[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 30th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17760 45 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 3292)
---------------------------------------
Vector Time (GMT): 2011/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1197313
77 A = 6723145
52 meter
Y = 4913100
47 meter E =
0010959
Z = 4425337
88 I = 51
93473
XDOT = -5442
182263 Wp = 119
83103
YDOT = -4325
981479 meter/sec RA = 60
43526 deg
ZDOT = 3318
940242 TA = 296
93708
MA = 297
04899
Ha = 190
306 n
mi
Hp = 183
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3928194
80 X = -1273661
52
Y = 16119096
03 feet Y = 4899284
64 meter
Z = 14518825
07 Z = 4419335
72
XDOT = -17854
928684 XDOT = -5409
526652
YDOT = -14192
852620 feet/sec YDOT = -4386
656569 meter/sec
ZDOT = 10888
911555 ZDOT = 3292
581573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5778209
95 X = 1761198
39
Y = 15574927
34 feet Y = 4747237
85 meter
Z = 14494349
95 Z = 4417877
87
XDOT = -21666
735138 XDOT = -6604
020870
YDOT = -2031
016407 feet/sec YDOT = -619
053801 meter/sec
ZDOT = 10782
392021 ZDOT = 3286
473088
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 11117
55344018
00016717 00000-0 10270-3 0 9008
2 25544 51
6434 60
7907 0002328 158
1228 202
0035 15
74187386 32935
Satellite: ISS
Catalog Number: 25544
Epoch time: 11117
55344018 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 60
7907 deg
Eccentricity:
0002328
Arg of perigee: 158
1228 deg
Mean anomaly: 202
0035 deg
Mean motion: 15
74187386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 287
Coasting Arc #2 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2011/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5063257
55 A = 6728158
94 meter
Y = 3409234
37 meter E =
0004830
Z = -2833753
15 I = 51
93536
XDOT = -952
606477 Wp = 87
12439
YDOT = 5664
604365 meter/sec RA = 55
27182 deg
ZDOT = 5120
578639 TA = 240
54339
MA = 240
59159
Ha = 190
187 n
mi
Hp = 183
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16611737
35 X = 5038524
44
Y = 11185152
14 feet Y = 3465716
40 meter
Z = -9297090
38 Z = -2809215
94
XDOT = -3125
349333 XDOT = -1040
753316
YDOT = 18584
659991 feet/sec YDOT = 5653
459070 meter/sec
ZDOT = 16799
798686 ZDOT = 5115
736545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20065623
86 X = 6116002
15
Y = -512279
94 feet Y = -156142
93 meter
Z = -9197915
22 Z = -2803524
56
XDOT = 8077
506667 XDOT = 2462
024032
YDOT = 15565
348730 feet/sec YDOT = 4744
318293 meter/sec
ZDOT = 16779
984407 ZDOT = 5114
539247
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 11118
50566776
00016717 00000-0 10270-3 0 9012
2 25544 51
6432 55
8992 0002194 160
7644 199
3602 15
74209460 33087
Satellite: ISS
Catalog Number: 25544
Epoch time: 11118
50566776 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 55
8992 deg
Eccentricity:
0002194
Arg of perigee: 160
7644 deg
Mean anomaly: 199
3602 deg
Mean motion: 15
74209460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 313
Coasting Arc #3 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2011/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 508511
72 A = 6722395
57 meter
Y = -4944786
74 meter E =
0010158
Z = -4534925
05 I = 51
89958
XDOT = 6100
453550 Wp = 82
07012
YDOT = 3491
212956 meter/sec RA = 50
19996 deg
ZDOT = -3127
249604 TA = 156
85068
MA = 156
80489
Ha = 190
011 n
mi
Hp = 183
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1668345
53 X = 585797
50
Y = -16223053
61 feet Y = -4938668
27 meter
Z = -14878363
03 Z = -4532266
79
XDOT = 20014
611383 XDOT = 6076
152473
YDOT = 11454
110747 feet/sec YDOT = 3559
295954 meter/sec
ZDOT = -10260
005262 ZDOT = -3097
672501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8191322
16 X = -2496714
99
Y = -14113785
46 feet Y = -4301881
81 meter
Z = -14867408
40 Z = -4531586
08
XDOT = 21930
535673 XDOT = 6684
427273
YDOT = -2061
861336 feet/sec YDOT = -628
455335 meter/sec
ZDOT = -10140
444659 ZDOT = -3090
807532
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 11119
52133378
00016717 00000-0 10270-3 0 9024
2 25544 51
6443 50
6813 0002240 164
0929 196
0305 15
74302494 33242
Satellite: ISS
Catalog Number: 25544
Epoch time: 11119
52133378 = yrday
fracday
Element set: 902
Inclination: 51
6443 deg
RA of node: 50
6813 deg
Eccentricity:
0002240
Arg of perigee: 164
0929 deg
Mean anomaly: 196
0305 deg
Mean motion: 15
74302494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 280
Coasting Arc #4 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2011/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5578998
75 A = 6728251
82 meter
Y = -2678900
30 meter E =
0014802
Z = 2619936
15 I = 51
89949
XDOT = 218
801198 Wp = 110
90176
YDOT = -5622
617080 meter/sec RA = 45
03583 deg
ZDOT = -5264
684611 TA = 39
40255
MA = 39
29498
Ha = 189
930 n
mi
Hp = 183
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18303801
68 X = -5561355
46
Y = -8789042
98 feet Y = -2741189
34 meter
Z = 8595591
03 Z = 2592875
96
XDOT = 717
851699 XDOT = 307
233311
YDOT = -18446
906429 feet/sec YDOT = -5619
675983 meter/sec
ZDOT = -17272
587305 ZDOT = -5263
406727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19926862
85 X = -6073707
80
Y = 4131016
11 feet Y = 1259133
71 meter
Z = 8486192
34 Z = 2586591
43
XDOT = -10223
969739 XDOT = -3116
265976
YDOT = -13719
593041 feet/sec YDOT = -4181
731959 meter/sec
ZDOT = -17267
183572 ZDOT = -5263
037553
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 11120
53695629
00016717 00000-0 10270-3 0 9030
2 25544 51
6447 45
4638 0002273 170
3510 189
7698 15
74356916 33405
Satellite: ISS
Catalog Number: 25544
Epoch time: 11120
53695629 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 45
4638 deg
Eccentricity:
0002273
Arg of perigee: 170
3510 deg
Mean anomaly: 189
7698 deg
Mean motion: 15
74356916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3340
Checksum: 319
Coasting Arc #5 (Orbit 3355)
---------------------------------------
Vector Time (GMT): 2011/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 90979
94 A = 6721500
80 meter
Y = 4845007
49 meter E =
0009446
Z = 4654347
23 I = 51
85540
XDOT = -6648
047058 Wp = 128
85629
YDOT = -2635
732609 meter/sec RA = 39
95826 deg
ZDOT = 2863
979722 TA = 292
88310
MA = 292
98279
Ha = 189
673 n
mi
Hp = 183
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 298490
60 X = 14185
05
Y = 15895693
88 feet Y = 4845595
55 meter
Z = 15270168
07 Z = 4654602
63
XDOT = -21811
178011 XDOT = -6631
992595
YDOT = -8647
416697 feet/sec YDOT = -2709
985316 meter/sec
ZDOT = 9396
258929 ZDOT = 2831
722043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10011156
96 X = 3051400
64
Y = 12349644
17 feet Y = 3764171
54 meter
Z = 15270993
37 Z = 4654598
78
XDOT = -21621
383050 XDOT = -6590
197554
YDOT = 6030
287706 feet/sec YDOT = 1838
031693 meter/sec
ZDOT = 9265
833683 ZDOT = 2824
226107
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 11121
55253441
00016717 00000-0 10270-3 0 9046
2 25544 51
6450 40
2459 0002350 176
5033 183
6147 15
74435483 33563
Satellite: ISS
Catalog Number: 25544
Epoch time: 11121
55253441 = yrday
fracday
Element set: 904
Inclination: 51
6450 deg
RA of node: 40
2459 deg
Eccentricity:
0002350
Arg of perigee: 176
5033 deg
Mean anomaly: 183
6147 deg
Mean motion: 15
74435483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3356
Checksum: 283
Coasting Arc #6 (Orbit 3370)
---------------------------------------
Vector Time (GMT): 2011/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6003738
00 A = 6728428
35 meter
Y = 1921273
76 meter E =
0004405
Z = -2353047
04 I = 51
85537
XDOT = 377
954189 Wp = 65
41197
YDOT = 5448
720785 meter/sec RA = 34
79262 deg
ZDOT = 5422
935835 TA = 268
18581
MA = 268
23627
Ha = 189
515 n
mi
Hp = 183
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19697303
14 X = 5993238
60
Y = 6303391
59 feet Y = 1988352
52 meter
Z = -7719970
61 Z = -2323905
87
XDOT = 1240
007181 XDOT = 290
653368
YDOT = 17876
380529 feet/sec YDOT = 5452
459124 meter/sec
ZDOT = 17791
784236 ZDOT = 5424
559960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19274410
73 X = 5874840
39
Y = -7617027
39 feet Y = -2321669
95 meter
Z = -7602133
08 Z = -2317130
16
XDOT = 11637
637323 XDOT = 3547
151856
YDOT = 11717
223015 feet/sec YDOT = 3571
409575 meter/sec
ZDOT = 17798
112580 ZDOT = 5424
864714
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 11122
50460016
00016717 00000-0 10270-3 0 9051
2 25544 51
6455 35
3538 0002308 181
5874 178
5282 15
74494583 33719
Satellite: ISS
Catalog Number: 25544
Epoch time: 11122
50460016 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 35
3538 deg
Eccentricity:
0002308
Arg of perigee: 181
5874 deg
Mean anomaly: 178
5282 deg
Mean motion: 15
74494583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3371
Checksum: 304
Coasting Arc #7 (Orbit 3386)
---------------------------------------
Vector Time (GMT): 2011/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -513887
93 A = 6720419
76 meter
Y = -4662162
61 meter E =
0011249
Z = -4823011
88 I = 51
80419
XDOT = 7061
102562 Wp = 82
74923
YDOT = 1782
835720 meter/sec RA = 29
70677 deg
ZDOT = -2479
252959 TA = 163
06088
MA = 163
02329
Ha = 189
309 n
mi
Hp = 182
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1685984
02 X = -438286
81
Y = -15295809
08 feet Y = -4667486
36 meter
Z = -15823529
80 Z = -4825324
89
XDOT = 23166
346988 XDOT = 7052
685722
YDOT = 5849
198555 feet/sec YDOT = 1861
750266 meter/sec
ZDOT = -8134
032018 ZDOT = -2444
969913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11098766
22 X = -3382903
94
Y = -10645763
14 feet Y = -3244828
61 meter
Z = -15832672
81 Z = -4825798
67
XDOT = 20720
074194 XDOT = 6315
478614
YDOT = -9727
973483 feet/sec YDOT = -2965
086318 meter/sec
ZDOT = -7995
386643 ZDOT = -2436
993849
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 11123
52009400
00016717 00000-0 10270-3 0 9061
2 25544 51
6462 30
1354 0002271 185
9981 174
1156 15
74576252 33875
Satellite: ISS
Catalog Number: 25544
Epoch time: 11123
52009400 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 30
1354 deg
Eccentricity:
0002271
Arg of perigee: 185
9981 deg
Mean anomaly: 174
1156 deg
Mean motion: 15
74576252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3387
Checksum: 290
Coasting Arc #8 (Orbit 3402)
---------------------------------------
Vector Time (GMT): 2011/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6317210
87 A = 6728855
25 meter
Y = -1185916
86 meter E =
0014793
Z = 1963848
30 I = 51
80500
XDOT = -775
366139 Wp = 121
35188
YDOT = -5214
775546 meter/sec RA = 24
54180 deg
ZDOT = -5619
874553 TA = 36
82151
MA = 36
72000
Ha = 189
265 n
mi
Hp = 183
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20725757
45 X = -6313020
38
Y = -3890803
34 feet Y = -1256536
41 meter
Z = 6443071
85 Z = 1933168
90
XDOT = -2543
852162 XDOT = -689
695110
YDOT = -17108
843655 feet/sec YDOT = -5222
966865 meter/sec
ZDOT = -18437
908639 ZDOT = -5623
433508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18178190
14 X = -5540712
35
Y = 10762545
82 feet Y = 3280423
96 meter
Z = 6318983
96 Z = 1926026
31
XDOT = -12323
979638 XDOT = -3756
348994
YDOT = -9935
915016 feet/sec YDOT = -3028
466897 meter/sec
ZDOT = -18452
059159 ZDOT = -5624
187632
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 11124
53554539
00016717 00000-0 10270-3 0 9072
2 25544 51
6459 24
9167 0002404 191
1602 168
9509 15
74601285 34038
Satellite: ISS
Catalog Number: 25544
Epoch time: 11124
53554539 = yrday
fracday
Element set: 907
Inclination: 51
6459 deg
RA of node: 24
9167 deg
Eccentricity:
0002404
Arg of perigee: 191
1602 deg
Mean anomaly: 168
9509 deg
Mean motion: 15
74601285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3403
Checksum: 304
Coasting Arc #9 (Orbit 3418)
---------------------------------------
Vector Time (GMT): 2011/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 798000
72 A = 6719391
11 meter
Y = 4442340
18 meter E =
0006872
Z = 4975981
81 I = 51
74608
XDOT = -7379
785121 Wp = 143
16406
YDOT = -928
431994 meter/sec RA = 19
44500 deg
ZDOT = 2005
546677 TA = 287
43696
MA = 287
51207
Ha = 188
938 n
mi
Hp = 182
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2618112
61 X = 724093
56
Y = 14574606
87 feet Y = 4450850
33 meter
Z = 16325399
64 Z = 4979679
33
XDOT = -24211
893440 XDOT = -7378
597448
YDOT = -3046
036725 feet/sec YDOT = -1010
950722 meter/sec
ZDOT = 6579
877549 ZDOT = 1969
697999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11661713
35 X = 3554490
23
Y = 9099260
99 feet Y = 2773454
75 meter
Z = 16340142
10 Z = 4980475
31
XDOT = -19341
150572 XDOT = -5895
182694
YDOT = 13192
203031 feet/sec YDOT = 4020
983484 meter/sec
ZDOT = 6434
860482 ZDOT = 1961
345475
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 11125
55095154
00016717 00000-0 10270-3 0 9089
2 25544 51
6462 19
6974 0002354 198
2995 161
8084 15
74694533 34191
Satellite: ISS
Catalog Number: 25544
Epoch time: 11125
55095154 = yrday
fracday
Element set: 908
Inclination: 51
6462 deg
RA of node: 19
6974 deg
Eccentricity:
0002354
Arg of perigee: 198
2995 deg
Mean anomaly: 161
8084 deg
Mean motion: 15
74694533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3419
Checksum: 334
Coasting Arc #10 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2011/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6540870
98 A = 6729037
65 meter
Y = 437815
96 meter E =
0006137
Z = -1508547
59 I = 51
74998
XDOT = 999
883577 Wp = 41
30258
YDOT = 4968
851115 meter/sec RA = 14
28139 deg
ZDOT = 5795
286140 TA = 302
10488
MA = 302
16443
Ha = 188
747 n
mi
Hp = 182
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21459550
47 X = 6542817
43
Y = 1436404
06 feet Y = 510970
94 meter
Z = -4949303
13 Z = -1476766
94
XDOT = 3280
457931 XDOT = 916
093871
YDOT = 16302
004971 feet/sec YDOT = 4979
563478 meter/sec
ZDOT = 19013
405970 ZDOT = 5799
940483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16645038
46 X = 5073407
72
Y = -13666546
55 feet Y = -4165563
39 meter
Z = -4820722
41 Z = -1469356
19
XDOT = 12473
739407 XDOT = 3801
995771
YDOT = 8500
144908 feet/sec YDOT = 2590
844168 meter/sec
ZDOT = 19031
989292 ZDOT = 5800
950336
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 11126
50285605
00016717 00000-0 10270-3 0 9098
2 25544 51
6464 14
8040 0002373 205
5005 154
6042 15
74771039 34347
Satellite: ISS
Catalog Number: 25544
Epoch time: 11126
50285605 = yrday
fracday
Element set: 909
Inclination: 51
6464 deg
RA of node: 14
8040 deg
Eccentricity:
0002373
Arg of perigee: 205
5005 deg
Mean anomaly: 154
6042 deg
Mean motion: 15
74771039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 279
Coasting Arc #11 (Orbit 3449)
---------------------------------------
Vector Time (GMT): 2011/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -895468
91 A = 6718302
51 meter
Y = -4253572
43 meter E =
0012595
Z = -5133491
68 I = 51
68425
XDOT = 7563
456762 Wp = 86
98366
YDOT = 98
119048 meter/sec RA = 9
17094 deg
ZDOT = -1402
941651 TA = 169
58939
MA = 169
56328
Ha = 188
498 n
mi
Hp = 182
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2937890
13 X = -822900
36
Y = -13955290
13 feet Y = -4263179
95 meter
Z = -16842164
31 Z = -5137665
96
XDOT = 24814
490689 XDOT = 7568
612720
YDOT = 321
912888 feet/sec YDOT = 182
727150 meter/sec
ZDOT = -4602
826938 ZDOT = -1366
185602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11763108
74 X = -3585395
55
Y = -8027991
30 feet Y = -2446931
75 meter
Z = -16858838
86 Z = -5138574
09
XDOT = 17448
923019 XDOT = 5318
431736
YDOT = -16229
422165 feet/sec YDOT = -4946
727876 meter/sec
ZDOT = -4454
093917 ZDOT = -1357
607826
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 11127
51817875
00016717 00000-0 10270-3 0 9102
2 25544 51
6461 9
5839 0002356 213
2998 146
8018 15
74844232 34509
Satellite: ISS
Catalog Number: 25544
Epoch time: 11127
51817875 = yrday
fracday
Element set: 910
Inclination: 51
6461 deg
RA of node: 9
5839 deg
Eccentricity:
0002356
Arg of perigee: 213
2998 deg
Mean anomaly: 146
8018 deg
Mean motion: 15
74844232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3450
Checksum: 315
Coasting Arc #12 (Orbit 3465)
---------------------------------------
Vector Time (GMT): 2011/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6652685
38 A = 6729421
24 meter
Y = 264752
38 meter E =
0013883
Z = 923535
75 I = 51
69109
XDOT = -1022
757280 Wp = 135
61853
YDOT = -4785
247952 meter/sec RA = 4
01231 deg
ZDOT = -5951
806526 TA = 34
29708
MA = 34
20752
Ha = 188
465 n
mi
Hp = 182
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21826395
62 X = -6659637
83
Y = 868610
16 feet Y = 190319
07 meter
Z = 3029972
93 Z = 891200
04
XDOT = -3355
502886 XDOT = -940
258823
YDOT = -15699
632389 feet/sec YDOT = -4796
223342 meter/sec
ZDOT = -19526
924297 ZDOT = -5956
575051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14780530
89 X = -4505105
81
Y = 16107695
26 feet Y = 4909625
52 meter
Z = 2899107
63 Z = 883648
01
XDOT = -12245
325433 XDOT = -3732
375192
YDOT = -7691
410888 feet/sec YDOT = -2344
342039 meter/sec
ZDOT = -19545
975554 ZDOT = -5957
613349
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 11128
53346035
00016717 00000-0 10270-3 0 9111
2 25544 51
6461 4
3639 0002522 214
9486 145
1513 15
74850507 34666
Satellite: ISS
Catalog Number: 25544
Epoch time: 11128
53346035 = yrday
fracday
Element set: 911
Inclination: 51
6461 deg
RA of node: 4
3639 deg
Eccentricity:
0002522
Arg of perigee: 214
9486 deg
Mean anomaly: 145
1513 deg
Mean motion: 15
74850507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3466
Checksum: 291
Coasting Arc #13 (Orbit 3481)
---------------------------------------
Vector Time (GMT): 2011/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 859305
15 A = 6717516
73 meter
Y = 4126301
11 meter E =
0003225
Z = 5230182
47 I = 51
62123
XDOT = -7639
661591 Wp = 162
55508
YDOT = 701
832028 meter/sec RA = 358
88528 deg
ZDOT = 698
338420 TA = 280
78633
MA = 280
82263
Ha = 188
128 n
mi
Hp = 182
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2819242
62 X = 787692
90
Y = 13537733
29 feet Y = 4135509
67 meter
Z = 17159391
30 Z = 5234183
27
XDOT = -25064
506532 XDOT = -7650
334214
YDOT = 2302
598517 feet/sec YDOT = 616
340981 meter/sec
ZDOT = 2291
136549 ZDOT = 661
199040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11647592
10 X = 3550186
07
Y = 7416421
81 feet Y = 2260525
37 meter
Z = 17175370
37 Z = 5235052
89
XDOT = -15165
448654 XDOT = -4622
428750
YDOT = 18835
943229 feet/sec YDOT = 5741
195496 meter/sec
ZDOT = 2140
810182 ZDOT = 652
518944
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 11129
54869632
00016717 00000-0 10270-3 0 9127
2 25544 51
6461 359
1431 0002462 224
0922 136
0045 15
74953426 34828
Satellite: ISS
Catalog Number: 25544
Epoch time: 11129
54869632 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 359
1431 deg
Eccentricity:
0002462
Arg of perigee: 224
0922 deg
Mean anomaly: 136
0045 deg
Mean motion: 15
74953426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3482
Checksum: 299
Coasting Arc #14 (Orbit 3496)
---------------------------------------
Vector Time (GMT): 2011/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6652548
20 A = 6729216
50 meter
Y = -944852
31 meter E =
0009273
Z = -268950
45 I = 51
63007
XDOT = 906
887705 Wp = 40
63553
YDOT = 4703
677814 meter/sec RA = 353
73246 deg
ZDOT = 6030
507048 TA = 316
44043
MA = 316
51362
Ha = 187
928 n
mi
Hp = 182
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21825945
53 X = 6663925
79
Y = -3099909
14 feet Y = -870395
85 meter
Z = -882383
36 Z = -236604
77
XDOT = 2975
353362 XDOT = 824
927759
YDOT = 15432
013827 feet/sec YDOT = 4713
360678 meter/sec
ZDOT = 19785
128109 ZDOT = 6034
713817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12572778
34 X = 3832182
84
Y = -18114097
00 feet Y = -5521176
76 meter
Z = -751445
33 Z = -229040
54
XDOT = 11936
938576 XDOT = 3638
378878
YDOT = 7483
477441 feet/sec YDOT = 2280
963924 meter/sec
ZDOT = 19801
912675 ZDOT = 6035
622983
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 11130
50044186
00016717 00000-0 10270-3 0 9135
2 25544 51
6455 354
2480 0002555 231
5113 128
5822 15
75031352 34970
Satellite: ISS
Catalog Number: 25544
Epoch time: 11130
50044186 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 354
2480 deg
Eccentricity:
0002555
Arg of perigee: 231
5113 deg
Mean anomaly: 128
5822 deg
Mean motion: 15
75031352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3497
Checksum: 279
Coasting Arc #15 (Orbit 3512)
---------------------------------------
Vector Time (GMT): 2011/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -691249
38 A = 6716972
70 meter
Y = -4125376
14 meter E =
0012976
Z = -5266656
84 I = 51
55804
XDOT = 7559
134664 Wp = 97
24870
YDOT = -1426
038709 meter/sec RA = 348
58627 deg
ZDOT = 123
530814 TA = 173
93383
MA = 173
91810
Ha = 187
715 n
mi
Hp = 182
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2267878
55 X = -619482
74
Y = -13534698
61 feet Y = -4132704
71 meter
Z = -17279057
87 Z = -5269840
71
XDOT = 24800
310577 XDOT = 7573
918995
YDOT = -4678
604687 feet/sec YDOT = -1341
425214 meter/sec
ZDOT = 405
284824 ZDOT = 160
289041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11525136
10 X = -3512861
48
Y = -7420535
75 feet Y = -2261779
30 meter
Z = -17291734
08 Z = -5270520
55
XDOT = 12522
148916 XDOT = 3816
750990
YDOT = -20750
153683 feet/sec YDOT = -6324
646843 meter/sec
ZDOT = 554
097960 ZDOT = 168
889058
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 11131
51559578
00016717 00000-0 10270-3 0 9144
2 25544 51
6446 349
0261 0002594 237
6875 122
4038 15
75100892 35131
Satellite: ISS
Catalog Number: 25544
Epoch time: 11131
51559578 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 349
0261 deg
Eccentricity:
0002594
Arg of perigee: 237
6875 deg
Mean anomaly: 122
4038 deg
Mean motion: 15
75100892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3513
Checksum: 309
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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