[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 31st 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) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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 2852)
---------------------------------------
Vector Time (GMT): 2011/089/13:13:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2240940
42 A = 6728828
39 meter
Y = -4678039
15 meter E =
0010402
Z = 4278468
74 I = 51
50025
XDOT = 6857
789300 Wp = 99
96021
YDOT = -70
639647 meter/sec RA = 203
40132 deg
ZDOT = 3505
694307 TA = 314
43524
MA = 314
52030
Ha = 192
955 n
mi
Hp = 185
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7352166
73 X = -2209246
90
Y = -15347897
47 feet Y = -4702921
06 meter
Z = 14036970
95 Z = 4267659
86
XDOT = 22499
308728 XDOT = 6841
039714
YDOT = -231
757372 feet/sec YDOT = 5
955020 meter/sec
ZDOT = 11501
621743 ZDOT = 3538
968323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13264975
81 X = -4043164
63
Y = -10718006
35 feet Y = -3266848
33 meter
Z = 13993342
07 Z = 4265170
66
XDOT = 19413
405215 XDOT = 5917
205909
YDOT = -8796
176801 feet/sec YDOT = -2681
074689 meter/sec
ZDOT = 11636
042389 ZDOT = 3546
665720
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 11089
60519053
00016717 00000-0 10270-3 0 9005
2 25544 51
6455 204
1331 0001509 33
4324 326
6934 15
72399756 28531
Satellite: ISS
Catalog Number: 25544
Epoch time: 11089
60519053 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 204
1331 deg
Eccentricity:
0001509
Arg of perigee: 33
4324 deg
Mean anomaly: 326
6934 deg
Mean motion: 15
72399756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2853
Checksum: 300
Coasting Arc #2 (Orbit 2867)
---------------------------------------
Vector Time (GMT): 2011/090/13:13:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5678470
23 A = 6731307
24 meter
Y = 1031522
67 meter E =
0006090
Z = -3468593
82 I = 51
53787
XDOT = -3676
946467 Wp = 81
45741
YDOT = -5005
886814 meter/sec RA = 198
22035 deg
ZDOT = 4538
533633 TA = 237
40506
MA = 237
46387
Ha = 192
844 n
mi
Hp = 185
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18630151
69 X = -5672733
24
Y = 3384260
73 feet Y = 968054
26 meter
Z = -11379900
97 Z = -3496165
73
XDOT = -12063
472662 XDOT = -3642
743571
YDOT = -16423
513169 feet/sec YDOT = -5046
812912 meter/sec
ZDOT = 14890
202207 ZDOT = 4520
754844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15161335
47 X = -4621175
05
Y = 11230398
05 feet Y = 3423025
32 meter
Z = -11491300
42 Z = -3502548
37
XDOT = -17335
147767 XDOT = -5283
753039
YDOT = -8265
720601 feet/sec YDOT = -2519
391639 meter/sec
ZDOT = 14818
410756 ZDOT = 4516
651598
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 11090
55850096
00016717 00000-0 10270-3 0 9017
2 25544 51
6456 199
2505 0001647 31
8939 328
2323 15
72435775 28684
Satellite: ISS
Catalog Number: 25544
Epoch time: 11090
55850096 = yrday
fracday
Element set: 901
Inclination: 51
6456 deg
RA of node: 199
2505 deg
Eccentricity:
0001647
Arg of perigee: 31
8939 deg
Mean anomaly: 328
2323 deg
Mean motion: 15
72435775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2868
Checksum: 325
Coasting Arc #3 (Orbit 2883)
---------------------------------------
Vector Time (GMT): 2011/091/13:13:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4083044
51 A = 6730795
78 meter
Y = 3924079
92 meter E =
0006863
Z = -3645447
66 I = 51
56529
XDOT = -5959
461377 Wp = 70
87817
YDOT = 2158
337169 meter/sec RA = 193
14225 deg
ZDOT = -4355
980909 TA = 152
83163
MA = 152
79570
Ha = 192
865 n
mi
Hp = 185
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13395815
33 X = 4056570
07
Y = 12874277
97 feet Y = 3969590
56 meter
Z = -11960130
13 Z = -3625677
11
XDOT = -19552
038638 XDOT = -5961
992939
YDOT = 7081
158691 feet/sec YDOT = 2091
680199 meter/sec
ZDOT = -14291
275947 ZDOT = -4384
938204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17860850
14 X = 5443987
12
Y = 5299871
82 feet Y = 1615400
93 meter
Z = -11880277
99 Z = -3621108
73
XDOT = -13695
223276 XDOT = -4174
304055
YDOT = 13888
771102 feet/sec YDOT = 4233
297432 meter/sec
ZDOT = -14408
286617 ZDOT = -4391
645761
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 11091
57532480
00016717 00000-0 10270-3 0 9025
2 25544 51
6451 194
0411 0001726 35
9917 324
1362 15
72488389 28842
Satellite: ISS
Catalog Number: 25544
Epoch time: 11091
57532480 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 194
0411 deg
Eccentricity:
0001726
Arg of perigee: 35
9917 deg
Mean anomaly: 324
1362 deg
Mean motion: 15
72488389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2884
Checksum: 311
Coasting Arc #4 (Orbit 2899)
---------------------------------------
Vector Time (GMT): 2011/092/13:13:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4613754
19 A = 6728747
61 meter
Y = -2647968
20 meter E =
0011929
Z = 4113647
92 I = 51
59027
XDOT = 5545
500693 Wp = 69
53570
YDOT = 3791
072973 meter/sec RA = 187
96272 deg
ZDOT = -3766
471199 TA = 59
14170
MA = 59
02441
Ha = 192
670 n
mi
Hp = 185
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15136988
81 X = 4623038
03
Y = -8687559
71 feet Y = -2596322
03 meter
Z = 13496220
22 Z = 4136084
36
XDOT = 18193
899913 XDOT = 5520
992854
YDOT = 12437
903456 feet/sec YDOT = 3852
948671 meter/sec
ZDOT = -12357
188973 ZDOT = -3739
591149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9172073
15 X = 2795647
90
Y = -14765482
89 feet Y = -4500519
19 meter
Z = 13586893
42 Z = 4141285
12
XDOT = 20898
508789 XDOT = 6369
865479
YDOT = 1672
256328 feet/sec YDOT = 509
703729 meter/sec
ZDOT = -12248
605116 ZDOT = -3733
374839
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 11092
59210636
00016717 00000-0 10270-3 0 9035
2 25544 51
6456 188
8313 0001947 35
1284 325
0007 15
72587449 29005
Satellite: ISS
Catalog Number: 25544
Epoch time: 11092
59210636 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 188
8313 deg
Eccentricity:
0001947
Arg of perigee: 35
1284 deg
Mean anomaly: 325
0007 deg
Mean motion: 15
72587449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2900
Checksum: 304
Coasting Arc #5 (Orbit 2915)
---------------------------------------
Vector Time (GMT): 2011/093/13:13:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5475441
35 A = 6732450
39 meter
Y = -2591318
80 meter E =
0014951
Z = 2920948
40 I = 51
63287
XDOT = 4468
525885 Wp = 77
01279
YDOT = -3757
626255 meter/sec RA = 182
88561 deg
ZDOT = 5024
673995 TA = 316
62645
MA = 316
74401
Ha = 192
802 n
mi
Hp = 185
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17964046
42 X = -5460247
26
Y = -8501702
10 feet Y = -2652463
25 meter
Z = 9583164
04 Z = 2894385
81
XDOT = 14660
517995 XDOT = 4485
803232
YDOT = -12328
170128 feet/sec YDOT = -3707
559359 meter/sec
ZDOT = 16485
150901 ZDOT = 5046
424514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19879540
53 X = -6059283
95
Y = 1354654
02 feet Y = 412898
54 meter
Z = 9475849
10 Z = 2888238
81
XDOT = 6810
319454 XDOT = 2075
785369
YDOT = -16409
910163 feet/sec YDOT = -5001
740618 meter/sec
ZDOT = 16573
066962 ZDOT = 5051
470810
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 11093
60884773
00016717 00000-0 10270-3 0 9048
2 25544 51
6451 183
6216 0001983 40
2215 319
9094 15
72632912 29167
Satellite: ISS
Catalog Number: 25544
Epoch time: 11093
60884773 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 183
6216 deg
Eccentricity:
0001983
Arg of perigee: 40
2215 deg
Mean anomaly: 319
9094 deg
Mean motion: 15
72632912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2916
Checksum: 309
Coasting Arc #6 (Orbit 2930)
---------------------------------------
Vector Time (GMT): 2011/094/13:13:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3121329
39 A = 6726570
59 meter
Y = 3780635
80 meter E =
0011730
Z = -4616413
37 I = 51
64365
XDOT = -6807
856373 Wp = 100
07369
YDOT = -2048
594396 meter/sec RA = 177
71533 deg
ZDOT = 2929
621257 TA = 198
97339
MA = 199
01713
Ha = 192
710 n
mi
Hp = 185
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10240582
00 X = -3140947
36
Y = 12403660
75 feet Y = 3745621
08 meter
Z = -15145713
17 Z = -4631624
88
XDOT = -22335
486788 XDOT = -6798
674281
YDOT = -6721
110224 feet/sec YDOT = -2124
672368 meter/sec
ZDOT = 9611
618297 ZDOT = 2896
570981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2550007
57 X = -777242
31
Y = 15822485
94 feet Y = 4822693
71 meter
Z = -15207213
66 Z = -4635158
72
XDOT = -21585
999962 XDOT = -6579
412788
YDOT = 5617
187306 feet/sec YDOT = 1712
118691 meter/sec
ZDOT = 9478
076290 ZDOT = 2888
917653
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 11094
56200581
00016717 00000-0 10270-3 0 9054
2 25544 51
6442 178
7374 0002221 42
5157 317
6177 15
72699020 29310
Satellite: ISS
Catalog Number: 25544
Epoch time: 11094
56200581 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 178
7374 deg
Eccentricity:
0002221
Arg of perigee: 42
5157 deg
Mean anomaly: 317
6177 deg
Mean motion: 15
72699020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2931
Checksum: 298
Coasting Arc #7 (Orbit 2946)
---------------------------------------
Vector Time (GMT): 2011/095/13:13:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6286732
21 A = 6733668
13 meter
Y = 951934
41 meter E =
0006543
Z = -2215938
16 I = 51
69826
XDOT = -2640
145123 Wp = 117
38762
YDOT = 4707
906949 meter/sec RA = 172
63335 deg
ZDOT = -5483
062398 TA = 87
40636
MA = 87
33146
Ha = 192
727 n
mi
Hp = 185
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20625761
84 X = 6286384
97
Y = 3123144
38 feet Y = 1022234
36 meter
Z = -7270138
33 Z = -2185397
88
XDOT = -8661
893449 XDOT = -2665
957666
YDOT = 15445
888941 feet/sec YDOT = 4678
238513 meter/sec
ZDOT = -17989
049862 ZDOT = -5495
951375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19307684
50 X = 5884982
24
Y = -8010535
56 feet Y = -2441611
24 meter
Z = -7146721
83 Z = -2178320
81
XDOT = 76
845809 XDOT = 23
422602
YDOT = 16235
436839 feet/sec YDOT = 4948
561149 meter/sec
ZDOT = -18041
180752 ZDOT = -5498
951893
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 11095
57866818
00016717 00000-0 10270-3 0 9068
2 25544 51
6440 173
5265 0002334 45
7190 314
4163 15
72751423 29470
Satellite: ISS
Catalog Number: 25544
Epoch time: 11095
57866818 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 173
5265 deg
Eccentricity:
0002334
Arg of perigee: 45
7190 deg
Mean anomaly: 314
4163 deg
Mean motion: 15
72751423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2947
Checksum: 312
Coasting Arc #8 (Orbit 2962)
---------------------------------------
Vector Time (GMT): 2011/096/13:13:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1461399
09 A = 6724831
84 meter
Y = -4319754
85 meter E =
0008381
Z = 4938222
68 I = 51
69952
XDOT = 7404
187026 Wp = 53
61191
YDOT = 71
401055 meter/sec RA = 167
47539 deg
ZDOT = -2121
344752 TA = 56
97357
MA = 56
89308
Ha = 192
511 n
mi
Hp = 184
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4794616
45 X = 1485605
59
Y = -14172424
05 feet Y = -4303276
98 meter
Z = 16201517
98 Z = 4945381
25
XDOT = 24291
952185 XDOT = 7413
143506
YDOT = 234
255430 feet/sec YDOT = 154
249127 meter/sec
ZDOT = -6959
792492 ZDOT = -2085
353147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3554063
71 X = -1083278
62
Y = -14500855
93 feet Y = -4419860
89 meter
Z = 16230494
26 Z = 4947054
65
XDOT = 19677
754751 XDOT = 5997
779648
YDOT = -12477
005766 feet/sec YDOT = -3802
991357 meter/sec
ZDOT = -6814
323966 ZDOT = -2077
005945
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 11096
59528773
00016717 00000-0 10270-3 0 9077
2 25544 51
6437 168
3157 0002302 44
8212 315
3136 15
72840360 29635
Satellite: ISS
Catalog Number: 25544
Epoch time: 11096
59528773 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 168
3157 deg
Eccentricity:
0002302
Arg of perigee: 44
8212 deg
Mean anomaly: 315
3136 deg
Mean motion: 15
72840360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2963
Checksum: 306
Coasting Arc #9 (Orbit 2978)
---------------------------------------
Vector Time (GMT): 2011/097/13:13:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6505538
12 A = 6734586
49 meter
Y = 829659
52 meter E =
0016703
Z = 1494687
35 I = 51
76108
XDOT = 701
835351 Wp = 59
79669
YDOT = -5018
867001 meter/sec RA = 162
38586 deg
ZDOT = 5800
825579 TA = 316
63759
MA = 316
76889
Ha = 192
759 n
mi
Hp = 184
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21343628
99 X = -6521593
00
Y = 2721980
04 feet Y = 756820
93 meter
Z = 4903829
89 Z = 1463044
17
XDOT = 2302
609420 XDOT = 729
725533
YDOT = -16466
099084 feet/sec YDOT = -5010
862496 meter/sec
ZDOT = 19031
579983 ZDOT = 5804
303052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16418599
13 X = -5004389
02
Y = 13950895
15 feet Y = 4252232
84 meter
Z = 4775913
38 Z = 1455698
40
XDOT = -6139
887149 XDOT = -1871
437603
YDOT = -13791
783549 feet/sec YDOT = -4203
735626 meter/sec
ZDOT = 19045
692356 ZDOT = 5805
127030
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 11097
61187120
00016717 00000-0 10270-3 0 9089
2 25544 51
6431 163
1041 0002716 49
8101 310
3299 15
72833035 29798
Satellite: ISS
Catalog Number: 25544
Epoch time: 11097
61187120 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 163
1041 deg
Eccentricity:
0002716
Arg of perigee: 49
8101 deg
Mean anomaly: 310
3299 deg
Mean motion: 15
72833035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2979
Checksum: 291
Coasting Arc #10 (Orbit 2993)
---------------------------------------
Vector Time (GMT): 2011/098/13:17:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1541936
30 A = 6725839
18 meter
Y = 4620962
50 meter E =
0012485
Z = -4648974
75 I = 51
76225
XDOT = -7109
459440 Wp = 99
58611
YDOT = 522
744581 meter/sec RA = 157
21739 deg
ZDOT = 2882
113734 TA = 198
89409
MA = 198
94045
Ha = 192
588 n
mi
Hp = 184
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5058846
14 X = -1570910
19
Y = 15160638
13 feet Y = 4603557
52 meter
Z = -15252541
83 Z = -4656536
01
XDOT = -23324
998164 XDOT = -7128
777339
YDOT = 1715
041276 feet/sec YDOT = 443
134351 meter/sec
ZDOT = 9455
753721 ZDOT = 2847
528860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4648782
14 X = 1416948
80
Y = 15260752
64 feet Y = 4651477
40 meter
Z = -15283165
86 Z = -4658308
95
XDOT = -17034
129624 XDOT = -5192
002709
YDOT = 14503
827662 feet/sec YDOT = 4420
766672 meter/sec
ZDOT = 9315
933104 ZDOT = 2839
496410
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 11098
56487713
00016717 00000-0 10270-3 0 9096
2 25544 51
6437 158
2181 0002662 52
4203 307
7201 15
72922589 29940
Satellite: ISS
Catalog Number: 25544
Epoch time: 11098
56487713 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 158
2181 deg
Eccentricity:
0002662
Arg of perigee: 52
4203 deg
Mean anomaly: 307
7201 deg
Mean motion: 15
72922589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2994
Checksum: 320
Coasting Arc #11 (Orbit 3009)
---------------------------------------
Vector Time (GMT): 2011/099/13:17:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6215317
49 A = 6732897
50 meter
Y = -1286827
47 meter E =
0007104
Z = -2246205
13 I = 51
81461
XDOT = -869
655494 Wp = 115
40811
YDOT = 5332
830018 meter/sec RA = 152
14151 deg
ZDOT = -5477
869999 TA = 89
70726
MA = 89
62585
Ha = 192
556 n
mi
Hp = 184
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20391461
57 X = 6240156
78
Y = -4221874
89 feet Y = -1217185
17 meter
Z = -7369439
42 Z = -2215950
71
XDOT = -2853
200439 XDOT = -902
613024
YDOT = 17496
161478 feet/sec YDOT = 5322
920632 meter/sec
ZDOT = -17972
014432 ZDOT = -5482
174941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14031833
66 X = 4276902
90
Y = -15444473
32 feet Y = -4707475
47 meter
Z = -7247099
95 Z = -2208916
07
XDOT = 6955
344312 XDOT = 2119
988946
YDOT = 14734
832555 feet/sec YDOT = 4491
176963 meter/sec
ZDOT = -17989
490204 ZDOT = -5483
196614
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 11099
58137921
00016717 00000-0 10270-3 0 9104
2 25544 51
6439 153
0059 0002736 57
1373 303
0053 15
73001157 30105
Satellite: ISS
Catalog Number: 25544
Epoch time: 11099
58137921 = yrday
fracday
Element set: 910
Inclination: 51
6439 deg
RA of node: 153
0059 deg
Eccentricity:
0002736
Arg of perigee: 57
1373 deg
Mean anomaly: 303
0053 deg
Mean motion: 15
73001157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3010
Checksum: 273
Coasting Arc #12 (Orbit 3025)
---------------------------------------
Vector Time (GMT): 2011/100/13:17:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -11411
20 A = 6724333
74 meter
Y = -4593890
60 meter E =
0009231
Z = 4905385
25 I = 51
81212
XDOT = 6961
399243 Wp = 58
45165
YDOT = -2419
702731 meter/sec RA = 146
98853 deg
ZDOT = -2242
046437 TA = 53
32440
MA = 53
23959
Ha = 192
465 n
mi
Hp = 184
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -37438
33 X = 16129
97
Y = -15071819
54 feet Y = -4593864
12 meter
Z = 16093783
63 Z = 4905396
80
XDOT = 22839
236362 XDOT = 6998
830870
YDOT = -7938
657253 feet/sec YDOT = -2341
646893 meter/sec
ZDOT = -7355
795396 ZDOT = -2208
137048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9188469
92 X = -2800645
63
Y = -11946949
29 feet Y = -3641430
14 meter
Z = 16093894
52 Z = 4905419
05
XDOT = 12606
563016 XDOT = 3842
480407
YDOT = -19454
632287 feet/sec YDOT = -5929
771921 meter/sec
ZDOT = -7218
645129 ZDOT = -2200
243035
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 11100
59784063
00016717 00000-0 10270-3 0 9114
2 25544 51
6428 147
7938 0002809 60
1471 299
9971 15
73076116 30269
Satellite: ISS
Catalog Number: 25544
Epoch time: 11100
59784063 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 147
7938 deg
Eccentricity:
0002809
Arg of perigee: 60
1471 deg
Mean anomaly: 299
9971 deg
Mean motion: 15
73076116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3026
Checksum: 317
Coasting Arc #13 (Orbit 3041)
---------------------------------------
Vector Time (GMT): 2011/101/13:17:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5832301
74 A = 6733566
78 meter
Y = 2898647
95 meter E =
0017041
Z = 1677545
07 I = 51
86873
XDOT = -852
442811 Wp = 63
73591
YDOT = -5061
170669 meter/sec RA = 141
90763 deg
ZDOT = 5744
243865 TA = 314
75181
MA = 314
89036
Ha = 192
512 n
mi
Hp = 184
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19134848
22 X = -5872430
68
Y = 9509999
82 feet Y = 2833203
28 meter
Z = 5503756
81 Z = 1649114
33
XDOT = -2796
728382 XDOT = -823
688853
YDOT = -16604
890645 feet/sec YDOT = -5070
542272 meter/sec
ZDOT = 18845
944439 ZDOT = 5740
172698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9235192
25 X = -2814886
60
Y = 19301465
52 feet Y = 5883086
69 meter
Z = 5388738
74 Z = 1642487
57
XDOT = -11115
847152 XDOT = -3388
110212
YDOT = -10610
519220 feet/sec YDOT = -3234
086258 meter/sec
ZDOT = 18829
553882 ZDOT = 5739
248023
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 11101
61426362
00016717 00000-0 10270-3 0 9124
2 25544 51
6432 142
5815 0002944 62
3700 297
7762 15
73102594 30422
Satellite: ISS
Catalog Number: 25544
Epoch time: 11101
61426362 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 142
5815 deg
Eccentricity:
0002944
Arg of perigee: 62
3700 deg
Mean anomaly: 297
7762 deg
Mean motion: 15
73102594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3042
Checksum: 280
Coasting Arc #14 (Orbit 3056)
---------------------------------------
Vector Time (GMT): 2011/102/13:17:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1415103
66 A = 6723348
12 meter
Y = 4165025
72 meter E =
0016052
Z = -5098703
41 I = 51
85898
XDOT = -6272
288186 Wp = 96
40557
YDOT = 4132
291765 meter/sec RA = 136
76584 deg
ZDOT = 1637
397200 TA = 189
29226
MA = 189
32200
Ha = 192
361 n
mi
Hp = 184
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4642728
53 X = 1393192
80
Y = 13664782
54 feet Y = 4180727
54 meter
Z = -16728029
57 Z = -5091882
28
XDOT = -20578
373313 XDOT = -6325
984221
YDOT = 13557
387680 feet/sec YDOT = 4061
851072 meter/sec
ZDOT = 5372
038057 ZDOT = 1606
796006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12288492
76 X = 3745532
59
Y = 7628518
22 feet Y = 2325172
35 meter
Z = -16700504
15 Z = -5090313
66
XDOT = -6917
734747 XDOT = -2108
525551
YDOT = 22614
042668 feet/sec YDOT = 6892
760205 meter/sec
ZDOT = 5248
210491 ZDOT = 1599
654558
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 11102
56712133
00016717 00000-0 10270-3 0 9134
2 25544 51
6438 137
6946 0002813 65
3617 294
7839 15
73158619 30570
Satellite: ISS
Catalog Number: 25544
Epoch time: 11102
56712133 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 137
6946 deg
Eccentricity:
0002813
Arg of perigee: 65
3617 deg
Mean anomaly: 294
7839 deg
Mean motion: 15
73158619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3057
Checksum: 318
Coasting Arc #15 (Orbit 3072)
---------------------------------------
Vector Time (GMT): 2011/103/13:17:40
019
Vector Time (MET): N/A
Weight (LBS) : 879245
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5065644
44 A = 6733761
54 meter
Y = -4263638
77 meter E =
0010603
Z = -1210183
24 I = 51
91496
XDOT = 2288
798277 Wp = 127
49533
YDOT = 4382
107463 meter/sec RA = 131
67820 deg
ZDOT = -5899
547354 TA = 65
70940
MA = 65
59869
Ha = 192
337 n
mi
Hp = 183
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16619568
37 X = 5118823
59
Y = -13988316
16 feet Y = -4206694
39 meter
Z = -3970417
46 Z = -1185445
04
XDOT = 7509
180699 XDOT = 2268
285387
YDOT = 14376
992989 feet/sec YDOT = 4407
587136 meter/sec
ZDOT = -19355
470320 ZDOT = -5888
478529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3753035
04 X = 1143925
08
Y = -21414547
25 feet Y = -6527154
00 meter
Z = -3870290
78 Z = -1179664
63
XDOT = 13521
610808 XDOT = 4121
386974
YDOT = 5834
662046 feet/sec YDOT = 1778
404992 meter/sec
ZDOT = -19310
766869 ZDOT = -5885
921742
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 11103
58346487
00016717 00000-0 10270-3 0 9143
2 25544 51
6425 132
4812 0002922 70
7830 289
3648 15
73229570 30730
Satellite: ISS
Catalog Number: 25544
Epoch time: 11103
58346487 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 132
4812 deg
Eccentricity:
0002922
Arg of perigee: 70
7830 deg
Mean anomaly: 289
3648 deg
Mean motion: 15
73229570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3073
Checksum: 307
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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