[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 17th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
060/10:21:47
799 3
0 4
9 4
9
N/A -3
9 -0
0 220
3
000/00:01:35
599 0
1 0
0 201
9
Coasting Arc #1 (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 = -5873122
99 A = 6771043
62 meter
Y = 889702
48 meter E =
0030728
Z = 3241690
94 I = 51
74774
XDOT = -3408
697978 Wp = 63
14996
YDOT = -4960
136361 meter/sec RA = 16
86945 deg
ZDOT = -4766
002363 TA = 79
25979
MA = 78
91399
Ha = 220
711 n
mi
Hp = 200
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19268776
22 X = -5898382
49
Y = 2918971
38 feet Y = 823884
36 meter
Z = 10635468
96 Z = 3213098
64
XDOT = -11183
392316 XDOT = -3329
827573
YDOT = -16273
413257 feet/sec YDOT = -4997
813526 meter/sec
ZDOT = -15636
490692 ZDOT = -4782
369856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17374204
59 X = -5295657
56
Y = -8967978
75 feet Y = -2733439
92 meter
Z = 10518160
63 Z = 3205935
36
XDOT = -96
951686 XDOT = -29
550874
YDOT = -18417
882273 feet/sec YDOT = -5613
770517 meter/sec
ZDOT = -15703
162965 ZDOT = -4786
324072
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
53877858
00016717 00000-0 10270-3 0 9001
2 25544 51
6391 17
2329 0020608 45
6497 314
6342 15
58926090 38898
Satellite: ISS
Catalog Number: 25544
Epoch time: 12046
53877858 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 17
2329 deg
Eccentricity:
0020608
Arg of perigee: 45
6497 deg
Mean anomaly: 314
6342 deg
Mean motion: 15
58926090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3889
Checksum: 333
Coasting Arc #2 (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 = 6645678
68 A = 6775332
16 meter
Y = 1225162
90 meter E =
0032344
Z = -214111
93 I = 51
73314
XDOT = -694
133309 Wp = 47
18677
YDOT = 4714
997397 meter/sec RA = 11
87761 deg
ZDOT = 6030
467578 TA = 310
50158
MA = 310
78296
Ha = 220
676 n
mi
Hp = 200
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21803407
74 X = 6632524
83
Y = 4019563
32 feet Y = 1299405
43 meter
Z = -702466
97 Z = -181860
09
XDOT = -2277
340253 XDOT = -776
099850
YDOT = 15469
151565 feet/sec YDOT = 4706
776837 meter/sec
ZDOT = 19784
998614 ZDOT = 6026
896510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15584617
13 X = 4750191
30
Y = 15774452
76 feet Y = 4808053
20 meter
Z = -570339
50 Z = -173839
48
XDOT = -9667
822886 XDOT = -2946
752416
YDOT = 10179
246576 feet/sec YDOT = 3102
634356 meter/sec
ZDOT = 19769
940729 ZDOT = 6025
877934
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
50033665
00016717 00000-0 10270-3 0 9010
2 25544 51
6392 12
4050 0020577 49
6888 310
6061 15
58954639 39042
Satellite: ISS
Catalog Number: 25544
Epoch time: 12047
50033665 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 12
4050 deg
Eccentricity:
0020577
Arg of perigee: 49
6888 deg
Mean anomaly: 310
6061 deg
Mean motion: 15
58954639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 306
Coasting Arc #3 (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 = -5295438
33 A = 6771384
23 meter
Y = -3014791
43 meter E =
0023408
Z = -2985157
37 I = 51
69131
XDOT = 4726
320034 Wp = 61
79704
YDOT = -3390
916705 meter/sec RA = 6
88479 deg
ZDOT = -4978
521191 TA = 152
30420
MA = 152
17933
Ha = 220
675 n
mi
Hp = 200
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17373485
33 X = -5246831
89
Y = -9891048
01 feet Y = -3073736
52 meter
Z = -9793823
41 Z = -3010763
69
XDOT = 15506
299323 XDOT = 4788
070626
YDOT = -11125
054808 feet/sec YDOT = -3337
718826 meter/sec
ZDOT = -16333
730942 ZDOT = -4955
411500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8848098
25 X = -2696900
35
Y = -17869519
71 feet Y = -5446629
61 meter
Z = -9898546
51 Z = -3017076
98
XDOT = 17855
026799 XDOT = 5442
212168
YDOT = 120
127700 feet/sec YDOT = 36
614923 meter/sec
ZDOT = -16238
679030 ZDOT = -4949
549368
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
52598057
00016717 00000-0 10270-3 0 9025
2 25544 51
6401 7
2534 0020625 53
0320 307
2720 15
58980679 39201
Satellite: ISS
Catalog Number: 25544
Epoch time: 12048
52598057 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 7
2534 deg
Eccentricity:
0020625
Arg of perigee: 53
0320 deg
Mean anomaly: 307
2720 deg
Mean motion: 15
58980679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3920
Checksum: 290
Coasting Arc #4 (Orbit 3935)
---------------------------------------
Vector Time (GMT): 2012/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2173084
72 A = 6764419
64 meter
Y = 4009727
13 meter E =
0023331
Z = 4974324
71 I = 51
63856
XDOT = -7281
787956 Wp = 69
67550
YDOT = 1393
508782 meter/sec RA = 1
85821 deg
ZDOT = 2057
998948 TA =
38058
MA =
37881
Ha = 220
528 n
mi
Hp = 200
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7129543
05 X = 2103922
16
Y = 13155272
73 feet Y = 4033641
29 meter
Z = 16319962
95 Z = 4984713
10
XDOT = -23890
380433 XDOT = -7306
826273
YDOT = 4571
879207 feet/sec YDOT = 1311
939382 meter/sec
ZDOT = 6751
965054 ZDOT = 2022
564488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1251604
15 X = -381488
95
Y = 14864202
66 feet Y = 4530608
97 meter
Z = 16362204
67 Z = 4987199
98
XDOT = -21487
371954 XDOT = -6549
350971
YDOT = -9081
070964 feet/sec YDOT = -2767
910430 meter/sec
ZDOT = 6606
556938 ZDOT = 2013
678555
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 12049
55160496
00016717 00000-0 10270-3 0 9032
2 25544 51
6406 2
1036 0020390 56
7785 303
5321 15
59034829 39362
Satellite: ISS
Catalog Number: 25544
Epoch time: 12049
55160496 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 2
1036 deg
Eccentricity:
0020390
Arg of perigee: 56
7785 deg
Mean anomaly: 303
5321 deg
Mean motion: 15
59034829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 298
Coasting Arc #5 (Orbit 3950)
---------------------------------------
Vector Time (GMT): 2012/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1645085
47 A = 6764134
81 meter
Y = -4146664
89 meter E =
0031683
Z = -5109255
86 I = 51
60688
XDOT = 7416
366190 Wp = 76
39877
YDOT = 908
624248 meter/sec RA = 356
80550 deg
ZDOT = 1666
460018 TA = 209
63662
MA = 209
81652
Ha = 220
674 n
mi
Hp = 199
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5397262
04 X = 1716150
93
Y = -13604543
60 feet Y = -4127871
38 meter
Z = -16762650
46 Z = -5101091
57
XDOT = 24331
910072 XDOT = 7397
559524
YDOT = 2981
050681 feet/sec YDOT = 991
453539 meter/sec
ZDOT = 5467
388511 ZDOT = 1702
441614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11865089
56 X = 3616479
30
Y = -8635211
41 feet Y = -2632012
44 meter
Z = -16728815
51 Z = -5098942
97
XDOT = 18410
925459 XDOT = 5611
650080
YDOT = 14521
448294 feet/sec YDOT = 4426
137440 meter/sec
ZDOT = 5614
836586 ZDOT = 1711
402191
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 12050
51311362
00016717 00000-0 10270-3 0 9041
2 25544 51
6408 357
2743 0020502 60
2204 300
0987 15
59014481 39513
Satellite: ISS
Catalog Number: 25544
Epoch time: 12050
51311362 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 357
2743 deg
Eccentricity:
0020502
Arg of perigee: 60
2204 deg
Mean anomaly: 300
0987 deg
Mean motion: 15
59014481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 268
Coasting Arc #6 (Orbit 3966)
---------------------------------------
Vector Time (GMT): 2012/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4970344
65 A = 6770740
64 meter
Y = 3282785
73 meter E =
0032330
Z = 3201480
58 I = 51
59971
XDOT = -5154
159792 Wp = 74
97161
YDOT = -3088
070603 meter/sec RA = 351
77002 deg
ZDOT = -4786
875314 TA = 67
86482
MA = 67
52196
Ha = 220
701 n
mi
Hp = 199
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16306905
01 X = -5022235
63
Y = 10770294
39 feet Y = 3226914
33 meter
Z = 10503545
22 Z = 3177209
34
XDOT = -16909
973070 XDOT = -5095
992416
YDOT = -10131
465234 feet/sec YDOT = -3145
382660 meter/sec
ZDOT = -15704
971504 ZDOT = -4811
771784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19579005
27 X = -5967680
81
Y = 814466
56 feet Y = 248249
41 meter
Z = 10403751
79 Z = 3171063
55
XDOT = -9146
607094 XDOT = -2787
885842
YDOT = -15911
111163 feet/sec YDOT = -4849
706682 meter/sec
ZDOT = -15806
780171 ZDOT = -4817
906596
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 12051
53870341
00016717 00000-0 10270-3 0 9052
2 25544 51
6415 352
1232 0020519 64
0098 296
3168 15
59061999 39670
Satellite: ISS
Catalog Number: 25544
Epoch time: 12051
53870341 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 352
1232 deg
Eccentricity:
0020519
Arg of perigee: 64
0098 deg
Mean anomaly: 296
3168 deg
Mean motion: 15
59061999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 316
Coasting Arc #7 (Orbit 3981)
---------------------------------------
Vector Time (GMT): 2012/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6558895
29 A = 6774998
62 meter
Y = -1648724
83 meter E =
0031852
Z = -130657
40 I = 51
58414
XDOT = 1256
181297 Wp = 58
73437
YDOT = 4607
314724 meter/sec RA = 346
76765 deg
ZDOT = 6018
012394 TA = 299
85298
MA = 300
16917
Ha = 220
653 n
mi
Hp = 199
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21518685
32 X = 6577478
88
Y = -5409202
18 feet Y = -1575275
32 meter
Z = -428666
01 Z = -98750
18
XDOT = 4121
329714 XDOT = 1175
334664
YDOT = 15115
861955 feet/sec YDOT = 4620
910572 meter/sec
ZDOT = 19744
135150 ZDOT = 6023
917952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21344875
78 X = 6505918
14
Y = 6066686
53 feet Y = 1849126
06 meter
Z = -297713
35 Z = -90743
03
XDOT = -3644
257261 XDOT = -1110
769613
YDOT = 13537
638086 feet/sec YDOT = 4126
272089 meter/sec
ZDOT = 19767
954859 ZDOT = 6025
272641
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 12052
50017719
00016717 00000-0 10270-3 0 9063
2 25544 51
6414 347
2950 0020472 67
5524 292
7797 15
59071904 39823
Satellite: ISS
Catalog Number: 25544
Epoch time: 12052
50017719 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 347
2950 deg
Eccentricity:
0020472
Arg of perigee: 67
5524 deg
Mean anomaly: 292
7797 deg
Mean motion: 15
59071904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3982
Checksum: 320
Coasting Arc #8 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2012/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6006868
13 A = 6770691
77 meter
Y = -606533
58 meter E =
0024430
Z = -3092067
41 I = 51
54195
XDOT = 3011
515403 Wp = 76
60197
YDOT = -5074
719884 meter/sec RA = 341
76362 deg
ZDOT = -4881
914248 TA = 138
99852
MA = 138
81460
Ha = 220
589 n
mi
Hp = 199
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19707572
62 X = -5984619
11
Y = -1989939
56 feet Y = -673581
99 meter
Z = -10144578
11 Z = -3121193
70
XDOT = 9880
299880 XDOT = 3091
752789
YDOT = -16649
343451 feet/sec YDOT = -5040
595107 meter/sec
ZDOT = -16016
779028 ZDOT = -4867
089408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16219475
11 X = -4943696
01
Y = -11262374
14 feet Y = -3432771
64 meter
Z = -10263931
94 Z = -3128446
46
XDOT = 15975
552784 XDOT = 4869
348489
YDOT = -8545
804630 feet/sec YDOT = -2604
761251 meter/sec
ZDOT = -15955
577111 ZDOT = -4863
259903
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 12053
52573104
00016717 00000-0 10270-3 0 9072
2 25544 51
6424 342
1434 0020500 71
3849 288
9530 15
59118503 39986
Satellite: ISS
Catalog Number: 25544
Epoch time: 12053
52573104 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 342
1434 deg
Eccentricity:
0020500
Arg of perigee: 71
3849 deg
Mean anomaly: 288
9530 deg
Mean motion: 15
59118503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 302
Coasting Arc #9 (Orbit 4013)
---------------------------------------
Vector Time (GMT): 2012/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3500080
25 A = 6763800
73 meter
Y = 2842791
07 meter E =
0024212
Z = 5020072
57 I = 51
49040
XDOT = -6135
534196 Wp = 84
68326
YDOT = 4253
571898 meter/sec RA = 336
72391 deg
ZDOT = 1863
555030 TA = 347
25730
MA = 347
31839
Ha = 220
396 n
mi
Hp = 199
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11483202
92 X = 3443645
57
Y = 9326742
35 feet Y = 2881616
13 meter
Z = 16470054
36 Z = 5036938
07
XDOT = -20129
705366 XDOT = -6191
695034
YDOT = 13955
288380 feet/sec YDOT = 4184
646757 meter/sec
ZDOT = 6114
025689 ZDOT = 1833
612617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5670577
60 X = 1728392
05
Y = 13580216
98 feet Y = 4139250
14 meter
Z = 16538954
61 Z = 5041073
36
XDOT = -23367
601914 XDOT = -7122
445063
YDOT = 2439
308005 feet/sec YDOT = 743
501080 meter/sec
ZDOT = 5990
928300 ZDOT = 1826
034946
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 12054
55126504
00016717 00000-0 10270-3 0 9085
2 25544 51
6421 336
9930 0020301 75
3960 284
9445 15
59167754 40145
Satellite: ISS
Catalog Number: 25544
Epoch time: 12054
55126504 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 336
9930 deg
Eccentricity:
0020301
Arg of perigee: 75
3960 deg
Mean anomaly: 284
9445 deg
Mean motion: 15
59167754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4014
Checksum: 304
Coasting Arc #10 (Orbit 4028)
---------------------------------------
Vector Time (GMT): 2012/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3659
57 A = 6764020
10 meter
Y = -4551289
77 meter E =
0032512
Z = -5031602
50 I = 51
46366
XDOT = 7106
027719 Wp = 88
22694
YDOT = -2104
280713 meter/sec RA = 331
65982 deg
ZDOT = 1909
922520 TA = 200
31319
MA = 200
44282
Ha = 220
540 n
mi
Hp = 199
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12006
46 X = 71676
14
Y = -14932053
04 feet Y = -4550910
02 meter
Z = -16507882
21 Z = -5031436
79
XDOT = 23313
739234 XDOT = 7119
752250
YDOT = -6903
808114 feet/sec YDOT = -2024
739777 meter/sec
ZDOT = 6266
149999 ZDOT = 1944
476285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6862278
98 X = 2091622
63
Y = -13263118
75 feet Y = -4042598
59 meter
Z = -16506826
93 Z = -5031280
85
XDOT = 22903
937706 XDOT = 6981
120213
YDOT = 3922
971963 feet/sec YDOT = 1195
721854 meter/sec
ZDOT = 6407
962007 ZDOT = 1953
146820
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 12055
51268869
00016717 00000-0 10270-3 0 9094
2 25544 51
6425 332
1637 0020385 78
6433 281
7011 15
59157130 40291
Satellite: ISS
Catalog Number: 25544
Epoch time: 12055
51268869 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 332
1637 deg
Eccentricity:
0020385
Arg of perigee: 78
6433 deg
Mean anomaly: 281
7011 deg
Mean motion: 15
59157130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 309
Coasting Arc #11 (Orbit 4044)
---------------------------------------
Vector Time (GMT): 2012/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3363733
66 A = 6770973
63 meter
Y = 5052665
68 meter E =
0033367
Z = 2972875
36 I = 51
46035
XDOT = -5798
938965 Wp = 88
05898
YDOT = -912
127365 meter/sec RA = 326
61595 deg
ZDOT = -4961
900990 TA = 57
72329
MA = 57
40044
Ha = 220
561 n
mi
Hp = 199
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11035871
58 X = -3434424
96
Y = 16576987
15 feet Y = 5014655
39 meter
Z = 9753528
07 Z = 2956362
47
XDOT = -19025
390305 XDOT = -5764
204892
YDOT = -2992
543850 feet/sec YDOT = -976
780988 meter/sec
ZDOT = -16279
202724 ZDOT = -4989
987150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17244858
83 X = -5256232
97
Y = 10026244
46 feet Y = 3055999
31 meter
Z = 9685429
28 Z = 2952118
84
XDOT = -14961
107263 XDOT = -4560
145494
YDOT = -9738
651834 feet/sec YDOT = -2968
341079 meter/sec
ZDOT = -16394
248672 ZDOT = -4996
966995
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 12056
53818822
00016717 00000-0 10270-3 0 9109
2 25544 51
6421 327
0120 0020403 82
6670 277
6803 15
59178548 40453
Satellite: ISS
Catalog Number: 25544
Epoch time: 12056
53818822 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 327
0120 deg
Eccentricity:
0020403
Arg of perigee: 82
6670 deg
Mean anomaly: 277
6803 deg
Mean motion: 15
59178548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4045
Checksum: 296
Coasting Arc #12 (Orbit 4060)
---------------------------------------
Vector Time (GMT): 2012/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5393732
83 A = 6774589
14 meter
Y = -4082144
63 meter E =
0031163
Z = 188988
58 I = 51
44827
XDOT = 2737
776350 Wp = 71
07784
YDOT = 3932
246855 meter/sec RA = 321
60464 deg
ZDOT = 6001
000048 TA = 290
96871
MA = 291
30189
Ha = 220
460 n
mi
Hp = 199
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17695973
86 X = 5438061
27
Y = -13392862
97 feet Y = -4021580
71 meter
Z = 620041
28 Z = 215298
87
XDOT = 8982
205874 XDOT = 2664
450487
YDOT = 12901
072360 feet/sec YDOT = 3962
452931 meter/sec
ZDOT = 19688
320366 ZDOT = 6014
121434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21698170
35 X = 6613602
32
Y = -4643256
51 feet Y = -1415264
58 meter
Z = 728212
23 Z = 221959
09
XDOT = 2228
170120 XDOT = 679
146253
YDOT = 13858
649042 feet/sec YDOT = 4224
116228 meter/sec
ZDOT = 19741
779259 ZDOT = 6017
294318
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 12057
56366870
00016717 00000-0 10270-3 0 9115
2 25544 51
6423 321
8608 0020313 86
1337 274
2141 15
59207695 40619
Satellite: ISS
Catalog Number: 25544
Epoch time: 12057
56366870 = yrday
fracday
Element set: 911
Inclination: 51
6423 deg
RA of node: 321
8608 deg
Eccentricity:
0020313
Arg of perigee: 86
1337 deg
Mean anomaly: 274
2141 deg
Mean motion: 15
59207695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4061
Checksum: 298
Coasting Arc #13 (Orbit 4075)
---------------------------------------
Vector Time (GMT): 2012/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5647600
05 A = 6769541
99 meter
Y = 1630233
86 meter E =
0025064
Z = -3379597
79 I = 51
40913
XDOT = 1006
949446 Wp = 89
42842
YDOT = -6027
832058 meter/sec RA = 316
58785 deg
ZDOT = -4619
851737 TA = 130
19139
MA = 129
97173
Ha = 220
331 n
mi
Hp = 199
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18528871
57 X = -5648992
73
Y = 5348536
29 feet Y = 1567070
86 meter
Z = -11087919
26 Z = -3407036
85
XDOT = 3303
639916 XDOT = 1096
721040
YDOT = -19776
351897 feet/sec YDOT = -6016
070156 meter/sec
ZDOT = -15156
993887 ZDOT = -4614
741533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19037517
80 X = -5802635
43
Y = -2643730
92 feet Y = -805809
18 meter
Z = -11200512
41 Z = -3413916
18
XDOT = 10971
277841 XDOT = 3344
045486
YDOT = -15286
028889 feet/sec YDOT = -4659
181605 meter/sec
ZDOT = -15135
559229 ZDOT = -4613
318453
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 12058
52503889
00016717 00000-0 10270-3 0 9126
2 25544 51
6428 317
0305 0020184 89
8414 270
5055 15
59240835 40769
Satellite: ISS
Catalog Number: 25544
Epoch time: 12058
52503889 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 317
0305 deg
Eccentricity:
0020184
Arg of perigee: 89
8414 deg
Mean anomaly: 270
5055 deg
Mean motion: 15
59240835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4076
Checksum: 309
Coasting Arc #14 (Orbit 4091)
---------------------------------------
Vector Time (GMT): 2012/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4118482
27 A = 6762988
83 meter
Y = 1525711
33 meter E =
0024075
Z = 5122967
37 I = 51
36588
XDOT = -4115
973525 Wp = 98
73495
YDOT = 6346
118950 meter/sec RA = 311
53317 deg
ZDOT = 1409
688399 TA = 337
64803
MA = 337
75277
Ha = 220
174 n
mi
Hp = 199
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13512080
94 X = 4076229
36
Y = 5005614
61 feet Y = 1571530
84 meter
Z = 16807635
72 Z = 5142871
86
XDOT = -13503
850149 XDOT = -4193
479085
YDOT = 20820
600230 feet/sec YDOT = 6299
658332 meter/sec
ZDOT = 4624
961939 ZDOT = 1389
504675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10374492
29 X = 3162145
25
Y = 9861928
82 feet Y = 3005915
91 meter
Z = 16889091
07 Z = 5147794
96
XDOT = -19890
562460 XDOT = -6062
643438
YDOT = 13094
631407 feet/sec YDOT = 3991
243653 meter/sec
ZDOT = 4541
725987 ZDOT = 1384
318081
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 12059
55048296
00016717 00000-0 10270-3 0 9137
2 25544 51
6425 311
8789 0020189 93
6836 266
6628 15
59287105 40921
Satellite: ISS
Catalog Number: 25544
Epoch time: 12059
55048296 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 311
8789 deg
Eccentricity:
0020189
Arg of perigee: 93
6836 deg
Mean anomaly: 266
6628 deg
Mean motion: 15
59287105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4092
Checksum: 342
Coasting Arc #15 (Orbit 4105)
---------------------------------------
Vector Time (GMT): 2012/060/10:22:35
599
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3123019
12 A = 6765035
68 meter
Y = -2886436
67 meter E =
0031117
Z = -5288294
28 I = 51
34529
XDOT = 4823
257372 Wp = 95
52937
YDOT = -5928
094885 meter/sec RA = 306
81569 deg
ZDOT = 386
288085 TA = 178
18263
MA = 178
17130
Ha = 220
266 n
mi
Hp = 201
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10246125
73 X = -3064821
20
Y = -9469936
58 feet Y = -2921035
10 meter
Z = -17350046
85 Z = -5303324
09
XDOT = 15824
335211 XDOT = 4887
311564
YDOT = -19449
130200 feet/sec YDOT = -5873
800076 meter/sec
ZDOT = 1267
349359 ZDOT = 409
874952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -108273
00 X = -33001
61
Y = -13875078
97 feet Y = -4229124
07 meter
Z = -17411415
14 Z = -5306999
34
XDOT = 23983
602898 XDOT = 7310
202163
YDOT = -1903
406049 feet/sec YDOT = -580
158164 meter/sec
ZDOT = 1364
495754 ZDOT = 415
898306
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 12060
44773383
00016717 00000-0 10270-3 0 9140
2 25544 51
6421 307
3704 0016326 98
1817 262
1190 15
58393770 41067
Satellite: ISS
Catalog Number: 25544
Epoch time: 12060
44773383 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 307
3704 deg
Eccentricity:
0016326
Arg of perigee: 98
1817 deg
Mean anomaly: 262
1190 deg
Mean motion: 15
58393770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4106
Checksum: 301
Coasting Arc #16 (Orbit 4121)
---------------------------------------
Vector Time (GMT): 2012/061/10:22:35
599
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 648711
06 A = 6769452
64 meter
Y = 5280055
97 meter E =
0025912
Z = 4163554
51 I = 51
34248
XDOT = -5701
000218 Wp = 91
20576
YDOT = 3617
339182 meter/sec RA = 301
75690 deg
ZDOT = -3679
841663 TA = 36
67729
MA = 36
50021
Ha = 220
184 n
mi
Hp = 202
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2128317
11 X = 569394
82
Y = 17323018
28 feet Y = 5286866
99 meter
Z = 13659955
73 Z = 4166512
96
XDOT = -18704
068957 XDOT = -5723
150688
YDOT = 11867
910703 feet/sec YDOT = 3553
463044 meter/sec
ZDOT = -12072
971335 ZDOT = -3707
590526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10928070
22 X = -3330875
80
Y = 13596838
54 feet Y = 4144316
39 meter
Z = 13671662
29 Z = 4167122
67
XDOT = -20529
039972 XDOT = -6257
251383
YDOT = -4182
060873 feet/sec YDOT = -1274
692154 meter/sec
ZDOT = -12186
988696 ZDOT = -3714
594155
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 12061
47374093
00016717 00000-0 10270-3 0 9150
2 25544 51
6416 302
2225 0016314 101
8147 258
4838 15
58419245 41229
Satellite: ISS
Catalog Number: 25544
Epoch time: 12061
47374093 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 302
2225 deg
Eccentricity:
0016314
Arg of perigee: 101
8147 deg
Mean anomaly: 258
4838 deg
Mean motion: 15
58419245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4122
Checksum: 293
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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