[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 30th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 32291 73 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
334/23:11:31
342 2
9 3
3 3
3
N/A 1
1 -0
3 224
6
000/00:01:02
684 -1
0 -0
0 197
9
341/20:07:18
799 1
5 2
0 2
0
N/A 0
8 -0
2 223
6
000/00:00:37
599 1
0 -0
0 199
5
Coasting Arc #1 (Orbit 2609)
---------------------------------------
Vector Time (GMT): 2011/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2062910
80 A = 6764549
49 meter
Y = 3912199
92 meter E =
0035000
Z = 5091496
82 I = 51
90602
XDOT = -5483
880268 Wp = 104
43771
YDOT = -5129
616855 meter/sec RA = 53
31929 deg
ZDOT = 1701
351051 TA = 329
15312
MA = 329
35831
Ha = 224
736 n
mi
Hp = 196
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6768080
06 X = -2131238
13
Y = 12835301
59 feet Y = 3888748
63 meter
Z = 16704385
89 Z = 5081309
60
XDOT = -17991
733164 XDOT = -5434
377182
YDOT = -16829
451623 feet/sec YDOT = -5190
664355 meter/sec
ZDOT = 5581
860402 ZDOT = 1674
829983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8982255
69 X = -2737791
53
Y = -11457315
87 feet Y = -3492189
88 meter
Z = 16662454
15 Z = 5078716
02
XDOT = 21828
380617 XDOT = 6653
290412
YDOT = -9064
856447 feet/sec YDOT = -2762
968245 meter/sec
ZDOT = 5473
931089 ZDOT = 1668
454196
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 11332
55100281
00016717 00000-0 10270-3 0 9009
2 25544 51
6435 53
6813 0030275 101
5186 258
9372 15
58847892 26103
Satellite: ISS
Catalog Number: 25544
Epoch time: 11332
55100281 = yrday
fracday
Element set: 900
Inclination: 51
6435 deg
RA of node: 53
6813 deg
Eccentricity:
0030275
Arg of perigee: 101
5186 deg
Mean anomaly: 258
9372 deg
Mean motion: 15
58847892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2610
Checksum: 296
Coasting Arc #2 (Orbit 2624)
---------------------------------------
Vector Time (GMT): 2011/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4447952
55 A = 6764899
55 meter
Y = -958006
44 meter E =
0043115
Z = -5045374
53 I = 51
88764
XDOT = 3634
882234 Wp = 104
36658
YDOT = 6422
634209 meter/sec RA = 48
28801 deg
ZDOT = 1988
783762 TA = 184
92409
MA = 184
96663
Ha = 224
585 n
mi
Hp = 196
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14593020
17 X = 4482844
12
Y = -3143065
75 feet Y = -908071
19 meter
Z = -16553066
05 Z = -5023681
69
XDOT = 11925
466648 XDOT = 3553
131751
YDOT = 21071
634544 feet/sec YDOT = 6462
824431 meter/sec
ZDOT = 6524
881109 ZDOT = 2006
244011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2786782
26 X = -849411
23
Y = 14764740
61 feet Y = 4500292
94 meter
Z = -16464366
83 Z = -5018339
01
XDOT = -22953
142862 XDOT = -6996
117944
YDOT = 3008
564898 feet/sec YDOT = 917
010581 meter/sec
ZDOT = 6595
688625 ZDOT = 2010
365893
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 11333
51260990
00016717 00000-0 10270-3 0 9011
2 25544 51
6428 48
8539 0030320 104
5792 255
8729 15
58885813 26256
Satellite: ISS
Catalog Number: 25544
Epoch time: 11333
51260990 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 48
8539 deg
Eccentricity:
0030320
Arg of perigee: 104
5792 deg
Mean anomaly: 255
8729 deg
Mean motion: 15
58885813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2625
Checksum: 321
Coasting Arc #3 (Orbit 2640)
---------------------------------------
Vector Time (GMT): 2011/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5666748
15 A = 6771524
82 meter
Y = -2090754
67 meter E =
0043318
Z = 3011744
39 I = 51
88966
XDOT = -514
373324 Wp = 104
36066
YDOT = -5848
061119 meter/sec RA = 43
27548 deg
ZDOT = -4978
595526 TA = 41
08943
MA = 40
76399
Ha = 224
515 n
mi
Hp = 196
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18591693
41 X = -5657578
27
Y = -6859431
32 feet Y = -2154072
64 meter
Z = 9881051
13 Z = 2984237
44
XDOT = -1687
576522 XDOT = -424
755786
YDOT = -19186
552228 feet/sec YDOT = -5853
311755 meter/sec
ZDOT = -16333
974823 ZDOT = -4980
877052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13289904
82 X = 4050762
99
Y = -14774507
47 feet Y = -4503269
88 meter
Z = 9768848
05 Z = 2977544
89
XDOT = 17329
805701 XDOT = 5282
124778
YDOT = 4675
220307 feet/sec YDOT = 1425
007149 meter/sec
ZDOT = -16342
816264 ZDOT = -4981
290397
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 11334
53828018
00016717 00000-0 10270-3 0 9026
2 25544 51
6429 43
7029 0030289 108
1226 252
3232 15
58963584 26412
Satellite: ISS
Catalog Number: 25544
Epoch time: 11334
53828018 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 43
7029 deg
Eccentricity:
0030289
Arg of perigee: 108
1226 deg
Mean anomaly: 252
3232 deg
Mean motion: 15
58963584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2641
Checksum: 302
Coasting Arc #4 (Orbit 2647)
---------------------------------------
Vector Time (GMT): 2011/334/23:12:02
684
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 464864
43 A = 6766863
43 meter
Y = -4684044
08 meter E =
0038440
Z = -4891253
48 I = 51
85879
XDOT = 6534
572534 Wp = 100
82821
YDOT = 3155
481871 meter/sec RA = 40
98221 deg
ZDOT = -2423
926920 TA = 145
54141
MA = 145
29158
Ha = 224
645 n
mi
Hp = 197
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1525145
78 X = 540968
64
Y = -15367598
70 feet Y = -4678419
88 meter
Z = -16047419
57 Z = -4888810
58
XDOT = 21438
886265 XDOT = 6510
576652
YDOT = 10352
630809 feet/sec YDOT = 3228
421438 meter/sec
ZDOT = -7952
516143 ZDOT = -2392
240043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11952817
89 X = -3643218
89
Y = -9795502
22 feet Y = -2985669
08 meter
Z = -16037054
43 Z = -4888094
19
XDOT = 19736
874476 XDOT = 6015
799340
YDOT = -11399
914624 feet/sec YDOT = -3474
693977 meter/sec
ZDOT = -7823
325180 ZDOT = -2384
549515
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 11334
98700123
00016717 00000-0 10270-3 0 9032
2 25544 51
6434 41
4500 0028482 112
7535 247
6634 15
58385642 26486
Satellite: ISS
Catalog Number: 25544
Epoch time: 11334
98700123 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 41
4500 deg
Eccentricity:
0028482
Arg of perigee: 112
7535 deg
Mean anomaly: 247
6634 deg
Mean motion: 15
58385642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2648
Checksum: 302
Coasting Arc #5 (Orbit 2663)
---------------------------------------
Vector Time (GMT): 2011/335/23:12:02
684
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3357853
67 A = 6765068
93 meter
Y = 2635667
45 meter E =
0030355
Z = 5222152
72 I = 51
82983
XDOT = -5650
854892 Wp = 109
86119
YDOT = -5121
663666 meter/sec RA = 35
95253 deg
ZDOT = -1053
716385 TA = 350
13473
MA = 350
19420
Ha = 224
515 n
mi
Hp = 197
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11016580
27 X = -3412445
00
Y = 8647202
93 feet Y = 2597812
41 meter
Z = 17133046
98 Z = 5205707
73
XDOT = -18539
550170 XDOT = -5588
044669
YDOT = -16803
358485 feet/sec YDOT = -5184
503756 meter/sec
ZDOT = -3457
074754 ZDOT = -1081
015967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1362035
47 X = 415148
41
Y = 14021020
22 feet Y = 4273606
96 meter
Z = 17065647
06 Z = 5201609
22
XDOT = -23079
099069 XDOT = -7034
509396
YDOT = 6564
282606 feet/sec YDOT = 2000
793338 meter/sec
ZDOT = -3568
175273 ZDOT = -1087
579823
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 11336
01300610
00016717 00000-0 10270-3 0 9046
2 25544 51
6432 36
3022 0028281 116
5334 243
8726 15
58479789 26646
Satellite: ISS
Catalog Number: 25544
Epoch time: 11336
01300610 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 36
3022 deg
Eccentricity:
0028281
Arg of perigee: 116
5334 deg
Mean anomaly: 243
8726 deg
Mean motion: 15
58479789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2664
Checksum: 296
Coasting Arc #6 (Orbit 2678)
---------------------------------------
Vector Time (GMT): 2011/336/23:12:02
684
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5604956
58 A = 6770538
70 meter
Y = -155625
05 meter E =
0034152
Z = -3833980
53 I = 51
82359
XDOT = 3012
647559 Wp = 116
58670
YDOT = 5645
023288 meter/sec RA = 30
93123 deg
ZDOT = 4189
078239 TA = 197
52281
MA = 197
64093
Ha = 224
337 n
mi
Hp = 198
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18388965
14 X = 5624905
12
Y = -510580
88 feet Y = -92835
31 meter
Z = -12578676
28 Z = -3806703
05
XDOT = 9884
014302 XDOT = 2928
949985
YDOT = 18520
417612 feet/sec YDOT = 5678
244431 meter/sec
ZDOT = 13743
695010 ZDOT = 4203
510664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9166710
39 X = 2794013
33
Y = -16036750
86 feet Y = -4888001
66 meter
Z = -12467231
90 Z = -3800012
28
XDOT = 19746
991722 XDOT = 6018
883077
YDOT = 593
438984 feet/sec YDOT = 180
880202 meter/sec
ZDOT = 13802
180751 ZDOT = 4206
904693
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 11336
97485017
00016717 00000-0 10270-3 0 9057
2 25544 51
6437 31
4757 0028301 119
8343 240
5630 15
58497146 26792
Satellite: ISS
Catalog Number: 25544
Epoch time: 11336
97485017 = yrday
fracday
Element set: 905
Inclination: 51
6437 deg
RA of node: 31
4757 deg
Eccentricity:
0028301
Arg of perigee: 119
8343 deg
Mean anomaly: 240
5630 deg
Mean motion: 15
58497146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2679
Checksum: 323
Coasting Arc #7 (Orbit 2694)
---------------------------------------
Vector Time (GMT): 2011/337/23:12:02
684
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6312580
25 A = 6776225
88 meter
Y = -2183796
76 meter E =
0042023
Z = 1014095
15 I = 51
81634
XDOT = 699
462554 Wp = 123
55367
YDOT = -4847
466376 meter/sec RA = 25
94018 deg
ZDOT = -5931
712107 TA = 45
43767
MA = 45
09533
Ha = 224
318 n
mi
Hp = 198
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20710565
14 X = -6292617
77
Y = -7164687
55 feet Y = -2254276
33 meter
Z = 3327083
84 Z = 983476
78
XDOT = 2294
824651 XDOT = 782
431329
YDOT = -15903
761077 feet/sec YDOT = -4839
180430 meter/sec
ZDOT = -19460
997726 ZDOT = -5928
112738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16658026
86 X = -5077366
59
Y = 14268350
97 feet Y = 4348993
37 meter
Z = 3202193
73 Z = 976028
65
XDOT = -11465
195521 XDOT = -3494
591595
YDOT = -8904
186162 feet/sec YDOT = -2713
995942 meter/sec
ZDOT = -19445
884448 ZDOT = -5927
105580
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 11338
00077705
00016717 00000-0 10270-3 0 9065
2 25544 51
6439 26
3267 0028446 123
8452 236
5416 15
58513376 26958
Satellite: ISS
Catalog Number: 25544
Epoch time: 11338
00077705 = yrday
fracday
Element set: 906
Inclination: 51
6439 deg
RA of node: 26
3267 deg
Eccentricity:
0028446
Arg of perigee: 123
8452 deg
Mean anomaly: 236
5416 deg
Mean motion: 15
58513376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2695
Checksum: 317
Coasting Arc #8 (Orbit 2710)
---------------------------------------
Vector Time (GMT): 2011/338/23:12:02
684
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5244432
34 A = 6774451
79 meter
Y = 3752763
25 meter E =
0037582
Z = 2068232
57 I = 51
78377
XDOT = -4371
803523 Wp = 108
38011
YDOT = 3001
321558 meter/sec RA = 20
95944 deg
ZDOT = 5545
675549 TA = 274
49342
MA = 274
92265
Ha = 223
992 n
mi
Hp = 198
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17206142
84 X = 5192031
20
Y = 12312215
40 feet Y = 3811116
63 meter
Z = 6785539
92 Z = 2093583
20
XDOT = -14343
187411 XDOT = -4431
980165
YDOT = 9846
855505 feet/sec YDOT = 2952
096650 meter/sec
ZDOT = 18194
473585 ZDOT = 5524
291051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19148097
84 X = 5836340
22
Y = -8920803
38 feet Y = -2719060
87 meter
Z = 6888771
12 Z = 2099697
44
XDOT = 843
988673 XDOT = 257
247748
YDOT = 16028
805747 feet/sec YDOT = 4885
579992 meter/sec
ZDOT = 18106
864952 ZDOT = 5518
972437
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 11339
02666039
00016717 00000-0 10270-3 0 9073
2 25544 51
6438 21
1783 0028156 127
2410 233
1320 15
58614380 27116
Satellite: ISS
Catalog Number: 25544
Epoch time: 11339
02666039 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 21
1783 deg
Eccentricity:
0028156
Arg of perigee: 127
2410 deg
Mean anomaly: 233
1320 deg
Mean motion: 15
58614380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2711
Checksum: 283
Coasting Arc #9 (Orbit 2725)
---------------------------------------
Vector Time (GMT): 2011/339/23:12:02
684
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2423884
49 A = 6767342
73 meter
Y = -4415768
05 meter E =
0033930
Z = -4537708
56 I = 51
73163
XDOT = 6952
885690 Wp = 115
60979
YDOT = -604
210014 meter/sec RA = 15
95143 deg
ZDOT = -3158
690672 TA = 122
87341
MA = 122
54641
Ha = 223
787 n
mi
Hp = 198
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7952376
94 X = -2352282
68
Y = -14487427
97 feet Y = -4442472
80 meter
Z = -14887495
29 Z = -4549310
29
XDOT = 22811
304758 XDOT = 6974
469881
YDOT = -1982
316319 feet/sec YDOT = -526
337712 meter/sec
ZDOT = -10363
158373 ZDOT = -3124
860704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16484026
63 X = -5024331
32
Y = 30251
32 feet Y = 9220
60 meter
Z = -14934501
50 Z = -4552036
06
XDOT = 9130
483287 XDOT = 2782
971306
YDOT = -19864
664378 feet/sec YDOT = -6054
749702 meter/sec
ZDOT = -10224
921427 ZDOT = -3116
556051
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 11339
98838948
00016717 00000-0 10270-3 0 9089
2 25544 51
6435 16
3503 0028021 130
9595 229
3992 15
58671708 27260
Satellite: ISS
Catalog Number: 25544
Epoch time: 11339
98838948 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 16
3503 deg
Eccentricity:
0028021
Arg of perigee: 130
9595 deg
Mean anomaly: 229
3992 deg
Mean motion: 15
58671708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2726
Checksum: 343
Coasting Arc #10 (Orbit 2741)
---------------------------------------
Vector Time (GMT): 2011/340/23:12:02
684
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1137388
60 A = 6763947
05 meter
Y = 4034947
11 meter E =
0029406
Z = 5287781
11 I = 51
69154
XDOT = -7495
750876 Wp = 129
64722
YDOT = -1707
766752 meter/sec RA = 10
91280 deg
ZDOT = -326
367152 TA = 323
35094
MA = 323
55172
Ha = 223
682 n
mi
Hp = 198
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3731589
91 X = -1208111
10
Y = 13238015
46 feet Y = 4021832
31 meter
Z = 17348363
22 Z = 5282084
11
XDOT = -24592
358518 XDOT = -7474
511727
YDOT = -5602
909292 feet/sec YDOT = -1791
470058 meter/sec
ZDOT = -1070
758374 ZDOT = -362
730576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9988885
33 X = 3044612
25
Y = 9497953
61 feet Y = 2894976
26 meter
Z = 17324738
67 Z = 5280580
35
XDOT = -15594
736016 XDOT = -4753
275538
YDOT = 18521
522279 feet/sec YDOT = 5645
359991 meter/sec
ZDOT = -1219
137463 ZDOT = -371
593099
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 11341
01419532
00016717 00000-0 10270-3 0 9091
2 25544 51
6436 11
2018 0028066 134
6545 225
6905 15
58749368 27420
Satellite: ISS
Catalog Number: 25544
Epoch time: 11341
01419532 = yrday
fracday
Element set: 909
Inclination: 51
6436 deg
RA of node: 11
2018 deg
Eccentricity:
0028066
Arg of perigee: 134
6545 deg
Mean anomaly: 225
6905 deg
Mean motion: 15
58749368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2742
Checksum: 305
Coasting Arc #11 (Orbit 2754)
---------------------------------------
Vector Time (GMT): 2011/341/20:07:37
599
Vector Time (MET): N/A
Weight (LBS) : 871530
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4645705
78 A = 6769762
65 meter
Y = -2748676
53 meter E =
0033261
Z = -4122750
82 I = 51
68159
XDOT = 5538
063923 Wp = 131
26953
YDOT = 3656
254520 meter/sec RA = 6
51581 deg
ZDOT = 3801
455232 TA = 178
04893
MA = 178
03592
Ha = 223
563 n
mi
Hp = 199
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15241816
87 X = 4696124
61
Y = -9017967
61 feet Y = -2696443
11 meter
Z = -13526085
36 Z = -4100059
44
XDOT = 18169
501061 XDOT = 5478
300311
YDOT = 11995
585695 feet/sec YDOT = 3717
850046 meter/sec
ZDOT = 12471
965983 ZDOT = 3828
214695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11934685
04 X = 3637692
00
Y = -13179729
81 feet Y = -4017181
65 meter
Z = -13433157
55 Z = -4094426
42
XDOT = 19887
724145 XDOT = 6061
778319
YDOT = 5181
322929 feet/sec YDOT = 1579
267229 meter/sec
ZDOT = 12580
940767 ZDOT = 3834
670746
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 11341
84763459
00016717 00000-0 10270-3 0 9104
2 25544 51
6436 7
0169 0026631 137
9099 222
4108 15
58428341 27555
Satellite: ISS
Catalog Number: 25544
Epoch time: 11341
84763459 = yrday
fracday
Element set: 910
Inclination: 51
6436 deg
RA of node: 7
0169 deg
Eccentricity:
0026631
Arg of perigee: 137
9099 deg
Mean anomaly: 222
4108 deg
Mean motion: 15
58428341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2755
Checksum: 313
Coasting Arc #12 (Orbit 2770)
---------------------------------------
Vector Time (GMT): 2011/342/20:07:37
599
Vector Time (MET): N/A
Weight (LBS) : 871530
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6509931
79 A = 6775923
87 meter
Y = 1003833
30 meter E =
0039914
Z = 1486531
17 I = 51
67201
XDOT = -2053
085242 Wp = 133
46666
YDOT = -4634
252264 meter/sec RA = 1
51124 deg
ZDOT = -5791
559380 TA = 30
23572
MA = 30
00599
Ha = 223
503 n
mi
Hp = 199
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21358043
93 X = -6527894
41
Y = 3293416
35 feet Y = 930934
66 meter
Z = 4877070
76 Z = 1454862
00
XDOT = -6735
843970 XDOT = -1972
976823
YDOT = -15204
239710 feet/sec YDOT = -4656
762580 meter/sec
ZDOT = -19001
179068 ZDOT = -5801
339314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19263696
16 X = -5871574
59
Y = 9857408
12 feet Y = 3004538
00 meter
Z = 4747627
44 Z = 1447076
84
XDOT = -10351
054066 XDOT = -3155
001279
YDOT = -10944
144887 feet/sec YDOT = -3335
775362 meter/sec
ZDOT = -19040
709092 ZDOT = -5803
608131
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 11342
87360901
00016717 00000-0 10270-3 0 9114
2 25544 51
6434 1
8685 0026733 141
8208 218
4847 15
58449183 27717
Satellite: ISS
Catalog Number: 25544
Epoch time: 11342
87360901 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 1
8685 deg
Eccentricity:
0026733
Arg of perigee: 141
8208 deg
Mean anomaly: 218
4847 deg
Mean motion: 15
58449183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2771
Checksum: 315
Coasting Arc #13 (Orbit 2786)
---------------------------------------
Vector Time (GMT): 2011/343/20:07:37
599
Vector Time (MET): N/A
Weight (LBS) : 871530
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6530328
62 A = 6775412
57 meter
Y = 871320
58 meter E =
0031715
Z = 1599556
27 I = 51
64108
XDOT = -2049
868283 Wp = 118
92518
YDOT = 4665
064726 meter/sec RA = 356
52159 deg
ZDOT = 5726
517590 TA = 258
58567
MA = 258
94208
Ha = 223
199 n
mi
Hp = 199
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21424962
65 X = 6512329
56
Y = 2858663
30 feet Y = 944245
88 meter
Z = 5247888
04 Z = 1631237
31
XDOT = -6725
289643 XDOT = -2129
700260
YDOT = 15305
330466 feet/sec YDOT = 4641
694767 meter/sec
ZDOT = 18787
787370 ZDOT = 5716
365898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21133218
65 X = 6441405
04
Y = -4383374
46 feet Y = -1336052
54 meter
Z = 5377211
87 Z = 1638974
18
XDOT = -1706
400234 XDOT = -520
110791
YDOT = 15166
177597 feet/sec YDOT = 4622
650932 meter/sec
ZDOT = 18745
900116 ZDOT = 5713
750355
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 11343
89954255
00016717 00000-0 10270-3 0 9129
2 25544 51
6435 356
7202 0026514 145
4402 214
8483 15
58533375 27878
Satellite: ISS
Catalog Number: 25544
Epoch time: 11343
89954255 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 356
7202 deg
Eccentricity:
0026514
Arg of perigee: 145
4402 deg
Mean anomaly: 214
8483 deg
Mean motion: 15
58533375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2787
Checksum: 321
Coasting Arc #14 (Orbit 2801)
---------------------------------------
Vector Time (GMT): 2011/344/20:07:37
599
Vector Time (MET): N/A
Weight (LBS) : 871530
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4545516
23 A = 6768649
91 meter
Y = -2709352
58 meter E =
0029084
Z = -4226007
06 I = 51
58934
XDOT = 5601
085632 Wp = 132
50557
YDOT = -3761
042986 meter/sec RA = 351
50965 deg
ZDOT = -3648
492062 TA = 100
28089
MA = 99
95284
Ha = 222
910 n
mi
Hp = 199
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14913111
00 X = -4494352
59
Y = -8888952
05 feet Y = -2759896
70 meter
Z = -13864852
57 Z = -4247965
39
XDOT = 18376
265196 XDOT = 5660
449883
YDOT = -12339
379874 feet/sec YDOT = -3698
075805 meter/sec
ZDOT = -11970
118315 ZDOT = -3621
138134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16992965
15 X = -5179455
78
Y = -3188289
98 feet Y = -971790
79 meter
Z = -13954297
81 Z = -4253269
97
XDOT = 12783
917986 XDOT = 3896
538202
YDOT = -16738
364656 feet/sec YDOT = -5101
853547 meter/sec
ZDOT = -11858
046428 ZDOT = -3614
332551
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 11344
86131939
00016717 00000-0 10270-3 0 9134
2 25544 51
6438 351
8926 0026410 149
2280 211
0430 15
58598032 28021
Satellite: ISS
Catalog Number: 25544
Epoch time: 11344
86131939 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 351
8926 deg
Eccentricity:
0026410
Arg of perigee: 149
2280 deg
Mean anomaly: 211
0430 deg
Mean motion: 15
58598032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2802
Checksum: 299
Coasting Arc #15 (Orbit 2817)
---------------------------------------
Vector Time (GMT): 2011/345/20:07:37
599
Vector Time (MET): N/A
Weight (LBS) : 871530
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1331449
29 A = 6764157
37 meter
Y = 3994314
42 meter E =
0028123
Z = 5282349
59 I = 51
54504
XDOT = -7406
894681 Wp = 148
44063
YDOT = 2032
728984 meter/sec RA = 346
46455 deg
ZDOT = 305
620362 TA = 298
50772
MA = 298
79064
Ha = 222
736 n
mi
Hp = 199
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4368271
96 X = 1261024
39
Y = 13104706
11 feet Y = 4008809
04 meter
Z = 17330543
29 Z = 5288647
25
XDOT = -24300
835567 XDOT = -7430
559209
YDOT = 6669
058348 feet/sec YDOT = 1949
768189 meter/sec
ZDOT = 1002
691477 ZDOT = 269
580403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8733003
09 X = 2661819
34
Y = 10661617
06 feet Y = 3249660
88 meter
Z = 17355904
80 Z = 5290079
78
XDOT = -19445
795405 XDOT = -5927
078439
YDOT = 14406
478739 feet/sec YDOT = 4391
094720 meter/sec
ZDOT = 855
294558 ZDOT = 260
693781
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 11345
88717738
00016717 00000-0 10270-3 0 9145
2 25544 51
6438 346
7440 0026457 152
9729 207
2810 15
58673986 28183
Satellite: ISS
Catalog Number: 25544
Epoch time: 11345
88717738 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 346
7440 deg
Eccentricity:
0026457
Arg of perigee: 152
9729 deg
Mean anomaly: 207
2810 deg
Mean motion: 15
58673986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2818
Checksum: 352
Coasting Arc #16 (Orbit 2832)
---------------------------------------
Vector Time (GMT): 2011/346/20:07:37
599
Vector Time (MET): N/A
Weight (LBS) : 871530
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2306832
81 A = 6767540
04 meter
Y = -4539691
38 meter E =
0033573
Z = -4489376
87 I = 51
52718
XDOT = 6940
819947 Wp = 144
48184
YDOT = 348
294628 meter/sec RA = 341
41176 deg
ZDOT = 3199
619019 TA = 157
87905
MA = 157
73384
Ha = 222
568 n
mi
Hp = 200
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7568349
13 X = 2379233
62
Y = -14894000
60 feet Y = -4513489
60 meter
Z = -14728926
74 Z = -4477995
00
XDOT = 22771
718985 XDOT = 6920
866258
YDOT = 1142
698910 feet/sec YDOT = 425
799174 meter/sec
ZDOT = 10497
437728 ZDOT = 3233
289015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1436544
61 X = 437858
80
Y = -16686130
35 feet Y = -5085932
53 meter
Z = -14682024
34 Z = -4475081
02
XDOT = 20228
283925 XDOT = 6165
580940
YDOT = -7658
611959 feet/sec YDOT = -2334
344925 meter/sec
ZDOT = 10634
940798 ZDOT = 3241
529955
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 11346
84888401
00016717 00000-0 10270-3 0 9159
2 25544 51
6437 341
9157 0026337 156
5914 203
6446 15
58719170 28335
Satellite: ISS
Catalog Number: 25544
Epoch time: 11346
84888401 = yrday
fracday
Element set: 915
Inclination: 51
6437 deg
RA of node: 341
9157 deg
Eccentricity:
0026337
Arg of perigee: 156
5914 deg
Mean anomaly: 203
6446 deg
Mean motion: 15
58719170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2833
Checksum: 328
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list