245441 meter/sec
ZDOT = 19773
776939 ZDOT = 6027
047211
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 12047
50027498
00016717 00000-0 10270-3 0 9130
2 25544 51
6393 12
3952 0020688 49
6279 310
6678 15
58967174 39042
Satellite: ISS
Catalog Number: 25544
Epoch time: 12047
50027498 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 12
3952 deg
Eccentricity:
0020688
Arg of perigee: 49
6279 deg
Mean anomaly: 310
6678 deg
Mean motion: 15
58967174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 336
Coasting Arc #15 (Orbit 3919)
---------------------------------------
Vector Time (GMT): 2012/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5267528
82 A = 6771276
02 meter
Y = -3034183
04 meter E =
0023598
Z = -3014955
08 I = 51
69113
XDOT = 4766
095186 Wp = 61
49256
YDOT = -3368
547531 meter/sec RA = 6
87498 deg
ZDOT = -4955
475633 TA = 152
99637
MA = 152
87339
Ha = 220
699 n
mi
Hp = 200
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17281918
69 X = -5218562
86
Y = -9954668
75 feet Y = -3092814
01 meter
Z = -9891584
91 Z = -3040424
94
XDOT = 15636
795229 XDOT = 4827
480738
YDOT = -11051
665127 feet/sec YDOT = -3314
906902 meter/sec
ZDOT = -16258
122155 ZDOT = -4932
173607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8736118
03 X = -2662768
78
Y = -17870894
86 feet Y = -5447048
75 meter
Z = -9995746
81 Z = -3046703
63
XDOT = 17921
880551 XDOT = 5462
589192
YDOT = 245
426637 feet/sec YDOT = 74
806039 meter/sec
ZDOT = -16162
283633 ZDOT = -4926
264051
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 12048
52591123
00016717 00000-0 10270-3 0 9145
2 25544 51
6402 7
2436 0020738 52
9742 307
3307 15
58991853 39202
Satellite: ISS
Catalog Number: 25544
Epoch time: 12048
52591123 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 7
2436 deg
Eccentricity:
0020738
Arg of perigee: 52
9742 deg
Mean anomaly: 307
3307 deg
Mean motion: 15
58991853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3920
Checksum: 301
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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