[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 22nd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 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
There are no maneuvers
Coasting Arc #1 (Orbit 1563)
---------------------------------------
Vector Time (GMT): 2011/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5494868
21 A = 6767143
16 meter
Y = -3433292
03 meter E =
0016949
Z = 1912697
36 I = 51
90057
XDOT = 1206
912195 Wp = 155
00952
YDOT = -5077
915721 meter/sec RA = 45
38112 deg
ZDOT = -5644
468985 TA = 3
90397
MA = 3
89076
Ha = 211
474 n
mi
Hp = 203
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18027782
84 X = -5465359
64
Y = -11264081
46 feet Y = -3494573
93 meter
Z = 6275253
80 Z = 1886075
03
XDOT = 3959
685679 XDOT = 1291
024652
YDOT = -16659
828480 feet/sec YDOT = -5063
949242 meter/sec
ZDOT = -18518
599032 ZDOT = -5638
401250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17505100
97 X = 5335554
78
Y = 12116056
69 feet Y = 3692974
08 meter
Z = 6167001
35 Z = 1879702
01
XDOT = -3980
991677 XDOT = -1213
406263
YDOT = 15170
122733 feet/sec YDOT = 4623
853409 meter/sec
ZDOT = -18493
591400 ZDOT = -5636
846659
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 11262
53570691
00016717 00000-0 10270-3 0 9005
2 25544 51
6381 45
8190 0011439 210
5566 149
4926 15
61269149 15641
Satellite: ISS
Catalog Number: 25544
Epoch time: 11262
53570691 = yrday
fracday
Element set: 900
Inclination: 51
6381 deg
RA of node: 45
8190 deg
Eccentricity:
0011439
Arg of perigee: 210
5566 deg
Mean anomaly: 149
4926 deg
Mean motion: 15
61269149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 310
Coasting Arc #2 (Orbit 1579)
---------------------------------------
Vector Time (GMT): 2011/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3668815
48 A = 6766523
28 meter
Y = 5285072
76 meter E =
0008202
Z = 2099661
54 I = 51
87873
XDOT = -5129
363804 Wp = 124
74724
YDOT = 1349
547627 meter/sec RA = 40
39400 deg
ZDOT = 5545
888112 TA = 258
47926
MA = 258
57136
Ha = 211
125 n
mi
Hp = 203
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12036796
20 X = 3599244
30
Y = 17339477
54 feet Y = 5325710
79 meter
Z = 6888653
33 Z = 2117315
45
XDOT = -16828
621405 XDOT = -5171
014423
YDOT = 4427
649696 feet/sec YDOT = 1291
955288 meter/sec
ZDOT = 18195
170972 ZDOT = 5520
868424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11456988
38 X = -3492090
06
Y = -17699934
15 feet Y = -5394939
93 meter
Z = 6960261
30 Z = 2121487
64
XDOT = 15775
298322 XDOT = 4808
310929
YDOT = -3070
908611 feet/sec YDOT = -936
012945 meter/sec
ZDOT = 18093
171418 ZDOT = 5514
798648
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 11263
55981007
00016717 00000-0 10270-3 0 9016
2 25544 51
6395 40
6581 0011458 214
2740 145
7678 15
61340053 15804
Satellite: ISS
Catalog Number: 25544
Epoch time: 11263
55981007 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 40
6581 deg
Eccentricity:
0011458
Arg of perigee: 214
2740 deg
Mean anomaly: 145
7678 deg
Mean motion: 15
61340053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 294
Coasting Arc #3 (Orbit 1594)
---------------------------------------
Vector Time (GMT): 2011/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 166353
95 A = 6758063
65 meter
Y = -4628733
31 meter E =
0007211
Z = -4923586
37 I = 51
82679
XDOT = 6834
499964 Wp = 137
30811
YDOT = 2658
057335 meter/sec RA = 35
36895 deg
ZDOT = -2275
077170 TA = 110
58777
MA = 110
51040
Ha = 210
876 n
mi
Hp = 204
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 545780
66 X = 242018
82
Y = -15186132
91 feet Y = -4626450
19 meter
Z = -16153498
58 Z = -4922594
23
XDOT = 22422
900145 XDOT = 6815
320975
YDOT = 8720
660547 feet/sec YDOT = 2734
377558 meter/sec
ZDOT = -7464
163944 ZDOT = -2241
921958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -848222
89 X = -258538
34
Y = 15176837
26 feet Y = 4625900
00 meter
Z = -16149184
32 Z = -4922271
38
XDOT = -21240
953526 XDOT = -6474
242635
YDOT = -8961
113148 feet/sec YDOT = -2731
347288 meter/sec
ZDOT = -7329
257466 ZDOT = -2233
957676
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 11264
51989029
00016717 00000-0 10270-3 0 9026
2 25544 51
6397 35
8204 0011244 218
5882 141
4472 15
61343935 15954
Satellite: ISS
Catalog Number: 25544
Epoch time: 11264
51989029 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 35
8204 deg
Eccentricity:
0011244
Arg of perigee: 218
5882 deg
Mean anomaly: 141
4472 deg
Mean motion: 15
61343935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 314
Coasting Arc #4 (Orbit 1610)
---------------------------------------
Vector Time (GMT): 2011/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4168435
13 A = 6758222
31 meter
Y = 2040713
87 meter E =
0005080
Z = 4912282
00 I = 51
80200
XDOT = -5219
340395 Wp = 199
04855
YDOT = -5144
402885 meter/sec RA = 30
30610 deg
ZDOT = -2297
211394 TA = 273
29385
MA = 273
35197
Ha = 210
753 n
mi
Hp = 204
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13675968
28 X = -4214807
84
Y = 6695255
49 feet Y = 1993840
88 meter
Z = 16116410
76 Z = 4891919
09
XDOT = -17123
820193 XDOT = -5150
267376
YDOT = -16877
962222 feet/sec YDOT = -5202
382665 meter/sec
ZDOT = -7536
782788 ZDOT = -2322
398750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13748053
66 X = 4190406
75
Y = -6746875
67 feet Y = -2056447
70 meter
Z = 16033338
39 Z = 4886961
54
XDOT = 16648
332376 XDOT = 5074
411708
YDOT = 15812
579109 feet/sec YDOT = 4819
674112 meter/sec
ZDOT = -7639
082607 ZDOT = -2328
392379
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 11265
54395631
00016717 00000-0 10270-3 0 9031
2 25544 51
6400 30
6589 0011140 221
9366 138
0938 15
61338495 16111
Satellite: ISS
Catalog Number: 25544
Epoch time: 11265
54395631 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 30
6589 deg
Eccentricity:
0011140
Arg of perigee: 221
9366 deg
Mean anomaly: 138
0938 deg
Mean motion: 15
61338495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1611
Checksum: 296
Coasting Arc #5 (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 = 6333250
89 A = 6766537
89 meter
Y = 1196124
04 meter E =
0004523
Z = -2062372
78 I = 51
80436
XDOT = 826
544089 Wp = 235
84443
YDOT = 5226
698700 meter/sec RA = 25
27707 deg
ZDOT = 5558
382107 TA = 101
33873
MA = 101
28791
Ha = 210
322 n
mi
Hp = 204
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20778382
19 X = 6329423
47
Y = 3924291
47 feet Y = 1266924
77 meter
Z = -6766314
91 Z = -2031615
44
XDOT = 2711
758822 XDOT = 741
035242
YDOT = 17147
961615 feet/sec YDOT = 5235
463941 meter/sec
ZDOT = 18236
161768 ZDOT = 5562
189332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20896253
11 X = -6369177
95
Y = -3488085
58 feet Y = -1063168
49 meter
Z = -6641092
70 Z = -2024205
05
XDOT = -3213
881941 XDOT = -979
591216
YDOT = -15566
945105 feet/sec YDOT = -4744
804868 meter/sec
ZDOT = 18251
360940 ZDOT = 5563
014814
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
50399630
00016717 00000-0 10270-3 0 9042
2 25544 51
6408 25
8199 0011091 226
6937 133
3296 15
61393314 16265
Satellite: ISS
Catalog Number: 25544
Epoch time: 11266
50399630 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 25
8199 deg
Eccentricity:
0011091
Arg of perigee: 226
6937 deg
Mean anomaly: 133
3296 deg
Mean motion: 15
61393314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1626
Checksum: 311
Coasting Arc #6 (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 = -5333075
71 A = 6766417
77 meter
Y = -3641990
91 meter E =
0012876
Z = -1990220
70 I = 51
77692
XDOT = 4230
019084 Wp = 198
76695
YDOT = -3136
443549 meter/sec RA = 20
28263 deg
ZDOT = -5597
318621 TA = 3
25011
MA = 3
24175
Ha = 210
004 n
mi
Hp = 204
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17496967
56 X = -5282285
81
Y = -11948789
06 feet Y = -3701344
84 meter
Z = -6529595
46 Z = -2016004
89
XDOT = 13878
015369 XDOT = 4291
967634
YDOT = -10290
169123 feet/sec YDOT = -3088
795075 meter/sec
ZDOT = -18363
906237 ZDOT = -5576
618522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17899756
23 X = 5455845
70
Y = 11275476
26 feet Y = 3436765
16 meter
Z = -6634411
23 Z = -2022168
54
XDOT = -12764
130902 XDOT = -3890
507099
YDOT = 9511
131159 feet/sec YDOT = 2898
992777 meter/sec
ZDOT = -18279
399366 ZDOT = -5571
560927
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
52802040
00016717 00000-0 10270-3 0 9050
2 25544 51
6410 20
6587 0011083 230
4948 129
5230 15
61437112 16426
Satellite: ISS
Catalog Number: 25544
Epoch time: 11267
52802040 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 20
6587 deg
Eccentricity:
0011083
Arg of perigee: 230
4948 deg
Mean anomaly: 129
5230 deg
Mean motion: 15
61437112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1642
Checksum: 270
Coasting Arc #7 (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 = 1548201
90 A = 6757770
94 meter
Y = 4415586
80 meter E =
0010434
Z = 4882178
37 I = 51
72056
XDOT = -7302
383211 Wp = 197
91882
YDOT = -59
527452 meter/sec RA = 15
25018 deg
ZDOT = 2361
146300 TA = 228
96280
MA = 229
05303
Ha = 209
691 n
mi
Hp = 205
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5079402
57 X = 1474994
20
Y = 14486833
33 feet Y = 4432491
01 meter
Z = 16017645
59 Z = 4889521
16
XDOT = -23957
950166 XDOT = -7312
644822
YDOT = -195
300040 feet/sec YDOT = -141
244261 meter/sec
ZDOT = 7746
542978 ZDOT = 2325
646510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5775891
51 X = -1760491
73
Y = -14190034
25 feet Y = -4325122
44 meter
Z = 16047294
04 Z = 4891215
22
XDOT = 22943
550376 XDOT = 6993
194155
YDOT = -710
979013 feet/sec YDOT = -216
706403 meter/sec
ZDOT = 7601
946359 ZDOT = 2317
073250
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
55202219
00016717 00000-0 10270-3 0 9067
2 25544 51
6420 15
4972 0011046 234
8552 125
1570 15
61495986 16584
Satellite: ISS
Catalog Number: 25544
Epoch time: 11268
55202219 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 15
4972 deg
Eccentricity:
0011046
Arg of perigee: 234
8552 deg
Mean anomaly: 125
1570 deg
Mean motion: 15
61495986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 305
Coasting Arc #8 (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 = 3190798
56 A = 6757655
22 meter
Y = -3372529
98 meter E =
0009483
Z = -4915576
92 I = 51
69086
XDOT = 6685
850607 Wp = 165
05460
YDOT = 3016
410639 meter/sec RA = 10
17954 deg
ZDOT = 2262
392947 TA = 127
05170
MA = 126
96494
Ha = 209
445 n
mi
Hp = 205
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10468499
23 X = 3252152
75
Y = -11064730
92 feet Y = -3336506
12 meter
Z = -16127220
86 Z = -4899926
51
XDOT = 21935
205402 XDOT = 6640
633277
YDOT = 9896
360365 feet/sec YDOT = 3090
923393 meter/sec
ZDOT = 7422
549039 ZDOT = 2294
762642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9736205
42 X = -2967595
41
Y = 11801797
53 feet Y = 3597187
89 meter
Z = -16063277
32 Z = -4896086
93
XDOT = -21688
861716 XDOT = -6610
765051
YDOT = -7575
013544 feet/sec YDOT = -2308
864128 meter/sec
ZDOT = 7554
212383 ZDOT = 2302
523934
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
51200673
00016717 00000-0 10270-3 0 9077
2 25544 51
6421 10
6592 0010878 238
6039 121
4054 15
61527099 16738
Satellite: ISS
Catalog Number: 25544
Epoch time: 11269
51200673 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 10
6592 deg
Eccentricity:
0010878
Arg of perigee: 238
6039 deg
Mean anomaly: 121
4054 deg
Mean motion: 15
61527099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 299
Coasting Arc #9 (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 = -6351622
74 A = 6766210
09 meter
Y = 1058121
62 meter E =
0010709
Z = 2054523
45 I = 51
68916
XDOT = -2570
427433 Wp = 160
89564
YDOT = -4640
503020 meter/sec RA = 5
14266 deg
ZDOT = -5558
341099 TA = 356
31214
MA = 356
32002
Ha = 209
259 n
mi
Hp = 205
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20838657
28 X = -6372963
38
Y = 3471527
63 feet Y = 986974
83 meter
Z = 6740562
48 Z = 2023615
04
XDOT = -8433
160869 XDOT = -2491
343735
YDOT = -15224
747441 feet/sec YDOT = -4668
805650 meter/sec
ZDOT = -18236
027229 ZDOT = -5570
635641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20483942
71 X = 6243505
74
Y = -5328342
84 feet Y = -1624078
90 meter
Z = 6614618
49 Z = 2016135
72
XDOT = 9265
032933 XDOT = 2823
982038
YDOT = 12925
055301 feet/sec YDOT = 3939
556856 meter/sec
ZDOT = -18285
822747 ZDOT = -5573
518773
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
53596955
00016717 00000-0 10270-3 0 9083
2 25544 51
6420 5
4982 0010837 242
4800 117
5255 15
61512670 16891
Satellite: ISS
Catalog Number: 25544
Epoch time: 11270
53596955 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 5
4982 deg
Eccentricity:
0010837
Arg of perigee: 242
4800 deg
Mean anomaly: 117
5255 deg
Mean motion: 15
61512670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 308
Coasting Arc #10 (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 = 6244309
56 A = 6765957
09 meter
Y = 1623288
77 meter E =
0003261
Z = 2033259
05 I = 51
65922
XDOT = -2954
474116 Wp = 76
50940
YDOT = 4391
084724 meter/sec RA =
13912 deg
ZDOT = 5561
002137 TA = 306
02372
MA = 306
05394
Ha = 208
788 n
mi
Hp = 205
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20486579
91 X = 6215816
19
Y = 5325750
56 feet Y = 1692957
37 meter
Z = 6670797
40 Z = 2063524
90
XDOT = -9693
156547 XDOT = -3030
371199
YDOT = 14406
445946 feet/sec YDOT = 4357
622235 meter/sec
ZDOT = 18244
757668 ZDOT = 5546
464277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20897569
60 X = -6369579
21
Y = -3113979
35 feet Y = -949140
90 meter
Z = 6793955
45 Z = 2070797
62
XDOT = 7982
621015 XDOT = 2433
102885
YDOT = -13847
213258 feet/sec YDOT = -4220
630601 meter/sec
ZDOT = 18185
287838 ZDOT = 5542
875733
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
55990944
00016717 00000-0 10270-3 0 9093
2 25544 51
6425
3360 0010762 247
2124 112
7896 15
61567330 17059
Satellite: ISS
Catalog Number: 25544
Epoch time: 11271
55990944 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node:
3360 deg
Eccentricity:
0010762
Arg of perigee: 247
2124 deg
Mean anomaly: 112
7896 deg
Mean motion: 15
61567330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 296
Coasting Arc #11 (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 = -2855052
32 A = 6757364
90 meter
Y = -3661751
66 meter E =
0001662
Z = -4910830
75 I = 51
59943
XDOT = 6941
067560 Wp = 90
42038
YDOT = -2389
023647 meter/sec RA = 355
09736 deg
ZDOT = -2254
687551 TA = 157
58034
MA = 157
57308
Ha = 208
432 n
mi
Hp = 205
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9366969
56 X = -2790037
41
Y = -12013620
94 feet Y = -3693315
50 meter
Z = -16111649
44 Z = -4924542
57
XDOT = 22772
531364 XDOT = 6978
219242
YDOT = -7838
004092 feet/sec YDOT = -2311
196842 meter/sec
ZDOT = -7397
268869 ZDOT = -2220
876894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10685633
62 X = 3256981
13
Y = 10774474
59 feet Y = 3284059
86 meter
Z = -16167262
78 Z = -4927781
70
XDOT = -20885
205969 XDOT = -6365
810779
YDOT = 9823
387697 feet/sec YDOT = 2994
168570 meter/sec
ZDOT = -7259
436819 ZDOT = -2212
676342
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
51983503
00016717 00000-0 10270-3 0 9105
2 25544 51
6418 355
4976 0010822 251
3156 108
6826 15
61576730 17204
Satellite: ISS
Catalog Number: 25544
Epoch time: 11272
51983503 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 355
4976 deg
Eccentricity:
0010822
Arg of perigee: 251
3156 deg
Mean anomaly: 108
6826 deg
Mean motion: 15
61576730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 303
Coasting Arc #12 (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 = -1986947
31 A = 6757495
29 meter
Y = 4262453
20 meter E =
0004466
Z = 4856667
22 I = 51
57047
XDOT = -7263
189276 Wp = 281
75494
YDOT = -653
822411 meter/sec RA = 350
01608 deg
ZDOT = -2398
642336 TA = 191
74621
MA = 191
75663
Ha = 207
979 n
mi
Hp = 205
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6518856
01 X = -2058056
38
Y = 13984426
51 feet Y = 4239836
63 meter
Z = 15933947
59 Z = 4846841
53
XDOT = -23829
361143 XDOT = -7243
685943
YDOT = -2145
086650 feet/sec YDOT = -734
934927 meter/sec
ZDOT = -7869
561470 ZDOT = -2433
880006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4579170
48 X = 1395731
16
Y = -14777441
91 feet Y = -4504164
29 meter
Z = 15893670
52 Z = 4844390
77
XDOT = 22769
003711 XDOT = 6939
992331
YDOT = -1559
284352 feet/sec YDOT = -475
269870 meter/sec
ZDOT = -8013
013488 ZDOT = -2442
366511
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
54373377
00016717 00000-0 10270-3 0 9112
2 25544 51
6420 350
3353 0010742 256
0337 103
9625 15
61655385 17360
Satellite: ISS
Catalog Number: 25544
Epoch time: 11273
54373377 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 350
3353 deg
Eccentricity:
0010742
Arg of perigee: 256
0337 deg
Mean anomaly: 103
9625 deg
Mean motion: 15
61655385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1736
Checksum: 296
Coasting Arc #13 (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 = 5720138
56 A = 6766169
43 meter
Y = -3079014
52 meter E =
0007148
Z = -1878395
31 I = 51
56870
XDOT = 3790
195081 Wp = 302
36467
YDOT = 3603
060290 meter/sec RA = 344
97146 deg
ZDOT = 5624
112829 TA = 36
86661
MA = 36
81749
Ha = 207
553 n
mi
Hp = 205
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18766858
81 X = 5763268
58
Y = -10101753
67 feet Y = -3014807
35 meter
Z = -6162714
27 Z = -1850501
67
XDOT = 12435
023232 XDOT = 3722
302013
YDOT = 11821
063943 feet/sec YDOT = 3645
065177 meter/sec
ZDOT = 18451
813743 ZDOT = 5642
360755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16973307
89 X = -5173464
24
Y = 12943595
85 feet Y = 3945208
01 meter
Z = -6048934
61 Z = -1843715
27
XDOT = -13091
277312 XDOT = -3990
221325
YDOT = -8490
744290 feet/sec YDOT = -2587
978860 meter/sec
ZDOT = 18525
894543 ZDOT = 5646
692657
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
50362131
00016717 00000-0 10270-3 0 9126
2 25544 51
6412 345
4959 0010675 260
4276 99
5674 15
61624953 17512
Satellite: ISS
Catalog Number: 25544
Epoch time: 11274
50362131 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 345
4959 deg
Eccentricity:
0010675
Arg of perigee: 260
4276 deg
Mean anomaly: 99
5674 deg
Mean motion: 15
61624953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 312
Coasting Arc #14 (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 = -6365737
77 A = 6765249
53 meter
Y = 433416
84 meter E =
0008320
Z = -2233531
33 I = 51
53665
XDOT = 1563
069722 Wp = 229
11779
YDOT = -5180
558708 meter/sec RA = 339
95917 deg
ZDOT = -5452
246915 TA = 335
84070
MA = 335
87969
Ha = 206
984 n
mi
Hp = 205
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20884966
43 X = -6359261
02
Y = 1421971
27 feet Y = 362267
41 meter
Z = -7327858
68 Z = -2264440
60
XDOT = 5128
181504 XDOT = 1647
369810
YDOT = -16996
583689 feet/sec YDOT = -5162
608328 meter/sec
ZDOT = -17887
949195 ZDOT = -5444
448536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20270962
10 X = 6178589
25
Y = -5042916
50 feet Y = -1537080
95 meter
Z = -7453752
52 Z = -2271903
77
XDOT = -2551
680414 XDOT = -777
752190
YDOT = 16172
859308 feet/sec YDOT = 4929
487517 meter/sec
ZDOT = -17855
866180 ZDOT = -5442
468012
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
52748061
00016717 00000-0 10270-3 0 9130
2 25544 51
6405 340
3335 0010499 263
9091 96
0869 15
61682746 17672
Satellite: ISS
Catalog Number: 25544
Epoch time: 11275
52748061 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 340
3335 deg
Eccentricity:
0010499
Arg of perigee: 263
9091 deg
Mean anomaly: 96
0869 deg
Mean motion: 15
61682746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1767
Checksum: 326
Coasting Arc #15 (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 = 3692780
32 A = 6756542
50 meter
Y = 2663603
62 meter E =
0006811
Z = 4998005
11 I = 51
48015
XDOT = -5904
244045 Wp = 237
82638
YDOT = 4493
449482 meter/sec RA = 334
90337 deg
ZDOT = 1966
048010 TA = 193
05503
MA = 193
07266
Ha = 206
665 n
mi
Hp = 205
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12115420
99 X = 3638441
42
Y = 8738857
01 feet Y = 2704594
89 meter
Z = 16397654
57 Z = 5015812
63
XDOT = -19370
879413 XDOT = -5963
602603
YDOT = 14742
288326 feet/sec YDOT = 4427
092786 meter/sec
ZDOT = 6450
288746 ZDOT = 1937
220749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13468992
92 X = -4105349
04
Y = -6273705
40 feet Y = -1912225
41 meter
Z = 16470002
22 Z = 5020056
68
XDOT = 15765
351525 XDOT = 4805
279145
YDOT = -17208
201167 feet/sec YDOT = -5245
059716 meter/sec
ZDOT = 6332
617289 ZDOT = 1930
181750
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
55131706
00016717 00000-0 10270-3 0 9147
2 25544 51
6409 335
1705 0010546 268
2558 91
7391 15
61730233 17833
Satellite: ISS
Catalog Number: 25544
Epoch time: 11276
55131706 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 335
1705 deg
Eccentricity:
0010546
Arg of perigee: 268
2558 deg
Mean anomaly: 91
7391 deg
Mean motion: 15
61730233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1783
Checksum: 304
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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