[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 7th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 684)
---------------------------------------
Vector Time (GMT): 2012/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4941868
19 A = 6772920
20 meter
Y = 3072979
76 meter E =
0006332
Z = 3464089
94 I = 51
94161
XDOT = -581
381949 Wp = 123
36704
YDOT = -6119
953415 meter/sec RA = 120
34731 deg
ZDOT = 4590
162725 TA = 277
14616
MA = 277
21816
Ha = 213
919 n
mi
Hp = 211
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16213478
33 X = -4992691
54
Y = 10081954
58 feet Y = 3017432
96 meter
Z = 11365124
47 Z = 3439958
49
XDOT = -1907
421092 XDOT = -535
202412
YDOT = -20078
587321 feet/sec YDOT = -6126
196051 meter/sec
ZDOT = 15059
588992 ZDOT = 4587
451246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13268747
61 X = -4044314
27
Y = 13809817
36 feet Y = 4209232
33 meter
Z = 11265789
95 Z = 3433812
78
XDOT = -5914
739691 XDOT = -1802
812658
YDOT = -17985
011614 feet/sec YDOT = -5481
831540 meter/sec
ZDOT = 15048
848481 ZDOT = 4586
889017
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 12097
55695963
00016717 00000-0 10270-3 0 9004
2 25544 51
6396 120
9751 0007841 244
8748 115
1594 15
58054558 6855
Satellite: ISS
Catalog Number: 25544
Epoch time: 12097
55695963 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 120
9751 deg
Eccentricity:
0007841
Arg of perigee: 244
8748 deg
Mean anomaly: 115
1594 deg
Mean motion: 15
58054558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 685
Checksum: 343
Coasting Arc #2 (Orbit 699)
---------------------------------------
Vector Time (GMT): 2012/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4443026
82 A = 6766821
20 meter
Y = -35389
47 meter E =
0005575
Z = -5108544
17 I = 51
93675
XDOT = -1925
004107 Wp = 89
39295
YDOT = 7222
047171 meter/sec RA = 115
34201 deg
ZDOT = -1725
816332 TA = 164
01188
MA = 163
99428
Ha = 213
809 n
mi
Hp = 211
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14576859
64 X = 4467908
86
Y = -116107
20 feet Y = 14433
86 meter
Z = -16760315
53 Z = -5086899
39
XDOT = -6315
630273 XDOT = -1997
235676
YDOT = 23694
380483 feet/sec YDOT = 7200
116558 meter/sec
ZDOT = -5662
127072 ZDOT = -1735
344166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14122952
86 X = 4304676
03
Y = -4001679
22 feet Y = -1219711
83 meter
Z = -16671390
48 Z = -5081439
82
XDOT = -71
123801 XDOT = -21
678534
YDOT = 23481
600845 feet/sec YDOT = 7157
191938 meter/sec
ZDOT = -5701
756225 ZDOT = -1737
895297
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 12098
51903648
00016717 00000-0 10270-3 0 9014
2 25544 51
6402 116
1501 0007985 248
4823 111
5481 15
58095845 7003
Satellite: ISS
Catalog Number: 25544
Epoch time: 12098
51903648 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 116
1501 deg
Eccentricity:
0007985
Arg of perigee: 248
4823 deg
Mean anomaly: 111
5481 deg
Mean motion: 15
58095845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 700
Checksum: 301
Coasting Arc #3 (Orbit 715)
---------------------------------------
Vector Time (GMT): 2012/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3096224
02 A = 6766613
80 meter
Y = -3171116
34 meter E =
0003392
Z = 5116184
18 I = 51
94751
XDOT = 3801
489007 Wp = 279
65475
YDOT = -6445
429553 meter/sec RA = 110
32014 deg
ZDOT = -1694
814154 TA = 186
63426
MA = 186
63875
Ha = 213
458 n
mi
Hp = 211
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10158215
28 X = -3085387
49
Y = -10403924
99 feet Y = -3205679
32 meter
Z = 16785381
17 Z = 5101169
15
XDOT = 12472
076793 XDOT = 3881
513720
YDOT = -21146
422418 feet/sec YDOT = -6402
471614 meter/sec
ZDOT = -5560
413891 ZDOT = -1676
151629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12773451
44 X = -3893348
00
Y = -7094341
64 feet Y = -2162355
33 meter
Z = 16723913
09 Z = 5097448
71
XDOT = 5530
288451 XDOT = 1685
631920
YDOT = -22880
348247 feet/sec YDOT = -6973
930146 meter/sec
ZDOT = -5483
289167 ZDOT = -1671
306538
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 12099
54523075
00016717 00000-0 10270-3 0 9021
2 25544 51
6390 111
0025 0007891 252
6509 107
3783 15
58141739 7167
Satellite: ISS
Catalog Number: 25544
Epoch time: 12099
54523075 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 111
0025 deg
Eccentricity:
0007891
Arg of perigee: 252
6509 deg
Mean anomaly: 107
3783 deg
Mean motion: 15
58141739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 716
Checksum: 302
Coasting Arc #4 (Orbit 730)
---------------------------------------
Vector Time (GMT): 2012/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1262184
17 A = 6772509
43 meter
Y = 5674833
64 meter E =
0003334
Z = -3473921
84 I = 51
97773
XDOT = -4778
198006 Wp = 232
92460
YDOT = 3872
918189 meter/sec RA = 105
31578 deg
ZDOT = 4585
570013 TA = 86
44724
MA = 86
40911
Ha = 213
072 n
mi
Hp = 211
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4141024
18 X = 1215508
97
Y = 18618220
61 feet Y = 5688687
07 meter
Z = -11397381
35 Z = -3467903
69
XDOT = -15676
502643 XDOT = -4843
426592
YDOT = 12706
424503 feet/sec YDOT = 3819
120868 meter/sec
ZDOT = 15044
521040 ZDOT = 4562
198863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9566022
31 X = 2915723
60
Y = 16517601
60 feet Y = 5034564
97 meter
Z = -11373063
61 Z = -3466509
79
XDOT = -10061
006556 XDOT = -3066
594798
YDOT = 16130
483339 feet/sec YDOT = 4916
571322 meter/sec
ZDOT = 14948
214097 ZDOT = 4556
215657
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 12100
50726753
00016717 00000-0 10270-3 0 9039
2 25544 51
6397 106
1774 0007864 256
9052 103
1225 15
58161976 7317
Satellite: ISS
Catalog Number: 25544
Epoch time: 12100
50726753 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 106
1774 deg
Eccentricity:
0007864
Arg of perigee: 256
9052 deg
Mean anomaly: 103
1225 deg
Mean motion: 15
58161976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 731
Checksum: 300
Coasting Arc #5 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2012/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 672359
06 A = 6777293
37 meter
Y = -6701556
77 meter E =
0009737
Z = 693167
80 I = 52
00050
XDOT = 4788
989187 Wp = 163
49110
YDOT = -141
083065 meter/sec RA = 100
34116 deg
ZDOT = -5997
752337 TA = 9
04412
MA = 9
02660
Ha = 212
748 n
mi
Hp = 211
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2205902
44 X = 743879
97
Y = -21986734
80 feet Y = -6693638
13 meter
Z = 2274172
58 Z = 696607
96
XDOT = 15711
906780 XDOT = 4819
346870
YDOT = -462
870948 feet/sec YDOT = -87
359986 meter/sec
ZDOT = -19677
665148 ZDOT = -5974
413690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4829905
01 X = -1472155
05
Y = -21561255
86 feet Y = -6571870
78 meter
Z = 2288806
94 Z = 697628
36
XDOT = 13310
755991 XDOT = 4057
118426
YDOT = -5064
365809 feet/sec YDOT = -1543
618699 meter/sec
ZDOT = -19581
752988 ZDOT = -5968
518311
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 12101
53341850
00016717 00000-0 10270-3 0 9045
2 25544 51
6390 101
0297 0007826 260
9277 99
0993 15
58207100 7478
Satellite: ISS
Catalog Number: 25544
Epoch time: 12101
53341850 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 101
0297 deg
Eccentricity:
0007826
Arg of perigee: 260
9277 deg
Mean anomaly: 99
0993 deg
Mean motion: 15
58207100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 297
Coasting Arc #6 (Orbit 762)
---------------------------------------
Vector Time (GMT): 2012/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2377395
97 A = 6775053
34 meter
Y = 5899986
15 meter E =
0006202
Z = 2321921
11 I = 51
99807
XDOT = -3921
722970 Wp = 57
98069
YDOT = -3725
576196 meter/sec RA = 95
37555 deg
ZDOT = 5443
854880 TA = 327
81434
MA = 327
85218
Ha = 212
329 n
mi
Hp = 211
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7799855
54 X = -2454473
54
Y = 19356909
93 feet Y = 5872969
70 meter
Z = 7617851
42 Z = 2310184
49
XDOT = -12866
545177 XDOT = -3906
216491
YDOT = -12223
019017 feet/sec YDOT = -3769
344566 meter/sec
ZDOT = 17860
416274 ZDOT = 5424
840945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1005235
47 X = -306395
77
Y = 20862802
43 feet Y = 6358982
18 meter
Z = 7569170
72 Z = 2307083
24
XDOT = -14764
611317 XDOT = -4500
253529
YDOT = -7171
896133 feet/sec YDOT = -2185
993941 meter/sec
ZDOT = 17782
562871 ZDOT = 5420
125163
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 12102
55954473
00016717 00000-0 10270-3 0 9050
2 25544 51
6390 95
8827 0008017 264
1092 95
9149 15
58268820 7633
Satellite: ISS
Catalog Number: 25544
Epoch time: 12102
55954473 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 95
8827 deg
Eccentricity:
0008017
Arg of perigee: 264
1092 deg
Mean anomaly: 95
9149 deg
Mean motion: 15
58268820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 763
Checksum: 327
Coasting Arc #7 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2012/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3606411
64 A = 6768483
24 meter
Y = -3439902
31 meter E =
0003597
Z = -4582625
20 I = 51
97751
XDOT = 2372
642829 Wp = 24
91286
YDOT = 6608
451516 meter/sec RA = 90
38465 deg
ZDOT = -3091
059175 TA = 214
31420
MA = 214
33744
Ha = 211
855 n
mi
Hp = 211
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11832059
18 X = 3666870
66
Y = -11285768
74 feet Y = -3399235
22 meter
Z = -15034859
56 Z = -4564958
48
XDOT = 7784
261250 XDOT = 2313
585125
YDOT = 21681
271378 feet/sec YDOT = 6634
653612 meter/sec
ZDOT = -10141
270258 ZDOT = -3079
676538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7269262
32 X = 2215671
16
Y = -14721072
90 feet Y = -4486983
02 meter
Z = -14961986
52 Z = -4560413
49
XDOT = 13804
038029 XDOT = 4207
470791
YDOT = 17084
344357 feet/sec YDOT = 5207
308160 meter/sec
ZDOT = -10095
003366 ZDOT = -3076
957026
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 12103
52151996
00016717 00000-0 10270-3 0 9068
2 25544 51
6387 91
0563 0007875 268
6762 91
3491 15
58260271 7786
Satellite: ISS
Catalog Number: 25544
Epoch time: 12103
52151996 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 91
0563 deg
Eccentricity:
0007875
Arg of perigee: 268
6762 deg
Mean anomaly: 91
3491 deg
Mean motion: 15
58260271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 328
Coasting Arc #8 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2012/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4178559
79 A = 6765277
20 meter
Y = 9577
99 meter E =
0005579
Z = 5325334
32 I = 51
96612
XDOT = -391
001347 Wp = 280
11018
YDOT = -7656
049133 meter/sec RA = 85
36701 deg
ZDOT = -292
337175 TA = 172
66696
MA = 172
65879
Ha = 211
892 n
mi
Hp = 211
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13709185
65 X = -4204225
55
Y = 31423
85 feet Y = -37292
59 meter
Z = 17471569
30 Z = 5304972
76
XDOT = -1282
812819 XDOT = -303
940690
YDOT = -25118
271434 feet/sec YDOT = -7659
934778 meter/sec
ZDOT = -959
111465 ZDOT = -294
024928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12861752
55 X = -3920262
18
Y = 5043346
66 feet Y = 1537212
06 meter
Z = 17387882
80 Z = 5299826
68
XDOT = -9936
872576 XDOT = -3028
758761
YDOT = -22004
978521 feet/sec YDOT = -6707
117453 meter/sec
ZDOT = -965
444596 ZDOT = -294
267513
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 12104
54760258
00016717 00000-0 10270-3 0 9079
2 25544 51
6386 85
9087 0007961 272
9843 87
0400 15
58294419 7943
Satellite: ISS
Catalog Number: 25544
Epoch time: 12104
54760258 = yrday
fracday
Element set: 907
Inclination: 51
6386 deg
RA of node: 85
9087 deg
Eccentricity:
0007961
Arg of perigee: 272
9843 deg
Mean anomaly: 87
0400 deg
Mean motion: 15
58294419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 794
Checksum: 336
Coasting Arc #9 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2012/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3981499
17 A = 6769418
99 meter
Y = 3401915
41 meter E =
0001930
Z = -4290653
76 I = 51
97677
XDOT = -1732
143337 Wp = 181
83680
YDOT = 6556
473667 meter/sec RA = 80
35182 deg
ZDOT = 3589
147758 TA = 124
60050
MA = 124
58230
Ha = 212
569 n
mi
Hp = 211
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13062661
32 X = 3964005
32
Y = 11161139
79 feet Y = 3446340
97 meter
Z = -14076948
04 Z = -4271354
53
XDOT = -5682
884964 XDOT = -1822
765643
YDOT = 21510
740377 feet/sec YDOT = 6536
597250 meter/sec
ZDOT = 11775
419154 ZDOT = 3580
512662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16396014
60 X = 4997505
25
Y = 5347354
44 feet Y = 1629873
63 meter
Z = -13997897
47 Z = -4266559
15
XDOT = 3214
009322 XDOT = 979
630041
YDOT = 20892
358458 feet/sec YDOT = 6367
990858 meter/sec
ZDOT = 11739
404056 ZDOT = 3578
170356
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 12105
50953290
00016717 00000-0 10270-3 0 9087
2 25544 51
6386 81
0827 0007934 276
9592 83
0660 15
58317824 8094
Satellite: ISS
Catalog Number: 25544
Epoch time: 12105
50953290 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 81
0827 deg
Eccentricity:
0007934
Arg of perigee: 276
9592 deg
Mean anomaly: 83
0660 deg
Mean motion: 15
58317824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 325
Coasting Arc #10 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2012/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2973052
49 A = 6775624
75 meter
Y = -5811213
58 meter E =
0006464
Z = 1802202
85 I = 51
99226
XDOT = 3647
646945 Wp = 131
27621
YDOT = -3633
818214 meter/sec RA = 75
36589 deg
ZDOT = -5690
802341 TA = 28
98307
MA = 28
94719
Ha = 212
623 n
mi
Hp = 211
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9754109
21 X = -2916604
04
Y = -19065661
36 feet Y = -5844144
35 meter
Z = 5912739
00 Z = 1787897
41
XDOT = 11967
345620 XDOT = 3715
654530
YDOT = -11921
975769 feet/sec YDOT = -3592
648098 meter/sec
ZDOT = -18670
611356 ZDOT = -5672
916833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16520270
80 X = -5035378
54
Y = -13653171
53 feet Y = -4161486
68 meter
Z = 5854411
32 Z = 1784424
57
XDOT = 5398
038919 XDOT = 1645
322262
YDOT = -14518
642226 feet/sec YDOT = -4425
282150 meter/sec
ZDOT = -18596
804581 ZDOT = -5668
306036
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 12106
53556867
00016717 00000-0 10270-3 0 9091
2 25544 51
6388 75
9345 0008019 281
2123 78
8130 15
58385815 8254
Satellite: ISS
Catalog Number: 25544
Epoch time: 12106
53556867 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 75
9345 deg
Eccentricity:
0008019
Arg of perigee: 281
2123 deg
Mean anomaly: 78
8130 deg
Mean motion: 15
58385815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 825
Checksum: 329
Coasting Arc #11 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2012/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1241340
80 A = 6776090
45 meter
Y = 6525686
76 meter E =
0009788
Z = 1304473
90 I = 51
98580
XDOT = -4948
896176 Wp = 25
02484
YDOT = -232
371813 meter/sec RA = 70
39956 deg
ZDOT = 5864
487214 TA = 349
13234
MA = 349
15347
Ha = 212
718 n
mi
Hp = 211
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4072640
43 X = 1161940
14
Y = 21409733
48 feet Y = 6539124
35 meter
Z = 4279770
01 Z = 1310310
91
XDOT = -16236
536012 XDOT = -4974
418329
YDOT = -762
374714 feet/sec YDOT = -287
855670 meter/sec
ZDOT = 19240
443616 ZDOT = 5840
383696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12477812
27 X = 3803237
18
Y = 17862417
82 feet Y = 5444464
95 meter
Z = 4303225
49 Z = 1311623
13
XDOT = -13922
122387 XDOT = -4243
462903
YDOT = 5108
197531 feet/sec YDOT = 1556
978608 meter/sec
ZDOT = 19141
393411 ZDOT = 5834
296712
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 12107
56157935
00016717 00000-0 10270-3 0 9100
2 25544 51
6389 70
7863 0007963 283
5649 76
4618 15
58441445 8413
Satellite: ISS
Catalog Number: 25544
Epoch time: 12107
56157935 = yrday
fracday
Element set: 910
Inclination: 51
6389 deg
RA of node: 70
7863 deg
Eccentricity:
0007963
Arg of perigee: 283
5649 deg
Mean anomaly: 76
4618 deg
Mean motion: 15
58441445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 841
Checksum: 337
Coasting Arc #12 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2012/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 951604
55 A = 6770057
85 meter
Y = -5398368
10 meter E =
0004704
Z = -3975698
64 I = 51
95542
XDOT = 5244
152730 Wp = 346
49648
YDOT = 3892
463054 meter/sec RA = 65
41688 deg
ZDOT = -4024
718068 TA = 241
70687
MA = 241
75435
Ha = 212
978 n
mi
Hp = 211
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3122062
19 X = 1031212
62
Y = -17711181
43 feet Y = -5387281
89 meter
Z = -13043630
71 Z = -3970881
94
XDOT = 17205
225491 XDOT = 5219
787932
YDOT = 12770
548076 feet/sec YDOT = 3950
969843 meter/sec
ZDOT = -13204
455604 ZDOT = -3999
301594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4650519
53 X = -1417478
35
Y = -17387744
82 feet Y = -5299784
62 meter
Z = -13023383
59 Z = -3969527
32
XDOT = 19810
699075 XDOT = 6038
301078
YDOT = 4526
870737 feet/sec YDOT = 1379
790201 meter/sec
ZDOT = -13100
316646 ZDOT = -3992
976514
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 12108
52344392
00016717 00000-0 10270-3 0 9113
2 25544 51
6397 65
9595 0008024 288
6262 71
4021 15
58458566 8567
Satellite: ISS
Catalog Number: 25544
Epoch time: 12108
52344392 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 65
9595 deg
Eccentricity:
0008024
Arg of perigee: 288
6262 deg
Mean anomaly: 71
4021 deg
Mean motion: 15
58458566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 324
Coasting Arc #13 (Orbit 871)
---------------------------------------
Vector Time (GMT): 2012/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3158577
84 A = 6764835
64 meter
Y = 2816521
72 meter E =
0005013
Z = 5281593
39 I = 51
92529
XDOT = -4297
897961 Wp = 287
31547
YDOT = -6305
995348 meter/sec RA = 60
40198 deg
ZDOT = 794
585530 TA = 155
13713
MA = 155
11297
Ha = 213
174 n
mi
Hp = 210
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10362788
19 X = -3215495
03
Y = 9240556
82 feet Y = 2780882
74 meter
Z = 17328062
31 Z = 5266110
54
XDOT = -14100
715095 XDOT = -4230
923563
YDOT = -20688
961117 feet/sec YDOT = -6353
682563 meter/sec
ZDOT = 2606
907908 ZDOT = 773
869546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5311218
58 X = -1618859
42
Y = 12914167
93 feet Y = 3936238
39 meter
Z = 17264189
43 Z = 5262124
94
XDOT = -20859
503999 XDOT = -6357
976819
YDOT = -11941
691978 feet/sec YDOT = -3639
827715 meter/sec
ZDOT = 2522
301800 ZDOT = 768
797589
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 12109
54940739
00016717 00000-0 10270-3 0 9124
2 25544 51
6404 60
8117 0008147 291
9488 68
0801 15
58503610 8720
Satellite: ISS
Catalog Number: 25544
Epoch time: 12109
54940739 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 60
8117 deg
Eccentricity:
0008147
Arg of perigee: 291
9488 deg
Mean anomaly: 68
0801 deg
Mean motion: 15
58503610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 872
Checksum: 308
Coasting Arc #14 (Orbit 886)
---------------------------------------
Vector Time (GMT): 2012/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4798085
82 A = 6767058
72 meter
Y = 385568
58 meter E =
0003124
Z = -4759054
74 I = 51
91706
XDOT = 2142
222868 Wp = 91
12690
YDOT = 6848
609101 meter/sec RA = 55
37650 deg
ZDOT = 2716
125290 TA = 205
59246
MA = 205
60793
Ha = 213
391 n
mi
Hp = 210
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15741751
37 X = 4816536
42
Y = 1264988
79 feet Y = 439326
56 meter
Z = -15613696
65 Z = -4735700
77
XDOT = 7028
290249 XDOT = 2052
286623
YDOT = 22469
189963 feet/sec YDOT = 6872
062098 meter/sec
ZDOT = 8911
172210 ZDOT = 2726
313290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14664012
09 X = 4469590
89
Y = -6112008
72 feet Y = -1862940
26 meter
Z = -15517749
66 Z = -4729810
10
XDOT = 16025
083292 XDOT = 4884
445387
YDOT = 15730
608102 feet/sec YDOT = 4794
689350 meter/sec
ZDOT = 8952
449490 ZDOT = 2728
706605
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 12110
51122644
00016717 00000-0 10270-3 0 9131
2 25544 51
6406 55
9845 0008129 295
6618 64
3697 15
58518561 8870
Satellite: ISS
Catalog Number: 25544
Epoch time: 12110
51122644 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 55
9845 deg
Eccentricity:
0008129
Arg of perigee: 295
6618 deg
Mean anomaly: 64
3697 deg
Mean motion: 15
58518561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 887
Checksum: 325
Coasting Arc #15 (Orbit 902)
---------------------------------------
Vector Time (GMT): 2012/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5333587
49 A = 6773732
56 meter
Y = -3293244
04 meter E =
0006259
Z = 2562976
99 I = 51
92263
XDOT = 839
896753 Wp = 83
74478
YDOT = -5489
749794 meter/sec RA = 50
37674 deg
ZDOT = -5294
382309 TA = 67
51879
MA = 67
45253
Ha = 213
384 n
mi
Hp = 210
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17498646
61 X = -5308815
92
Y = -10804606
42 feet Y = -3352748
86 meter
Z = 8408717
15 Z = 2537126
62
XDOT = 2755
566775 XDOT = 926
941146
YDOT = -18010
990137 feet/sec YDOT = -5479
871167 meter/sec
ZDOT = -17370
020699 ZDOT = -5290
090310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20571378
95 X = -6270156
30
Y = -1237345
38 feet Y = -377142
87 meter
Z = 8302771
92 Z = 2530684
88
XDOT = -6073
031168 XDOT = -1851
059900
YDOT = -15728
501387 feet/sec YDOT = -4794
047223 meter/sec
ZDOT = -17351
895941 ZDOT = -5288
857883
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 12111
53714241
00016717 00000-0 10270-3 0 9145
2 25544 51
6415 50
8362 0008124 299
6566 60
3779 15
58565587 9035
Satellite: ISS
Catalog Number: 25544
Epoch time: 12111
53714241 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 50
8362 deg
Eccentricity:
0008124
Arg of perigee: 299
6566 deg
Mean anomaly: 60
3779 deg
Mean motion: 15
58565587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 903
Checksum: 314
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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