[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 29th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 720)
---------------------------------------
Vector Time (GMT): 2011/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4956673
14 A = 6762566
43 meter
Y = 388147
66 meter E =
0012431
Z = 4571794
60 I = 51
39895
XDOT = -3260
081770 Wp = 49
51068
YDOT = 6279
698953 meter/sec RA = 317
24773 deg
ZDOT = 3003
952768 TA = 10
49885
MA = 10
47292
Ha = 214
447 n
mi
Hp = 203
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16262050
98 X = 4929755
81
Y = 1273450
34 feet Y = 443425
10 meter
Z = 14999326
13 Z = 4595808
41
XDOT = -10695
806332 XDOT = -3344
652708
YDOT = 20602
686854 feet/sec YDOT = 6242
769479 meter/sec
ZDOT = 9855
488084 ZDOT = 2987
910945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7994482
62 X = -2436718
30
Y = -14114873
71 feet Y = -4302213
51 meter
Z = 15096832
45 Z = 4601514
53
XDOT = 22064
146821 XDOT = 6725
151951
YDOT = -2034
786900 feet/sec YDOT = -620
203047 meter/sec
ZDOT = 9789
941647 ZDOT = 2983
974214
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 11208
55334818
00016717 00000-0 10270-3 0 9006
2 25544 51
6417 317
5435 0011692 9
4538 350
6836 15
60231764 7218
Satellite: ISS
Catalog Number: 25544
Epoch time: 11208
55334818 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 317
5435 deg
Eccentricity:
0011692
Arg of perigee: 9
4538 deg
Mean anomaly: 350
6836 deg
Mean motion: 15
60231764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 298
Coasting Arc #2 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2011/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2265582
49 A = 6760028
82 meter
Y = -3692238
18 meter E =
0019300
Z = -5202674
46 I = 51
36894
XDOT = 5703
925760 Wp = 60
46026
YDOT = -5008
285216 meter/sec RA = 312
16949 deg
ZDOT = 1082
790336 TA = 219
88367
MA = 220
02564
Ha = 214
694 n
mi
Hp = 202
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7433013
41 X = -2198853
65
Y = -12113642
33 feet Y = -3717199
56 meter
Z = -17069141
92 Z = -5213518
81
XDOT = 18713
667193 XDOT = 5754
245558
YDOT = -16431
381941 feet/sec YDOT = -4944
219226 meter/sec
ZDOT = 3552
461733 ZDOT = 1110
621040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5715246
46 X = -1742007
12
Y = 12954851
47 feet Y = 3948638
73 meter
Z = -17112960
18 Z = -5216030
26
XDOT = -23238
024690 XDOT = -7082
949926
YDOT = -5462
877265 feet/sec YDOT = -1665
084990 meter/sec
ZDOT = 3665
806678 ZDOT = 1117
337875
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 11209
51411855
00016717 00000-0 10270-3 0 9011
2 25544 51
6418 312
7111 0011866 13
2522 346
8943 15
60238813 7360
Satellite: ISS
Catalog Number: 25544
Epoch time: 11209
51411855 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 312
7111 deg
Eccentricity:
0011866
Arg of perigee: 13
2522 deg
Mean anomaly: 346
8943 deg
Mean motion: 15
60238813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 285
Coasting Arc #3 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2011/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1078391
12 A = 6767029
48 meter
Y = 5804205
58 meter E =
0019540
Z = 3305570
00 I = 51
37246
XDOT = -5880
422830 Wp = 55
71874
YDOT = 1585
659909 meter/sec RA = 307
10400 deg
ZDOT = -4672
031166 TA = 85
57140
MA = 85
34818
Ha = 214
882 n
mi
Hp = 202
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3538028
61 X = -1159272
19
Y = 19042669
22 feet Y = 5791693
76 meter
Z = 10845045
92 Z = 3300135
48
XDOT = -19292
725821 XDOT = -5875
021618
YDOT = 5202
296290 feet/sec YDOT = 1519
932146 meter/sec
ZDOT = -15328
186241 ZDOT = -4700
584270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17523753
26 X = 5341239
99
Y = -8279178
21 feet Y = -2523493
52 meter
Z = 10822624
38 Z = 3298735
91
XDOT = 14890
630044 XDOT = 4538
664037
YDOT = 11197
174026 feet/sec YDOT = 3412
898643 meter/sec
ZDOT = -15444
256606 ZDOT = -4707
409413
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 11210
53892853
00016717 00000-0 10270-3 0 9027
2 25544 51
6416 307
5550 0011871 17
4396 342
7165 15
60222901 7528
Satellite: ISS
Catalog Number: 25544
Epoch time: 11210
53892853 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 307
5550 deg
Eccentricity:
0011871
Arg of perigee: 17
4396 deg
Mean anomaly: 342
7165 deg
Mean motion: 15
60222901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 289
Coasting Arc #4 (Orbit 767)
---------------------------------------
Vector Time (GMT): 2011/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3687947
38 A = 6771638
29 meter
Y = -5660979
24 meter E =
0023892
Z = 148005
50 I = 51
37109
XDOT = 3945
089425 Wp = 33
72507
YDOT = 2738
686194 meter/sec RA = 302
07991 deg
ZDOT = 6003
166995 TA = 327
88142
MA = 328
02676
Ha = 214
970 n
mi
Hp = 202
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12099564
89 X = 3750256
49
Y = -18572766
52 feet Y = -5619389
99 meter
Z = 485582
36 Z = 166071
93
XDOT = 12943
206775 XDOT = 3885
010189
YDOT = 8985
190924 feet/sec YDOT = 2782
466160 meter/sec
ZDOT = 19695
429772 ZDOT = 6022
186024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22112958
06 X = -6740029
62
Y = 1512346
76 feet Y = 460963
29 meter
Z = 559294
50 Z = 170472
96
XDOT = -427
904334 XDOT = -130
425241
YDOT = -14037
669603 feet/sec YDOT = -4278
681695 meter/sec
ZDOT = 19772
523468 ZDOT = 6026
665153
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 11211
56372598
00016717 00000-0 10270-3 0 9031
2 25544 51
6420 302
3992 0012075 20
6414 339
5227 15
60234231 7689
Satellite: ISS
Catalog Number: 25544
Epoch time: 11211
56372598 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 302
3992 deg
Eccentricity:
0012075
Arg of perigee: 20
6414 deg
Mean anomaly: 339
5227 deg
Mean motion: 15
60234231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 284
Coasting Arc #5 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2011/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4819423
02 A = 6766025
57 meter
Y = 3149532
38 meter E =
0015507
Z = -3574179
07 I = 51
33649
XDOT = -789
582034 Wp = 41
03810
YDOT = -6215
989906 meter/sec RA = 297
05228 deg
ZDOT = -4412
225948 TA = 181
45355
MA = 181
45806
Ha = 215
010 n
mi
Hp = 202
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15811755
30 X = -4836921
27
Y = 10333111
47 feet Y = 3095541
02 meter
Z = -11726309
28 Z = -3597633
51
XDOT = -2590
492237 XDOT = -698
581734
YDOT = -20393
667671 feet/sec YDOT = -6224
310430 meter/sec
ZDOT = -14475
806917 ZDOT = -4415
840957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17830500
58 X = 5434736
58
Y = 6050657
31 feet Y = 1844240
35 meter
Z = -11821756
34 Z = -3603271
33
XDOT = -14095
081314 XDOT = -4296
180785
YDOT = 13221
934935 feet/sec YDOT = 4030
045768 meter/sec
ZDOT = -14490
142603 ZDOT = -4416
595465
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 11212
52446223
00016717 00000-0 10270-3 0 9046
2 25544 51
6409 297
5659 0011966 24
2163 335
9553 15
60262542 7835
Satellite: ISS
Catalog Number: 25544
Epoch time: 11212
52446223 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 297
5659 deg
Eccentricity:
0011966
Arg of perigee: 24
2163 deg
Mean anomaly: 335
9553 deg
Mean motion: 15
60262542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 305
Coasting Arc #6 (Orbit 798)
---------------------------------------
Vector Time (GMT): 2011/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4181182
84 A = 6759528
45 meter
Y = 845996
10 meter E =
0012431
Z = 5235356
80 I = 51
30252
XDOT = -2338
486584 Wp = 41
22776
YDOT = 7288
465109 meter/sec RA = 291
97857 deg
ZDOT = 698
114605 TA = 42
13695
MA = 42
04144
Ha = 214
897 n
mi
Hp = 202
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13717791
46 X = 4145980
21
Y = 2775577
75 feet Y = 892555
63 meter
Z = 17176367
46 Z = 5255583
00
XDOT = -7672
200080 XDOT = -2423
205045
YDOT = 23912
287102 feet/sec YDOT = 7261
841016 meter/sec
ZDOT = 2290
402246 ZDOT = 686
548992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6401365
87 X = -1951136
32
Y = -12331935
00 feet Y = -3758773
79 meter
Z = 17258479
87 Z = 5260384
66
XDOT = 22527
369246 XDOT = 6866
342146
YDOT = -8592
343179 feet/sec YDOT = -2618
946201 meter/sec
ZDOT = 2243
029352 ZDOT = 683
675346
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 11213
54923547
00016717 00000-0 10270-3 0 9059
2 25544 51
6410 292
4092 0012019 27
5632 332
6159 15
60317729 7990
Satellite: ISS
Catalog Number: 25544
Epoch time: 11213
54923547 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 292
4092 deg
Eccentricity:
0012019
Arg of perigee: 27
5632 deg
Mean anomaly: 332
6159 deg
Mean motion: 15
60317729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 799
Checksum: 303
Coasting Arc #7 (Orbit 813)
---------------------------------------
Vector Time (GMT): 2011/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2261513
02 A = 6763112
15 meter
Y = -4635677
76 meter E =
0016536
Z = -4383097
13 I = 51
30307
XDOT = 4414
776841 Wp = 64
07322
YDOT = -5304
177801 meter/sec RA = 286
89528 deg
ZDOT = 3348
932113 TA = 239
85865
MA = 240
02262
Ha = 215
111 n
mi
Hp = 201
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7419662
15 X = -2188216
05
Y = -15208916
53 feet Y = -4660557
47 meter
Z = -14380239
94 Z = -4393905
38
XDOT = 14484
175986 XDOT = 4457
492908
YDOT = -17402
158139 feet/sec YDOT = -5254
570296 meter/sec
ZDOT = 10987
310082 ZDOT = 3370
482305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6952328
00 X = -2119069
58
Y = 15387334
72 feet Y = 4690059
62 meter
Z = -14423900
11 Z = -4396404
75
XDOT = -21476
053673 XDOT = -6545
901160
YDOT = 626
360768 feet/sec YDOT = 190
914762 meter/sec
ZDOT = 11075
123093 ZDOT = 3375
697519
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 11214
50995232
00016717 00000-0 10270-3 0 9067
2 25544 51
6398 287
5761 0012204 31
7037 328
4851 15
60328910 8149
Satellite: ISS
Catalog Number: 25544
Epoch time: 11214
50995232 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 287
5761 deg
Eccentricity:
0012204
Arg of perigee: 31
7037 deg
Mean anomaly: 328
4851 deg
Mean motion: 15
60328910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 814
Checksum: 300
Coasting Arc #8 (Orbit 829)
---------------------------------------
Vector Time (GMT): 2011/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -289345
28 A = 6770570
58 meter
Y = 6627789
51 meter E =
0019324
Z = 1346401
87 I = 51
32009
XDOT = -4941
176368 Wp = 80
47768
YDOT = 975
621332 meter/sec RA = 281
85050 deg
ZDOT = -5790
223304 TA = 84
76155
MA = 84
54107
Ha = 215
261 n
mi
Hp = 201
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -949295
53 X = -369977
47
Y = 21744716
24 feet Y = 6624103
02 meter
Z = 4417328
98 Z = 1344800
50
XDOT = -16211
208557 XDOT = -4923
591317
YDOT = 3200
857389 feet/sec YDOT = 920
464488 meter/sec
ZDOT = -18996
795617 ZDOT = -5814
184420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17067583
77 X = 5202199
53
Y = -13508953
74 feet Y = -4117529
10 meter
Z = 4410486
89 Z = 1344316
40
XDOT = 11978
152053 XDOT = 3650
940746
YDOT = 8819
901723 feet/sec YDOT = 2688
306045 meter/sec
ZDOT = -19094
173441 ZDOT = -5819
904065
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 11215
53470465
00016717 00000-0 10270-3 0 9078
2 25544 51
6395 282
4188 0012348 35
0496 325
1470 15
60336985 8308
Satellite: ISS
Catalog Number: 25544
Epoch time: 11215
53470465 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 282
4188 deg
Eccentricity:
0012348
Arg of perigee: 35
0496 deg
Mean anomaly: 325
1470 deg
Mean motion: 15
60336985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 830
Checksum: 310
Coasting Arc #9 (Orbit 845)
---------------------------------------
Vector Time (GMT): 2011/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2552261
89 A = 6769080
00 meter
Y = -5814956
21 meter E =
0025127
Z = 2301100
12 I = 51
30955
XDOT = 3891
784483 Wp = 56
72813
YDOT = 3855
432840 meter/sec RA = 276
82729 deg
ZDOT = 5397
216760 TA = 329
15061
MA = 329
29802
Ha = 215
301 n
mi
Hp = 201
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8373562
63 X = 2605917
98
Y = -19077940
31 feet Y = -5786115
30 meter
Z = 7549541
07 Z = 2313629
06
XDOT = 12768
321794 XDOT = 3822
164650
YDOT = 12649
057875 feet/sec YDOT = 3898
563766 meter/sec
ZDOT = 17707
404068 ZDOT = 5415
953799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19759438
48 X = -6022676
85
Y = 6547787
91 feet Y = 1995765
75 meter
Z = 7600723
13 Z = 2316700
41
XDOT = 1431
960017 XDOT = 436
461413
YDOT = -16431
537420 feet/sec YDOT = -5008
332605 meter/sec
ZDOT = 17783
320220 ZDOT = 5420
356003
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 11216
55944581
00016717 00000-0 10270-3 0 9087
2 25544 51
6392 277
2620 0012398 39
0247 321
1801 15
60327856 8469
Satellite: ISS
Catalog Number: 25544
Epoch time: 11216
55944581 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 277
2620 deg
Eccentricity:
0012398
Arg of perigee: 39
0247 deg
Mean anomaly: 321
1801 deg
Mean motion: 15
60327856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 846
Checksum: 310
Coasting Arc #10 (Orbit 860)
---------------------------------------
Vector Time (GMT): 2011/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3982271
66 A = 6761171
27 meter
Y = 2524634
45 meter E =
0023566
Z = -4867634
38 I = 51
28032
XDOT = -1650
799307 Wp = 57
45418
YDOT = -7107
669385 meter/sec RA = 271
76860 deg
ZDOT = -2331
721844 TA = 189
56053
MA = 189
60546
Ha = 215
404 n
mi
Hp = 201
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13065195
74 X = -3986560
78
Y = 8282921
43 feet Y = 2480078
47 meter
Z = -15969929
06 Z = -4886990
39
XDOT = -5416
008225 XDOT = -1559
870299
YDOT = -23319
125278 feet/sec YDOT = -7125
621127 meter/sec
ZDOT = -7650
006051 ZDOT = -2339
520762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14895343
15 X = 4540100
59
Y = 3861793
92 feet Y = 1177074
79 meter
Z = -16048677
87 Z = -4891637
02
XDOT = -13144
735974 XDOT = -4006
515525
YDOT = 18722
089287 feet/sec YDOT = 5706
492815 meter/sec
ZDOT = -7681
335645 ZDOT = -2341
271105
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 11217
52013010
00016717 00000-0 10270-3 0 9090
2 25544 51
6389 272
4270 0012378 42
4245 317
7865 15
60336118 8616
Satellite: ISS
Catalog Number: 25544
Epoch time: 11217
52013010 = yrday
fracday
Element set: 909
Inclination: 51
6389 deg
RA of node: 272
4270 deg
Eccentricity:
0012378
Arg of perigee: 42
4245 deg
Mean anomaly: 317
7865 deg
Mean motion: 15
60336118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 861
Checksum: 290
Coasting Arc #11 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2011/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4127290
52 A = 6760320
71 meter
Y = 1885786
82 meter E =
0018000
Z = 5002782
70 I = 51
27841
XDOT = -1077
667502 Wp = 48
68717
YDOT = 7375
160249 meter/sec RA = 266
67806 deg
ZDOT = -1874
876164 TA = 59
62200
MA = 59
44418
Ha = 215
270 n
mi
Hp = 201
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13540979
40 X = 4081594
14
Y = 6186964
63 feet Y = 1931684
90 meter
Z = 16413329
07 Z = 5022722
01
XDOT = -3535
654534 XDOT = -1150
950156
YDOT = 24196
719977 feet/sec YDOT = 7362
699481 meter/sec
ZDOT = -6151
168518 ZDOT = -1880
288986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4859126
18 X = -1481061
66
Y = -13977236
28 feet Y = -4260261
62 meter
Z = 16494234
89 Z = 5027442
79
XDOT = 18844
430067 XDOT = 5743
782285
YDOT = -13898
437249 feet/sec YDOT = -4236
243673 meter/sec
ZDOT = -6173
514939 ZDOT = -1881
687353
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 11218
54484722
00016717 00000-0 10270-3 0 9107
2 25544 51
6390 267
2701 0012433 45
6883 314
5291 15
60401766 8771
Satellite: ISS
Catalog Number: 25544
Epoch time: 11218
54484722 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 267
2701 deg
Eccentricity:
0012433
Arg of perigee: 45
6883 deg
Mean anomaly: 314
5291 deg
Mean motion: 15
60401766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 877
Checksum: 302
Coasting Arc #12 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2011/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2996675
85 A = 6767936
54 meter
Y = -5426114
15 meter E =
0017392
Z = -2713383
11 I = 51
30695
XDOT = 3503
557842 Wp = 52
06691
YDOT = -4491
333510 meter/sec RA = 261
61405 deg
ZDOT = 5145
273210 TA = 277
01755
MA = 277
21532
Ha = 215
437 n
mi
Hp = 200
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9831613
68 X = -2922596
29
Y = -17802211
77 feet Y = -5459210
39 meter
Z = -8902175
56 Z = -2727761
29
XDOT = 11494
612342 XDOT = 3528
525882
YDOT = -14735
346160 feet/sec YDOT = -4452
015391 meter/sec
ZDOT = 16880
817619 ZDOT = 5162
353602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5717411
38 X = -1742666
99
Y = 19489788
57 feet Y = 5940487
56 meter
Z = -8960326
41 Z = -2731107
49
XDOT = -17058
750155 XDOT = -5199
507047
YDOT = 2739
105071 feet/sec YDOT = 834
879226 meter/sec
ZDOT = 16950
421347 ZDOT = 5166
488427
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 11219
50551210
00016717 00000-0 10270-3 0 9112
2 25544 51
6391 262
4355 0012596 49
9654 310
2605 15
60409623 8926
Satellite: ISS
Catalog Number: 25544
Epoch time: 11219
50551210 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 262
4355 deg
Eccentricity:
0012596
Arg of perigee: 49
9654 deg
Mean anomaly: 310
2605 deg
Mean motion: 15
60409623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 292
Coasting Arc #13 (Orbit 907)
---------------------------------------
Vector Time (GMT): 2011/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 778000
20 A = 6770691
64 meter
Y = 6655622
47 meter E =
0016337
Z = -982952
71 I = 51
32208
XDOT = -4910
969570 Wp = 90
42332
YDOT = -282
613966 meter/sec RA = 256
58911 deg
ZDOT = -5885
570297 TA = 100
29095
MA = 100
10671
Ha = 215
561 n
mi
Hp = 200
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2552494
10 X = 708292
85
Y = 21836031
74 feet Y = 6663932
88 meter
Z = -3224910
47 Z = -979341
97
XDOT = -16112
104888 XDOT = -4878
853718
YDOT = -927
211176 feet/sec YDOT = -337
351329 meter/sec
ZDOT = -19309
613836 ZDOT = -5909
349454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13361387
28 X = 4072550
84
Y = -17461192
15 feet Y = -5322171
37 meter
Z = -3210553
59 Z = -978576
73
XDOT = 9559
224494 XDOT = 2913
651626
YDOT = 10831
452271 feet/sec YDOT = 3301
426652 meter/sec
ZDOT = -19406
210701 ZDOT = -5915
013022
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 11220
53020843
00016717 00000-0 10270-3 0 9121
2 25544 51
6395 257
2779 0012711 53
4380 306
7944 15
60417270 9088
Satellite: ISS
Catalog Number: 25544
Epoch time: 11220
53020843 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 257
2779 deg
Eccentricity:
0012711
Arg of perigee: 53
4380 deg
Mean anomaly: 306
7944 deg
Mean motion: 15
60417270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 908
Checksum: 293
Coasting Arc #14 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2011/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1818776
46 A = 6763730
63 meter
Y = -5016042
42 meter E =
0021262
Z = 4135898
84 I = 51
30546
XDOT = 4734
729804 Wp = 78
38225
YDOT = 4789
545957 meter/sec RA = 251
54891 deg
ZDOT = 3714
718272 TA = 333
33391
MA = 333
44310
Ha = 215
589 n
mi
Hp = 200
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5967114
37 X = 1854640
59
Y = -16456832
08 feet Y = -4995503
59 meter
Z = 13569221
91 Z = 4144820
95
XDOT = 15533
890433 XDOT = 4662
775195
YDOT = 15713
733454 feet/sec YDOT = 4842
089944 meter/sec
ZDOT = 12187
395905 ZDOT = 3737
544793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15548998
98 X = -4739334
89
Y = 7979411
70 feet Y = 2432124
69 meter
Z = 13605703
90 Z = 4147018
55
XDOT = 51
812717 XDOT = 15
792516
YDOT = -20904
258471 feet/sec YDOT = -6371
617982 meter/sec
ZDOT = 12279
925343 ZDOT = 3742
921245
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 11221
55489378
00016717 00000-0 10270-3 0 9137
2 25544 51
6381 252
1210 0012836 57
5082 302
7313 15
60417769 9246
Satellite: ISS
Catalog Number: 25544
Epoch time: 11221
55489378 = yrday
fracday
Element set: 913
Inclination: 51
6381 deg
RA of node: 252
1210 deg
Eccentricity:
0012836
Arg of perigee: 57
5082 deg
Mean anomaly: 302
7313 deg
Mean motion: 15
60417769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 924
Checksum: 297
Coasting Arc #15 (Orbit 938)
---------------------------------------
Vector Time (GMT): 2011/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4023374
14 A = 6759133
74 meter
Y = 1357355
07 meter E =
0026509
Z = -5281094
43 I = 51
30165
XDOT = -2816
370770 Wp = 77
88632
YDOT = -7115
798490 meter/sec RA = 246
46577 deg
ZDOT = 323
562070 TA = 195
17649
MA = 195
25617
Ha = 215
616 n
mi
Hp = 200
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13200046
39 X = -4012599
33
Y = 4453264
67 feet Y = 1312423
90 meter
Z = -17326425
30 Z = -5300613
25
XDOT = -9240
061580 XDOT = -2738
162977
YDOT = -23345
795572 feet/sec YDOT = -7146
855607 meter/sec
ZDOT = 1061
555349 ZDOT = 310
069878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12694894
09 X = 3869403
72
Y = 5491404
41 feet Y = 1673780
06 meter
Z = -17405802
09 Z = -5305288
48
XDOT = -8419
213925 XDOT = -2566
176404
YDOT = 22584
513722 feet/sec YDOT = 6883
759782 meter/sec
ZDOT = 1007
043146 ZDOT = 306
946751
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 11222
51552493
00016717 00000-0 10270-3 0 9144
2 25544 51
6391 247
2864 0012684 60
5107 299
7313 15
60421434 9395
Satellite: ISS
Catalog Number: 25544
Epoch time: 11222
51552493 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 247
2864 deg
Eccentricity:
0012684
Arg of perigee: 60
5107 deg
Mean anomaly: 299
7313 deg
Mean motion: 15
60421434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 303
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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