[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 4th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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 1119)
---------------------------------------
Vector Time (GMT): 2012/125/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6528448
98 A = 6784119
64 meter
Y = 1675297
24 meter E =
0008025
Z = -727399
42 I = 51
54790
XDOT = -568
187593 Wp = 211
03223
YDOT = -4807
536778 meter/sec RA = 340
69140 deg
ZDOT = -5950
335128 TA = 336
84290
MA = 336
87905
Ha = 216
284 n
mi
Hp = 214
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21418795
87 X = -6543163
66
Y = 5496382
04 feet Y = 1602209
80 meter
Z = -2386481
05 Z = -759150
80
XDOT = -1864
132524 XDOT = -485
480491
YDOT = -15772
758459 feet/sec YDOT = -4813
428245 meter/sec
ZDOT = -19522
096878 ZDOT = -5952
894454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19166326
21 X = -5841896
23
Y = 10999387
82 feet Y = 3352613
41 meter
Z = -2517087
81 Z = -767208
36
XDOT = -5082
163503 XDOT = -1549
043436
YDOT = -13341
380697 feet/sec YDOT = -4066
452836 meter/sec
ZDOT = -19532
134973 ZDOT = -5953
394740
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 12125
45714929
00016717 00000-0 10270-3 0 9009
2 25544 51
6415 341
0681 0010881 276
0733 83
9181 15
55836115 11207
Satellite: ISS
Catalog Number: 25544
Epoch time: 12125
45714929 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 341
0681 deg
Eccentricity:
0010881
Arg of perigee: 276
0733 deg
Mean anomaly: 83
9181 deg
Mean motion: 15
55836115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1120
Checksum: 290
Coasting Arc #2 (Orbit 1135)
---------------------------------------
Vector Time (GMT): 2012/126/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6131230
12 A = 6780645
80 meter
Y = -258584
21 meter E =
0004746
Z = 2876580
36 I = 51
50792
XDOT = -2140
189690 Wp = 30
62977
YDOT = 5367
794671 meter/sec RA = 335
69928 deg
ZDOT = 5044
521986 TA = 2
20885
MA = 2
20676
Ha = 216
612 n
mi
Hp = 214
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20115584
39 X = 6119691
85
Y = -848373
40 feet Y = -190085
56 meter
Z = 9437599
60 Z = 2906338
29
XDOT = -7021
619719 XDOT = -2224
560134
YDOT = 17610
874905 feet/sec YDOT = 5343
389927 meter/sec
ZDOT = 16550
268984 ZDOT = 5033
919935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18998373
49 X = 5790704
24
Y = -6488096
45 feet Y = -1977571
80 meter
Z = 9559872
82 Z = 2913849
23
XDOT = -2321
389222 XDOT = -707
559435
YDOT = 17521
953912 feet/sec YDOT = 5340
691552 meter/sec
ZDOT = 16506
179492 ZDOT = 5031
083509
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 12126
48482162
00016717 00000-0 10270-3 0 9015
2 25544 51
6410 335
9300 0010904 281
6150 78
3780 15
55875964 11368
Satellite: ISS
Catalog Number: 25544
Epoch time: 12126
48482162 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 335
9300 deg
Eccentricity:
0010904
Arg of perigee: 281
6150 deg
Mean anomaly: 78
3780 deg
Mean motion: 15
55875964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1136
Checksum: 297
Coasting Arc #3 (Orbit 1150)
---------------------------------------
Vector Time (GMT): 2012/127/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4901116
38 A = 6775497
89 meter
Y = -1343444
93 meter E =
0006433
Z = -4483151
73 I = 51
46313
XDOT = 4410
802342 Wp = 344
57887
YDOT = -5397
055510 meter/sec RA = 330
68930 deg
ZDOT = -3197
572978 TA = 253
17301
MA = 253
24357
Ha = 216
986 n
mi
Hp = 214
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16079778
14 X = -4863950
80
Y = -4407627
72 feet Y = -1398044
22 meter
Z = -14708503
06 Z = -4506871
47
XDOT = 14471
136293 XDOT = 4486
358933
YDOT = -17706
875032 feet/sec YDOT = -5347
308576 meter/sec
ZDOT = -10490
724994 ZDOT = -3175
961735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16576402
35 X = -5052487
44
Y = 580863
58 feet Y = 177047
22 meter
Z = -14805809
40 Z = -4512810
71
XDOT = 8609
004636 XDOT = 2624
024613
YDOT = -20038
014998 feet/sec YDOT = -6107
586971 meter/sec
ZDOT = -10401
403021 ZDOT = -3170
347641
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 12127
44825116
00016717 00000-0 10270-3 0 9023
2 25544 51
6403 331
1139 0011114 284
8765 75
1158 15
55911761 11516
Satellite: ISS
Catalog Number: 25544
Epoch time: 12127
44825116 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 331
1139 deg
Eccentricity:
0011114
Arg of perigee: 284
8765 deg
Mean anomaly: 75
1158 deg
Mean motion: 15
55911761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1151
Checksum: 283
Coasting Arc #4 (Orbit 1166)
---------------------------------------
Vector Time (GMT): 2012/128/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3056955
18 A = 6772297
60 meter
Y = 2990101
74 meter E =
0007975
Z = 5257953
10 I = 51
42660
XDOT = -5947
307769 Wp = 285
11073
YDOT = 4780
071144 meter/sec RA = 325
66029 deg
ZDOT = 742
385224 TA = 157
79135
MA = 157
75679
Ha = 217
255 n
mi
Hp = 214
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10029380
51 X = 2997749
62
Y = 9810045
06 feet Y = 3023955
07 meter
Z = 17250502
30 Z = 5272660
35
XDOT = -19512
164596 XDOT = -6003
923882
YDOT = 15682
648111 feet/sec YDOT = 4713
248058 meter/sec
ZDOT = 2435
647060 ZDOT = 713
355756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12514400
39 X = 3814389
24
Y = 6175559
48 feet Y = 1882310
53 meter
Z = 17310619
14 Z = 5276276
71
XDOT = -13125
429637 XDOT = -4000
630953
YDOT = 20133
521640 feet/sec YDOT = 6136
697396 meter/sec
ZDOT = 2315
908950 ZDOT = 705
889048
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 12128
47589831
00016717 00000-0 10270-3 0 9039
2 25544 51
6405 325
9760 0010994 288
8521 71
1440 15
55922618 11678
Satellite: ISS
Catalog Number: 25544
Epoch time: 12128
47589831 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 325
9760 deg
Eccentricity:
0010994
Arg of perigee: 288
8521 deg
Mean anomaly: 71
1440 deg
Mean motion: 15
55922618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1167
Checksum: 321
Coasting Arc #5 (Orbit 1181)
---------------------------------------
Vector Time (GMT): 2012/129/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -935249
75 A = 6773185
35 meter
Y = -4432992
49 meter E =
0002580
Z = -5036592
64 I = 51
40435
XDOT = 6576
180773 Wp = 65
07581
YDOT = -3487
054026 meter/sec RA = 320
62411 deg
ZDOT = 1849
829289 TA = 222
88810
MA = 222
90822
Ha = 217
499 n
mi
Hp = 214
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3068404
70 X = -861142
66
Y = -14543938
63 feet Y = -4443036
23 meter
Z = -16524254
07 Z = -5040956
49
XDOT = 21575
396237 XDOT = 6605
698786
YDOT = -11440
465964 feet/sec YDOT = -3413
350226 meter/sec
ZDOT = 6068
993729 ZDOT = 1881
847900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7628759
28 X = -2325245
83
Y = -12734413
58 feet Y = -3881449
26 meter
Z = -16541734
29 Z = -5041920
61
XDOT = 15589
145958 XDOT = 4751
571688
YDOT = -17386
040180 feet/sec YDOT = -5299
265047 meter/sec
ZDOT = 6200
884921 ZDOT = 1890
029724
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 12129
43930403
00016717 00000-0 10270-3 0 9042
2 25544 51
6395 321
1584 0011145 292
4475 67
5498 15
55965291 11829
Satellite: ISS
Catalog Number: 25544
Epoch time: 12129
43930403 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 321
1584 deg
Eccentricity:
0011145
Arg of perigee: 292
4475 deg
Mean anomaly: 67
5498 deg
Mean motion: 15
55965291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1182
Checksum: 315
Coasting Arc #6 (Orbit 1197)
---------------------------------------
Vector Time (GMT): 2012/130/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1162943
84 A = 6777558
99 meter
Y = 5451768
37 meter E =
0006753
Z = 3859546
33 I = 51
39710
XDOT = -6283
072184 Wp = 8
86935
YDOT = 1569
149338 meter/sec RA = 315
59858 deg
ZDOT = -4102
170941 TA = 124
37755
MA = 124
31366
Ha = 217
797 n
mi
Hp = 213
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3815432
55 X = -1242569
15
Y = 17886379
18 feet Y = 5438318
06 meter
Z = 12662553
58 Z = 3853703
83
XDOT = -20613
753883 XDOT = -6280
224174
YDOT = 5148
127750 feet/sec YDOT = 1498
904429 meter/sec
ZDOT = -13458
566081 ZDOT = -4132
687017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2579560
98 X = 786250
19
Y = 18123109
28 feet Y = 5523923
71 meter
Z = 12638003
17 Z = 3852063
37
XDOT = -16132
693295 XDOT = -4917
244916
YDOT = 11786
224501 feet/sec YDOT = 3592
441228 meter/sec
ZDOT = -13584
094555 ZDOT = -4140
432020
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 12130
46692357
00016717 00000-0 10270-3 0 9051
2 25544 51
6401 316
0211 0011334 296
6168 63
3824 15
56012636 11983
Satellite: ISS
Catalog Number: 25544
Epoch time: 12130
46692357 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 316
0211 deg
Eccentricity:
0011334
Arg of perigee: 296
6168 deg
Mean anomaly: 63
3824 deg
Mean motion: 15
56012636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1198
Checksum: 288
Coasting Arc #7 (Orbit 1212)
---------------------------------------
Vector Time (GMT): 2012/131/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2922917
61 A = 6782379
46 meter
Y = -5794455
88 meter E =
0012268
Z = -1941415
67 I = 51
39059
XDOT = 5215
667035 Wp = 333
72889
YDOT = 760
609000 meter/sec RA = 310
58853 deg
ZDOT = 5579
623510 TA = 4
75505
MA = 4
74341
Ha = 218
056 n
mi
Hp = 213
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9589624
70 X = 2996926
15
Y = -19010682
01 feet Y = -5761356
05 meter
Z = -6369473
99 Z = -1927036
89
XDOT = 17111
768486 XDOT = 5179
669440
YDOT = 2495
436351 feet/sec YDOT = 818
732107 meter/sec
ZDOT = 18305
851412 ZDOT = 5604
873719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2041341
41 X = 622200
86
Y = -21212170
82 feet Y = -6465469
67 meter
Z = -6309822
93 Z = -1923234
03
XDOT = 15194
584703 XDOT = 4631
309417
YDOT = -4016
576023 feet/sec YDOT = -1224
252372 meter/sec
ZDOT = 18409
515845 ZDOT = 5611
220430
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 12131
43030694
00016717 00000-0 10270-3 0 9060
2 25544 51
6387 311
2034 0011301 299
9172 60
0858 15
55980338 12132
Satellite: ISS
Catalog Number: 25544
Epoch time: 12131
43030694 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 311
2034 deg
Eccentricity:
0011301
Arg of perigee: 299
9172 deg
Mean anomaly: 60
0858 deg
Mean motion: 15
55980338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1213
Checksum: 286
Coasting Arc #8 (Orbit 1228)
---------------------------------------
Vector Time (GMT): 2012/132/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4168340
23 A = 6783791
68 meter
Y = 5338479
50 meter E =
0002702
Z = -353745
49 I = 51
37665
XDOT = -3584
396956 Wp = 219
22469
YDOT = -3196
286653 meter/sec RA = 305
59155 deg
ZDOT = -5976
582139 TA = 324
60321
MA = 324
62114
Ha = 218
249 n
mi
Hp = 213
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13675656
93 X = -4226007
97
Y = 17514696
53 feet Y = 5291544
13 meter
Z = -1160582
31 Z = -374134
90
XDOT = -11759
832532 XDOT = -3519
356069
YDOT = -10486
504766 feet/sec YDOT = -3236
005572 meter/sec
ZDOT = -19608
209119 ZDOT = -5993
837232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5981830
13 X = -1823261
82
Y = 21396334
42 feet Y = 6521602
73 meter
Z = -1244877
52 Z = -379438
67
XDOT = -13193
554366 XDOT = -4021
395371
YDOT = -4837
597600 feet/sec YDOT = -1474
499748 meter/sec
ZDOT = -19678
789109 ZDOT = -5998
094920
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 12132
45790186
00016717 00000-0 10270-3 0 9073
2 25544 51
6387 306
0664 0011262 304
0041 56
0042 15
56012781 12298
Satellite: ISS
Catalog Number: 25544
Epoch time: 12132
45790186 = yrday
fracday
Element set: 907
Inclination: 51
6387 deg
RA of node: 306
0664 deg
Eccentricity:
0011262
Arg of perigee: 304
0041 deg
Mean anomaly: 56
0042 deg
Mean motion: 15
56012781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1229
Checksum: 275
Coasting Arc #9 (Orbit 1244)
---------------------------------------
Vector Time (GMT): 2012/133/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4788342
94 A = 6780834
83 meter
Y = -4031103
94 meter E =
0010670
Z = 2589244
76 I = 51
34932
XDOT = 1687
474769 Wp = 23
17693
YDOT = 5360
587574 meter/sec RA = 300
58846 deg
ZDOT = 5227
313115 TA = 6
12819
MA = 6
11514
Ha = 218
267 n
mi
Hp = 213
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15709786
55 X = 4820485
68
Y = -13225406
63 feet Y = -3977378
12 meter
Z = 8494897
52 Z = 2612584
28
XDOT = 5536
334543 XDOT = 1602
013002
YDOT = 17587
229572 feet/sec YDOT = 5378
979898 meter/sec
ZDOT = 17149
977410 ZDOT = 5235
303451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9138777
01 X = 2785499
23
Y = -18345201
90 feet Y = -5591617
54 meter
Z = 8591180
35 Z = 2618591
77
XDOT = 10616
466031 XDOT = 3235
898846
YDOT = 13331
768114 feet/sec YDOT = 4063
522921 meter/sec
ZDOT = 17182
287867 ZDOT = 5237
161342
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 12133
48548219
00016717 00000-0 10270-3 0 9086
2 25544 51
6377 300
9270 0011286 307
0669 52
9452 15
56049562 12453
Satellite: ISS
Catalog Number: 25544
Epoch time: 12133
48548219 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 300
9270 deg
Eccentricity:
0011286
Arg of perigee: 307
0669 deg
Mean anomaly: 52
9452 deg
Mean motion: 15
56049562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1245
Checksum: 313
Coasting Arc #10 (Orbit 1259)
---------------------------------------
Vector Time (GMT): 2012/134/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4810493
42 A = 6775695
54 meter
Y = 2041636
58 meter E =
0010496
Z = -4319123
86 I = 51
31681
XDOT = 207
267701 Wp = 358
74845
YDOT = -6840
171272 meter/sec RA = 295
56940 deg
ZDOT = -3453
706018 TA = 235
94919
MA = 236
04888
Ha = 218
567 n
mi
Hp = 213
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15782458
71 X = -4811984
47
Y = 6698282
73 feet Y = 1987834
44 meter
Z = -14170353
88 Z = -4342496
69
XDOT = 680
012141 XDOT = 300
517876
YDOT = -22441
506797 feet/sec YDOT = -6837
331992 meter/sec
ZDOT = -11331
056488 ZDOT = -3452
472797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11544825
28 X = -3518862
75
Y = 12567166
70 feet Y = 3830472
41 meter
Z = -14266578
21 Z = -4348453
04
XDOT = -7643
505977 XDOT = -2329
740622
YDOT = -19917
257082 feet/sec YDOT = -6070
779959 meter/sec
ZDOT = -11325
337149 ZDOT = -3451
962763
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 12134
44882840
00016717 00000-0 10270-3 0 9095
2 25544 51
6369 296
1104 0011198 311
6954 48
3241 15
56059773 12603
Satellite: ISS
Catalog Number: 25544
Epoch time: 12134
44882840 = yrday
fracday
Element set: 909
Inclination: 51
6369 deg
RA of node: 296
1104 deg
Eccentricity:
0011198
Arg of perigee: 311
6954 deg
Mean anomaly: 48
3241 deg
Mean motion: 15
56059773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1260
Checksum: 312
Coasting Arc #11 (Orbit 1275)
---------------------------------------
Vector Time (GMT): 2012/135/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4306927
99 A = 6772157
98 meter
Y = 411571
45 meter E =
0007759
Z = 5213200
95 I = 51
29219
XDOT = -1903
051822 Wp = 321
53926
YDOT = 7361
893418 meter/sec RA = 290
52991 deg
ZDOT = 997
787345 TA = 118
90204
MA = 118
82418
Ha = 218
765 n
mi
Hp = 212
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14130341
19 X = 4276680
88
Y = 1350300
03 feet Y = 459564
97 meter
Z = 17103677
67 Z = 5234050
50
XDOT = -6243
608341 XDOT = -1990
079632
YDOT = 24153
193630 feet/sec YDOT = 7340
125697 meter/sec
ZDOT = 3273
580529 ZDOT = 988
331085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13257662
62 X = 4040935
57
Y = -4773673
87 feet Y = -1455015
79 meter
Z = 17189300
79 Z = 5239298
88
XDOT = 4313
798739 XDOT = 1314
845856
YDOT = 23546
159820 feet/sec YDOT = 7176
869513 meter/sec
ZDOT = 3234
035430 ZDOT = 985
733999
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 12135
47638488
00016717 00000-0 10270-3 0 9108
2 25544 51
6367 290
9711 0011191 315
7017 44
3241 15
56023230 12767
Satellite: ISS
Catalog Number: 25544
Epoch time: 12135
47638488 = yrday
fracday
Element set: 910
Inclination: 51
6367 deg
RA of node: 290
9711 deg
Eccentricity:
0011191
Arg of perigee: 315
7017 deg
Mean anomaly: 44
3241 deg
Mean motion: 15
56023230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1276
Checksum: 289
Coasting Arc #12 (Orbit 1290)
---------------------------------------
Vector Time (GMT): 2012/136/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3431234
15 A = 6772549
24 meter
Y = -2878650
89 meter E =
0007989
Z = -5083813
78 I = 51
28422
XDOT = 3239
082188 Wp = 46
94331
YDOT = -6753
482924 meter/sec RA = 285
48381 deg
ZDOT = 1644
917527 TA = 238
97414
MA = 239
05262
Ha = 218
805 n
mi
Hp = 212
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11257329
87 X = -3374093
18
Y = -9444392
67 feet Y = -2916701
49 meter
Z = -16679179
07 Z = -5100344
00
XDOT = 10626
910067 XDOT = 3306
369548
YDOT = -22157
096207 feet/sec YDOT = -6716
885307 meter/sec
ZDOT = 5396
711048 ZDOT = 1660
816330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14185279
26 X = -4323673
12
Y = -3527139
74 feet Y = -1075072
19 meter
Z = -16746826
00 Z = -5104432
56
XDOT = -573
222443 XDOT = -174
718201
YDOT = -23522
711902 feet/sec YDOT = -7169
722588 meter/sec
ZDOT = 5462
661261 ZDOT = 1665
019152
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 12136
43970396
00016717 00000-0 10270-3 0 9113
2 25544 51
6364 286
1534 0011094 318
9639 41
0679 15
56092611 12916
Satellite: ISS
Catalog Number: 25544
Epoch time: 12136
43970396 = yrday
fracday
Element set: 911
Inclination: 51
6364 deg
RA of node: 286
1534 deg
Eccentricity:
0011094
Arg of perigee: 318
9639 deg
Mean anomaly: 41
0679 deg
Mean motion: 15
56092611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1291
Checksum: 313
Coasting Arc #13 (Orbit 1306)
---------------------------------------
Vector Time (GMT): 2012/137/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2286407
61 A = 6776977
26 meter
Y = 5020144
75 meter E =
0011537
Z = 3941669
06 I = 51
29169
XDOT = -4177
561739 Wp = 20
27669
YDOT = 5042
987587 meter/sec RA = 280
44729 deg
ZDOT = -3985
400028 TA = 111
56118
MA = 111
43818
Ha = 219
076 n
mi
Hp = 212
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7501337
29 X = 2210953
39
Y = 16470291
16 feet Y = 5045290
78 meter
Z = 12931985
09 Z = 3952593
33
XDOT = -13705
911218 XDOT = -4214
282519
YDOT = 16545
234866 feet/sec YDOT = 4996
066291 meter/sec
ZDOT = -13075
459408 ZDOT = -4005
783786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14145651
32 X = 4311594
52
Y = 11237894
66 feet Y = 3425310
29 meter
Z = 12976404
09 Z = 3955207
97
XDOT = -3709
234225 XDOT = -1130
574592
YDOT = 19917
902724 feet/sec YDOT = 6070
976750 meter/sec
ZDOT = -13159
672826 ZDOT = -4011
068277
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 12137
46723217
00016717 00000-0 10270-3 0 9126
2 25544 51
6362 281
0148 0011193 322
4703 37
5669 15
56095898 13078
Satellite: ISS
Catalog Number: 25544
Epoch time: 12137
46723217 = yrday
fracday
Element set: 912
Inclination: 51
6362 deg
RA of node: 281
0148 deg
Eccentricity:
0011193
Arg of perigee: 322
4703 deg
Mean anomaly: 37
5669 deg
Mean motion: 15
56095898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1307
Checksum: 308
Coasting Arc #14 (Orbit 1321)
---------------------------------------
Vector Time (GMT): 2012/138/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1022795
80 A = 6781774
51 meter
Y = -6381095
69 meter E =
0014431
Z = -2024838
32 I = 51
30431
XDOT = 4692
319211 Wp = 352
71410
YDOT = -2505
585095 meter/sec RA = 275
42913 deg
ZDOT = 5535
645889 TA = 344
76117
MA = 344
80459
Ha = 219
151 n
mi
Hp = 212
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3355629
25 X = -941528
70
Y = -20935353
32 feet Y = -6392078
76 meter
Z = -6643170
34 Z = -2029609
95
XDOT = 15394
748068 XDOT = 4693
097059
YDOT = -8220
423541 feet/sec YDOT = -2453
108545 meter/sec
ZDOT = 18161
567877 ZDOT = 5558
443138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12833240
41 X = -3911571
68
Y = -16870215
02 feet Y = -5142041
54 meter
Z = -6662189
15 Z = -2030635
25
XDOT = 8339
737384 XDOT = 2541
951955
YDOT = -13540
740998 feet/sec YDOT = -4127
217856 meter/sec
ZDOT = 18255
462185 ZDOT = 5564
264874
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 12138
43052799
00016717 00000-0 10270-3 0 9135
2 25544 51
6370 276
1969 0011100 326
5215 33
5236 15
56126097 13223
Satellite: ISS
Catalog Number: 25544
Epoch time: 12138
43052799 = yrday
fracday
Element set: 913
Inclination: 51
6370 deg
RA of node: 276
1969 deg
Eccentricity:
0011100
Arg of perigee: 326
5215 deg
Mean anomaly: 33
5236 deg
Mean motion: 15
56126097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1322
Checksum: 292
Coasting Arc #15 (Orbit 1337)
---------------------------------------
Vector Time (GMT): 2012/139/10:14:11
384
Vector Time (MET): N/A
Weight (LBS) : 911760
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -304431
29 A = 6783290
39 meter
Y = 6770129
30 meter E =
0002704
Z = -317383
76 I = 51
30794
XDOT = -4779
198019 Wp = 56
26368
YDOT = -493
194820 meter/sec RA = 270
42504 deg
ZDOT = -5971
513097 TA = 127
17248
MA = 127
14779
Ha = 219
375 n
mi
Hp = 211
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -998790
33 X = -378571
82
Y = 22211710
29 feet Y = 6766310
43 meter
Z = -1041285
30 Z = -319042
41
XDOT = -15679
783526 XDOT = -4744
319013
YDOT = -1618
093242 feet/sec YDOT = -546
443416 meter/sec
ZDOT = -19591
578403 ZDOT = -5994
645961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9986523
01 X = 3043892
21
Y = 19864830
19 feet Y = 6054800
24 meter
Z = -1048718
65 Z = -319649
44
XDOT = -12919
093813 XDOT = -3937
739794
YDOT = 5461
499792 feet/sec YDOT = 1664
665137 meter/sec
ZDOT = -19686
578807 ZDOT = -6000
469220
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 12139
45802888
00016717 00000-0 10270-3 0 9141
2 25544 51
6368 271
0582 0011349 330
8819 29
1701 15
56190616 13381
Satellite: ISS
Catalog Number: 25544
Epoch time: 12139
45802888 = yrday
fracday
Element set: 914
Inclination: 51
6368 deg
RA of node: 271
0582 deg
Eccentricity:
0011349
Arg of perigee: 330
8819 deg
Mean anomaly: 29
1701 deg
Mean motion: 15
56190616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1338
Checksum: 316
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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