[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 17th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11517 38 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 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 3591)
---------------------------------------
Vector Time (GMT): 2011/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5831757
37 A = 6728336
54 meter
Y = 3062285
82 meter E =
0006414
Z = -1354585
89 I = 51
45619
XDOT = -1220
258424 Wp = 161
78319
YDOT = -4892
610207 meter/sec RA = 322
86609 deg
ZDOT = -5820
574810 TA = 33
14122
MA = 33
10106
Ha = 187
313 n
mi
Hp = 183
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19133062
24 X = -5858986
55
Y = 10046869
50 feet Y = 2996919
44 meter
Z = -4444179
42 Z = -1382982
99
XDOT = -4003
472521 XDOT = -1137
181786
YDOT = -16051
870759 feet/sec YDOT = -4905
790883 meter/sec
ZDOT = -19096
374049 ZDOT = -5826
301552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3449514
03 X = -1051411
88
Y = 21309122
71 feet Y = 6495020
60 meter
Z = -4559224
77 Z = -1389651
71
XDOT = -13614
575299 XDOT = -4149
722551
YDOT = -6285
452048 feet/sec YDOT = -1915
805784 meter/sec
ZDOT = -19119
292343 ZDOT = -5827
560306
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 11136
52905431
00016717 00000-0 10270-3 0 9008
2 25544 51
6444 323
2713 0003384 284
0288 76
0499 15
75053725 35921
Satellite: ISS
Catalog Number: 25544
Epoch time: 11136
52905431 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 323
2713 deg
Eccentricity:
0003384
Arg of perigee: 284
0288 deg
Mean anomaly: 76
0499 deg
Mean motion: 15
75053725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3592
Checksum: 303
Coasting Arc #2 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2011/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1053727
73 A = 6718404
42 meter
Y = 4401531
67 meter E =
0004505
Z = 4965059
93 I = 51
39819
XDOT = -6437
187679 Wp = 20
80159
YDOT = 3751
387636 meter/sec RA = 317
67718 deg
ZDOT = -1954
761397 TA = 88
17342
MA = 88
12182
Ha = 187
316 n
mi
Hp = 183
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3457111
97 X = 980310
88
Y = 14440720
71 feet Y = 4412904
05 meter
Z = 16289566
70 Z = 4970001
18
XDOT = -21119
382148 XDOT = -6469
161948
YDOT = 12307
702218 feet/sec YDOT = 3679
224537 meter/sec
ZDOT = -6413
259177 ZDOT = -1986
111030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13663379
59 X = 4164598
10
Y = 5757934
76 feet Y = 1755018
51 meter
Z = 16309330
66 Z = 4971083
99
XDOT = -1991
451811 XDOT = -606
994512
YDOT = 23294
551215 feet/sec YDOT = 7100
179210 meter/sec
ZDOT = -6540
288982 ZDOT = -1993
480082
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 11137
54420412
00016717 00000-0 10270-3 0 9013
2 25544 51
6439 318
0492 0003380 285
3116 74
7674 15
75055721 36087
Satellite: ISS
Catalog Number: 25544
Epoch time: 11137
54420412 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 318
0492 deg
Eccentricity:
0003380
Arg of perigee: 285
3116 deg
Mean anomaly: 74
7674 deg
Mean motion: 15
75055721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 294
Coasting Arc #3 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2011/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5391958
39 A = 6727084
67 meter
Y = -3442480
35 meter E =
0011691
Z = 2060101
50 I = 51
40599
XDOT = 1209
354989 Wp = 58
94714
YDOT = 5218
617614 meter/sec RA = 312
55059 deg
ZDOT = 5537
964302 TA = 324
14373
MA = 324
22215
Ha = 187
250 n
mi
Hp = 183
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17690152
19 X = 5420044
40
Y = -11294226
87 feet Y = -3382027
43 meter
Z = 6758863
18 Z = 2086363
72
XDOT = 3967
700095 XDOT = 1124
006771
YDOT = 17121
448864 feet/sec YDOT = 5231
663422 meter/sec
ZDOT = 18169
174220 ZDOT = 5543
632791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 857566
02 X = 261386
12
Y = -20935986
57 feet Y = -6381288
71 meter
Z = 6865298
49 Z = 2092542
98
XDOT = 14716
881639 XDOT = 4485
705524
YDOT = 6586
479451 feet/sec YDOT = 2007
558937 meter/sec
ZDOT = 18191
838419 ZDOT = 5544
872350
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 11138
55932552
00016717 00000-0 10270-3 0 9029
2 25544 51
6437 312
8269 0003353 289
2581 70
8220 15
75121412 36241
Satellite: ISS
Catalog Number: 25544
Epoch time: 11138
55932552 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 312
8269 deg
Eccentricity:
0003353
Arg of perigee: 289
2581 deg
Mean anomaly: 70
8220 deg
Mean motion: 15
75121412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 294
Coasting Arc #4 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2011/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1078137
61 A = 6719397
73 meter
Y = -4727134
24 meter E =
0007692
Z = -4659458
34 I = 51
36103
XDOT = 5905
275031 Wp = 107
45690
YDOT = -4081
118191 meter/sec RA = 307
34742 deg
ZDOT = 2775
480268 TA = 190
03221
MA = 190
04757
Ha = 187
317 n
mi
Hp = 183
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3537196
89 X = -1002562
80
Y = -15508970
60 feet Y = -4738767
41 meter
Z = -15286936
82 Z = -4664513
06
XDOT = 19374
261913 XDOT = 5936
989111
YDOT = -13389
495376 feet/sec YDOT = -4014
904887 meter/sec
ZDOT = 9105
906391 ZDOT = 2804
244755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14787299
60 X = -4507168
92
Y = -5810113
76 feet Y = -1770922
67 meter
Z = -15307145
94 Z = -4665618
08
XDOT = -730
573278 XDOT = -222
678735
YDOT = -22425
084232 feet/sec YDOT = -6835
165674 meter/sec
ZDOT = 9222
503107 ZDOT = 2811
018947
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 11139
51097745
00016717 00000-0 10270-3 0 9033
2 25544 51
6444 307
9315 0003257 293
3395 66
7426 15
75163115 36392
Satellite: ISS
Catalog Number: 25544
Epoch time: 11139
51097745 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 307
9315 deg
Eccentricity:
0003257
Arg of perigee: 293
3395 deg
Mean anomaly: 66
7426 deg
Mean motion: 15
75163115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 319
Coasting Arc #5 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2011/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4925622
09 A = 6725223
62 meter
Y = 3630717
52 meter E =
0001331
Z = -2790456
08 I = 51
36400
XDOT = -1265
038035 Wp = 113
11639
YDOT = -5630
548648 meter/sec RA = 302
22857 deg
ZDOT = -5095
453213 TA = 98
96844
MA = 98
95338
Ha = 187
334 n
mi
Hp = 182
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16160177
45 X = -4952299
83
Y = 11911802
90 feet Y = 3575487
45 meter
Z = -9155039
62 Z = -2814449
10
XDOT = -4150
387255 XDOT = -1177
229306
YDOT = -18472
928634 feet/sec YDOT = -5644
203409 meter/sec
ZDOT = -16717
366184 ZDOT = -5101
386262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1221862
75 X = 372423
77
Y = 19993973
24 feet Y = 6094163
04 meter
Z = -9252308
87 Z = -2820103
74
XDOT = -16242
394881 XDOT = -4950
681960
YDOT = -6750
758493 feet/sec YDOT = -2057
631189 meter/sec
ZDOT = -16741
088480 ZDOT = -5102
683769
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 11140
52604524
00016717 00000-0 10270-3 0 9046
2 25544 51
6447 302
7102 0003348 300
4904 59
5929 15
75226627 36553
Satellite: ISS
Catalog Number: 25544
Epoch time: 11140
52604524 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node: 302
7102 deg
Eccentricity:
0003348
Arg of perigee: 300
4904 deg
Mean anomaly: 59
5929 deg
Mean motion: 15
75226627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3655
Checksum: 293
Coasting Arc #6 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2011/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1166670
29 A = 6720979
37 meter
Y = 5112539
24 meter E =
0008284
Z = 4200921
97 I = 51
33354
XDOT = -5369
031801 Wp = 55
98134
YDOT = 4190
422057 meter/sec RA = 297
01398 deg
ZDOT = -3599
049043 TA = 70
81761
MA = 70
72798
Ha = 187
352 n
mi
Hp = 182
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3827658
42 X = 1089006
90
Y = 16773422
69 feet Y = 5125150
89 meter
Z = 13782552
39 Z = 4206401
63
XDOT = -17614
933729 XDOT = -5398
007364
YDOT = 13748
103863 feet/sec YDOT = 4130
220721 meter/sec
ZDOT = -11807
903683 ZDOT = -3625
201621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16209320
37 X = 4940600
85
Y = 5714181
66 feet Y = 1741682
57 meter
Z = 13804473
51 Z = 4207603
53
XDOT = 2776
836936 XDOT = 846
379898
YDOT = 20981
268385 feet/sec YDOT = 6395
090604 meter/sec
ZDOT = -11913
939450 ZDOT = -3631
368744
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 11141
54108653
00016717 00000-0 10270-3 0 9052
2 25544 51
6442 297
4880 0003329 301
9418 58
1422 15
75224875 36710
Satellite: ISS
Catalog Number: 25544
Epoch time: 11141
54108653 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 297
4880 deg
Eccentricity:
0003329
Arg of perigee: 301
9418 deg
Mean anomaly: 58
1422 deg
Mean motion: 15
75224875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 306
Coasting Arc #7 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2011/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4457775
65 A = 6723106
70 meter
Y = -3629488
59 meter E =
0009619
Z = 3476796
31 I = 51
32949
XDOT = 1436
868504 Wp = 81
02733
YDOT = 6086
242276 meter/sec RA = 291
89805 deg
ZDOT = 4502
148143 TA = 320
49066
MA = 320
56075
Ha = 187
201 n
mi
Hp = 182
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14625248
19 X = 4481140
38
Y = -11907770
95 feet Y = -3579508
76 meter
Z = 11406812
03 Z = 3498508
48
XDOT = 4714
135512 XDOT = 1346
833635
YDOT = 19967
986469 feet/sec YDOT = 6101
806324 meter/sec
ZDOT = 14770
827240 ZDOT = 4508
910376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2703260
36 X = -823953
76
Y = -18610993
21 feet Y = -5672630
73 meter
Z = 11494849
68 Z = 3503630
18
XDOT = 18139
610939 XDOT = 5528
953414
YDOT = 6523
257423 feet/sec YDOT = 1988
288862 meter/sec
ZDOT = 14797
899750 ZDOT = 4510
399844
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 11142
55609798
00016717 00000-0 10270-3 0 9061
2 25544 51
6450 292
2661 0003393 305
4704 54
6143 15
75308429 36873
Satellite: ISS
Catalog Number: 25544
Epoch time: 11142
55609798 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 292
2661 deg
Eccentricity:
0003393
Arg of perigee: 305
4704 deg
Mean anomaly: 54
6143 deg
Mean motion: 15
75308429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 318
Coasting Arc #8 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2011/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1370967
53 A = 6722683
49 meter
Y = -5502062
49 meter E =
0003207
Z = -3612696
69 I = 51
31856
XDOT = 4865
257974 Wp = 65
33340
YDOT = -4072
998359 meter/sec RA = 286
67857 deg
ZDOT = 4361
144595 TA = 251
16850
MA = 251
20328
Ha = 187
371 n
mi
Hp = 182
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4497924
98 X = -1291790
75
Y = -18051386
11 feet Y = -5516950
47 meter
Z = -11852679
42 Z = -3619164
98
XDOT = 15962
132462 XDOT = 4889
255841
YDOT = -13362
855509 feet/sec YDOT = -4018
458286 meter/sec
ZDOT = 14308
217175 ZDOT = 4384
837886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17843832
64 X = -5438800
19
Y = -5202537
03 feet Y = -1585733
29 meter
Z = -11878599
41 Z = -3620597
10
XDOT = -4001
587161 XDOT = -1219
683767
YDOT = -19131
053252 feet/sec YDOT = -5831
145031 meter/sec
ZDOT = 14404
289575 ZDOT = 4390
427462
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 11143
50764737
00016717 00000-0 10270-3 0 9073
2 25544 51
6458 287
3711 0003409 311
3566 48
7304 15
75329628 37027
Satellite: ISS
Catalog Number: 25544
Epoch time: 11143
50764737 = yrday
fracday
Element set: 907
Inclination: 51
6458 deg
RA of node: 287
3711 deg
Eccentricity:
0003409
Arg of perigee: 311
3566 deg
Mean anomaly: 48
7304 deg
Mean motion: 15
75329628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3702
Checksum: 314
Coasting Arc #9 (Orbit 3717)
---------------------------------------
Vector Time (GMT): 2011/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4068645
67 A = 6720789
61 meter
Y = 3420688
62 meter E =
0007178
Z = -4120463
42 I = 51
30485
XDOT = -1709
043669 Wp = 43
45883
YDOT = -6516
148631 meter/sec RA = 281
56121 deg
ZDOT = -3720
669264 TA = 188
25919
MA = 188
27101
Ha = 187
425 n
mi
Hp = 182
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13348575
04 X = -4086577
64
Y = 11222731
70 feet Y = 3375090
59 meter
Z = -13518580
78 Z = -4140272
19
XDOT = -5607
098651 XDOT = -1617
977508
YDOT = -21378
440391 feet/sec YDOT = -6534
750754 meter/sec
ZDOT = -12206
920159 ZDOT = -3728
751050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3368881
25 X = 1026835
01
Y = 17047192
19 feet Y = 5195984
18 meter
Z = -13598899
46 Z = -4144944
56
XDOT = -20133
666996 XDOT = -6136
741700
YDOT = -5788
108814 feet/sec YDOT = -1764
215566 meter/sec
ZDOT = -12239
332283 ZDOT = -3730
548480
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 11144
52260528
00016717 00000-0 10270-3 0 9086
2 25544 51
6457 282
1491 0003530 315
7091 44
3790 15
75375907 37189
Satellite: ISS
Catalog Number: 25544
Epoch time: 11144
52260528 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 282
1491 deg
Eccentricity:
0003530
Arg of perigee: 315
7091 deg
Mean anomaly: 44
3790 deg
Mean motion: 15
75375907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3718
Checksum: 309
Coasting Arc #10 (Orbit 3733)
---------------------------------------
Vector Time (GMT): 2011/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1644461
96 A = 6724621
68 meter
Y = 5860679
52 meter E =
0011040
Z = 2849418
79 I = 51
31284
XDOT = -4478
511540 Wp = 86
79592
YDOT = 3718
213725 meter/sec RA = 276
34180 deg
ZDOT = -5045
552794 TA = 60
30622
MA = 60
19637
Ha = 187
455 n
mi
Hp = 182
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5395216
41 X = 1564962
51
Y = 19227951
17 feet Y = 5878624
20 meter
Z = 9348486
84 Z = 2857214
86
XDOT = -14693
279332 XDOT = -4495
246041
YDOT = 12198
863926 feet/sec YDOT = 3668
039037 meter/sec
ZDOT = -16553
650898 ZDOT = -5067
349856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19479535
39 X = 5937362
39
Y = 4334062
42 feet Y = 1321022
23 meter
Z = 9379780
18 Z = 2858957
00
XDOT = 4214
911243 XDOT = 1284
704947
YDOT = 17195
918094 feet/sec YDOT = 5241
315835 meter/sec
ZDOT = -16642
025899 ZDOT = -5072
489494
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 11145
53753568
00016717 00000-0 10270-3 0 9090
2 25544 51
6456 276
9263 0003515 319
6088 40
4814 15
75405396 37346
Satellite: ISS
Catalog Number: 25544
Epoch time: 11145
53753568 = yrday
fracday
Element set: 909
Inclination: 51
6456 deg
RA of node: 276
9263 deg
Eccentricity:
0003515
Arg of perigee: 319
6088 deg
Mean anomaly: 40
4814 deg
Mean motion: 15
75405396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3734
Checksum: 330
Coasting Arc #11 (Orbit 3749)
---------------------------------------
Vector Time (GMT): 2011/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3788892
64 A = 6718414
97 meter
Y = -3025575
29 meter E =
0004900
Z = 4646653
54 I = 51
29154
XDOT = 2081
375370 Wp = 98
20883
YDOT = 6879
138645 meter/sec RA = 271
21662 deg
ZDOT = 2778
867774 TA = 324
24927
MA = 324
28207
Ha = 187
290 n
mi
Hp = 182
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12430750
12 X = 3799870
88
Y = -9926428
13 feet Y = -2983144
51 meter
Z = 15244926
30 Z = 4665086
55
XDOT = 6828
659351 XDOT = 1990
797519
YDOT = 22569
352509 feet/sec YDOT = 6901
907225 meter/sec
ZDOT = 9117
020256 ZDOT = 2788
759567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3221442
09 X = -981895
55
Y = -15504702
24 feet Y = -4725833
24 meter
Z = 15319654
74 Z = 4669430
76
XDOT = 22048
853182 XDOT = 6720
490450
YDOT = 4476
620067 feet/sec YDOT = 1364
473796 meter/sec
ZDOT = 9156
757869 ZDOT = 2790
979798
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 11146
55243600
00016717 00000-0 10270-3 0 9106
2 25544 51
6466 271
7038 0003674 323
2379 36
8532 15
75494297 37502
Satellite: ISS
Catalog Number: 25544
Epoch time: 11146
55243600 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 271
7038 deg
Eccentricity:
0003674
Arg of perigee: 323
2379 deg
Mean anomaly: 36
8532 deg
Mean motion: 15
75494297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3750
Checksum: 312
Coasting Arc #12 (Orbit 3764)
---------------------------------------
Vector Time (GMT): 2011/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2003196
30 A = 6726230
08 meter
Y = -6107837
94 meter E =
0008890
Z = -1964710
97 I = 51
31868
XDOT = 4253
869217 Wp = 15
76733
YDOT = -3184
606788 meter/sec RA = 266
00665 deg
ZDOT = 5577
356459 TA = 322
24283
MA = 322
30517
Ha = 187
543 n
mi
Hp = 182
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6572166
33 X = -1925204
10
Y = -20038838
37 feet Y = -6129802
68 meter
Z = -6445902
13 Z = -1974253
57
XDOT = 13956
263834 XDOT = 4262
069918
YDOT = -10448
185000 feet/sec YDOT = -3136
991977 meter/sec
ZDOT = 18298
413578 ZDOT = 5598
041633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20870484
05 X = -6361323
54
Y = -2945380
79 feet Y = -897752
06 meter
Z = -6484265
20 Z = -1976404
03
XDOT = -3508
067101 XDOT = -1069
258852
YDOT = -15508
088570 feet/sec YDOT = -4726
865396 meter/sec
ZDOT = 18382
262423 ZDOT = 5602
913586
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 11147
50388208
00016717 00000-0 10270-3 0 9117
2 25544 51
6469 266
8079 0003817 329
5160 30
5782 15
75491168 37659
Satellite: ISS
Catalog Number: 25544
Epoch time: 11147
50388208 = yrday
fracday
Element set: 911
Inclination: 51
6469 deg
RA of node: 266
8079 deg
Eccentricity:
0003817
Arg of perigee: 329
5160 deg
Mean anomaly: 30
5782 deg
Mean motion: 15
75491168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3765
Checksum: 330
Coasting Arc #13 (Orbit 3780)
---------------------------------------
Vector Time (GMT): 2011/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3691116
18 A = 6716650
24 meter
Y = 2489830
58 meter E =
0013139
Z = -5040369
76 I = 51
29041
XDOT = -2494
142000 Wp = 60
73807
YDOT = -7084
092391 meter/sec RA = 260
86827 deg
ZDOT = -1669
837516 TA = 193
09571
MA = 193
12985
Ha = 187
586 n
mi
Hp = 181
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12109961
21 X = -3694198
12
Y = 8168735
50 feet Y = 2448537
46 meter
Z = -16536646
20 Z = -5058308
69
XDOT = -8182
880578 XDOT = -2406
629084
YDOT = -23241
772935 feet/sec YDOT = -7111
493952 meter/sec
ZDOT = -5478
469540 ZDOT = -1681
742213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2300542
15 X = 701205
25
Y = 14341442
97 feet Y = 4371271
82 meter
Z = -16609352
40 Z = -5062530
61
XDOT = -23458
425723 XDOT = -7150
128160
YDOT = -2648
835523 feet/sec YDOT = -807
365068 meter/sec
ZDOT = -5526
356576 ZDOT = -1684
433484
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 11148
51872981
00016717 00000-0 10270-3 0 9126
2 25544 51
6472 261
5854 0003881 332
5428 27
5530 15
75541732 37816
Satellite: ISS
Catalog Number: 25544
Epoch time: 11148
51872981 = yrday
fracday
Element set: 912
Inclination: 51
6472 deg
RA of node: 261
5854 deg
Eccentricity:
0003881
Arg of perigee: 332
5428 deg
Mean anomaly: 27
5530 deg
Mean motion: 15
75541732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3781
Checksum: 316
Coasting Arc #14 (Orbit 3796)
---------------------------------------
Vector Time (GMT): 2011/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2353543
62 A = 6727294
46 meter
Y = 6229820
85 meter E =
0010640
Z = 923392
09 I = 51
33279
XDOT = -4252
292799 Wp = 113
93825
YDOT = 2491
101560 meter/sec RA = 255
67445 deg
ZDOT = -5918
989704 TA = 55
93057
MA = 55
82962
Ha = 187
642 n
mi
Hp = 181
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7721599
81 X = 2279219
91
Y = 20439044
77 feet Y = 6255723
94 meter
Z = 3029501
61 Z = 934645
84
XDOT = -13951
091860 XDOT = -4251
078968
YDOT = 8172
905381 feet/sec YDOT = 2443
557216 meter/sec
ZDOT = -19419
257560 ZDOT = -5939
644425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21802635
86 X = 6645443
41
Y = 1321456
25 feet Y = 402779
86 meter
Z = 3074793
91 Z = 937197
18
XDOT = 1901
657312 XDOT = 579
625149
YDOT = 14376
104604 feet/sec YDOT = 4381
836683 meter/sec
ZDOT = -19502
957956 ZDOT = -5944
501585
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 11149
53355029
00016717 00000-0 10270-3 0 9139
2 25544 51
6473 256
3625 0003839 337
5099 22
5897 15
75582526 37971
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
53355029 = yrday
fracday
Element set: 913
Inclination: 51
6473 deg
RA of node: 256
3625 deg
Eccentricity:
0003839
Arg of perigee: 337
5099 deg
Mean anomaly: 22
5897 deg
Mean motion: 15
75582526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3797
Checksum: 344
Coasting Arc #15 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2011/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3786490
04 A = 6715400
97 meter
Y = -1851049
16 meter E =
0003136
Z = 5226852
83 I = 51
30295
XDOT = 2890
700196 Wp = 22
61676
YDOT = 7129
437959 meter/sec RA = 250
51655 deg
ZDOT = 433
496163 TA = 63
26559
MA = 63
23350
Ha = 187
496 n
mi
Hp = 181
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12422867
58 X = 3781515
95
Y = -6072995
92 feet Y = -1808734
76 meter
Z = 17148467
30 Z = 5245235
55
XDOT = 9483
924526 XDOT = 2808
656730
YDOT = 23390
544485 feet/sec YDOT = 7161
304742 meter/sec
ZDOT = 1422
231507 ZDOT = 447
340943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -743747
22 X = -226694
15
Y = -13714798
00 feet Y = -4180270
43 meter
Z = 17222949
95 Z = 5249555
14
XDOT = 24232
297612 XDOT = 7386
004312
YDOT = 530
558771 feet/sec YDOT = 161
714313 meter/sec
ZDOT = 1477
978991 ZDOT = 450
487996
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 11150
54834147
00016717 00000-0 10270-3 0 9146
2 25544 51
6480 251
1391 0004025 341
3347 18
7669 15
75669643 38138
Satellite: ISS
Catalog Number: 25544
Epoch time: 11150
54834147 = yrday
fracday
Element set: 914
Inclination: 51
6480 deg
RA of node: 251
1391 deg
Eccentricity:
0004025
Arg of perigee: 341
3347 deg
Mean anomaly: 18
7669 deg
Mean motion: 15
75669643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3813
Checksum: 308
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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