[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 25th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 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
278/21:06:37
059 -8
0 10
1 10
1
N/A -0
2 -0
0 211
4
000/00:03:14
118 -6
2 -0
1 207
1
Coasting Arc #1 (Orbit 1625)
---------------------------------------
Vector Time (GMT): 2011/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6333987
11 A = 6766499
77 meter
Y = 1201752
83 meter E =
0004453
Z = -2056531
57 I = 51
80334
XDOT = 817
796197 Wp = 236
76246
YDOT = 5225
267292 meter/sec RA = 25
27926 deg
ZDOT = 5561
134387 TA = 100
48829
MA = 100
43811
Ha = 210
267 n
mi
Hp = 204
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20780797
61 X = 6330068
31
Y = 3942758
62 feet Y = 1272561
28 meter
Z = -6747150
82 Z = -2025770
87
XDOT = 2683
058388 XDOT = 732
290636
YDOT = 17143
265395 feet/sec YDOT = 5233
934728 meter/sec
ZDOT = 18245
191558 ZDOT = 5564
899123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20898938
35 X = -6369996
41
Y = -3506501
56 feet Y = -1068781
68 meter
Z = -6621915
28 Z = -2018359
78
XDOT = -3186
378651 XDOT = -971
208213
YDOT = -15562
655377 feet/sec YDOT = -4743
497359 meter/sec
ZDOT = 18260
217736 ZDOT = 5565
714366
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 11266
50398417
00016717 00000-0 10270-3 0 9000
2 25544 51
6396 25
8223 0011026 226
9477 133
0757 15
61410014 16265
Satellite: ISS
Catalog Number: 25544
Epoch time: 11266
50398417 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 25
8223 deg
Eccentricity:
0011026
Arg of perigee: 226
9477 deg
Mean anomaly: 133
0757 deg
Mean motion: 15
61410014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1626
Checksum: 289
Coasting Arc #2 (Orbit 1641)
---------------------------------------
Vector Time (GMT): 2011/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5323336
02 A = 6766317
62 meter
Y = -3649288
40 meter E =
0012747
Z = -2002843
85 I = 51
77578
XDOT = 4245
742865 Wp = 198
93531
YDOT = -3125
712893 meter/sec RA = 20
28460 deg
ZDOT = -5591
355691 TA = 3
22919
MA = 3
22097
Ha = 209
927 n
mi
Hp = 204
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17465013
20 X = -5272403
92
Y = -11972730
98 feet Y = -3708532
63 meter
Z = -6571010
00 Z = -2028580
38
XDOT = 13929
602577 XDOT = 4307
541288
YDOT = -10254
963559 feet/sec YDOT = -3077
889425 meter/sec
ZDOT = -18344
342817 ZDOT = -5570
579572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17868488
14 X = 5446315
18
Y = 11300629
42 feet Y = 3444431
85 meter
Z = -6675631
19 Z = -2034732
39
XDOT = -12815
068695 XDOT = -3906
032938
YDOT = 9480
190759 feet/sec YDOT = 2889
562143 meter/sec
ZDOT = -18259
526916 ZDOT = -5565
503804
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 11267
52799373
00016717 00000-0 10270-3 0 9010
2 25544 51
6399 20
6608 0011008 230
8065 129
2115 15
61464226 16422
Satellite: ISS
Catalog Number: 25544
Epoch time: 11267
52799373 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 20
6608 deg
Eccentricity:
0011008
Arg of perigee: 230
8065 deg
Mean anomaly: 129
2115 deg
Mean motion: 15
61464226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1642
Checksum: 296
Coasting Arc #3 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2011/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1518198
84 A = 6757623
05 meter
Y = 4415331
31 meter E =
0010332
Z = 4891574
29 I = 51
71934
XDOT = -7310
530554 Wp = 198
33511
YDOT = -82
830194 meter/sec RA = 15
25152 deg
ZDOT = 2335
481116 TA = 228
81206
MA = 228
90121
Ha = 209
593 n
mi
Hp = 205
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4980967
32 X = 1444950
58
Y = 14485995
12 feet Y = 4431899
79 meter
Z = 16048472
09 Z = 4898771
22
XDOT = -23984
680294 XDOT = -7320
406307
YDOT = -271
752606 feet/sec YDOT = -164
635957 meter/sec
ZDOT = 7662
339621 ZDOT = 2299
942687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5677376
68 X = -1730464
41
Y = -14194649
82 feet Y = -4326529
26 meter
Z = 16077526
46 Z = 4900430
06
XDOT = 22973
621661 XDOT = 7002
359882
YDOT = -643
272519 feet/sec YDOT = -196
069464 meter/sec
ZDOT = 7517
586987 ZDOT = 2291
360514
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 11268
55197395
00016717 00000-0 10270-3 0 9021
2 25544 51
6408 15
4991 0010961 235
2249 124
7877 15
61533637 16585
Satellite: ISS
Catalog Number: 25544
Epoch time: 11268
55197395 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 15
4991 deg
Eccentricity:
0010961
Arg of perigee: 235
2249 deg
Mean anomaly: 124
7877 deg
Mean motion: 15
61533637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 330
Coasting Arc #4 (Orbit 1672)
---------------------------------------
Vector Time (GMT): 2011/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3233703
92 A = 6757578
98 meter
Y = -3352997
95 meter E =
0009370
Z = -4900729
59 I = 51
68997
XDOT = 6659
244564 Wp = 165
31489
YDOT = 3044
499243 meter/sec RA = 10
18033 deg
ZDOT = 2303
141637 TA = 127
20973
MA = 127
12419
Ha = 209
326 n
mi
Hp = 205
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10609264
83 X = 3294764
38
Y = -11000649
45 feet Y = -3316495
94 meter
Z = -16078509
14 Z = -4884871
46
XDOT = 21847
915236 XDOT = 6613
517170
YDOT = 9988
514576 feet/sec YDOT = 3118
711625 meter/sec
ZDOT = 7556
238966 ZDOT = 2335
380836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9880947
96 X = -3011712
94
Y = 11748057
75 feet Y = 3580808
00 meter
Z = -16013720
72 Z = -4880982
07
XDOT = -21611
593375 XDOT = -6587
213661
YDOT = -7662
758795 feet/sec YDOT = -2335
608881 meter/sec
ZDOT = 7687
369145 ZDOT = 2343
110115
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 11269
51193181
00016717 00000-0 10270-3 0 9038
2 25544 51
6410 10
6608 0010784 239
0308 120
9790 15
61575230 16735
Satellite: ISS
Catalog Number: 25544
Epoch time: 11269
51193181 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 10
6608 deg
Eccentricity:
0010784
Arg of perigee: 239
0308 deg
Mean anomaly: 120
9790 deg
Mean motion: 15
61575230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 287
Coasting Arc #5 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2011/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6375435
29 A = 6766130
30 meter
Y = 1014182
48 meter E =
0010743
Z = 2001903
51 I = 51
68835
XDOT = -2492
836456 Wp = 160
98764
YDOT = -4653
289222 meter/sec RA = 5
14359 deg
ZDOT = -5583
041462 TA = 356
83475
MA = 356
84154
Ha = 209
118 n
mi
Hp = 205
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20916782
44 X = -6396027
20
Y = 3327370
36 feet Y = 942773
58 meter
Z = 6567924
90 Z = 1970881
25
XDOT = -8178
597295 XDOT = -2413
495556
YDOT = -15266
696921 feet/sec YDOT = -4680
722746 meter/sec
ZDOT = -18317
065163 ZDOT = -5594
958437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20573630
73 X = 6270842
65
Y = -5191662
54 feet Y = -1582418
74 meter
Z = 6441519
81 Z = 1963375
24
XDOT = 9024
736169 XDOT = 2750
739584
YDOT = 12983
148428 feet/sec YDOT = 3957
263641 meter/sec
ZDOT = -18365
322203 ZDOT = -5597
750208
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 11270
53585929
00016717 00000-0 10270-3 0 9048
2 25544 51
6408 5
4994 0010733 242
9640 117
0421 15
61571523 16894
Satellite: ISS
Catalog Number: 25544
Epoch time: 11270
53585929 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 5
4994 deg
Eccentricity:
0010733
Arg of perigee: 242
9640 deg
Mean anomaly: 117
0421 deg
Mean motion: 15
61571523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 306
Coasting Arc #6 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2011/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6204997
14 A = 6765625
81 meter
Y = 1680127
90 meter E =
0003367
Z = 2105066
43 I = 51
65766
XDOT = -3058
709820 Wp = 78
64506
YDOT = 4363
668787 meter/sec RA =
13956 deg
ZDOT = 5526
379388 TA = 304
73193
MA = 304
76363
Ha = 208
628 n
mi
Hp = 205
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20357602
17 X = 6175522
28
Y = 5512230
65 feet Y = 1749351
41 meter
Z = 6906385
91 Z = 2135138
91
XDOT = -10035
137204 XDOT = -3134
124392
YDOT = 14316
498644 feet/sec YDOT = 4329
043364 meter/sec
ZDOT = 18131
165971 ZDOT = 5511
336319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20787817
63 X = -6336126
81
Y = -3313319
83 feet Y = -1009899
88 meter
Z = 7028753
04 Z = 2142363
93
XDOT = 8317
024259 XDOT = 2535
028994
YDOT = -13802
194517 feet/sec YDOT = -4206
908889 meter/sec
ZDOT = 18069
640365 ZDOT = 5507
626383
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 11271
55975668
00016717 00000-0 10270-3 0 9055
2 25544 51
6413
3367 0010648 247
7447 112
2580 15
61637467 17053
Satellite: ISS
Catalog Number: 25544
Epoch time: 11271
55975668 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node:
3367 deg
Eccentricity:
0010648
Arg of perigee: 247
7447 deg
Mean anomaly: 112
2580 deg
Mean motion: 15
61637467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 312
Coasting Arc #7 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2011/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2735711
35 A = 6756978
07 meter
Y = -3701958
33 meter E =
0002019
Z = -4948288
70 I = 51
59777
XDOT = 7002
742863 Wp = 88
23359
YDOT = -2307
863927 meter/sec RA = 355
09586 deg
ZDOT = -2145
650758 TA = 160
88194
MA = 160
87436
Ha = 208
252 n
mi
Hp = 205
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8975430
94 X = -2670073
74
Y = -12145532
59 feet Y = -3732184
15 meter
Z = -16234542
98 Z = -4961419
24
XDOT = 22974
878158 XDOT = 7038
452728
YDOT = -7571
732045 feet/sec YDOT = -2229
355483 meter/sec
ZDOT = -7039
536609 ZDOT = -2111
543987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10312708
72 X = 3143313
62
Y = 10953937
67 feet Y = 3338760
20 meter
Z = -16287786
73 Z = -4964517
40
XDOT = -21103
730032 XDOT = -6432
416914
YDOT = 9611
122246 feet/sec YDOT = 2929
470061 meter/sec
ZDOT = -6900
503691 ZDOT = -2103
273525
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 11272
51963595
00016717 00000-0 10270-3 0 9069
2 25544 51
6406 355
4980 0010699 251
9283 108
0708 15
61656745 17203
Satellite: ISS
Catalog Number: 25544
Epoch time: 11272
51963595 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 355
4980 deg
Eccentricity:
0010699
Arg of perigee: 251
9283 deg
Mean anomaly: 108
0708 deg
Mean motion: 15
61656745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 326
Coasting Arc #8 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2011/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2145248
52 A = 6757461
48 meter
Y = 4246749
73 meter E =
0004038
Z = 4802366
93 I = 51
57007
XDOT = -7205
164202 Wp = 285
77823
YDOT = -773
706244 meter/sec RA = 350
01371 deg
ZDOT = -2535
096741 TA = 189
14904
MA = 189
15640
Ha = 207
777 n
mi
Hp = 205
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7038216
93 X = -2215906
44
Y = 13932905
95 feet Y = 4222365
45 meter
Z = 15755797
01 Z = 4791773
29
XDOT = -23638
990165 XDOT = -7183
661736
YDOT = -2538
406311 feet/sec YDOT = -854
158718 meter/sec
ZDOT = -8317
246525 ZDOT = -2570
047658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5099538
99 X = 1554339
48
Y = -14799421
94 feet Y = -4510863
81 meter
Z = 15712393
75 Z = 4789137
62
XDOT = 22631
657569 XDOT = 6898
129227
YDOT = -1180
617644 feet/sec YDOT = -359
852258 meter/sec
ZDOT = -8459
523376 ZDOT = -2578
462725
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 11273
54347838
00016717 00000-0 10270-3 0 9070
2 25544 51
6408 350
3351 0010604 256
6980 103
2994 15
61745580 17360
Satellite: ISS
Catalog Number: 25544
Epoch time: 11273
54347838 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 350
3351 deg
Eccentricity:
0010604
Arg of perigee: 256
6980 deg
Mean anomaly: 103
2994 deg
Mean motion: 15
61745580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1736
Checksum: 314
Coasting Arc #9 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2011/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5820026
83 A = 6766117
39 meter
Y = -2979608
84 meter E =
0007225
Z = -1724573
37 I = 51
56833
XDOT = 3587
963932 Wp = 307
89425
YDOT = 3709
514267 meter/sec RA = 344
97029 deg
ZDOT = 5687
588878 TA = 33
10541
MA = 33
06022
Ha = 207
308 n
mi
Hp = 205
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19094576
21 X = 5861290
60
Y = -9775619
55 feet Y = -2914295
08 meter
Z = -5658049
11 Z = -1696199
01
XDOT = 11771
535209 XDOT = 3518
587146
YDOT = 12170
322397 feet/sec YDOT = 3749
249388 meter/sec
ZDOT = 18660
068496 ZDOT = 5704
850746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17345390
26 X = -5286874
95
Y = 12672775
71 feet Y = 3862662
04 meter
Z = -5542318
14 Z = -1689298
57
XDOT = -12509
760577 XDOT = -3812
975024
YDOT = -8913
430425 feet/sec YDOT = -2716
813594 meter/sec
ZDOT = 18730
127261 ZDOT = 5708
942789
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 11274
50330648
00016717 00000-0 10270-3 0 9089
2 25544 51
6400 345
4952 0010529 261
1998 98
7966 15
61723902 17518
Satellite: ISS
Catalog Number: 25544
Epoch time: 11274
50330648 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 345
4952 deg
Eccentricity:
0010529
Arg of perigee: 261
1998 deg
Mean anomaly: 98
7966 deg
Mean motion: 15
61723902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 321
Coasting Arc #10 (Orbit 1766)
---------------------------------------
Vector Time (GMT): 2011/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6309271
21 A = 6764566
15 meter
Y = 261573
20 meter E =
0007788
Z = -2412472
16 I = 51
53425
XDOT = 1834
048909 Wp = 233
19348
YDOT = -5195
596910 meter/sec RA = 339
95702 deg
ZDOT = -5352
507802 TA = 333
92303
MA = 333
96224
Ha = 206
705 n
mi
Hp = 205
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20699708
69 X = -6300007
80
Y = 858179
79 feet Y = 191070
79 meter
Z = -7914934
91 Z = -2443100
34
XDOT = 6017
220829 XDOT = 1918
012499
YDOT = -17045
921620 feet/sec YDOT = -5174
618153 meter/sec
ZDOT = -17560
721134 ZDOT = -5343
393813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20183638
08 X = 6151972
89
Y = -4454774
37 feet Y = -1357815
23 meter
Z = -8039673
26 Z = -2450492
41
XDOT = -3373
560595 XDOT = -1028
261269
YDOT = 16382
858303 feet/sec YDOT = 4993
495211 meter/sec
ZDOT = -17523
279846 ZDOT = -5341
095697
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 11275
52709548
00016717 00000-0 10270-3 0 9092
2 25544 51
6393 340
3322 0010353 264
6425 95
3551 15
61794313 17676
Satellite: ISS
Catalog Number: 25544
Epoch time: 11275
52709548 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 340
3322 deg
Eccentricity:
0010353
Arg of perigee: 264
6425 deg
Mean anomaly: 95
3551 deg
Mean motion: 15
61794313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1767
Checksum: 312
Coasting Arc #11 (Orbit 1782)
---------------------------------------
Vector Time (GMT): 2011/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3454794
57 A = 6755878
01 meter
Y = 2838876
16 meter E =
0006964
Z = 5070455
75 I = 51
47791
XDOT = -6086
727734 Wp = 242
65068
YDOT = 4353
490307 meter/sec RA = 334
89716 deg
ZDOT = 1708
443983 TA = 190
81379
MA = 190
82877
Ha = 206
388 n
mi
Hp = 205
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11334627
86 X = 3398161
48
Y = 9313898
18 feet Y = 2877193
31 meter
Z = 16635353
53 Z = 5087101
55
XDOT = -19969
579181 XDOT = -6143
256280
YDOT = 14283
104683 feet/sec YDOT = 4285
108782 meter/sec
ZDOT = 5605
131178 ZDOT = 1678
737092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12811543
31 X = -3904958
40
Y = -6988059
65 feet Y = -2129960
58 meter
Z = 16702959
47 Z = 5091062
05
XDOT = 16383
884399 XDOT = 4993
807965
YDOT = -16919
243529 feet/sec YDOT = -5156
985428 meter/sec
ZDOT = 5483
886535 ZDOT = 1671
488616
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 11276
55085439
00016717 00000-0 10270-3 0 9104
2 25544 51
6397 335
1686 0010390 269
0314 90
9652 15
61853490 17835
Satellite: ISS
Catalog Number: 25544
Epoch time: 11276
55085439 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 335
1686 deg
Eccentricity:
0010390
Arg of perigee: 269
0314 deg
Mean anomaly: 90
9652 deg
Mean motion: 15
61853490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1783
Checksum: 323
Coasting Arc #12 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2011/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1082769
29 A = 6757896
57 meter
Y = -4851033
85 meter E =
0002940
Z = -4579568
22 I = 51
45732
XDOT = 6952
585748 Wp = 192
17248
YDOT = -1281
827001 meter/sec RA = 329
80601 deg
ZDOT = 2998
471185 TA = 107
79172
MA = 107
75964
Ha = 206
422 n
mi
Hp = 205
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3552392
70 X = 1159180
77
Y = -15915465
38 feet Y = -4838498
62 meter
Z = -15024830
12 Z = -4574122
31
XDOT = 22810
320696 XDOT = 6951
836611
YDOT = -4205
469163 feet/sec YDOT = -1204
082986 meter/sec
ZDOT = 9837
503888 ZDOT = 3032
245106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -243047
78 X = -74080
96
Y = 16325973
52 feet Y = 4976156
73 meter
Z = -15002352
11 Z = -4572716
92
XDOT = -20182
603559 XDOT = -6151
657565
YDOT = 8875
505329 feet/sec YDOT = 2705
254024 meter/sec
ZDOT = 9975
116564 ZDOT = 3040
415529
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 11277
51060415
00016717 00000-0 10270-3 0 9119
2 25544 51
6392 330
3278 0010184 273
5334 86
4658 15
61892891 17987
Satellite: ISS
Catalog Number: 25544
Epoch time: 11277
51060415 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 330
3278 deg
Eccentricity:
0010184
Arg of perigee: 273
5334 deg
Mean anomaly: 86
4658 deg
Mean motion: 15
61892891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1798
Checksum: 320
Coasting Arc #13 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2011/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4808151
13 A = 6766065
14 meter
Y = 4593502
47 meter E =
0006069
Z = 1227010
48 I = 51
46017
XDOT = -4141
033086 Wp = 164
13190
YDOT = -2773
410470 meter/sec RA = 324
76009 deg
ZDOT = -5843
223502 TA = 2
45378
MA = 2
45080
Ha = 206
863 n
mi
Hp = 205
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15774774
05 X = -4865119
81
Y = 15070546
17 feet Y = 4539416
33 meter
Z = 4025624
94 Z = 1203513
86
XDOT = -13586
066556 XDOT = -4081
327198
YDOT = -9099
115716 feet/sec YDOT = -2819
384554 meter/sec
ZDOT = -19170
680782 ZDOT = -5863
195425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11995808
91 X = 3656322
56
Y = -18243597
08 feet Y = -5560648
39 meter
Z = 3929662
66 Z = 1197761
18
XDOT = 13844
178078 XDOT = 4219
705478
YDOT = 4955
402289 feet/sec YDOT = 1510
406618 meter/sec
ZDOT = -19251
839774 ZDOT = -5867
960763
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 11278
53430839
00016717 00000-0 10270-3 0 9124
2 25544 51
6397 325
1642 0010178 278
2320 81
7682 15
61952879 18146
Satellite: ISS
Catalog Number: 25544
Epoch time: 11278
53430839 = yrday
fracday
Element set: 912
Inclination: 51
6397 deg
RA of node: 325
1642 deg
Eccentricity:
0010178
Arg of perigee: 278
2320 deg
Mean anomaly: 81
7682 deg
Mean motion: 15
61952879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 324
Coasting Arc #14 (Orbit 1819)
---------------------------------------
Vector Time (GMT): 2011/278/21:08:14
118
Vector Time (MET): N/A
Weight (LBS) : 870493
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3290003
13 A = 6769036
11 meter
Y = 5234595
82 meter E =
0010938
Z = 2738477
84 I = 51
44222
XDOT = -5646
100838 Wp = 131
15286
YDOT = -857
622361 meter/sec RA = 322
82394 deg
ZDOT = -5137
587065 TA = 17
65614
MA = 17
61816
Ha = 211
389 n
mi
Hp = 207
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10793973
53 X = -3361595
90
Y = 17173870
79 feet Y = 5197404
87 meter
Z = 8984507
33 Z = 2722320
78
XDOT = -18523
952879 XDOT = -5611
133665
YDOT = -2813
721658 feet/sec YDOT = -920
565348 meter/sec
ZDOT = -16855
600608 ZDOT = -5164
930790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17905537
32 X = -5457607
78
Y = 9593071
22 feet Y = 2923968
11 meter
Z = 8918396
29 Z = 2718327
19
XDOT = -13939
856611 XDOT = -4248
868295
YDOT = -10225
904200 feet/sec YDOT = -3116
855600 meter/sec
ZDOT = -16966
895498 ZDOT = -5171
509748
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 11278
91824874
00016717 00000-0 10270-3 0 9133
2 25544 51
6398 323
2289 0006860 227
9666 132
0907 15
60042018 18201
Satellite: ISS
Catalog Number: 25544
Epoch time: 11278
91824874 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 323
2289 deg
Eccentricity:
0006860
Arg of perigee: 227
9666 deg
Mean anomaly: 132
0907 deg
Mean motion: 15
60042018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1820
Checksum: 318
Coasting Arc #15 (Orbit 1835)
---------------------------------------
Vector Time (GMT): 2011/279/21:08:14
118
Vector Time (MET): N/A
Weight (LBS) : 870493
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5389034
58 A = 6771767
01 meter
Y = -4014878
19 meter E =
0006668
Z = 808389
05 I = 51
42870
XDOT = 2304
728629 Wp = 54
91754
YDOT = 4293
823497 meter/sec RA = 317
80873 deg
ZDOT = 5930
252401 TA = 313
86928
MA = 313
92435
Ha = 211
078 n
mi
Hp = 207
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17680559
64 X = 5429602
20
Y = -13172172
53 feet Y = -3954387
81 meter
Z = 2652195
05 Z = 834667
83
XDOT = 7561
445634 XDOT = 2227
734884
YDOT = 14087
347431 feet/sec YDOT = 4319
166388 meter/sec
ZDOT = 19456
208664 ZDOT = 5941
261382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21811834
46 X = 6648247
14
Y = -3125990
23 feet Y = -952801
82 meter
Z = 2759441
83 Z = 841077
87
XDOT = -423
910133 XDOT = -129
207809
YDOT = 14342
251087 feet/sec YDOT = 4371
518131 meter/sec
ZDOT = 19500
782324 ZDOT = 5943
838452
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 11279
94315432
00016717 00000-0 10270-3 0 9143
2 25544 51
6400 318
0729 0006775 233
0162 127
0374 15
60085190 18367
Satellite: ISS
Catalog Number: 25544
Epoch time: 11279
94315432 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 318
0729 deg
Eccentricity:
0006775
Arg of perigee: 233
0162 deg
Mean anomaly: 127
0374 deg
Mean motion: 15
60085190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1836
Checksum: 294
Coasting Arc #16 (Orbit 1850)
---------------------------------------
Vector Time (GMT): 2011/280/21:08:14
118
Vector Time (MET): N/A
Weight (LBS) : 870493
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5351279
21 A = 6764979
29 meter
Y = 1087107
31 meter E =
0001824
Z = -3993172
12 I = 51
38536
XDOT = 1633
622029 Wp = 144
31103
YDOT = -6387
847716 meter/sec RA = 312
77919 deg
ZDOT = -3930
628661 TA = 84
75388
MA = 84
73306
Ha = 210
679 n
mi
Hp = 207
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17556690
31 X = -5343639
60
Y = 3566625
03 feet Y = 1027308
34 meter
Z = -13100958
38 Z = -4019150
21
XDOT = 5359
652325 XDOT = 1724
025095
YDOT = -20957
505629 feet/sec YDOT = -6369
074474 meter/sec
ZDOT = -12895
763325 ZDOT = -3922
472289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17143169
12 X = -5225237
95
Y = -4928024
81 feet Y = -1502061
96 meter
Z = -13206802
16 Z = -4025433
30
XDOT = 14160
654903 XDOT = 4316
167614
YDOT = -14811
569533 feet/sec YDOT = -4514
566394 meter/sec
ZDOT = -12862
179359 ZDOT = -3920
392269
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 11280
90397876
00016717 00000-0 10270-3 0 9154
2 25544 51
6405 313
2398 0006805 237
0802 122
9700 15
60142239 18512
Satellite: ISS
Catalog Number: 25544
Epoch time: 11280
90397876 = yrday
fracday
Element set: 915
Inclination: 51
6405 deg
RA of node: 313
2398 deg
Eccentricity:
0006805
Arg of perigee: 237
0802 deg
Mean anomaly: 122
9700 deg
Mean motion: 15
60142239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1851
Checksum: 300
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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