[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 22nd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 26909 78 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
334/22:27:31
878 -2
8 3
3 3
3
N/A -1
6 0
0 226
3
000/00:01:03
756 0
8 -0
0 196
3
Coasting Arc #1 (Orbit 2495)
---------------------------------------
Vector Time (GMT): 2011/322/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2193631
82 A = 6777317
27 meter
Y = -6388268
87 meter E =
0035050
Z = -628325
09 I = 51
99547
XDOT = 4308
402215 Wp = 81
30125
YDOT = 2041
849747 meter/sec RA = 104
78313 deg
ZDOT = -5997
838075 TA = 105
44945
MA = 105
06205
Ha = 225
727 n
mi
Hp = 197
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7196954
80 X = 2267955
99
Y = -20958887
36 feet Y = -6363322
75 meter
Z = -2061434
04 Z = -617487
91
XDOT = 14135
177872 XDOT = 4314
386308
YDOT = 6698
982108 feet/sec YDOT = 2090
062503 meter/sec
ZDOT = -19677
946440 ZDOT = -5976
893100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21090904
53 X = -6428507
70
Y = 6813731
58 feet Y = 2076825
39 meter
Z = -2016788
52 Z = -614717
14
XDOT = -2701
285644 XDOT = -823
351864
YDOT = -13882
960294 feet/sec YDOT = -4231
526298 meter/sec
ZDOT = -19592
545453 ZDOT = -5971
807854
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 11322
22767867
00016717 00000-0 10270-3 0 9001
2 25544 51
6420 105
4864 0030741 63
9736 296
4579 15
58208875 24969
Satellite: ISS
Catalog Number: 25544
Epoch time: 11322
22767867 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 105
4864 deg
Eccentricity:
0030741
Arg of perigee: 63
9736 deg
Mean anomaly: 296
4579 deg
Mean motion: 15
58208875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2496
Checksum: 334
Coasting Arc #2 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2011/323/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3493910
01 A = 6772466
58 meter
Y = 4677157
57 meter E =
0042729
Z = 3385039
88 I = 51
98643
XDOT = -2758
248426 Wp = 73
62189
YDOT = -5465
637302 meter/sec RA = 99
80942 deg
ZDOT = 4668
369894 TA = 325
92130
MA = 326
19493
Ha = 225
776 n
mi
Hp = 197
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11462959
34 X = -3562395
32
Y = 15345005
16 feet Y = 4637703
60 meter
Z = 11105773
88 Z = 3367899
94
XDOT = -9049
371477 XDOT = -2719
603934
YDOT = -17931
880911 feet/sec YDOT = -5496
265666 meter/sec
ZDOT = 15316
174192 ZDOT = 4655
064030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19191746
53 X = 5849644
34
Y = -318887
37 feet Y = -97196
87 meter
Z = 11035488
64 Z = 3363616
94
XDOT = -8565
907769 XDOT = -2610
888688
YDOT = 16824
608589 feet/sec YDOT = 5128
140698 meter/sec
ZDOT = 15262
181016 ZDOT = 4651
912774
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 11323
25378148
00016717 00000-0 10270-3 0 9016
2 25544 51
6419 100
3393 0030888 67
3853 293
0564 15
58273748 25125
Satellite: ISS
Catalog Number: 25544
Epoch time: 11323
25378148 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 100
3393 deg
Eccentricity:
0030888
Arg of perigee: 67
3853 deg
Mean anomaly: 293
0564 deg
Mean motion: 15
58273748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 315
Coasting Arc #3 (Orbit 2526)
---------------------------------------
Vector Time (GMT): 2011/324/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4161157
23 A = 6766067
79 meter
Y = -1594623
48 meter E =
0044020
Z = -5130838
63 I = 51
96997
XDOT = 723
760084 Wp = 72
59109
YDOT = 7411
327318 meter/sec RA = 94
80431 deg
ZDOT = -1715
745966 TA = 180
84380
MA = 180
85125
Ha = 225
527 n
mi
Hp = 197
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13652090
64 X = 4203604
40
Y = -5231704
34 feet Y = -1547853
56 meter
Z = -16833460
06 Z = -5110520
32
XDOT = 2374
540959 XDOT = 649
166270
YDOT = 24315
378339 feet/sec YDOT = 7419
003761 meter/sec
ZDOT = -5629
087816 ZDOT = -1712
411117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12703358
70 X = -3871983
73
Y = -7427313
91 feet Y = -2263845
28 meter
Z = -16750384
25 Z = -5105517
12
XDOT = 16881
911514 XDOT = 5145
606629
YDOT = -16203
887923 feet/sec YDOT = -4938
945039 meter/sec
ZDOT = -5615
943909 ZDOT = -1711
739703
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 11324
21571738
00016717 00000-0 10270-3 0 9024
2 25544 51
6420 95
5127 0030712 70
6628 289
7843 15
58357310 25276
Satellite: ISS
Catalog Number: 25544
Epoch time: 11324
21571738 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 95
5127 deg
Eccentricity:
0030712
Arg of perigee: 70
6628 deg
Mean anomaly: 289
7843 deg
Mean motion: 15
58357310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2527
Checksum: 304
Coasting Arc #4 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2011/325/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3971582
68 A = 6765873
53 meter
Y = -2012614
06 meter E =
0035779
Z = 5068402
44 I = 51
97183
XDOT = 1387
803532 Wp = 71
25992
YDOT = -7351
987151 meter/sec RA = 89
78165 deg
ZDOT = -1810
320127 TA = 36
23187
MA = 35
99006
Ha = 225
515 n
mi
Hp = 196
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13030126
90 X = -3973403
90
Y = -6603064
51 feet Y = -2057036
91 meter
Z = 16628616
93 Z = 5049103
70
XDOT = 4553
161194 XDOT = 1478
706136
YDOT = -24120
692753 feet/sec YDOT = -7335
959619 meter/sec
ZDOT = -5939
370495 ZDOT = -1803
357233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3343116
67 X = 1018981
96
Y = 14311488
22 feet Y = 4362141
61 meter
Z = 16549937
90 Z = 5044421
07
XDOT = -20416
789209 XDOT = -6223
037351
YDOT = 11686
557022 feet/sec YDOT = 3562
062580 meter/sec
ZDOT = -5910
451750 ZDOT = -1801
505693
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 11325
24174600
00016717 00000-0 10270-3 0 9036
2 25544 51
6420 90
3642 0030603 74
2178 286
2348 15
58445471 25436
Satellite: ISS
Catalog Number: 25544
Epoch time: 11325
24174600 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 90
3642 deg
Eccentricity:
0030603
Arg of perigee: 74
2178 deg
Mean anomaly: 286
2348 deg
Mean motion: 15
58445471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 286
Coasting Arc #5 (Orbit 2557)
---------------------------------------
Vector Time (GMT): 2011/326/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3101694
32 A = 6772008
64 meter
Y = 5003711
05 meter E =
0035284
Z = -3369453
76 I = 51
99106
XDOT = -3217
311517 Wp = 78
83388
YDOT = 5124
429160 meter/sec RA = 84
77739 deg
ZDOT = 4696
398280 TA = 242
08284
MA = 242
44055
Ha = 225
399 n
mi
Hp = 196
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10176162
46 X = 3061879
88
Y = 16416374
85 feet Y = 5038173
54 meter
Z = -11054638
33 Z = -3354482
02
XDOT = -10555
483979 XDOT = -3297
189553
YDOT = 16812
431627 feet/sec YDOT = 5088
004514 meter/sec
ZDOT = 15408
130841 ZDOT = 4680
574274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5724798
52 X = 1744918
59
Y = -18482935
80 feet Y = -5633598
83 meter
Z = -10993836
47 Z = -3350921
36
XDOT = 18336
207347 XDOT = 5588
875999
YDOT = -3352
424218 feet/sec YDOT = -1021
818902 meter/sec
ZDOT = 15343
159656 ZDOT = 4676
595063
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 11326
20361594
00016717 00000-0 10270-3 0 9044
2 25544 51
6418 85
5379 0030583 77
5955 282
8620 15
58450346 25580
Satellite: ISS
Catalog Number: 25544
Epoch time: 11326
20361594 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 85
5379 deg
Eccentricity:
0030583
Arg of perigee: 77
5955 deg
Mean anomaly: 282
8620 deg
Mean motion: 15
58450346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2558
Checksum: 328
Coasting Arc #6 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2011/327/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1483590
54 A = 6776663
33 meter
Y = -6596954
06 meter E =
0040140
Z = 374207
23 I = 52
00331
XDOT = 4536
588848 Wp = 95
48303
YDOT = -1393
525991 meter/sec RA = 79
80343 deg
ZDOT = -6031
327734 TA = 80
49612
MA = 80
04268
Ha = 225
369 n
mi
Hp = 196
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4867423
04 X = -1411529
71
Y = -21643550
06 feet Y = -6613141
58 meter
Z = 1227714
02 Z = 367174
53
XDOT = 14883
821680 XDOT = 4581
134191
YDOT = -4571
935665 feet/sec YDOT = -1342
545749 meter/sec
ZDOT = -19787
820649 ZDOT = -6009
180288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12881231
19 X = -3926199
27
Y = 18063153
98 feet Y = 5505649
33 meter
Z = 1199457
91 Z = 365594
77
XDOT = -12093
878756 XDOT = -3686
214245
YDOT = -7193
910922 feet/sec YDOT = -2192
704049 meter/sec
ZDOT = -19697
273440 ZDOT = -6003
728944
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 11327
22957379
00016717 00000-0 10270-3 0 9050
2 25544 51
6421 80
3886 0030621 81
6650 278
7975 15
58476783 25749
Satellite: ISS
Catalog Number: 25544
Epoch time: 11327
22957379 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 80
3886 deg
Eccentricity:
0030621
Arg of perigee: 81
6650 deg
Mean anomaly: 278
7975 deg
Mean motion: 15
58476783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 343
Coasting Arc #7 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2011/328/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -445093
78 A = 6773523
71 meter
Y = 6207607
86 meter E =
0044040
Z = 2627300
08 I = 51
98697
XDOT = -4967
597288 Wp = 82
32791
YDOT = -2611
596840 meter/sec RA = 74
83371 deg
ZDOT = 5259
794978 TA = 307
25177
MA = 307
65267
Ha = 225
197 n
mi
Hp = 196
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1460281
43 X = -527238
66
Y = 20366167
52 feet Y = 6202171
06 meter
Z = 8619750
91 Z = 2624938
68
XDOT = -16297
891365 XDOT = -4963
576444
YDOT = -8568
231104 feet/sec YDOT = -2667
125464 meter/sec
ZDOT = 17256
545203 ZDOT = 5235
671373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15971335
75 X = 4868063
14
Y = -12728064
13 feet Y = -3879513
95 meter
Z = 8609653
02 Z = 2624222
24
XDOT = 3929
642054 XDOT = 1197
754898
YDOT = 16690
934872 feet/sec YDOT = 5087
396949 meter/sec
ZDOT = 17158
212523 ZDOT = 5229
823177
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 11328
25549194
00016717 00000-0 10270-3 0 9067
2 25544 51
6417 75
2400 0030490 84
9343 275
5291 15
58569108 25906
Satellite: ISS
Catalog Number: 25544
Epoch time: 11328
25549194 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 75
2400 deg
Eccentricity:
0030490
Arg of perigee: 84
9343 deg
Mean anomaly: 275
5291 deg
Mean motion: 15
58569108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 317
Coasting Arc #8 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2011/329/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2556568
63 A = 6766493
50 meter
Y = -4023934
63 meter E =
0041609
Z = -4839240
81 I = 51
95427
XDOT = 4273
370941 Wp = 83
71425
YDOT = 5793
041210 meter/sec RA = 69
83415 deg
ZDOT = -2573
976837 TA = 161
05268
MA = 160
89740
Ha = 225
094 n
mi
Hp = 196
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8387692
35 X = 2624883
69
Y = -13201885
25 feet Y = -3994963
05 meter
Z = -15876774
31 Z = -4826655
20
XDOT = 14020
245871 XDOT = 4220
778571
YDOT = 19006
040714 feet/sec YDOT = 5840
534860 meter/sec
ZDOT = -8444
805895 ZDOT = -2553
343536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15401812
39 X = -4694472
42
Y = 3011074
02 feet Y = 917775
36 meter
Z = -15825066
45 Z = -4823480
25
XDOT = 4204
053743 XDOT = 1281
395581
YDOT = -22186
315908 feet/sec YDOT = -6762
389089 meter/sec
ZDOT = -8360
969890 ZDOT = -2548
423623
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 11329
21725714
00016717 00000-0 10270-3 0 9079
2 25544 51
6411 70
4120 0030427 88
4585 272
0055 15
58611629 26056
Satellite: ISS
Catalog Number: 25544
Epoch time: 11329
21725714 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 70
4120 deg
Eccentricity:
0030427
Arg of perigee: 88
4585 deg
Mean anomaly: 272
0055 deg
Mean motion: 15
58611629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 289
Coasting Arc #9 (Orbit 2620)
---------------------------------------
Vector Time (GMT): 2011/330/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4183184
77 A = 6764444
48 meter
Y = 738920
03 meter E =
0033453
Z = 5235722
19 I = 51
93712
XDOT = -2527
692402 Wp = 88
31003
YDOT = -7206
421909 meter/sec RA = 64
80925 deg
ZDOT = -996
091512 TA = 11
18192
MA = 11
10776
Ha = 225
149 n
mi
Hp = 196
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13724359
48 X = -4216571
19
Y = 2424278
32 feet Y = 691953
82 meter
Z = 17177566
24 Z = 5215318
95
XDOT = -8292
954074 XDOT = -2442
081994
YDOT = -23643
116498 feet/sec YDOT = -7234
209325 meter/sec
ZDOT = -3268
016771 ZDOT = -1008
164111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11460317
18 X = 3493104
68
Y = 8108911
66 feet Y = 2471596
27 meter
Z = 17094169
53 Z = 5210302
87
XDOT = -10367
432681 XDOT = -3159
993481
YDOT = 21688
841577 feet/sec YDOT = 6610
758913 meter/sec
ZDOT = -3316
769486 ZDOT = -1010
951339
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 11330
24310380
00016717 00000-0 10270-3 0 9084
2 25544 51
6415 65
2632 0030410 92
1795 268
2843 15
58678488 26213
Satellite: ISS
Catalog Number: 25544
Epoch time: 11330
24310380 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 65
2632 deg
Eccentricity:
0030410
Arg of perigee: 92
1795 deg
Mean anomaly: 268
2843 deg
Mean motion: 15
58678488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2621
Checksum: 301
Coasting Arc #10 (Orbit 2635)
---------------------------------------
Vector Time (GMT): 2011/331/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4974698
41 A = 6769833
20 meter
Y = 2578610
23 meter E =
0036471
Z = -3833959
15 I = 51
94066
XDOT = -92
279216 Wp = 96
76407
YDOT = 6389
492384 meter/sec RA = 59
79277 deg
ZDOT = 4207
761644 TA = 217
41285
MA = 217
66732
Ha = 224
919 n
mi
Hp = 196
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16321189
01 X = 4964119
00
Y = 8460007
32 feet Y = 2634181
65 meter
Z = -12578606
14 Z = -3809817
24
XDOT = -302
753334 XDOT = -184
161659
YDOT = 20962
901522 feet/sec YDOT = 6387
946224 meter/sec
ZDOT = 13804
992269 ZDOT = 4207
090913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5844164
62 X = -1781301
38
Y = -17500422
24 feet Y = -5334128
70 meter
Z = -12480193
43 Z = -3803962
96
XDOT = 13627
169754 XDOT = 4153
561341
YDOT = -14322
244878 feet/sec YDOT = -4365
420239 meter/sec
ZDOT = 13801
746352 ZDOT = 4206
772288
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 11331
20480168
00016717 00000-0 10270-3 0 9094
2 25544 51
6404 60
4350 0030445 95
6732 264
7896 15
58732798 26362
Satellite: ISS
Catalog Number: 25544
Epoch time: 11331
20480168 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 60
4350 deg
Eccentricity:
0030445
Arg of perigee: 95
6732 deg
Mean anomaly: 264
7896 deg
Mean motion: 15
58732798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 320
Coasting Arc #11 (Orbit 2651)
---------------------------------------
Vector Time (GMT): 2011/332/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4424211
67 A = 6775419
72 meter
Y = -5031785
48 meter E =
0042869
Z = 914366
80 I = 51
94421
XDOT = 3034
163638 Wp = 106
76461
YDOT = -3789
846135 meter/sec RA = 54
80927 deg
ZDOT = -5957
327235 TA = 63
34745
MA = 62
90904
Ha = 224
747 n
mi
Hp = 196
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14515130
16 X = -4372058
28
Y = -16508482
56 feet Y = -5080968
22 meter
Z = 2999891
09 Z = 893000
02
XDOT = 9954
605113 XDOT = 3105
256685
YDOT = -12433
878395 feet/sec YDOT = -3755
518111 meter/sec
ZDOT = -19545
036859 ZDOT = -5942
414924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -729006
16 X = -222201
08
Y = 21981839
56 feet Y = 6700064
70 meter
Z = 2913009
77 Z = 887885
38
XDOT = -14254
165244 XDOT = -4344
669566
YDOT = 2206
560545 feet/sec YDOT = 672
559654 meter/sec
ZDOT = -19483
813964 ZDOT = -5938
666496
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
23057594
00016717 00000-0 10270-3 0 9103
2 25544 51
6407 55
2848 0030368 99
0743 261
3850 15
58814222 26527
Satellite: ISS
Catalog Number: 25544
Epoch time: 11332
23057594 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 55
2848 deg
Eccentricity:
0030368
Arg of perigee: 99
0743 deg
Mean anomaly: 261
3850 deg
Mean motion: 15
58814222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2652
Checksum: 304
Coasting Arc #12 (Orbit 2667)
---------------------------------------
Vector Time (GMT): 2011/333/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2633761
25 A = 6773516
31 meter
Y = 5819204
56 meter E =
0042897
Z = 2221345
40 I = 51
91863
XDOT = -5370
989728 Wp = 93
05426
YDOT = 301
171618 meter/sec RA = 49
83546 deg
ZDOT = 5486
055163 TA = 291
60983
MA = 292
06631
Ha = 224
674 n
mi
Hp = 196
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8640948
97 X = 2557703
09
Y = 19091878
46 feet Y = 5848231
42 meter
Z = 7287878
60 Z = 2233956
01
XDOT = -17621
357374 XDOT = -5400
608603
YDOT = 988
095859 feet/sec YDOT = 240
943812 meter/sec
ZDOT = 17998
868644 ZDOT = 5459
890936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6481460
48 X = 1975549
15
Y = -19910044
25 feet Y = -6068581
49 meter
Z = 7338923
96 Z = 2236904
02
XDOT = 12332
680612 XDOT = 3759
001050
YDOT = 10721
652011 feet/sec YDOT = 3267
959533 meter/sec
ZDOT = 17891
956714 ZDOT = 5453
468406
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
25631455
00016717 00000-0 10270-3 0 9111
2 25544 51
6394 50
1347 0030408 103
2955 257
1594 15
58850784 26686
Satellite: ISS
Catalog Number: 25544
Epoch time: 11333
25631455 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 50
1347 deg
Eccentricity:
0030408
Arg of perigee: 103
2955 deg
Mean anomaly: 257
1594 deg
Mean motion: 15
58850784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2668
Checksum: 311
Coasting Arc #13 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2011/334/04:43:10
294
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 251241
32 A = 6766277
66 meter
Y = -4919125
10 meter E =
0039594
Z = -4670585
66 I = 51
87417
XDOT = 6360
583767 Wp = 97
14109
YDOT = 3081
587594 meter/sec RA = 44
83296 deg
ZDOT = -2929
463476 TA = 143
86671
MA = 143
59853
Ha = 224
649 n
mi
Hp = 196
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 824282
55 X = 328918
15
Y = -16138861
87 feet Y = -4915880
92 meter
Z = -15323443
77 Z = -4669176
80
XDOT = 20868
056977 XDOT = 6339
882918
YDOT = 10110
195519 feet/sec YDOT = 3152
600005 meter/sec
ZDOT = -9611
100644 ZDOT = -2898
613807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11338486
44 X = -3455970
67
Y = 11522573
94 feet Y = 3512080
54 meter
Z = -15317285
93 Z = -4668708
75
XDOT = -8212
964067 XDOT = -2503
311448
YDOT = -20577
232791 feet/sec YDOT = -6271
940555 meter/sec
ZDOT = -9485
322136 ZDOT = -2891
126187
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
21791212
00016717 00000-0 10270-3 0 9127
2 25544 51
6390 45
3052 0030554 106
6190 253
8324 15
58892424 26839
Satellite: ISS
Catalog Number: 25544
Epoch time: 11334
21791212 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 45
3052 deg
Eccentricity:
0030554
Arg of perigee: 106
6190 deg
Mean anomaly: 253
8324 deg
Mean motion: 15
58892424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 290
Coasting Arc #14 (Orbit 2694)
---------------------------------------
Vector Time (GMT): 2011/334/22:28:03
756
Vector Time (MET): N/A
Weight (LBS) : 886570
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1174264
53 A = 6766026
65 meter
Y = 4275086
41 meter E =
0037449
Z = 5083621
93 I = 51
85475
XDOT = -6448
315706 Wp = 108
46015
YDOT = -3839
763046 meter/sec RA = 41
12753 deg
ZDOT = 1717
654734 TA = 324
93692
MA = 325
18288
Ha = 226
309 n
mi
Hp = 196
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3852573
91 X = -1246677
45
Y = 14025874
04 feet Y = 4261549
89 meter
Z = 16678549
65 Z = 5077741
70
XDOT = -21155
891424 XDOT = -6413
243522
YDOT = -12597
647790 feet/sec YDOT = -3911
676067 meter/sec
ZDOT = 5635
350176 ZDOT = 1686
413757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7269979
83 X = 2215889
85
Y = 12630412
16 feet Y = 3849749
63 meter
Z = 16654175
72 Z = 5076192
76
XDOT = -22897
865576 XDOT = -6979
269428
YDOT = 5822
160464 feet/sec YDOT = 1774
594509 meter/sec
ZDOT = 5508
037023 ZDOT = 1678
849685
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
98719203
00016717 00000-0 10270-3 0 9132
2 25544 51
6420 41
4460 0032560 106
4500 254
0237 15
58343227 26956
Satellite: ISS
Catalog Number: 25544
Epoch time: 11334
98719203 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 41
4460 deg
Eccentricity:
0032560
Arg of perigee: 106
4500 deg
Mean anomaly: 254
0237 deg
Mean motion: 15
58343227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2695
Checksum: 282
Coasting Arc #15 (Orbit 2709)
---------------------------------------
Vector Time (GMT): 2011/335/22:28:03
756
Vector Time (MET): N/A
Weight (LBS) : 886570
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4000215
58 A = 6766190
51 meter
Y = -2044989
82 meter E =
0045643
Z = -5100636
60 I = 51
83254
XDOT = 5062
927425 Wp = 107
56513
YDOT = 5434
327912 meter/sec RA = 36
09643 deg
ZDOT = 1791
694343 TA = 179
78966
MA = 179
78773
Ha = 226
186 n
mi
Hp = 196
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13124066
86 X = 4047563
79
Y = -6709284
17 feet Y = -1999991
99 meter
Z = -16734372
06 Z = -5081088
58
XDOT = 16610
654280 XDOT = 4993
079652
YDOT = 17829
159817 feet/sec YDOT = 5490
554055 meter/sec
ZDOT = 5878
262280 ZDOT = 1816
120685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4198830
30 X = 1279803
47
Y = -14223131
41 feet Y = -4335210
45 meter
Z = -16654344
49 Z = -5076244
20
XDOT = 23305
806135 XDOT = 7103
609710
YDOT = -119
894929 feet/sec YDOT = -36
543974 meter/sec
ZDOT = 5977
599223 ZDOT = 1821
972243
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 11335
94911304
00016717 00000-0 10270-3 0 9146
2 25544 51
6429 36
6195 0032530 109
6721 250
7949 15
58359728 27107
Satellite: ISS
Catalog Number: 25544
Epoch time: 11335
94911304 = yrday
fracday
Element set: 914
Inclination: 51
6429 deg
RA of node: 36
6195 deg
Eccentricity:
0032530
Arg of perigee: 109
6721 deg
Mean anomaly: 250
7949 deg
Mean motion: 15
58359728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2710
Checksum: 317
Coasting Arc #16 (Orbit 2725)
---------------------------------------
Vector Time (GMT): 2011/336/22:28:03
756
Vector Time (MET): N/A
Weight (LBS) : 886570
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5864295
77 A = 6772386
70 meter
Y = -507394
80 meter E =
0044726
Z = 3298440
13 I = 51
82827
XDOT = -2193
440821 Wp = 107
05662
YDOT = -5665
267484 meter/sec RA = 31
08204 deg
ZDOT = -4731
446824 TA = 34
49455
MA = 34
20510
Ha = 226
228 n
mi
Hp = 196
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19239815
51 X = -5874209
44
Y = -1664681
09 feet Y = -573028
50 meter
Z = 10821653
96 Z = 3269927
12
XDOT = -7196
328152 XDOT = -2106
943017
YDOT = -18586
835579 feet/sec YDOT = -5689
312078 meter/sec
ZDOT = -15523
119502 ZDOT = -4741
892719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14237998
11 X = -4339741
82
Y = 13142586
61 feet Y = 4005860
40 meter
Z = 10705217
66 Z = 3262950
34
XDOT = -17561
477844 XDOT = -5352
738447
YDOT = -6239
168745 feet/sec YDOT = -1901
698633 meter/sec
ZDOT = -15565
318336 ZDOT = -4744
309029
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
97512873
00016717 00000-0 10270-3 0 9159
2 25544 51
6426 31
4712 0032627 113
4129 247
0462 15
58399970 27263
Satellite: ISS
Catalog Number: 25544
Epoch time: 11336
97512873 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 31
4712 deg
Eccentricity:
0032627
Arg of perigee: 113
4129 deg
Mean anomaly: 247
0462 deg
Mean motion: 15
58399970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2726
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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