[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 12th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 ET - UTC (sec) : 67 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
348/14:31:56
248 -1
0 1
4 1
4
N/A 0
9 0
1 230
5
000/00:07:48
495 -0
4 0
3 213
2
Coasting Arc #1 (Orbit 571)
---------------------------------------
Vector Time (GMT): 2012/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5631816
02 A = 6790991
02 meter
Y = -2037079
44 meter E =
0026010
Z = 3165873
71 I = 51
40576
XDOT = -553
656289 Wp = 54
86492
YDOT = 5963
038932 meter/sec RA = 315
15944 deg
ZDOT = 4808
543421 TA = 341
85785
MA = 341
95049
Ha = 229
538 n
mi
Hp = 213
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18477086
68 X = 5638797
23
Y = -6683331
50 feet Y = -1974062
32 meter
Z = 10386724
78 Z = 3193249
82
XDOT = -1816
457640 XDOT = -643
654162
YDOT = 19563
776023 feet/sec YDOT = 5956
343780 meter/sec
ZDOT = 15776
061093 ZDOT = 4805
635911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3646152
67 X = 1111347
33
Y = 19245752
70 feet Y = 5866105
42 meter
Z = 10500489
39 Z = 3200549
17
XDOT = -17602
193973 XDOT = -5365
148723
YDOT = -5289
138015 feet/sec YDOT = -1612
129267 meter/sec
ZDOT = 15763
197461 ZDOT = 4804
622586
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 12347
55778753
00016717 00000-0 10270-3 0 9001
2 25544 51
6461 315
4538 0016466 31
6189 328
5948 15
52064960 5726
Satellite: ISS
Catalog Number: 25544
Epoch time: 12347
55778753 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 315
4538 deg
Eccentricity:
0016466
Arg of perigee: 31
6189 deg
Mean anomaly: 328
5948 deg
Mean motion: 15
52064960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 572
Checksum: 331
Coasting Arc #2 (Orbit 586)
---------------------------------------
Vector Time (GMT): 2012/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5350829
79 A = 6788724
00 meter
Y = 1455076
65 meter E =
0022430
Z = -3942707
01 I = 51
37760
XDOT = 1212
867024 Wp = 45
44741
YDOT = -6397
941391 meter/sec RA = 310
17246 deg
ZDOT = -4005
974451 TA = 182
42919
MA = 182
44010
Ha = 229
846 n
mi
Hp = 213
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17555215
84 X = -5347550
21
Y = 4773873
51 feet Y = 1395259
20 meter
Z = -12935390
46 Z = -3968693
05
XDOT = 3979
222520 XDOT = 1303
780207
YDOT = -20990
621361 feet/sec YDOT = -6383
869478 meter/sec
ZDOT = -13142
960796 ZDOT = -3999
862426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2220974
81 X = -676953
12
Y = -17978846
39 feet Y = -5479952
38 meter
Z = -13043318
25 Z = -3975603
40
XDOT = 18882
701814 XDOT = 5755
447513
YDOT = 7186
299123 feet/sec YDOT = 2190
383973 meter/sec
ZDOT = -13116
755877 ZDOT = -3997
987191
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 12348
52362086
00016717 00000-0 10270-3 0 9018
2 25544 51
6465 310
6535 0016713 35
1626 325
0625 15
52050606 5876
Satellite: ISS
Catalog Number: 25544
Epoch time: 12348
52362086 = yrday
fracday
Element set: 901
Inclination: 51
6465 deg
RA of node: 310
6535 deg
Eccentricity:
0016713
Arg of perigee: 35
1626 deg
Mean anomaly: 325
0625 deg
Mean motion: 15
52050606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 587
Checksum: 288
Coasting Arc #3 (Orbit 588)
---------------------------------------
Vector Time (GMT): 2012/348/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1297413
55 A = 6786049
35 meter
Y = 4537172
83 meter E =
0023694
Z = 4868536
68 I = 51
36558
XDOT = -5943
401195 Wp = 44
18041
YDOT = 4243
337563 meter/sec RA = 309
58961 deg
ZDOT = -2347
061115 TA = 69
00697
MA = 68
75364
Ha = 230
455 n
mi
Hp = 213
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4256606
12 X = 1222931
17
Y = 14885737
63 feet Y = 4551264
19 meter
Z = 15972889
36 Z = 4874659
19
XDOT = -19499
347753 XDOT = -5979
007825
YDOT = 13921
711164 feet/sec YDOT = 4176
675972 meter/sec
ZDOT = -7700
331741 ZDOT = -2376
019901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10651487
88 X = -3246573
51
Y = 11200795
60 feet Y = 3414002
50 meter
Z = 15997657
92 Z = 4876086
13
XDOT = -21106
557372 XDOT = -6433
278687
YDOT = -8790
609844 feet/sec YDOT = -2679
377881 meter/sec
ZDOT = -7820
961472 ZDOT = -2383
829057
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 12348
65240770
00016717 00000-0 10270-3 0 9028
2 25544 51
6483 310
0145 0017136 38
7491 321
4886 15
51794294 5894
Satellite: ISS
Catalog Number: 25544
Epoch time: 12348
65240770 = yrday
fracday
Element set: 902
Inclination: 51
6483 deg
RA of node: 310
0145 deg
Eccentricity:
0017136
Arg of perigee: 38
7491 deg
Mean anomaly: 321
4886 deg
Mean motion: 15
51794294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 589
Checksum: 316
Coasting Arc #4 (Orbit 603)
---------------------------------------
Vector Time (GMT): 2012/349/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -835480
91 A = 6787687
31 meter
Y = -5062944
76 meter E =
0022318
Z = -4455256
79 I = 51
35308
XDOT = 5788
546979 Wp = 64
70472
YDOT = -3802
961436 meter/sec RA = 304
59824 deg
ZDOT = 3258
343064 TA = 238
21499
MA = 238
43256
Ha = 230
499 n
mi
Hp = 213
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2741079
11 X = -757161
34
Y = -16610711
17 feet Y = -5071849
14 meter
Z = -14616984
21 Z = -4459125
93
XDOT = 18991
295862 XDOT = 5814
814024
YDOT = -12476
907598 feet/sec YDOT = -3738
083846 meter/sec
ZDOT = 10690
101916 ZDOT = 3286
526792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12717539
92 X = 3876306
17
Y = -11011089
22 feet Y = -3356179
99 meter
Z = -14632346
37 Z = -4459939
17
XDOT = 19776
313304 XDOT = 6027
820295
YDOT = 8575
983906 feet/sec YDOT = 2613
959895 meter/sec
ZDOT = 10807
461288 ZDOT = 3294
114201
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 12349
61838937
00016717 00000-0 10270-3 0 9034
2 25544 51
6489 305
2162 0017152 42
2464 318
0006 15
51807818 6044
Satellite: ISS
Catalog Number: 25544
Epoch time: 12349
61838937 = yrday
fracday
Element set: 903
Inclination: 51
6489 deg
RA of node: 305
2162 deg
Eccentricity:
0017152
Arg of perigee: 42
2464 deg
Mean anomaly: 318
0006 deg
Mean motion: 15
51807818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 604
Checksum: 302
Coasting Arc #5 (Orbit 619)
---------------------------------------
Vector Time (GMT): 2012/350/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 348163
73 A = 6789853
95 meter
Y = 5588968
97 meter E =
0027174
Z = 3830515
74 I = 51
34369
XDOT = -5614
908289 Wp = 60
12981
YDOT = 3201
507001 meter/sec RA = 299
60827 deg
ZDOT = -4125
483027 TA = 73
56800
MA = 73
26950
Ha = 230
576 n
mi
Hp = 212
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1142269
46 X = 267033
19
Y = 18336512
35 feet Y = 5592408
29 meter
Z = 12567308
86 Z = 3832010
66
XDOT = -18421
615120 XDOT = -5630
250382
YDOT = 10503
631892 feet/sec YDOT = 3138
632269 meter/sec
ZDOT = -13535
049302 ZDOT = -4152
796707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14836062
82 X = -4522031
95
Y = 10829889
81 feet Y = 3300950
41 meter
Z = 12572765
95 Z = 3832179
06
XDOT = -17973
088917 XDOT = -5478
197502
YDOT = -8641
760379 feet/sec YDOT = -2634
008563 meter/sec
ZDOT = -13648
721507 ZDOT = -4160
130315
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 12350
64875994
00016717 00000-0 10270-3 0 9044
2 25544 51
6487 300
0979 0017151 46
1671 314
0895 15
51815462 6207
Satellite: ISS
Catalog Number: 25544
Epoch time: 12350
64875994 = yrday
fracday
Element set: 904
Inclination: 51
6487 deg
RA of node: 300
0979 deg
Eccentricity:
0017151
Arg of perigee: 46
1671 deg
Mean anomaly: 314
0895 deg
Mean motion: 15
51815462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 620
Checksum: 315
Coasting Arc #6 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2012/351/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -21797
85 A = 6791753
75 meter
Y = -6014158
87 meter E =
0021260
Z = -3156315
58 I = 51
33675
XDOT = 5395
702134 Wp = 55
05745
YDOT = -2527
858923 meter/sec RA = 294
62063 deg
ZDOT = 4814
445999 TA = 268
42007
MA = 268
66360
Ha = 230
560 n
mi
Hp = 212
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -71515
24 X = 60787
89
Y = -19731492
37 feet Y = -6013940
58 meter
Z = -10355366
06 Z = -3156221
41
XDOT = 17702
434822 XDOT = 5400
180886
YDOT = -8293
500402 feet/sec YDOT = -2467
496198 meter/sec
ZDOT = 15795
426505 ZDOT = 4840
668491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16394721
47 X = 4997111
10
Y = -10980637
10 feet Y = -3346898
19 meter
Z = -10354188
93 Z = -3155956
79
XDOT = 15881
954304 XDOT = 4840
819672
YDOT = 8823
937555 feet/sec YDOT = 2689
536167 meter/sec
ZDOT = 15904
484636 ZDOT = 4847
686917
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 12351
61472212
00016717 00000-0 10270-3 0 9059
2 25544 51
6493 295
2998 0017140 49
5611 310
7033 15
51845847 6352
Satellite: ISS
Catalog Number: 25544
Epoch time: 12351
61472212 = yrday
fracday
Element set: 905
Inclination: 51
6493 deg
RA of node: 295
2998 deg
Eccentricity:
0017140
Arg of perigee: 49
5611 deg
Mean anomaly: 310
7033 deg
Mean motion: 15
51845847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 305
Coasting Arc #7 (Orbit 650)
---------------------------------------
Vector Time (GMT): 2012/352/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -331878
08 A = 6793795
90 meter
Y = 6383223
52 meter E =
0027588
Z = 2289686
64 I = 51
33119
XDOT = -5181
400607 Wp = 77
26594
YDOT = 1686
018118 meter/sec RA = 289
63485 deg
ZDOT = -5390
233996 TA = 77
14418
MA = 76
83611
Ha = 230
648 n
mi
Hp = 212
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1088838
83 X = -414354
64
Y = 20942334
40 feet Y = 6379050
95 meter
Z = 7512095
26 Z = 2287874
51
XDOT = -16999
345824 XDOT = -5173
684611
YDOT = 5531
555505 feet/sec YDOT = 1628
119968 meter/sec
ZDOT = -17684
494738 ZDOT = -5415
385932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17849670
32 X = -5440579
51
Y = 11012783
46 feet Y = 3356696
40 meter
Z = 7503758
08 Z = 2287145
46
XDOT = -13373
107773 XDOT = -4076
123249
YDOT = -9417
742957 feet/sec YDOT = -2870
528053 meter/sec
ZDOT = -17789
003297 ZDOT = -5422
088205
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 12352
64507246
00016717 00000-0 10270-3 0 9060
2 25544 51
6489 290
1810 0017135 53
5195 306
7533 15
51836453 6511
Satellite: ISS
Catalog Number: 25544
Epoch time: 12352
64507246 = yrday
fracday
Element set: 906
Inclination: 51
6489 deg
RA of node: 290
1810 deg
Eccentricity:
0017135
Arg of perigee: 53
5195 deg
Mean anomaly: 306
7533 deg
Mean motion: 15
51836453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 651
Checksum: 305
Coasting Arc #8 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2012/353/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 540527
98 A = 6795011
86 meter
Y = -6612264
72 meter E =
0025284
Z = -1436142
54 I = 51
32675
XDOT = 4985
782842 Wp = 50
26180
YDOT = -826
504258 meter/sec RA = 284
65078 deg
ZDOT = 5765
510153 TA = 294
01475
MA = 294
27921
Ha = 230
595 n
mi
Hp = 212
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1773385
78 X = 621403
96
Y = -21693781
89 feet Y = -6605767
92 meter
Z = -4711753
73 Z = -1433320
61
XDOT = 16357
555255 XDOT = 4966
647073
YDOT = -2711
628143 feet/sec YDOT = -770
857420 meter/sec
ZDOT = 18915
715724 ZDOT = 5789
684175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18657193
28 X = 5686712
51
Y = -11215714
37 feet Y = -3418549
74 meter
Z = -4699210
91 Z = -1432319
49
XDOT = 10872
786939 XDOT = 3314
025459
YDOT = 10234
540742 feet/sec YDOT = 3119
488018 meter/sec
ZDOT = 19016
058688 ZDOT = 5796
094688
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 12353
61101516
00016717 00000-0 10270-3 0 9079
2 25544 51
6493 285
3828 0017106 56
6395 303
6391 15
51876212 6666
Satellite: ISS
Catalog Number: 25544
Epoch time: 12353
61101516 = yrday
fracday
Element set: 907
Inclination: 51
6493 deg
RA of node: 285
3828 deg
Eccentricity:
0017106
Arg of perigee: 56
6395 deg
Mean anomaly: 303
6391 deg
Mean motion: 15
51876212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 666
Checksum: 309
Coasting Arc #9 (Orbit 681)
---------------------------------------
Vector Time (GMT): 2012/354/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -795605
91 A = 6795869
81 meter
Y = 6733877
73 meter E =
0024650
Z = 432911
74 I = 51
32240
XDOT = -4810
514276 Wp = 89
79741
YDOT = -166
284445 meter/sec RA = 279
66780 deg
ZDOT = -5958
855704 TA = 85
52119
MA = 85
23963
Ha = 230
672 n
mi
Hp = 212
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2610255
60 X = -872949
39
Y = 22092774
72 feet Y = 6724548
30 meter
Z = 1420314
11 Z = 428859
19
XDOT = -15782
527151 XDOT = -4779
350660
YDOT = -545
552641 feet/sec YDOT = -219
904098 meter/sec
ZDOT = -19550
051523 ZDOT = -5982
149185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19269599
37 X = -5873373
89
Y = 11119195
07 feet Y = 3389130
66 meter
Z = 1402662
66 Z = 427531
58
XDOT = -8121
216407 XDOT = -2475
346761
YDOT = -11471
924296 feet/sec YDOT = -3496
642525 meter/sec
ZDOT = -19646
618418 ZDOT = -5988
289294
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 12354
64134538
00016717 00000-0 10270-3 0 9084
2 25544 51
6491 280
2636 0017049 60
7881 299
4973 15
51853449 6820
Satellite: ISS
Catalog Number: 25544
Epoch time: 12354
64134538 = yrday
fracday
Element set: 908
Inclination: 51
6491 deg
RA of node: 280
2636 deg
Eccentricity:
0017049
Arg of perigee: 60
7881 deg
Mean anomaly: 299
4973 deg
Mean motion: 15
51853449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 682
Checksum: 338
Coasting Arc #10 (Orbit 697)
---------------------------------------
Vector Time (GMT): 2012/355/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 943121
43 A = 6795715
19 meter
Y = -6699534
93 meter E =
0029812
Z = 490630
51 I = 51
31818
XDOT = 4698
148372 Wp = 57
87063
YDOT = 1116
374665 meter/sec RA = 274
68462 deg
ZDOT = 5962
339102 TA = 307
44569
MA = 307
71655
Ha = 230
608 n
mi
Hp = 212
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3094230
41 X = 1015583
57
Y = -21980101
49 feet Y = -6688583
23 meter
Z = 1609680
15 Z = 495387
83
XDOT = 15413
872613 XDOT = 4656
351997
YDOT = 3662
646539 feet/sec YDOT = 1168
678313 meter/sec
ZDOT = 19561
479994 ZDOT = 5985
061000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19270981
14 X = 5873795
05
Y = -11011893
16 feet Y = -3356425
03 meter
Z = 1630241
87 Z = 496897
72
XDOT = 5658
332973 XDOT = 1724
659890
YDOT = 12932
243922 feet/sec YDOT = 3941
747947 meter/sec
ZDOT = 19655
560164 ZDOT = 5991
014738
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 12355
67166361
00016717 00000-0 10270-3 0 9098
2 25544 51
6491 275
1450 0017068 63
8309 296
4596 15
51901931 6982
Satellite: ISS
Catalog Number: 25544
Epoch time: 12355
67166361 = yrday
fracday
Element set: 909
Inclination: 51
6491 deg
RA of node: 275
1450 deg
Eccentricity:
0017068
Arg of perigee: 63
8309 deg
Mean anomaly: 296
4596 deg
Mean motion: 15
51901931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 698
Checksum: 334
Coasting Arc #11 (Orbit 712)
---------------------------------------
Vector Time (GMT): 2012/356/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1167093
12 A = 6794894
54 meter
Y = 6527729
22 meter E =
0020700
Z = -1500028
49 I = 51
31376
XDOT = -4603
356038 Wp = 90
25859
YDOT = -2124
998175 meter/sec RA = 269
70086 deg
ZDOT = -5734
822703 TA = 106
15990
MA = 105
93197
Ha = 230
639 n
mi
Hp = 212
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3829045
68 X = -1232714
02
Y = 21416434
45 feet Y = 6514311
23 meter
Z = -4921353
32 Z = -1505857
20
XDOT = -15102
874141 XDOT = -4551
393225
YDOT = -6971
778791 feet/sec YDOT = -2176
184917 meter/sec
ZDOT = -18815
035115 ZDOT = -5757
059528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19085612
80 X = -5817294
78
Y = 10431594
94 feet Y = 3179550
14 meter
Z = -4946330
46 Z = -1507641
52
XDOT = -3172
804534 XDOT = -967
070822
YDOT = -14663
214706 feet/sec YDOT = -4469
347843 meter/sec
ZDOT = -18906
982707 ZDOT = -5762
848329
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 12356
63757917
00016717 00000-0 10270-3 0 9100
2 25544 51
6491 270
3459 0016918 67
7319 292
5624 15
51882174 7139
Satellite: ISS
Catalog Number: 25544
Epoch time: 12356
63757917 = yrday
fracday
Element set: 910
Inclination: 51
6491 deg
RA of node: 270
3459 deg
Eccentricity:
0016918
Arg of perigee: 67
7319 deg
Mean anomaly: 292
5624 deg
Mean motion: 15
51882174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 713
Checksum: 333
Coasting Arc #12 (Orbit 728)
---------------------------------------
Vector Time (GMT): 2012/357/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1330401
13 A = 6793375
63 meter
Y = -6210512
16 meter E =
0030790
Z = 2368457
33 I = 51
30979
XDOT = 4586
058136 Wp = 71
94703
YDOT = 3041
831017 meter/sec RA = 264
71469 deg
ZDOT = 5352
126648 TA = 314
64535
MA = 314
89597
Ha = 230
609 n
mi
Hp = 212
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4364833
09 X = 1388244
04
Y = -20375696
06 feet Y = -6195311
53 meter
Z = 7770529
31 Z = 2375060
45
XDOT = 15046
122492 XDOT = 4525
703410
YDOT = 9979
760556 feet/sec YDOT = 3092
777355 meter/sec
ZDOT = 17559
470630 ZDOT = 5374
259177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18433568
92 X = 5618551
81
Y = -9694642
77 feet Y = -2954927
12 meter
Z = 7798674
37 Z = 2377035
95
XDOT = 1156
650000 XDOT = 352
546920
YDOT = 16524
488726 feet/sec YDOT = 5036
664164 meter/sec
ZDOT = 17650
878589 ZDOT = 5379
987794
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 12357
66787875
00016717 00000-0 10270-3 0 9111
2 25544 51
6488 265
2268 0017027 70
7703 289
5289 15
51919591 7293
Satellite: ISS
Catalog Number: 25544
Epoch time: 12357
66787875 = yrday
fracday
Element set: 911
Inclination: 51
6488 deg
RA of node: 265
2268 deg
Eccentricity:
0017027
Arg of perigee: 70
7703 deg
Mean anomaly: 289
5289 deg
Mean motion: 15
51919591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 729
Checksum: 358
Coasting Arc #13 (Orbit 743)
---------------------------------------
Vector Time (GMT): 2012/358/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1599304
56 A = 6791267
37 meter
Y = 5758964
41 meter E =
0021151
Z = -3247045
87 I = 51
30624
XDOT = -4559
466927 Wp = 79
47921
YDOT = -3919
433963 meter/sec RA = 259
72613 deg
ZDOT = -4728
399939 TA = 138
22754
MA = 138
06588
Ha = 230
590 n
mi
Hp = 212
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5247062
20 X = -1647810
19
Y = 18894240
18 feet Y = 5740809
05 meter
Z = -10653037
64 Z = -3254932
58
XDOT = -14958
880994 XDOT = -4492
330566
YDOT = -12859
035313 feet/sec YDOT = -3970
044998 meter/sec
ZDOT = -15513
123158 ZDOT = -4750
386935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17704210
46 X = -5396243
35
Y = 8388799
28 feet Y = 2556906
02 meter
Z = -10686447
66 Z = -3257229
25
XDOT = 672
838472 XDOT = 205
081166
YDOT = -18363
421147 feet/sec YDOT = -5597
170766 meter/sec
ZDOT = -15603
827905 ZDOT = -4756
046745
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 12358
63377546
00016717 00000-0 10270-3 0 9120
2 25544 51
6483 260
4277 0016839 74
5561 285
7449 15
51923213 7448
Satellite: ISS
Catalog Number: 25544
Epoch time: 12358
63377546 = yrday
fracday
Element set: 912
Inclination: 51
6483 deg
RA of node: 260
4277 deg
Eccentricity:
0016839
Arg of perigee: 74
5561 deg
Mean anomaly: 285
7449 deg
Mean motion: 15
51923213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 744
Checksum: 332
Coasting Arc #14 (Orbit 759)
---------------------------------------
Vector Time (GMT): 2012/359/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1849637
28 A = 6789112
85 meter
Y = -5194825
67 meter E =
0027502
Z = 3935248
87 I = 51
30518
XDOT = 4594
294550 Wp = 86
58579
YDOT = 4679
379590 meter/sec RA = 254
73434 deg
ZDOT = 3995
155898 TA = 321
51068
MA = 321
70650
Ha = 230
602 n
mi
Hp = 211
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6068363
77 X = 1888472
87
Y = -17043391
32 feet Y = -5173925
12 meter
Z = 12910921
50 Z = 3944328
16
XDOT = 15073
144849 XDOT = 4522
219695
YDOT = 15352
295243 feet/sec YDOT = 4730
352482 meter/sec
ZDOT = 13107
466858 ZDOT = 4017
300193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16711559
78 X = 5093683
42
Y = -6858273
96 feet Y = -2090401
90 meter
Z = 12949207
25 Z = 3946918
37
XDOT = -1999
503067 XDOT = -609
448535
YDOT = 20187
994468 feet/sec YDOT = 6153
300714 meter/sec
ZDOT = 13198
741409 ZDOT = 4022
976381
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 12359
66405730
00016717 00000-0 10270-3 0 9132
2 25544 51
6480 255
3085 0016993 77
8850 282
4205 15
51931814 7601
Satellite: ISS
Catalog Number: 25544
Epoch time: 12359
66405730 = yrday
fracday
Element set: 913
Inclination: 51
6480 deg
RA of node: 255
3085 deg
Eccentricity:
0016993
Arg of perigee: 77
8850 deg
Mean anomaly: 282
4205 deg
Mean motion: 15
51931814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 760
Checksum: 317
Coasting Arc #15 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2012/360/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2219834
00 A = 6786838
23 meter
Y = 4535138
33 meter E =
0026597
Z = -4560599
36 I = 51
30571
XDOT = -4572
323978 Wp = 77
34540
YDOT = -5306
603913 meter/sec RA = 249
73906 deg
ZDOT = -3060
916824 TA = 161
83620
MA = 161
74101
Ha = 230
553 n
mi
Hp = 211
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7282919
94 X = -2248227
55
Y = 14879062
77 feet Y = 4510156
50 meter
Z = -14962596
34 Z = -4571451
68
XDOT = -15001
062920 XDOT = -4497
775363
YDOT = -17410
117824 feet/sec YDOT = -5357
317341 meter/sec
ZDOT = -10042
378032 ZDOT = -3082
948450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15813877
51 X = -4820069
86
Y = 4794085
97 feet Y = 1461237
40 meter
Z = -15008155
74 Z = -4574485
87
XDOT = 3029
743726 XDOT = 923
465888
YDOT = -21631
259875 feet/sec YDOT = -6593
208010 meter/sec
ZDOT = -10133
121719 ZDOT = -3088
575500
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 12360
62993585
00016717 00000-0 10270-3 0 9141
2 25544 51
6469 250
5090 0016812 81
6523 278
6534 15
51960208 7758
Satellite: ISS
Catalog Number: 25544
Epoch time: 12360
62993585 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 250
5090 deg
Eccentricity:
0016812
Arg of perigee: 81
6523 deg
Mean anomaly: 278
6534 deg
Mean motion: 15
51960208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 323
Coasting Arc #16 (Orbit 790)
---------------------------------------
Vector Time (GMT): 2012/361/14:35:50
495
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2596167
37 A = 6785130
05 meter
Y = -3808229
08 meter E =
0022078
Z = 4961012
87 I = 51
31129
XDOT = 4570
971905 Wp = 95
14395
YDOT = 5816
489998 meter/sec RA = 244
74197 deg
ZDOT = 2062
985503 TA = 334
67267
MA = 334
78074
Ha = 230
546 n
mi
Hp = 211
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8517609
48 X = 2614459
46
Y = -12494189
91 feet Y = -3779095
42 meter
Z = 16276288
93 Z = 4973668
87
XDOT = 14996
626984 XDOT = 4495
569488
YDOT = 19082
972436 feet/sec YDOT = 5867
183627 meter/sec
ZDOT = 6768
325141 ZDOT = 2085
008516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14849858
21 X = 4526236
78
Y = -2531708
27 feet Y = -771664
68 meter
Z = 16329243
65 Z = 4977153
47
XDOT = -3671
959456 XDOT = -1119
213242
YDOT = 22910
080516 feet/sec YDOT = 6982
992541 meter/sec
ZDOT = 6858
986615 ZDOT = 2090
619120
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 12361
66019962
00016717 00000-0 10270-3 0 9155
2 25544 51
6467 245
3899 0016932 85
3312 274
9773 15
51951770 7911
Satellite: ISS
Catalog Number: 25544
Epoch time: 12361
66019962 = yrday
fracday
Element set: 915
Inclination: 51
6467 deg
RA of node: 245
3899 deg
Eccentricity:
0016932
Arg of perigee: 85
3312 deg
Mean anomaly: 274
9773 deg
Mean motion: 15
51951770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 791
Checksum: 340
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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