[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 9th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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 215)
---------------------------------------
Vector Time (GMT): 2012/067/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3540014
20 A = 6767750
51 meter
Y = -3843013
79 meter E =
0026318
Z = 4290411
40 I = 51
28613
XDOT = 2622
593601 Wp = 121
50399
YDOT = 6329
165060 meter/sec RA = 271
48878 deg
ZDOT = 3475
955089 TA = 292
91594
MA = 293
19350
Ha = 219
506 n
mi
Hp = 201
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11614219
82 X = 3561882
98
Y = -12608312
95 feet Y = -3803304
32 meter
Z = 14076152
89 Z = 4307661
94
XDOT = 8604
309716 XDOT = 2534
739583
YDOT = 20764
977230 feet/sec YDOT = 6358
001758 meter/sec
ZDOT = 11404
052130 ZDOT = 3488
481077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16674739
32 X = 5082460
55
Y = -3716117
06 feet Y = -1132672
48 meter
Z = 14147129
76 Z = 4312045
15
XDOT = -5188
820615 XDOT = -1581
552524
YDOT = 20689
984091 feet/sec YDOT = 6306
307151 meter/sec
ZDOT = 11454
961632 ZDOT = 3491
472305
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 12067
49955175
00016717 00000-0 10270-3 0 9008
2 25544 51
6405 271
9782 0017009 129
4129 230
8535 15
58831568 2169
Satellite: ISS
Catalog Number: 25544
Epoch time: 12067
49955175 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 271
9782 deg
Eccentricity:
0017009
Arg of perigee: 129
4129 deg
Mean anomaly: 230
8535 deg
Mean motion: 15
58831568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 216
Checksum: 321
Coasting Arc #2 (Orbit 230)
---------------------------------------
Vector Time (GMT): 2012/068/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4238497
39 A = 6763477
94 meter
Y = 200857
37 meter E =
0029568
Z = -5290478
82 I = 51
27170
XDOT = -438
529668 Wp = 113
27113
YDOT = -7643
234930 meter/sec RA = 266
41673 deg
ZDOT = 49
907029 TA = 157
27327
MA = 157
14210
Ha = 219
306 n
mi
Hp = 201
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13905831
33 X = -4214728
78
Y = 658980
87 feet Y = 153592
02 meter
Z = -17357213
98 Z = -5311011
27
XDOT = -1438
745629 XDOT = -353
271316
YDOT = -25076
230086 feet/sec YDOT = -7647
662127 meter/sec
ZDOT = 163
736971 ZDOT = 47
984877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11807480
13 X = -3598919
94
Y = -7173598
34 feet Y = -2186512
77 meter
Z = -17441392
65 Z = -5316136
48
XDOT = 12309
746528 XDOT = 3752
010742
YDOT = -20730
824408 feet/sec YDOT = -6318
755279 meter/sec
ZDOT = 156
371661 ZDOT = 47
662082
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 12068
46113815
00016717 00000-0 10270-3 0 9014
2 25544 51
6394 267
1482 0016852 133
4009 226
8552 15
58911087 2313
Satellite: ISS
Catalog Number: 25544
Epoch time: 12068
46113815 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 267
1482 deg
Eccentricity:
0016852
Arg of perigee: 133
4009 deg
Mean anomaly: 226
8552 deg
Mean motion: 15
58911087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 231
Checksum: 301
Coasting Arc #3 (Orbit 246)
---------------------------------------
Vector Time (GMT): 2012/069/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3964856
06 A = 6767453
90 meter
Y = 3444103
21 meter E =
0022740
Z = 4244181
48 I = 51
28918
XDOT = -1883
787760 Wp = 114
20346
YDOT = 6555
898810 meter/sec RA = 261
34678 deg
ZDOT = -3554
387873 TA = 12
13774
MA = 12
08305
Ha = 218
963 n
mi
Hp = 201
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13008057
93 X = 3905431
60
Y = 11299551
22 feet Y = 3488109
02 meter
Z = 13924479
92 Z = 4263297
60
XDOT = -6180
406036 XDOT = -1939
690849
YDOT = 21508
854364 feet/sec YDOT = 6534
520058 meter/sec
ZDOT = -11661
377536 ZDOT = -3563
675869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4676551
33 X = 1425412
85
Y = 16517787
00 feet Y = 5034621
48 meter
Z = 14002612
27 Z = 4267996
22
XDOT = -15639
949052 XDOT = -4767
056471
YDOT = 14362
496129 feet/sec YDOT = 4377
688820 meter/sec
ZDOT = -11699
882823 ZDOT = -3566
124284
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 12069
48680205
00016717 00000-0 10270-3 0 9020
2 25544 51
6398 261
9977 0016647 137
3662 222
8788 15
58979462 2473
Satellite: ISS
Catalog Number: 25544
Epoch time: 12069
48680205 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 261
9977 deg
Eccentricity:
0016647
Arg of perigee: 137
3662 deg
Mean anomaly: 222
8788 deg
Mean motion: 15
58979462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 247
Checksum: 357
Coasting Arc #4 (Orbit 261)
---------------------------------------
Vector Time (GMT): 2012/070/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2786834
16 A = 6774104
17 meter
Y = -5967120
39 meter E =
0016722
Z = -1617775
75 I = 51
31585
XDOT = 3880
219673 Wp = 113
74462
YDOT = -3345
923805 meter/sec RA = 256
30926 deg
ZDOT = 5697
398068 TA = 228
46103
MA = 228
60458
Ha = 219
007 n
mi
Hp = 202
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9143156
71 X = -2712042
73
Y = -19577166
62 feet Y = -5997866
51 meter
Z = -5307663
24 Z = -1631131
60
XDOT = 12730
379504 XDOT = 3889
669486
YDOT = -10977
440305 feet/sec YDOT = -3302
479229 meter/sec
ZDOT = 18692
250880 ZDOT = 5716
271319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2662837
82 X = 811632
97
Y = -21428767
24 feet Y = -6531488
25 meter
Z = -5362022
58 Z = -1634344
48
XDOT = 14955
287827 XDOT = 4558
371730
YDOT = -2805
570517 feet/sec YDOT = -855
137894 meter/sec
ZDOT = 18769
833901 ZDOT = 5721
045373
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 12070
44833642
00016717 00000-0 10270-3 0 9034
2 25544 51
6385 257
1678 0016658 141
0087 219
2273 15
58982544 2620
Satellite: ISS
Catalog Number: 25544
Epoch time: 12070
44833642 = yrday
fracday
Element set: 903
Inclination: 51
6385 deg
RA of node: 257
1678 deg
Eccentricity:
0016658
Arg of perigee: 141
0087 deg
Mean anomaly: 219
2273 deg
Mean motion: 15
58982544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 262
Checksum: 318
Coasting Arc #5 (Orbit 277)
---------------------------------------
Vector Time (GMT): 2012/071/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 761805
13 A = 6773908
70 meter
Y = 6501882
45 meter E =
0024299
Z = -1703588
34 I = 51
32358
XDOT = -5096
842212 Wp = 144
01645
YDOT = -875
277997 meter/sec RA = 251
29389 deg
ZDOT = -5680
240641 TA = 54
80352
MA = 54
57621
Ha = 218
835 n
mi
Hp = 202
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2499360
65 X = 697318
79
Y = 21331635
33 feet Y = 6510040
68 meter
Z = -5589200
59 Z = -1700044
85
XDOT = -16721
923269 XDOT = -5059
082554
YDOT = -2871
646973 feet/sec YDOT = -932
063505 meter/sec
ZDOT = -18635
960108 ZDOT = -5704
909042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8833383
80 X = -2692415
38
Y = 19580967
25 feet Y = 5968278
82 meter
Z = -5575095
08 Z = -1699288
98
XDOT = -11318
448554 XDOT = -3449
863119
YDOT = -10384
156712 feet/sec YDOT = -3165
090966 meter/sec
ZDOT = -18737
027286 ZDOT = -5711
045917
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 12071
47394255
00016717 00000-0 10270-3 0 9041
2 25544 51
6384 252
0165 0016623 144
8527 215
3728 15
59021530 2785
Satellite: ISS
Catalog Number: 25544
Epoch time: 12071
47394255 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 252
0165 deg
Eccentricity:
0016623
Arg of perigee: 144
8527 deg
Mean anomaly: 215
3728 deg
Mean motion: 15
59021530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 278
Checksum: 300
Coasting Arc #6 (Orbit 293)
---------------------------------------
Vector Time (GMT): 2012/072/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1585018
25 A = 6767048
01 meter
Y = -4966899
46 meter E =
0024701
Z = 4309003
67 I = 51
31138
XDOT = 5057
564643 Wp = 133
86845
YDOT = 4633
415211 meter/sec RA = 246
25630 deg
ZDOT = 3451
246186 TA = 280
83438
MA = 281
11229
Ha = 218
640 n
mi
Hp = 202
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5200191
10 X = 1619509
16
Y = -16295601
91 feet Y = -4948981
61 meter
Z = 14137151
16 Z = 4316787
79
XDOT = 16593
059852 XDOT = 4988
611606
YDOT = 15201
493476 feet/sec YDOT = 4689
586761 meter/sec
ZDOT = 11322
986176 ZDOT = 3475
647728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12590184
14 X = 3837488
13
Y = -11539651
22 feet Y = -3517285
69 meter
Z = 14169381
95 Z = 4318827
62
XDOT = 5842
151763 XDOT = 1780
687857
YDOT = 20517
287460 feet/sec YDOT = 6253
669218 meter/sec
ZDOT = 11422
723904 ZDOT = 3481
646246
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 12072
49951766
00016717 00000-0 10270-3 0 9051
2 25544 51
6380 246
8645 0016484 148
6459 211
5683 15
59068599 2948
Satellite: ISS
Catalog Number: 25544
Epoch time: 12072
49951766 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 246
8645 deg
Eccentricity:
0016484
Arg of perigee: 148
6459 deg
Mean anomaly: 211
5683 deg
Mean motion: 15
59068599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 294
Checksum: 353
Coasting Arc #7 (Orbit 308)
---------------------------------------
Vector Time (GMT): 2012/073/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3806313
37 A = 6762860
21 meter
Y = 1868096
46 meter E =
0027180
Z = -5288631
11 I = 51
31047
XDOT = -3574
019599 Wp = 123
56544
YDOT = -6772
544181 meter/sec RA = 241
18433 deg
ZDOT = 165
892059 TA = 148
10705
MA = 147
94221
Ha = 218
497 n
mi
Hp = 202
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12487904
74 X = -3801229
01
Y = 6128925
40 feet Y = 1825560
03 meter
Z = -17351151
94 Z = -5307109
71
XDOT = -11725
786086 XDOT = -3498
827878
YDOT = -22219
633139 feet/sec YDOT = -6812
090645 meter/sec
ZDOT = 544
265287 ZDOT = 148
712735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13799731
39 X = -4206158
13
Y = -663289
67 feet Y = -202170
69 meter
Z = -17427031
46 Z = -5311759
19
XDOT = 501
780521 XDOT = 152
942703
YDOT = -24112
919291 feet/sec YDOT = -7349
617800 meter/sec
ZDOT = 474
264232 ZDOT = 144
555738
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 12073
46096512
00016717 00000-0 10270-3 0 9069
2 25544 51
6372 242
0339 0016591 152
0052 208
1999 15
59125853 3090
Satellite: ISS
Catalog Number: 25544
Epoch time: 12073
46096512 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 242
0339 deg
Eccentricity:
0016591
Arg of perigee: 152
0052 deg
Mean anomaly: 208
1999 deg
Mean motion: 15
59125853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 309
Checksum: 303
Coasting Arc #8 (Orbit 324)
---------------------------------------
Vector Time (GMT): 2012/074/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5080667
04 A = 6767251
51 meter
Y = 1620062
85 meter E =
0020682
Z = 4143516
00 I = 51
34150
XDOT = 902
003722 Wp = 126
96989
YDOT = 6673
329880 meter/sec RA = 236
11678 deg
ZDOT = -3714
639939 TA = 1
24249
MA = 1
23736
Ha = 218
183 n
mi
Hp = 202
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16668855
12 X = 5042045
44
Y = 5315166
82 feet Y = 1676662
26 meter
Z = 13594212
61 Z = 4168103
59
XDOT = 2959
329795 XDOT = 845
358919
YDOT = 21894
126902 feet/sec YDOT = 6683
099741 meter/sec
ZDOT = -12187
138906 ZDOT = -3710
395993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12127733
91 X = 3696533
30
Y = 12500856
10 feet Y = 3810260
94 meter
Z = 13694926
53 Z = 4174213
61
XDOT = -6723
610061 XDOT = -2049
356347
YDOT = 19857
568309 feet/sec YDOT = 6052
586821 meter/sec
ZDOT = -12170
158851 ZDOT = -3709
464418
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 12074
48647784
00016717 00000-0 10270-3 0 9076
2 25544 51
6374 236
8826 0016459 156
1830 204
0090 15
59167081 3250
Satellite: ISS
Catalog Number: 25544
Epoch time: 12074
48647784 = yrday
fracday
Element set: 907
Inclination: 51
6374 deg
RA of node: 236
8826 deg
Eccentricity:
0016459
Arg of perigee: 156
1830 deg
Mean anomaly: 204
0090 deg
Mean motion: 15
59167081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 325
Checksum: 320
Coasting Arc #9 (Orbit 339)
---------------------------------------
Vector Time (GMT): 2012/075/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4966710
62 A = 6773695
76 meter
Y = -4409053
56 meter E =
0014049
Z = -1370517
86 I = 51
38111
XDOT = 2354
080793 Wp = 128
28897
YDOT = -4439
924632 meter/sec RA = 231
08447 deg
ZDOT = 5784
327284 TA = 216
71992
MA = 216
81626
Ha = 218
162 n
mi
Hp = 202
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16294982
36 X = -4910380
97
Y = -14465398
81 feet Y = -4464279
49 meter
Z = -4496449
67 Z = -1394508
60
XDOT = 7723
362181 XDOT = 2375
455325
YDOT = -14566
681865 feet/sec YDOT = -4413
480045 meter/sec
ZDOT = 18977
451718 ZDOT = 5795
815312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7887663
21 X = -2404159
75
Y = -20289581
24 feet Y = -6184264
36 meter
Z = -4594554
89 Z = -1400420
33
XDOT = 11930
299047 XDOT = 3636
355150
YDOT = -8922
929031 feet/sec YDOT = -2719
708769 meter/sec
ZDOT = 19024
836846 ZDOT = 5798
770271
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 12075
44786712
00016717 00000-0 10270-3 0 9089
2 25544 51
6369 232
0519 0016539 159
3912 200
7914 15
59228208 3400
Satellite: ISS
Catalog Number: 25544
Epoch time: 12075
44786712 = yrday
fracday
Element set: 908
Inclination: 51
6369 deg
RA of node: 232
0519 deg
Eccentricity:
0016539
Arg of perigee: 159
3912 deg
Mean anomaly: 200
7914 deg
Mean motion: 15
59228208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 340
Checksum: 313
Coasting Arc #10 (Orbit 355)
---------------------------------------
Vector Time (GMT): 2012/076/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3180538
50 A = 6772654
84 meter
Y = 5617716
38 meter E =
0022674
Z = -2012373
18 I = 51
39815
XDOT = -5216
592052 Wp = 156
39262
YDOT = 978
177838 meter/sec RA = 226
07280 deg
ZDOT = -5556
148440 TA = 45
99113
MA = 45
80448
Ha = 217
879 n
mi
Hp = 202
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10434837
59 X = 3127259
18
Y = 18430828
01 feet Y = 5652985
10 meter
Z = -6602274
22 Z = -1997052
26
XDOT = -17114
803319 XDOT = -5200
152412
YDOT = 3209
244876 feet/sec YDOT = 919
934260 meter/sec
ZDOT = -18228
833463 ZDOT = -5581
450156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1288856
58 X = 392843
48
Y = 21159899
99 feet Y = 6449537
52 meter
Z = -6539783
08 Z = -1993325
88
XDOT = -15136
179020 XDOT = -4613
507365
YDOT = -4700
997905 feet/sec YDOT = -1432
864161 meter/sec
ZDOT = -18332
659127 ZDOT = -5587
794502
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 12076
47331611
00016717 00000-0 10270-3 0 9098
2 25544 51
6370 226
8997 0016284 162
7952 197
3759 15
59294602 3568
Satellite: ISS
Catalog Number: 25544
Epoch time: 12076
47331611 = yrday
fracday
Element set: 909
Inclination: 51
6370 deg
RA of node: 226
8997 deg
Eccentricity:
0016284
Arg of perigee: 162
7952 deg
Mean anomaly: 197
3759 deg
Mean motion: 15
59294602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 356
Checksum: 340
Coasting Arc #11 (Orbit 371)
---------------------------------------
Vector Time (GMT): 2012/077/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -234534
94 A = 6765438
45 meter
Y = -5010030
60 meter E =
0022639
Z = 4540381
02 I = 51
39571
XDOT = 6583
765355 Wp = 149
12112
YDOT = 2489
800703 meter/sec RA = 221
03562 deg
ZDOT = 3061
535510 TA = 270
05948
MA = 270
31890
Ha = 217
722 n
mi
Hp = 202
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -769471
60 X = -200550
11
Y = -16437108
27 feet Y = -5012462
93 meter
Z = 14896263
18 Z = 4539324
63
XDOT = 21600
280037 XDOT = 6540
562586
YDOT = 8168
637476 feet/sec YDOT = 2563
183119 meter/sec
ZDOT = 10044
407842 ZDOT = 3093
413459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6204163
10 X = 1891028
91
Y = -15244643
66 feet Y = -4646567
39 meter
Z = 14892228
56 Z = 4539151
27
XDOT = 14916
318453 XDOT = 4546
493864
YDOT = 16093
342066 feet/sec YDOT = 4905
250662 meter/sec
ZDOT = 10175
008654 ZDOT = 3101
342638
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 12077
49873207
00016717 00000-0 10270-3 0 9105
2 25544 51
6365 221
7469 0016355 167
1569 193
0006 15
59338183 3721
Satellite: ISS
Catalog Number: 25544
Epoch time: 12077
49873207 = yrday
fracday
Element set: 910
Inclination: 51
6365 deg
RA of node: 221
7469 deg
Eccentricity:
0016355
Arg of perigee: 167
1569 deg
Mean anomaly: 193
0006 deg
Mean motion: 15
59338183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 372
Checksum: 320
Coasting Arc #12 (Orbit 386)
---------------------------------------
Vector Time (GMT): 2012/078/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3132577
28 A = 6762284
71 meter
Y = 2909298
81 meter E =
0024710
Z = -5256286
23 I = 51
41041
XDOT = -5818
463539 Wp = 135
38784
YDOT = -4933
732224 meter/sec RA = 215
96673 deg
ZDOT = 721
665824 TA = 141
62061
MA = 141
44455
Ha = 217
525 n
mi
Hp = 202
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10277484
50 X = -3139343
41
Y = 9544943
61 feet Y = 2874230
04 meter
Z = -17245033
55 Z = -5271520
61
XDOT = -19089
447307 XDOT = -5766
366739
YDOT = -16186
785513 feet/sec YDOT = -4998
506517 meter/sec
ZDOT = 2367
670027 ZDOT = 693
527516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13187241
27 X = -4019471
14
Y = 4545795
98 feet Y = 1385558
62 meter
Z = -17307692
65 Z = -5275384
72
XDOT = -10475
858941 XDOT = -3193
041805
YDOT = -21624
922288 feet/sec YDOT = -6591
276313 meter/sec
ZDOT = 2252
535932 ZDOT = 686
572952
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 12078
46002997
00016717 00000-0 10270-3 0 9114
2 25544 51
6375 216
9166 0016363 169
9885 190
1600 15
59376626 3870
Satellite: ISS
Catalog Number: 25544
Epoch time: 12078
46002997 = yrday
fracday
Element set: 911
Inclination: 51
6375 deg
RA of node: 216
9166 deg
Eccentricity:
0016363
Arg of perigee: 169
9885 deg
Mean anomaly: 190
1600 deg
Mean motion: 15
59376626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 387
Checksum: 338
Coasting Arc #13 (Orbit 402)
---------------------------------------
Vector Time (GMT): 2012/079/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5599300
51 A = 6767836
23 meter
Y = -153126
19 meter E =
0019652
Z = 3774735
92 I = 51
45427
XDOT = 2991
328339 Wp = 138
61483
YDOT = 5698
414499 meter/sec RA = 210
90751 deg
ZDOT = -4208
046723 TA = 355
78049
MA = 355
79704
Ha = 217
243 n
mi
Hp = 203
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18370408
48 X = 5582260
10
Y = -502382
50 feet Y = -90606
18 meter
Z = 12384304
20 Z = 3801895
28
XDOT = 9814
069354 XDOT = 2947
826626
YDOT = 18695
585626 feet/sec YDOT = 5731
621649 meter/sec
ZDOT = -13805
927568 ZDOT = -4193
621550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17016718
01 X = 5186695
65
Y = 6736721
32 feet Y = 2053352
66 meter
Z = 12495726
48 Z = 3808697
43
XDOT = 2235
436436 XDOT = 681
361026
YDOT = 19840
398003 feet/sec YDOT = 6047
353311 meter/sec
ZDOT = -13747
076083 ZDOT = -4190
108790
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 12079
48538097
00016717 00000-0 10270-3 0 9123
2 25544 51
6371 211
7630 0016272 173
9644 186
1711 15
59398653 4033
Satellite: ISS
Catalog Number: 25544
Epoch time: 12079
48538097 = yrday
fracday
Element set: 912
Inclination: 51
6371 deg
RA of node: 211
7630 deg
Eccentricity:
0016272
Arg of perigee: 173
9644 deg
Mean anomaly: 186
1711 deg
Mean motion: 15
59398653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 403
Checksum: 320
Coasting Arc #14 (Orbit 417)
---------------------------------------
Vector Time (GMT): 2012/080/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6294213
92 A = 6773557
62 meter
Y = -2412501
59 meter E =
0011017
Z = -726489
92 I = 51
50257
XDOT = 1123
749852 Wp = 138
31849
YDOT = -4708
067094 meter/sec RA = 205
88877 deg
ZDOT = 5942
244937 TA = 213
81205
MA = 213
88235
Ha = 217
092 n
mi
Hp = 203
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20650308
14 X = -6263239
96
Y = -7915031
47 feet Y = -2482714
29 meter
Z = -2383497
13 Z = -756991
00
XDOT = 3686
843348 XDOT = 1147
447150
YDOT = -15446
414350 feet/sec YDOT = -4695
367344 meter/sec
ZDOT = 19495
554254 ZDOT = 5947
762177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16119503
71 X = -4913224
73
Y = -15120617
45 feet Y = -4608764
20 meter
Z = -2508492
82 Z = -764588
61
XDOT = 8033
269765 XDOT = 2448
540624
YDOT = -11779
348555 feet/sec YDOT = -3590
345440 meter/sec
ZDOT = 19518
451207 ZDOT = 5949
223928
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 12080
44661581
00016717 00000-0 10270-3 0 9137
2 25544 51
6388 206
9323 0016195 177
4234 182
7008 15
59478767 4186
Satellite: ISS
Catalog Number: 25544
Epoch time: 12080
44661581 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 206
9323 deg
Eccentricity:
0016195
Arg of perigee: 177
4234 deg
Mean anomaly: 182
7008 deg
Mean motion: 15
59478767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 418
Checksum: 327
Coasting Arc #15 (Orbit 433)
---------------------------------------
Vector Time (GMT): 2012/081/10:40:59
737
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4695405
83 A = 6770697
69 meter
Y = 4064615
41 meter E =
0019282
Z = -2672208
25 I = 51
52123
XDOT = -5089
093500 Wp = 169
44401
YDOT = 2478
872569 meter/sec RA = 200
88231 deg
ZDOT = -5196
137268 TA = 40
88021
MA = 40
73575
Ha = 216
858 n
mi
Hp = 203
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15404874
76 X = 4662586
38
Y = 13335352
41 feet Y = 4116938
47 meter
Z = -8767087
42 Z = -2649478
65
XDOT = -16696
500985 XDOT = -5091
193059
YDOT = 8132
784020 feet/sec YDOT = 2421
950718 meter/sec
ZDOT = -17047
694448 ZDOT = -5220
865094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9590265
30 X = 2923112
86
Y = 18021962
80 feet Y = 5493094
26 meter
Z = -8674057
89 Z = -2643852
85
XDOT = -17096
104599 XDOT = -5210
892682
YDOT = 882
643626 feet/sec YDOT = 269
029777 meter/sec
ZDOT = -17149
282594 ZDOT = -5227
101335
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 12081
47190034
00016717 00000-0 10270-3 0 9142
2 25544 51
6389 201
7790 0016015 181
4288 178
6824 15
59524438 4348
Satellite: ISS
Catalog Number: 25544
Epoch time: 12081
47190034 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 201
7790 deg
Eccentricity:
0016015
Arg of perigee: 181
4288 deg
Mean anomaly: 178
6824 deg
Mean motion: 15
59524438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 434
Checksum: 314
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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