[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 4th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 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 1297)
---------------------------------------
Vector Time (GMT): 2011/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1739960
44 A = 6766031
64 meter
Y = 5765187
19 meter E =
0014157
Z = -3104628
93 I = 51
90553
XDOT = -5823
288704 Wp = 127
93990
YDOT = 880
677892 meter/sec RA = 130
63249 deg
ZDOT = 4905
711309 TA = 196
45065
MA = 196
49664
Ha = 214
475 n
mi
Hp = 201
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5708531
63 X = -1789216
87
Y = 18914656
13 feet Y = 5745454
36 meter
Z = -10185790
46 Z = -3113201
52
XDOT = -19105
277901 XDOT = -5856
534839
YDOT = 2889
363163 feet/sec YDOT = 815
372621 meter/sec
ZDOT = 16094
853376 ZDOT = 4877
341027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11636972
04 X = 3546949
08
Y = -15944150
55 feet Y = -4859777
09 meter
Z = -10220901
24 Z = -3115330
70
XDOT = 17902
557871 XDOT = 5456
699639
YDOT = 2836
966817 feet/sec YDOT = 864
707486 meter/sec
ZDOT = 15979
310010 ZDOT = 4870
493691
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 11245
50640752
00016717 00000-0 10270-3 0 9009
2 25544 51
6393 131
5938 0011930 145
0836 215
1104 15
60741048 12980
Satellite: ISS
Catalog Number: 25544
Epoch time: 11245
50640752 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 131
5938 deg
Eccentricity:
0011930
Arg of perigee: 145
0836 deg
Mean anomaly: 215
1104 deg
Mean motion: 15
60741048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1298
Checksum: 283
Coasting Arc #2 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2011/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4325195
30 A = 6770051
80 meter
Y = -5152010
37 meter E =
0022713
Z = -654302
53 I = 51
93765
XDOT = 3278
246971 Wp = 145
12885
YDOT = 3499
722816 meter/sec RA = 125
64588 deg
ZDOT = -6006
800478 TA = 41
93404
MA = 41
76033
Ha = 214
482 n
mi
Hp = 201
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14190273
30 X = 4385663
10
Y = -16902921
17 feet Y = -5103305
31 meter
Z = -2146661
86 Z = -633143
81
XDOT = 10755
403449 XDOT = 3268
048615
YDOT = 11482
030237 feet/sec YDOT = 3536
325036 meter/sec
ZDOT = -19707
350651 ZDOT = -5990
899638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18835396
89 X = -5741028
97
Y = 11517972
86 feet Y = 3510678
13 meter
Z = -2060311
30 Z = -627982
88
XDOT = -5825
391767 XDOT = -1775
579411
YDOT = -12966
381910 feet/sec YDOT = -3952
153206 meter/sec
ZDOT = -19642
735202 ZDOT = -5987
105689
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 11246
53086967
00016717 00000-0 10270-3 0 9016
2 25544 51
6393 126
4349 0012040 149
8292 210
3560 15
60727420 13140
Satellite: ISS
Catalog Number: 25544
Epoch time: 11246
53086967 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 126
4349 deg
Eccentricity:
0012040
Arg of perigee: 149
8292 deg
Mean anomaly: 210
3560 deg
Mean motion: 15
60727420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 290
Coasting Arc #3 (Orbit 1329)
---------------------------------------
Vector Time (GMT): 2011/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4966595
75 A = 6763210
27 meter
Y = 2189662
43 meter E =
0020446
Z = 4030324
69 I = 51
93191
XDOT = 315
061703 Wp = 128
29903
YDOT = -6584
862557 meter/sec RA = 120
64897 deg
ZDOT = 3939
934088 TA = 280
92172
MA = 281
15171
Ha = 214
277 n
mi
Hp = 201
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16294605
49 X = -5010290
34
Y = 7183931
87 feet Y = 2133878
65 meter
Z = 13222850
04 Z = 4006090
95
XDOT = 1033
667003 XDOT = 369
532122
YDOT = -21603
879781 feet/sec YDOT = -6581
034755 meter/sec
ZDOT = 12926
292938 ZDOT = 3941
597005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17777572
96 X = 5418604
24
Y = -1919197
11 feet Y = -584971
28 meter
Z = 13124076
75 Z = 4000218
59
XDOT = -7558
081002 XDOT = -2303
703089
YDOT = 19015
842824 feet/sec YDOT = 5796
028893 meter/sec
ZDOT = 12933
322995 ZDOT = 3942
076849
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 11247
55530855
00016717 00000-0 10270-3 0 9020
2 25544 51
6392 121
2758 0011788 152
7735 207
4041 15
60784666 13303
Satellite: ISS
Catalog Number: 25544
Epoch time: 11247
55530855 = yrday
fracday
Element set: 902
Inclination: 51
6392 deg
RA of node: 121
2758 deg
Eccentricity:
0011788
Arg of perigee: 152
7735 deg
Mean anomaly: 207
4041 deg
Mean motion: 15
60784666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1330
Checksum: 307
Coasting Arc #4 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2011/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3649668
47 A = 6757867
21 meter
Y = 2038691
62 meter E =
0022428
Z = -5326677
53 I = 51
92894
XDOT = -3470
164849 Wp = 120
13986
YDOT = 6830
574299 meter/sec RA = 115
60594 deg
ZDOT = 226
380219 TA = 152
07049
MA = 151
94994
Ha = 213
973 n
mi
Hp = 201
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11973977
91 X = 3652475
96
Y = 6688620
80 feet Y = 2079520
12 meter
Z = -17475976
13 Z = -5308940
79
XDOT = -11385
055278 XDOT = -3547
387458
YDOT = 22410
020665 feet/sec YDOT = 6791
337021 meter/sec
ZDOT = 742
717254 ZDOT = 209
334713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9674715
31 X = -2948853
23
Y = -9850400
89 feet Y = -3002402
19 meter
Z = -17403822
08 Z = -5304684
97
XDOT = 16580
714166 XDOT = 5053
801678
YDOT = -17533
785034 feet/sec YDOT = -5344
297679 meter/sec
ZDOT = 673
018920 ZDOT = 205
136167
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 11248
51569847
00016717 00000-0 10270-3 0 9031
2 25544 51
6389 116
4385 0011686 157
2574 202
9102 15
60852665 13458
Satellite: ISS
Catalog Number: 25544
Epoch time: 11248
51569847 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 116
4385 deg
Eccentricity:
0011686
Arg of perigee: 157
2574 deg
Mean anomaly: 202
9102 deg
Mean motion: 15
60852665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 323
Coasting Arc #5 (Orbit 1360)
---------------------------------------
Vector Time (GMT): 2011/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1085286
49 A = 6763619
10 meter
Y = -5496976
19 meter E =
0017956
Z = 3767197
05 I = 51
96149
XDOT = 5044
802117 Wp = 122
24743
YDOT = -3928
168034 meter/sec RA = 110
56848 deg
ZDOT = -4273
101703 TA = 12
64525
MA = 12
60027
Ha = 213
766 n
mi
Hp = 201
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3560651
21 X = -1042037
69
Y = -18034698
80 feet Y = -5508870
67 meter
Z = 12359570
39 Z = 3762029
91
XDOT = 16551
188047 XDOT = 5109
110401
YDOT = -12887
690401 feet/sec YDOT = -3871
394454 meter/sec
ZDOT = -14019
362542 ZDOT = -4248
438132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1335133
80 X = -406948
78
Y = 18348301
86 feet Y = 5592562
41 meter
Z = 12338752
55 Z = 3760851
78
XDOT = -18144
711033 XDOT = -5530
507923
YDOT = 8051
622941 feet/sec YDOT = 2454
134672 meter/sec
ZDOT = -13918
742262 ZDOT = -4242
432642
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 11249
54009338
00016717 00000-0 10270-3 0 9040
2 25544 51
6394 111
2800 0011513 161
3245 198
8336 15
60910318 13619
Satellite: ISS
Catalog Number: 25544
Epoch time: 11249
54009338 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 111
2800 deg
Eccentricity:
0011513
Arg of perigee: 161
3245 deg
Mean anomaly: 198
8336 deg
Mean motion: 15
60910318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1361
Checksum: 283
Coasting Arc #6 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2011/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1651964
93 A = 6769647
56 meter
Y = 6563565
18 meter E =
0011328
Z = -219169
84 I = 51
99036
XDOT = -4628
936030 Wp = 104
08686
YDOT = -971
987157 meter/sec RA = 105
57740 deg
ZDOT = 6039
134603 TA = 253
55892
MA = 253
68346
Ha = 213
623 n
mi
Hp = 201
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5419832
46 X = -1724172
56
Y = 21534006
49 feet Y = 6544688
16 meter
Z = -719061
17 Z = -227370
52
XDOT = -15186
797998 XDOT = -4647
059597
YDOT = -3188
934241 feet/sec YDOT = -1023
851928 meter/sec
ZDOT = 19813
433738 ZDOT = 6016
603601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10659222
51 X = 3248931
02
Y = -19478691
45 feet Y = -5937105
15 meter
Z = -752743
71 Z = -229436
28
XDOT = 12591
028427 XDOT = 3837
745465
YDOT = 6159
186386 feet/sec YDOT = 1877
320010 meter/sec
ZDOT = 19721
696661 ZDOT = 6011
173142
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 11250
50044438
00016717 00000-0 10270-3 0 9059
2 25544 51
6384 106
4426 0011592 165
3040 194
8455 15
60912537 13761
Satellite: ISS
Catalog Number: 25544
Epoch time: 11250
50044438 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 106
4426 deg
Eccentricity:
0011592
Arg of perigee: 165
3040 deg
Mean anomaly: 194
8455 deg
Mean motion: 15
60912537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 294
Coasting Arc #7 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2011/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3622389
72 A = 6764482
55 meter
Y = -4517452
37 meter E =
0013169
Z = -3492121
77 I = 51
97927
XDOT = 2590
906916 Wp = 147
39119
YDOT = 5598
354115 meter/sec RA = 100
59106 deg
ZDOT = -4573
319477 TA = 73
57042
MA = 73
42572
Ha = 213
539 n
mi
Hp = 202
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11884480
70 X = 3689599
33
Y = -14821037
95 feet Y = -4476568
96 meter
Z = -11457092
42 Z = -3474361
06
XDOT = 8500
350774 XDOT = 2550
328434
YDOT = 18367
303528 feet/sec YDOT = 5627
100127 meter/sec
ZDOT = -15004
328994 ZDOT = -4560
831891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15100674
12 X = -4602685
47
Y = 11598738
69 feet Y = 3535295
55 meter
Z = -11384547
25 Z = -3470010
00
XDOT = -3189
769738 XDOT = -972
241816
YDOT = -18769
543596 feet/sec YDOT = -5720
956888 meter/sec
ZDOT = -14953
699123 ZDOT = -4557
887493
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 11251
52479580
00016717 00000-0 10270-3 0 9063
2 25544 51
6375 101
2830 0011539 169
6763 190
4633 15
60926574 13927
Satellite: ISS
Catalog Number: 25544
Epoch time: 11251
52479580 = yrday
fracday
Element set: 906
Inclination: 51
6375 deg
RA of node: 101
2830 deg
Eccentricity:
0011539
Arg of perigee: 169
6763 deg
Mean anomaly: 190
4633 deg
Mean motion: 15
60926574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 314
Coasting Arc #8 (Orbit 1407)
---------------------------------------
Vector Time (GMT): 2011/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4189822
40 A = 6757711
11 meter
Y = 325894
18 meter E =
0013363
Z = 5289727
09 I = 51
96114
XDOT = 236
669922 Wp = 162
22777
YDOT = -7651
342878 meter/sec RA = 95
55741 deg
ZDOT = 646
007903 TA = 281
56808
MA = 281
71807
Ha = 213
441 n
mi
Hp = 202
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13746136
48 X = -4218851
31
Y = 1069206
63 feet Y = 278879
06 meter
Z = 17354747
68 Z = 5269302
75
XDOT = 776
476122 XDOT = 319
073009
YDOT = -25102
830965 feet/sec YDOT = -7648
235507 meter/sec
ZDOT = 2119
448502 ZDOT = 647
358287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13750302
86 X = 4191092
31
Y = 1977428
04 feet Y = 602720
07 meter
Z = 17271528
23 Z = 5264361
80
XDOT = -6077
611084 XDOT = -1852
455858
YDOT = 23328
760562 feet/sec YDOT = 7110
606219 meter/sec
ZDOT = 2125
282798 ZDOT = 647
786197
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 11252
54912486
00016717 00000-0 10270-3 0 9074
2 25544 51
6373 96
1230 0011514 173
1387 186
9929 15
60945590 14081
Satellite: ISS
Catalog Number: 25544
Epoch time: 11252
54912486 = yrday
fracday
Element set: 907
Inclination: 51
6373 deg
RA of node: 96
1230 deg
Eccentricity:
0011514
Arg of perigee: 173
1387 deg
Mean anomaly: 186
9929 deg
Mean motion: 15
60945590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1408
Checksum: 319
Coasting Arc #9 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2011/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3283128
23 A = 6761784
04 meter
Y = 4129949
40 meter E =
0016459
Z = -4245589
48 I = 51
97590
XDOT = -2911
367108 Wp = 150
15793
YDOT = 6078
326892 meter/sec RA = 90
51189 deg
ZDOT = 3653
556182 TA = 157
10675
MA = 157
03330
Ha = 213
099 n
mi
Hp = 202
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10771418
08 X = 3257326
32
Y = 13549702
76 feet Y = 4166518
72 meter
Z = -13929099
35 Z = -4229703
31
XDOT = -9551
729358 XDOT = -2996
867822
YDOT = 19942
017361 feet/sec YDOT = 6045
292454 meter/sec
ZDOT = 11986
732879 ZDOT = 3639
204778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7904839
39 X = -2409395
04
Y = -15457202
47 feet Y = -4711355
31 meter
Z = -13864563
00 Z = -4225918
80
XDOT = 12314
894323 XDOT = 3753
579790
YDOT = -17020
032146 feet/sec YDOT = -5187
705798 meter/sec
ZDOT = 11927
997809 ZDOT = 3635
653732
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 11253
50941015
00016717 00000-0 10270-3 0 9082
2 25544 51
6360 91
2839 0011506 177
1663 182
9560 15
61011010 14236
Satellite: ISS
Catalog Number: 25544
Epoch time: 11253
50941015 = yrday
fracday
Element set: 908
Inclination: 51
6360 deg
RA of node: 91
2839 deg
Eccentricity:
0011506
Arg of perigee: 177
1663 deg
Mean anomaly: 182
9560 deg
Mean motion: 15
61011010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 272
Coasting Arc #10 (Orbit 1438)
---------------------------------------
Vector Time (GMT): 2011/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1191951
32 A = 6768912
85 meter
Y = -6592963
07 meter E =
0021925
Z = 861042
85 I = 51
99984
XDOT = 4559
290879 Wp = 150
87802
YDOT = -1610
978730 meter/sec RA = 85
51483 deg
ZDOT = -5978
968824 TA = 19
81290
MA = 19
72787
Ha = 212
814 n
mi
Hp = 202
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3910601
44 X = -1122321
67
Y = -21630456
27 feet Y = -6605902
79 meter
Z = 2824943
74 Z = 855422
20
XDOT = 14958
303408 XDOT = 4606
010718
YDOT = -5285
363287 feet/sec YDOT = -1559
733319 meter/sec
ZDOT = -19616
039449 ZDOT = -5956
706407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -129903
56 X = -39594
61
Y = 21983624
60 feet Y = 6700608
78 meter
Z = 2802342
54 Z = 854154
01
XDOT = -14189
611979 XDOT = -4324
993731
YDOT = 2423
979997 feet/sec YDOT = 738
829103 meter/sec
ZDOT = -19525
271358 ZDOT = -5951
302710
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 11254
53369159
00016717 00000-0 10270-3 0 9090
2 25544 51
6363 86
1242 0011274 181
4202 178
6924 15
61074010 14391
Satellite: ISS
Catalog Number: 25544
Epoch time: 11254
53369159 = yrday
fracday
Element set: 909
Inclination: 51
6363 deg
RA of node: 86
1242 deg
Eccentricity:
0011274
Arg of perigee: 181
4202 deg
Mean anomaly: 178
6924 deg
Mean motion: 15
61074010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1439
Checksum: 295
Coasting Arc #11 (Orbit 1454)
---------------------------------------
Vector Time (GMT): 2011/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1374805
93 A = 6765372
36 meter
Y = 5917151
55 meter E =
0015528
Z = 2979888
04 I = 51
98357
XDOT = -4569
265491 Wp = 129
01637
YDOT = -3597
380906 meter/sec RA = 80
53108 deg
ZDOT = 5008
260625 TA = 264
97061
MA = 265
14789
Ha = 212
698 n
mi
Hp = 202
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4510518
13 X = -1455346
15
Y = 19413226
87 feet Y = 5901327
62 meter
Z = 9776535
55 Z = 2973013
01
XDOT = -14991
028515 XDOT = -4553
028321
YDOT = -11802
430795 feet/sec YDOT = -3648
385904 meter/sec
ZDOT = 16431
301263 ZDOT = 4986
103128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7757209
69 X = 2364397
51
Y = -18373786
41 feet Y = -5600330
10 meter
Z = 9748254
70 Z = 2971268
03
XDOT = 11559
525431 XDOT = 3523
343351
YDOT = 13597
230078 feet/sec YDOT = 4144
435728 meter/sec
ZDOT = 16341
199900 ZDOT = 4980
797730
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 11255
55794934
00016717 00000-0 10270-3 0 9108
2 25544 51
6350 80
9626 0011520 185
5582 174
5449 15
61099695 14556
Satellite: ISS
Catalog Number: 25544
Epoch time: 11255
55794934 = yrday
fracday
Element set: 910
Inclination: 51
6350 deg
RA of node: 80
9626 deg
Eccentricity:
0011520
Arg of perigee: 185
5582 deg
Mean anomaly: 174
5449 deg
Mean motion: 15
61099695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 328
Coasting Arc #12 (Orbit 1469)
---------------------------------------
Vector Time (GMT): 2011/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3593721
72 A = 6757591
43 meter
Y = -2388449
58 meter E =
0015244
Z = -5209476
72 I = 51
95130
XDOT = 2839
134470 Wp = 125
92206
YDOT = 7013
963880 meter/sec RA = 75
50199 deg
ZDOT = -1268
510141 TA = 132
02335
MA = 131
89348
Ha = 212
597 n
mi
Hp = 202
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11790425
60 X = 3645469
36
Y = -7836120
68 feet Y = -2347973
62 meter
Z = -17091459
04 Z = -5191892
52
XDOT = 9314
745638 XDOT = 2766
654115
YDOT = 23011
692519 feet/sec YDOT = 7045
307420 meter/sec
ZDOT = -4161
778678 ZDOT = -1254
894492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12937523
72 X = -3943357
23
Y = 5957080
79 feet Y = 1815718
23 meter
Z = -17019711
04 Z = -5187607
93
XDOT = -5334
443374 XDOT = -1625
938340
YDOT = -23211
887490 feet/sec YDOT = -7074
983307 meter/sec
ZDOT = -4106
643576 ZDOT = -1251
704962
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 11256
51816994
00016717 00000-0 10270-3 0 9117
2 25544 51
6347 76
1240 0011425 188
1452 171
9520 15
61117734 14703
Satellite: ISS
Catalog Number: 25544
Epoch time: 11256
51816994 = yrday
fracday
Element set: 911
Inclination: 51
6347 deg
RA of node: 76
1240 deg
Eccentricity:
0011425
Arg of perigee: 188
1452 deg
Mean anomaly: 171
9520 deg
Mean motion: 15
61117734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1470
Checksum: 294
Coasting Arc #13 (Orbit 1485)
---------------------------------------
Vector Time (GMT): 2011/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4525491
80 A = 6760333
14 meter
Y = -2143212
36 meter E =
0009631
Z = 4532875
95 I = 51
95209
XDOT = 145
852020 Wp = 143
35614
YDOT = -7000
503982 meter/sec RA = 70
45266 deg
ZDOT = -3168
423634 TA = 338
19110
MA = 338
23208
Ha = 212
474 n
mi
Hp = 203
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14847414
05 X = -4523209
55
Y = -7031536
62 feet Y = -2193805
94 meter
Z = 14871640
25 Z = 4510896
86
XDOT = 478
517126 XDOT = 239
513830
YDOT = -22967
532748 feet/sec YDOT = -6998
349616 meter/sec
ZDOT = -10395
090663 ZDOT = -3167
486844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13864266
33 X = 4225828
38
Y = 8962272
76 feet Y = 2731700
74 meter
Z = 14782208
26 Z = 4505617
08
XDOT = -2949
518662 XDOT = -899
013288
YDOT = 21679
108826 feet/sec YDOT = 6607
792370 meter/sec
ZDOT = -10390
931767 ZDOT = -3167
156002
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 11257
54237944
00016717 00000-0 10270-3 0 9124
2 25544 51
6348 70
9630 0011412 192
6275 167
4597 15
61134201 14867
Satellite: ISS
Catalog Number: 25544
Epoch time: 11257
54237944 = yrday
fracday
Element set: 912
Inclination: 51
6348 deg
RA of node: 70
9630 deg
Eccentricity:
0011412
Arg of perigee: 192
6275 deg
Mean anomaly: 167
4597 deg
Mean motion: 15
61134201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1486
Checksum: 305
Coasting Arc #14 (Orbit 1500)
---------------------------------------
Vector Time (GMT): 2011/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3673224
88 A = 6768120
46 meter
Y = 5529607
69 meter E =
0004584
Z = -1333661
12 I = 51
96823
XDOT = -3365
466882 Wp = 149
32288
YDOT = 3645
437336 meter/sec RA = 65
44546 deg
ZDOT = 5850
336307 TA = 196
19612
MA = 196
21078
Ha = 212
124 n
mi
Hp = 203
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12051262
73 X = 3617597
43
Y = 18141757
51 feet Y = 5570372
78 meter
Z = -4375528
61 Z = -1315952
17
XDOT = -11041
558013 XDOT = -3434
400736
YDOT = 11960
096248 feet/sec YDOT = 3607
417755 meter/sec
ZDOT = 19194
016754 ZDOT = 5833
819018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9882568
38 X = -3012206
84
Y = -19424593
43 feet Y = -5920616
08 meter
Z = -4303668
46 Z = -1311758
15
XDOT = 11057
594109 XDOT = 3370
354684
YDOT = -9859
677363 feet/sec YDOT = -3005
229660 meter/sec
ZDOT = 19126
546360 ZDOT = 5829
771331
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 11258
50255263
00016717 00000-0 10270-3 0 9136
2 25544 51
6354 66
1238 0011413 195
7001 164
3803 15
61195241 15012
Satellite: ISS
Catalog Number: 25544
Epoch time: 11258
50255263 = yrday
fracday
Element set: 913
Inclination: 51
6354 deg
RA of node: 66
1238 deg
Eccentricity:
0011413
Arg of perigee: 195
7001 deg
Mean anomaly: 164
3803 deg
Mean motion: 15
61195241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1501
Checksum: 272
Coasting Arc #15 (Orbit 1516)
---------------------------------------
Vector Time (GMT): 2011/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1096405
78 A = 6765711
38 meter
Y = -6124193
07 meter E =
0013447
Z = -2638496
12 I = 51
94771
XDOT = 5456
219792 Wp = 178
57763
YDOT = 1282
182286 meter/sec RA = 60
46226 deg
ZDOT = -5257
024445 TA = 31
14598
MA = 31
06635
Ha = 211
824 n
mi
Hp = 203
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3597131
81 X = -1015024
95
Y = -20092496
95 feet Y = -6135998
94 meter
Z = -8656483
34 Z = -2643624
31
XDOT = 17900
983568 XDOT = 5467
014482
YDOT = 4206
634795 feet/sec YDOT = 1343
256997 meter/sec
ZDOT = -17247
455528 ZDOT = -5230
491864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1531047
61 X = 466663
31
Y = 20345691
08 feet Y = 6201366
64 meter
Z = -8677052
63 Z = -2644765
64
XDOT = -16014
044663 XDOT = -4881
080813
YDOT = -6085
477106 feet/sec YDOT = -1854
853422 meter/sec
ZDOT = -17139
439572 ZDOT = -5224
101181
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 11259
52671176
00016717 00000-0 10270-3 0 9145
2 25544 51
6360 60
9631 0011177 199
7272 160
3453 15
61249254 15177
Satellite: ISS
Catalog Number: 25544
Epoch time: 11259
52671176 = yrday
fracday
Element set: 914
Inclination: 51
6360 deg
RA of node: 60
9631 deg
Eccentricity:
0011177
Arg of perigee: 199
7272 deg
Mean anomaly: 160
3453 deg
Mean motion: 15
61249254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1517
Checksum: 306
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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