[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 4th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 34444 51 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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
There are no maneuvers
Coasting Arc #1 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2012/247/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4178014
29 A = 6788440
82 meter
Y = -3324
62 meter E =
0016951
Z = 5341503
47 I = 51
97559
XDOT = -109
928343 Wp = 38
42026
YDOT = -7669
501207 meter/sec RA = 88
72500 deg
ZDOT = -77
693031 TA = 52
39331
MA = 52
23955
Ha = 232
170 n
mi
Hp = 216
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13707395
95 X = -4203614
38
Y = -10907
54 feet Y = -50188
42 meter
Z = 17524617
69 Z = 5321144
71
XDOT = -360
657293 XDOT = -23
780807
YDOT = -25162
405536 feet/sec YDOT = -7670
248824 meter/sec
ZDOT = -254
898396 ZDOT = -78
017101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11758536
03 X = -3584001
78
Y = -7250780
72 feet Y = -2210037
96 meter
Z = 17440414
49 Z = 5315838
34
XDOT = 12357
318889 XDOT = 3766
510797
YDOT = -20757
965592 feet/sec YDOT = -6327
027912 meter/sec
ZDOT = -255
518122 ZDOT = -77
881923
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 12248
00856366
00016717 00000-0 10270-3 0 9008
2 25544 51
6448 89
2861 0015426 31
9551 328
2532 15
50323991 30271
Satellite: ISS
Catalog Number: 25544
Epoch time: 12248
00856366 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 89
2861 deg
Eccentricity:
0015426
Arg of perigee: 31
9551 deg
Mean anomaly: 328
2532 deg
Mean motion: 15
50323991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 303
Coasting Arc #2 (Orbit 3041)
---------------------------------------
Vector Time (GMT): 2012/248/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4216970
75 A = 6788519
57 meter
Y = 180287
12 meter E =
0026143
Z = -5336107
73 I = 51
97549
XDOT = 379
847464 Wp = 63
81109
YDOT = 7614
848848 meter/sec RA = 83
78798 deg
ZDOT = 570
823713 TA = 211
54881
MA = 211
70582
Ha = 232
100 n
mi
Hp = 216
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13835205
88 X = 4240562
96
Y = 591493
19 feet Y = 227575
40 meter
Z = -17506915
13 Z = -5315564
57
XDOT = 1246
218715 XDOT = 291
895480
YDOT = 24983
099894 feet/sec YDOT = 7618
604817 meter/sec
ZDOT = 1872
781211 ZDOT = 572
454754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11695566
80 X = 3564808
76
Y = 7612076
00 feet Y = 2320160
76 meter
Z = -17421965
44 Z = -5310215
07
XDOT = -11112
495937 XDOT = -3387
088761
YDOT = 21272
999698 feet/sec YDOT = 6484
010308 meter/sec
ZDOT = 1878
797645 ZDOT = 572
657522
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 12248
97545766
00016717 00000-0 10270-3 0 9014
2 25544 51
6461 84
4935 0015426 34
9913 325
2249 15
50340298 30428
Satellite: ISS
Catalog Number: 25544
Epoch time: 12248
97545766 = yrday
fracday
Element set: 901
Inclination: 51
6461 deg
RA of node: 84
4935 deg
Eccentricity:
0015426
Arg of perigee: 34
9913 deg
Mean anomaly: 325
2249 deg
Mean motion: 15
50340298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3042
Checksum: 316
Coasting Arc #3 (Orbit 3057)
---------------------------------------
Vector Time (GMT): 2012/249/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4271666
69 A = 6788576
46 meter
Y = -445965
82 meter E =
0019243
Z = 5248435
11 I = 51
97116
XDOT = -601
447860 Wp = 42
16390
YDOT = -7564
874555 meter/sec RA = 78
84944 deg
ZDOT = -1116
052186 TA = 58
57472
MA = 58
38669
Ha = 232
188 n
mi
Hp = 215
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14014654
50 X = -4291858
09
Y = -1463142
44 feet Y = -493846
80 meter
Z = 17219275
28 Z = 5227634
49
XDOT = -1973
254135 XDOT = -511
389625
YDOT = -24819
142240 feet/sec YDOT = -7571
096850 meter/sec
ZDOT = -3661
588538 ZDOT = -1118
754746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11548016
77 X = -3519835
51
Y = -8255216
00 feet Y = -2516189
84 meter
Z = 17133285
89 Z = 5222225
54
XDOT = 9979
899838 XDOT = 3041
873471
YDOT = -21693
007286 feet/sec YDOT = -6612
028621 meter/sec
ZDOT = -3672
027446 ZDOT = -1119
233965
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 12250
00677790
00016717 00000-0 10270-3 0 9025
2 25544 51
6449 79
3807 0015530 38
8718 321
3547 15
50421806 30587
Satellite: ISS
Catalog Number: 25544
Epoch time: 12250
00677790 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 79
3807 deg
Eccentricity:
0015530
Arg of perigee: 38
8718 deg
Mean anomaly: 321
3547 deg
Mean motion: 15
50421806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3058
Checksum: 306
Coasting Arc #4 (Orbit 3072)
---------------------------------------
Vector Time (GMT): 2012/250/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4385590
73 A = 6789000
98 meter
Y = 637997
37 meter E =
0025028
Z = -5161060
23 I = 51
96709
XDOT = 817
173570 Wp = 69
51518
YDOT = 7426
963102 meter/sec RA = 73
91191 deg
ZDOT = 1627
377270 TA = 216
07554
MA = 216
24468
Ha = 232
107 n
mi
Hp = 215
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14388421
04 X = 4403201
86
Y = 2093167
23 feet Y = 687137
97 meter
Z = -16932612
31 Z = -5139712
46
XDOT = 2681
015649 XDOT = 726
157553
YDOT = 24366
676843 feet/sec YDOT = 7435
592436 meter/sec
ZDOT = 5339
164273 ZDOT = 1631
125585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11712538
27 X = 3569981
67
Y = 8786622
83 feet Y = 2678162
64 meter
Z = -16844378
14 Z = -5134166
46
XDOT = -8722
964232 XDOT = -2658
759498
YDOT = 21797
312713 feet/sec YDOT = 6643
820915 meter/sec
ZDOT = 5353
928756 ZDOT = 1631
877485
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 12250
97361091
00016717 00000-0 10270-3 0 9036
2 25544 51
6462 74
5883 0015497 41
6973 318
5356 15
50437055 30736
Satellite: ISS
Catalog Number: 25544
Epoch time: 12250
97361091 = yrday
fracday
Element set: 903
Inclination: 51
6462 deg
RA of node: 74
5883 deg
Eccentricity:
0015497
Arg of perigee: 41
6973 deg
Mean anomaly: 318
5356 deg
Mean motion: 15
50437055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3073
Checksum: 316
Coasting Arc #5 (Orbit 3088)
---------------------------------------
Vector Time (GMT): 2012/251/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4519934
13 A = 6789475
02 meter
Y = -910466
07 meter E =
0021867
Z = 4974464
23 I = 51
95887
XDOT = -965
142866 Wp = 48
72218
YDOT = -7286
835080 meter/sec RA = 68
97195 deg
ZDOT = -2190
358268 TA = 62
64946
MA = 62
42706
Ha = 232
154 n
mi
Hp = 215
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14829180
22 X = -4533582
00
Y = -2987093
42 feet Y = -961086
87 meter
Z = 16320420
71 Z = 4952473
49
XDOT = -3166
479220 XDOT = -872
947969
YDOT = -23906
939240 feet/sec YDOT = -7297
112521 meter/sec
ZDOT = -7186
214791 ZDOT = -2194
822609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11833727
98 X = -3606920
29
Y = -9578512
96 feet Y = -2919530
75 meter
Z = 16229553
81 Z = 4946768
00
XDOT = 7640
815849 XDOT = 2328
920671
YDOT = -21759
392409 feet/sec YDOT = -6632
262806 meter/sec
ZDOT = -7203
943129 ZDOT = -2195
761866
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 12252
00486562
00016717 00000-0 10270-3 0 9044
2 25544 51
6449 69
4747 0015577 45
4065 314
8354 15
50522317 30896
Satellite: ISS
Catalog Number: 25544
Epoch time: 12252
00486562 = yrday
fracday
Element set: 904
Inclination: 51
6449 deg
RA of node: 69
4747 deg
Eccentricity:
0015577
Arg of perigee: 45
4065 deg
Mean anomaly: 314
8354 deg
Mean motion: 15
50522317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3089
Checksum: 314
Coasting Arc #6 (Orbit 3103)
---------------------------------------
Vector Time (GMT): 2012/252/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4702358
79 A = 6790248
35 meter
Y = 1090018
70 meter E =
0023102
Z = -4791733
21 I = 51
95037
XDOT = 1093
992730 Wp = 72
70001
YDOT = 7072
547473 meter/sec RA = 64
03358 deg
ZDOT = 2699
845466 TA = 223
83810
MA = 224
02168
Ha = 232
092 n
mi
Hp = 215
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15427686
31 X = 4713097
59
Y = 3576176
84 feet Y = 1142663
24 meter
Z = -15720909
48 Z = -4768863
38
XDOT = 3589
214995 XDOT = 1001
709519
YDOT = 23203
895909 feet/sec YDOT = 7084
265313 meter/sec
ZDOT = 8857
760714 ZDOT = 2704
935564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12263567
95 X = 3737935
51
Y = 10167069
97 feet Y = 3098922
93 meter
Z = -15626424
09 Z = -4762934
06
XDOT = -6523
245269 XDOT = -1988
285158
YDOT = 21425
397491 feet/sec YDOT = 6530
461155 meter/sec
ZDOT = 8878
089397 ZDOT = 2706
041648
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 12252
97163620
00016717 00000-0 10270-3 0 9058
2 25544 51
6455 64
6822 0015563 48
2594 311
9885 15
50535062 31043
Satellite: ISS
Catalog Number: 25544
Epoch time: 12252
97163620 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 64
6822 deg
Eccentricity:
0015563
Arg of perigee: 48
2594 deg
Mean anomaly: 311
9885 deg
Mean motion: 15
50535062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3104
Checksum: 305
Coasting Arc #7 (Orbit 3119)
---------------------------------------
Vector Time (GMT): 2012/253/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4902888
55 A = 6791107
54 meter
Y = -1340264
53 meter E =
0024429
Z = 4493208
66 I = 51
93875
XDOT = -1132
445220 Wp = 57
72242
YDOT = -6851
734024 meter/sec RA = 59
09229 deg
ZDOT = -3253
867350 TA = 65
01088
MA = 64
75735
Ha = 232
074 n
mi
Hp = 215
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16085592
34 X = -4909363
93
Y = -4397193
35 feet Y = -1395127
69 meter
Z = 14741498
23 Z = 4469375
09
XDOT = -3715
371456 XDOT = -1039
937062
YDOT = -22479
442337 feet/sec YDOT = -6863
880635 meter/sec
ZDOT = -10675
417814 ZDOT = -3259
143689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12667893
99 X = -3861174
09
Y = -10977197
01 feet Y = -3345849
65 meter
Z = 14643051
86 Z = 4463202
21
XDOT = 5661
347620 XDOT = 1725
578755
YDOT = -20914
808835 feet/sec YDOT = -6374
833733 meter/sec
ZDOT = -10696
532028 ZDOT = -3260
302962
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 12254
00282321
00016717 00000-0 10270-3 0 9065
2 25544 51
6443 59
5679 0015584 51
6628 308
5921 15
50625387 31203
Satellite: ISS
Catalog Number: 25544
Epoch time: 12254
00282321 = yrday
fracday
Element set: 906
Inclination: 51
6443 deg
RA of node: 59
5679 deg
Eccentricity:
0015584
Arg of perigee: 51
6628 deg
Mean anomaly: 308
5921 deg
Mean motion: 15
50625387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3120
Checksum: 302
Coasting Arc #8 (Orbit 3134)
---------------------------------------
Vector Time (GMT): 2012/254/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5134414
54 A = 6792152
84 meter
Y = 1481563
60 meter E =
0021053
Z = -4205180
73 I = 51
92595
XDOT = 1143
240026 Wp = 71
88935
YDOT = 6579
316072 meter/sec RA = 54
15263 deg
ZDOT = 3735
588489 TA = 236
33821
MA = 236
53918
Ha = 232
056 n
mi
Hp = 215
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16845192
07 X = 5137893
47
Y = 4860772
97 feet Y = 1538999
05 meter
Z = -13796524
70 Z = -4180229
77
XDOT = 3750
787486 XDOT = 1051
437259
YDOT = 21585
682652 feet/sec YDOT = 6591
587393 meter/sec
ZDOT = 12255
867745 ZDOT = 3740
918928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13345688
12 X = 4067765
74
Y = 11494048
96 feet Y = 3503386
12 meter
Z = -13693471
09 Z = -4173769
99
XDOT = -4849
959578 XDOT = -1478
267679
YDOT = 20172
297855 feet/sec YDOT = 6148
516386 meter/sec
ZDOT = 12277
228597 ZDOT = 3742
099276
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 12254
96952949
00016717 00000-0 10270-3 0 9071
2 25544 51
6443 54
7749 0015635 54
7455 305
5157 15
50637625 31359
Satellite: ISS
Catalog Number: 25544
Epoch time: 12254
96952949 = yrday
fracday
Element set: 907
Inclination: 51
6443 deg
RA of node: 54
7749 deg
Eccentricity:
0015635
Arg of perigee: 54
7455 deg
Mean anomaly: 305
5157 deg
Mean motion: 15
50637625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3135
Checksum: 334
Coasting Arc #9 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2012/255/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5373452
07 A = 6793272
44 meter
Y = -1684355
48 meter E =
0026494
Z = 3786676
93 I = 51
91122
XDOT = -1040
709040 Wp = 68
49828
YDOT = -6300
086556 meter/sec RA = 49
21021 deg
ZDOT = -4245
842331 TA = 66
34919
MA = 66
07131
Ha = 231
967 n
mi
Hp = 214
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17629435
91 X = -5372612
55
Y = -5526100
66 feet Y = -1744439
82 meter
Z = 12423480
73 Z = 3760575
32
XDOT = -3414
399738 XDOT = -949
557648
YDOT = -20669
575315 feet/sec YDOT = -6311
215046 meter/sec
ZDOT = -13929
928907 ZDOT = -4250
676173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13983813
48 X = -4262266
35
Y = -12184187
36 feet Y = -3713740
31 meter
Z = 12315689
64 Z = 3753822
20
XDOT = 4383
692560 XDOT = 1336
149492
YDOT = -19242
432372 feet/sec YDOT = -5865
093387 meter/sec
ZDOT = -13949
261089 ZDOT = -4251
734780
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 12256
00064654
00016717 00000-0 10270-3 0 9086
2 25544 51
6436 49
6599 0015591 57
8379 302
4282 15
50730907 31517
Satellite: ISS
Catalog Number: 25544
Epoch time: 12256
00064654 = yrday
fracday
Element set: 908
Inclination: 51
6436 deg
RA of node: 49
6599 deg
Eccentricity:
0015591
Arg of perigee: 57
8379 deg
Mean anomaly: 302
4282 deg
Mean motion: 15
50730907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 317
Coasting Arc #10 (Orbit 3165)
---------------------------------------
Vector Time (GMT): 2012/256/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5621630
66 A = 6794416
97 meter
Y = 1768232
23 meter E =
0020080
Z = -3389074
26 I = 51
89463
XDOT = 909
354692 Wp = 66
79234
YDOT = 5998
765779 meter/sec RA = 44
26911 deg
ZDOT = 4667
859026 TA = 253
89505
MA = 254
11622
Ha = 231
984 n
mi
Hp = 214
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18443670
14 X = 5617903
32
Y = 5801286
83 feet Y = 1831075
66 meter
Z = -11119010
03 Z = -3361774
08
XDOT = 2983
447151 XDOT = 819
532456
YDOT = 19680
990089 feet/sec YDOT = 6008
432943 meter/sec
ZDOT = 15314
498117 ZDOT = 4672
057881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14828406
30 X = 4519698
24
Y = 12507462
49 feet Y = 3812274
57 meter
Z = -11006272
30 Z = -3354711
80
XDOT = -4033
804369 XDOT = -1229
503572
YDOT = 18187
009452 feet/sec YDOT = 5543
400481 meter/sec
ZDOT = 15331
232798 ZDOT = 4672
959757
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 12256
96728631
00016717 00000-0 10270-3 0 9094
2 25544 51
6435 44
8662 0015700 61
2037 299
0689 15
50748726 31662
Satellite: ISS
Catalog Number: 25544
Epoch time: 12256
96728631 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 44
8662 deg
Eccentricity:
0015700
Arg of perigee: 61
2037 deg
Mean anomaly: 299
0689 deg
Mean motion: 15
50748726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3166
Checksum: 330
Coasting Arc #11 (Orbit 3181)
---------------------------------------
Vector Time (GMT): 2012/257/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5858164
48 A = 6795574
99 meter
Y = -1907385
50 meter E =
0027581
Z = 2850602
16 I = 51
87684
XDOT = -646
138668 Wp = 80
15616
YDOT = -5695
082286 meter/sec RA = 39
32576 deg
ZDOT = -5092
027168 TA = 67
58206
MA = 67
29012
Ha = 231
845 n
mi
Hp = 214
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19219699
73 X = -5850247
78
Y = -6257826
46 feet Y = -1972850
57 meter
Z = 9352369
30 Z = 2822163
12
XDOT = -2119
877519 XDOT = -557
671316
YDOT = -18684
653169 feet/sec YDOT = -5701
813729 meter/sec
ZDOT = -16706
125879 ZDOT = -5094
950539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15582710
35 X = -4749610
12
Y = -12958359
71 feet Y = -3949708
04 meter
Z = 9234939
77 Z = 2814809
64
XDOT = 4109
294522 XDOT = 1252
512970
YDOT = -16965
648636 feet/sec YDOT = -5171
129704 meter/sec
ZDOT = -16717
614610 ZDOT = -5095
528933
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 12257
99833132
00016717 00000-0 10270-3 0 9103
2 25544 51
6435 39
7506 0015614 64
1098 296
1661 15
50836866 31824
Satellite: ISS
Catalog Number: 25544
Epoch time: 12257
99833132 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 39
7506 deg
Eccentricity:
0015614
Arg of perigee: 64
1098 deg
Mean anomaly: 296
1661 deg
Mean motion: 15
50836866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3182
Checksum: 321
Coasting Arc #12 (Orbit 3196)
---------------------------------------
Vector Time (GMT): 2012/258/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6079606
13 A = 6796555
72 meter
Y = 1926309
34 meter E =
0021204
Z = -2347531
61 I = 51
85661
XDOT = 361
829329 Wp = 61
14450
YDOT = 5402
341556 meter/sec RA = 34
38329 deg
ZDOT = 5417
002241 TA = 272
80095
MA = 273
04362
Ha = 231
856 n
mi
Hp = 214
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19946214
34 X = 6069017
62
Y = 6319912
54 feet Y = 1994235
79 meter
Z = -7701875
35 Z = -2318023
25
XDOT = 1187
104099 XDOT = 275
077868
YDOT = 17724
217704 feet/sec YDOT = 5405
903398 meter/sec
ZDOT = 17772
317063 ZDOT = 5418
548574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16451053
35 X = 5014281
06
Y = 13000677
34 feet Y = 3962606
45 meter
Z = -7580031
48 Z = -2310393
59
XDOT = -4331
604703 XDOT = -1320
273113
YDOT = 15755
477496 feet/sec YDOT = 4802
269541 meter/sec
ZDOT = 17778
138774 ZDOT = 5418
776698
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 12258
96490235
00016717 00000-0 10270-3 0 9115
2 25544 51
6437 34
9565 0015713 67
6543 292
6272 15
50869682 31978
Satellite: ISS
Catalog Number: 25544
Epoch time: 12258
96490235 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 34
9565 deg
Eccentricity:
0015713
Arg of perigee: 67
6543 deg
Mean anomaly: 292
6272 deg
Mean motion: 15
50869682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3197
Checksum: 337
Coasting Arc #13 (Orbit 3212)
---------------------------------------
Vector Time (GMT): 2012/259/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6263103
35 A = 6797449
83 meter
Y = -1999929
41 meter E =
0027223
Z = 1700661
84 I = 51
83541
XDOT = 62
443293 Wp = 91
49688
YDOT = -5115
585894 meter/sec RA = 29
43892 deg
ZDOT = -5707
630523 TA = 69
93015
MA = 69
63734
Ha = 231
703 n
mi
Hp = 214
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20548239
33 X = -6248535
67
Y = -6561448
19 feet Y = -2069885
65 meter
Z = 5579599
23 Z = 1670271
62
XDOT = 204
866447 XDOT = 147
368588
YDOT = -16783
418288 feet/sec YDOT = -5114
413545 meter/sec
ZDOT = -18725
821926 ZDOT = -5707
120201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17144648
57 X = -5225688
89
Y = -13142610
87 feet Y = -4005867
79 meter
Z = 5454124
53 Z = 1662417
16
XDOT = 5025
503390 XDOT = 1531
773433
YDOT = -14434
747260 feet/sec YDOT = -4399
710965 meter/sec
ZDOT = -18723
165004 ZDOT = -5706
820693
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 12259
99587355
00016717 00000-0 10270-3 0 9120
2 25544 51
6445 29
8408 0015623 70
5562 289
7276 15
50941032 32130
Satellite: ISS
Catalog Number: 25544
Epoch time: 12259
99587355 = yrday
fracday
Element set: 912
Inclination: 51
6445 deg
RA of node: 29
8408 deg
Eccentricity:
0015623
Arg of perigee: 70
5562 deg
Mean anomaly: 289
7276 deg
Mean motion: 15
50941032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3213
Checksum: 324
Coasting Arc #14 (Orbit 3227)
---------------------------------------
Vector Time (GMT): 2012/260/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6408339
37 A = 6797967
63 meter
Y = 1962271
78 meter E =
0024064
Z = -1107647
33 I = 51
81104
XDOT = -491
432134 Wp = 60
30602
YDOT = 4871
568073 meter/sec RA = 24
49468 deg
ZDOT = 5894
757011 TA = 287
72046
MA = 287
98299
Ha = 231
667 n
mi
Hp = 213
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21024735
46 X = 6391301
28
Y = 6437899
53 feet Y = 2033838
41 meter
Z = -3634013
54 Z = -1076557
39
XDOT = -1612
310151 XDOT = -574
506048
YDOT = 15982
834886 feet/sec YDOT = 4865
608857 meter/sec
ZDOT = 19339
753972 ZDOT = 5892
167216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17847747
28 X = 5439993
37
Y = 12878681
35 feet Y = 3925422
07 meter
Z = -3505651
12 Z = -1068522
46
XDOT = -5851
835445 XDOT = -1783
639444
YDOT = 13271
365672 feet/sec YDOT = 4045
112257 meter/sec
ZDOT = 19328
519590 ZDOT = 5891
332771
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 12260
96237393
00016717 00000-0 10270-3 0 9134
2 25544 51
6447 25
0466 0015654 74
0637 286
2238 15
50994283 32282
Satellite: ISS
Catalog Number: 25544
Epoch time: 12260
96237393 = yrday
fracday
Element set: 913
Inclination: 51
6447 deg
RA of node: 25
0466 deg
Eccentricity:
0015654
Arg of perigee: 74
0637 deg
Mean anomaly: 286
2238 deg
Mean motion: 15
50994283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3228
Checksum: 320
Coasting Arc #15 (Orbit 3243)
---------------------------------------
Vector Time (GMT): 2012/261/23:02:49
964
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6485883
45 A = 6798249
51 meter
Y = -1986563
18 meter E =
0025205
Z = 378663
15 I = 51
78562
XDOT = 1051
935578 Wp = 100
64306
YDOT = -4642
706473 meter/sec RA = 19
54833 deg
ZDOT = -6003
944280 TA = 75
28908
MA = 75
00985
Ha = 231
529 n
mi
Hp = 213
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21279145
19 X = -6465026
72
Y = -6517595
73 feet Y = -2058975
71 meter
Z = 1242333
15 Z = 347205
62
XDOT = 3451
232212 XDOT = 1132
939186
YDOT = -15231
976617 feet/sec YDOT = -4630
490864 meter/sec
ZDOT = -19697
979921 ZDOT = -5998
636673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18270462
58 X = -5568836
99
Y = -12719162
24 feet Y = -3876800
65 meter
Z = 1112463
52 Z = 339078
88
XDOT = 7134
757391 XDOT = 2174
674053
YDOT = -12076
956180 feet/sec YDOT = -3681
056244 meter/sec
ZDOT = -19675
527009 ZDOT = -5997
100632
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 12261
99326961
00016717 00000-0 10270-3 0 9149
2 25544 51
6458 19
9309 0015589 77
0806 283
2085 15
51048028 32443
Satellite: ISS
Catalog Number: 25544
Epoch time: 12261
99326961 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 19
9309 deg
Eccentricity:
0015589
Arg of perigee: 77
0806 deg
Mean anomaly: 283
2085 deg
Mean motion: 15
51048028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3244
Checksum: 326
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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