Date:
July 16th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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
197/07:51:23
675 4
3 6
0 6
1
N/A 1
7 -0
7 197
4
000/00:17:47
351 -4
0 -0
2 185
4
Coasting Arc #1 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2010/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3808768
58 A = 6726570
52 meter
Y = 2684620
78 meter E =
0020806
Z = -4869185
89 I = 51
97283
XDOT = -1887
166029 Wp = 92
67874
YDOT = 7044
844476 meter/sec RA = 89
98242 deg
ZDOT = 2415
865911 TA = 200
80606
MA = 200
89087
Ha = 196
047 n
mi
Hp = 182
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12495959
90 X = 3802118
72
Y = 8807810
96 feet Y = 2727176
04 meter
Z = -15975019
34 Z = -4850699
14
XDOT = -6191
489597 XDOT = -1977
538104
YDOT = 23113
006812 feet/sec YDOT = 7023
235506 meter/sec
ZDOT = 7926
069261 ZDOT = 2406
479480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3587841
05 X = 1093573
95
Y = -14940214
46 feet Y = -4553777
37 meter
Z = -15901106
22 Z = -4846657
18
XDOT = 22703
238175 XDOT = 6919
946996
YDOT = -2916
177710 feet/sec YDOT = -888
850966 meter/sec
ZDOT = 7888
548714 ZDOT = 2404
429648
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 10195
51176443
00016717 00000-0 10270-3 0 9004
2 25544 51
6477 90
7181 0009668 74
3557 285
8671 15
72402376 27775
Satellite: ISS
Catalog Number: 25544
Epoch time: 10195
51176443 = yrday
fracday
Element set: 900
Inclination: 51
6477 deg
RA of node: 90
7181 deg
Eccentricity:
0009668
Arg of perigee: 74
3557 deg
Mean anomaly: 285
8671 deg
Mean motion: 15
72402376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 333
Coasting Arc #2 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2010/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 724915
79 A = 6735558
75 meter
Y = -6487609
90 meter E =
0014796
Z = -1659995
10 I = 52
00183
XDOT = 4694
938122 Wp = 107
10784
YDOT = 1986
788592 meter/sec RA = 84
91713 deg
ZDOT = -5760
697017 TA = 91
11638
MA = 90
94686
Ha = 196
029 n
mi
Hp = 182
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2378332
64 X = 805471
37
Y = -21284809
39 feet Y = -6479052
91 meter
Z = -5446178
15 Z = -1656278
42
XDOT = 15403
340296 XDOT = 4700
356515
YDOT = 6518
335275 feet/sec YDOT = 2039
320995 meter/sec
ZDOT = -18899
924595 ZDOT = -5737
876045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20591764
01 X = -6276369
67
Y = 5902579
33 feet Y = 1799106
18 meter
Z = -5431320
81 Z = -1655466
58
XDOT = 527
650212 XDOT = 160
827785
YDOT = -15326
459214 feet/sec YDOT = -4671
504768 meter/sec
ZDOT = -18808
682657 ZDOT = -5732
886474
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 10196
52862537
00016717 00000-0 10270-3 0 9013
2 25544 51
6476 85
5084 0009533 78
8559 281
3674 15
72392446 27938
Satellite: ISS
Catalog Number: 25544
Epoch time: 10196
52862537 = yrday
fracday
Element set: 901
Inclination: 51
6476 deg
RA of node: 85
5084 deg
Eccentricity:
0009533
Arg of perigee: 78
8559 deg
Mean anomaly: 281
3674 deg
Mean motion: 15
72392446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2793
Checksum: 345
Coasting Arc #3 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2010/197/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2987336
67 A = 6731260
31 meter
Y = -3937182
81 meter E =
0017071
Z = -4584716
41 I = 51
96868
XDOT = 3434
777927 Wp = 88
69348
YDOT = 6155
736105 meter/sec RA = 80
67175 deg
ZDOT = -3057
624248 TA = 151
00924
MA = 150
91433
Ha = 197
361 n
mi
Hp = 185
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9800973
31 X = 3053412
38
Y = -12917266
45 feet Y = -3903406
80 meter
Z = -15041720
49 Z = -4570043
93
XDOT = 11268
956455 XDOT = 3380
541284
YDOT = 20195
984598 feet/sec YDOT = 6193
842842 meter/sec
ZDOT = -10031
575616 ZDOT = -3041
069537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4460364
60 X = -1359519
13
Y = -15645491
02 feet Y = -4768745
66 meter
Z = -14983055
89 Z = -4566835
44
XDOT = 21824
051708 XDOT = 6651
970961
YDOT = 3292
116636 feet/sec YDOT = 1003
437151 meter/sec
ZDOT = -9965
389825 ZDOT = -3037
450819
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 10197
35483207
00016717 00000-0 10270-3 0 9029
2 25544 51
6438 81
2740 0008111 113
0231 247
1787 15
71159195 28069
Satellite: ISS
Catalog Number: 25544
Epoch time: 10197
35483207 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 81
2740 deg
Eccentricity:
0008111
Arg of perigee: 113
0231 deg
Mean anomaly: 247
1787 deg
Mean motion: 15
71159195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 292
Coasting Arc #4 (Orbit 2821)
---------------------------------------
Vector Time (GMT): 2010/198/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3876620
33 A = 6735181
10 meter
Y = -4294122
17 meter E =
0019978
Z = 3428621
58 I = 51
97634
XDOT = 2251
906280 Wp = 99
99336
YDOT = -5738
621957 meter/sec RA = 75
53391 deg
ZDOT = -4621
849339 TA = 39
67483
MA = 39
52884
Ha = 197
341 n
mi
Hp = 185
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12718570
63 X = -3844970
04
Y = -14088327
32 feet Y = -4337296
18 meter
Z = 11248758
46 Z = 3409865
61
XDOT = 7388
143963 XDOT = 2338
361154
YDOT = -18827
499859 feet/sec YDOT = -5712
955999 meter/sec
ZDOT = -15163
547701 ZDOT = -4610
700168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18899776
25 X = -5760651
80
Y = 2173190
10 feet Y = 662388
34 meter
Z = 11173776
22 Z = 3405766
99
XDOT = -10778
423564 XDOT = -3285
263502
YDOT = -15674
487995 feet/sec YDOT = -4777
583941 meter/sec
ZDOT = -15118
961027 ZDOT = -4608
259321
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 10198
37249997
00016717 00000-0 10270-3 0 9039
2 25544 51
6443 76
0704 0008032 116
7201 243
4784 15
71179772 28223
Satellite: ISS
Catalog Number: 25544
Epoch time: 10198
37249997 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 76
0704 deg
Eccentricity:
0008032
Arg of perigee: 116
7201 deg
Mean anomaly: 243
4784 deg
Mean motion: 15
71179772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2822
Checksum: 316
Coasting Arc #5 (Orbit 2837)
---------------------------------------
Vector Time (GMT): 2010/199/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -743877
76 A = 6735287
11 meter
Y = 5780094
98 meter E =
0019901
Z = 3363959
71 I = 51
96846
XDOT = -5085
982719 Wp = 101
39308
YDOT = -3394
137157 meter/sec RA = 70
49393 deg
ZDOT = 4680
237241 TA = 298
00339
MA = 298
20459
Ha = 197
217 n
mi
Hp = 185
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2440543
84 X = -824797
97
Y = 18963566
21 feet Y = 5771323
70 meter
Z = 11036613
23 Z = 3360150
00
XDOT = -16686
295009 XDOT = -5070
386487
YDOT = -11135
620595 feet/sec YDOT = -3450
924924 meter/sec
ZDOT = 15355
109060 ZDOT = 4655
567199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14169305
31 X = 4318804
26
Y = 12850692
92 feet Y = 3916891
20 meter
Z = 11021361
42 Z = 3359310
96
XDOT = -17765
561306 XDOT = -5414
943086
YDOT = 6427
621699 feet/sec YDOT = 1959
139094 meter/sec
ZDOT = 15256
484117 ZDOT = 4650
176359
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 10199
39015461
00016717 00000-0 10270-3 0 9040
2 25544 51
6445 70
8666 0008020 120
7750 239
4203 15
71193446 28387
Satellite: ISS
Catalog Number: 25544
Epoch time: 10199
39015461 = yrday
fracday
Element set: 904
Inclination: 51
6445 deg
RA of node: 70
8666 deg
Eccentricity:
0008020
Arg of perigee: 120
7750 deg
Mean anomaly: 239
4203 deg
Mean motion: 15
71193446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2838
Checksum: 301
Coasting Arc #6 (Orbit 2852)
---------------------------------------
Vector Time (GMT): 2010/200/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4674445
69 A = 6731033
10 meter
Y = 1525090
24 meter E =
0018141
Z = -4614612
01 I = 51
94359
XDOT = 654
476557 Wp = 115
90645
YDOT = 7044
270560 meter/sec RA = 65
35435 deg
ZDOT = 2992
364793 TA = 183
73921
MA = 183
75278
Ha = 197
099 n
mi
Hp = 185
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15336107
92 X = 4679461
30
Y = 5003576
89 feet Y = 1577391
28 meter
Z = -15139803
19 Z = -4591891
27
XDOT = 2147
232797 XDOT = 561
121287
YDOT = 23111
123883 feet/sec YDOT = 7051
066971 meter/sec
ZDOT = 9817
469792 ZDOT = 2995
318313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12719868
39 X = 3877015
88
Y = -10058786
34 feet Y = -3065918
08 meter
Z = -15048966
55 Z = -4586925
00
XDOT = 19654
587510 XDOT = 5990
718273
YDOT = 10155
291644 feet/sec YDOT = 3095
332893 meter/sec
ZDOT = 9829
242306 ZDOT = 2995
953055
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 10200
34419369
00016717 00000-0 10270-3 0 9054
2 25544 51
6450 65
9875 0007932 123
9805 236
2111 15
71213780 28531
Satellite: ISS
Catalog Number: 25544
Epoch time: 10200
34419369 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 65
9875 deg
Eccentricity:
0007932
Arg of perigee: 123
9805 deg
Mean anomaly: 236
2111 deg
Mean motion: 15
71213780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2853
Checksum: 299
Coasting Arc #7 (Orbit 2868)
---------------------------------------
Vector Time (GMT): 2010/201/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1900142
01 A = 6738626
92 meter
Y = -6200219
55 meter E =
0015086
Z = -1816424
38 I = 51
95660
XDOT = 5173
314301 Wp = 134
28076
YDOT = 72
102972 meter/sec RA = 60
30060 deg
ZDOT = -5697
088032 TA = 65
74756
MA = 65
59001
Ha = 197
015 n
mi
Hp = 185
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6234061
70 X = -1821844
98
Y = -20341927
67 feet Y = -6221030
04 meter
Z = -5959397
57 Z = -1825465
90
XDOT = 16972
815948 XDOT = 5199
798825
YDOT = 236
558307 feet/sec YDOT = 130
102932 meter/sec
ZDOT = -18691
233702 ZDOT = -5671
891849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20466123
99 X = -6238074
59
Y = -5776126
17 feet Y = -1760563
26 meter
Z = -5995506
76 Z = -1827430
46
XDOT = 9008
251524 XDOT = 2745
715064
YDOT = -12754
473948 feet/sec YDOT = -3887
563659 meter/sec
ZDOT = -18590
488747 ZDOT = -5666
380970
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 10201
36182266
00016717 00000-0 10270-3 0 9061
2 25544 51
6459 60
7835 0007894 128
0418 232
1457 15
71227324 28696
Satellite: ISS
Catalog Number: 25544
Epoch time: 10201
36182266 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 60
7835 deg
Eccentricity:
0007894
Arg of perigee: 128
0418 deg
Mean anomaly: 232
1457 deg
Mean motion: 15
71227324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2869
Checksum: 311
Coasting Arc #8 (Orbit 2884)
---------------------------------------
Vector Time (GMT): 2010/202/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4024003
01 A = 6728217
93 meter
Y = 1365279
79 meter E =
0009412
Z = 5208466
96 I = 51
90574
XDOT = -3647
158694 Wp = 108
76585
YDOT = -6702
484467 meter/sec RA = 55
18178 deg
ZDOT = -1062
263250 TA = 351
31636
MA = 351
33263
Ha = 196
956 n
mi
Hp = 185
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13202109
60 X = -4064272
33
Y = 4479264
40 feet Y = 1320055
04 meter
Z = 17088146
18 Z = 5188820
89
XDOT = -11965
743746 XDOT = -3566
778984
YDOT = -21989
778434 feet/sec YDOT = -6742
819585 meter/sec
ZDOT = -3485
115648 ZDOT = -1079
786787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3184131
45 X = -970523
27
Y = 13671130
63 feet Y = 4166960
62 meter
Z = 17009577
94 Z = 5184519
35
XDOT = -23988
507311 XDOT = -7311
697028
YDOT = -1169
651054 feet/sec YDOT = -356
509641 meter/sec
ZDOT = -3555
129078 ZDOT = -1083
603343
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 10202
37943712
00016717 00000-0 10270-3 0 9075
2 25544 51
6456 55
5800 0007730 131
9557 228
2265 15
71286796 28852
Satellite: ISS
Catalog Number: 25544
Epoch time: 10202
37943712 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 55
5800 deg
Eccentricity:
0007730
Arg of perigee: 131
9557 deg
Mean anomaly: 228
2265 deg
Mean motion: 15
71286796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2885
Checksum: 321
Coasting Arc #9 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2010/203/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4307280
86 A = 6739965
90 meter
Y = 5181117
92 meter E =
0014669
Z = 24934
40 I = 51
92722
XDOT = -3669
267703 Wp = 77
39856
YDOT = 3006
971018 meter/sec RA = 50
09574 deg
ZDOT = 6055
853552 TA = 282
87079
MA = 283
03462
Ha = 196
825 n
mi
Hp = 185
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14131498
87 X = 4248903
40
Y = 16998418
36 feet Y = 5228958
09 meter
Z = 81805
78 Z = 45717
94
XDOT = -12038
279865 XDOT = -3732
037380
YDOT = 9865
390480 feet/sec YDOT = 2965
587161 meter/sec
ZDOT = 19868
285932 ZDOT = 6037
876466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21832703
26 X = 6654607
95
Y = -3458043
82 feet Y = -1054011
76 meter
Z = 164865
27 Z = 50250
94
XDOT = 2015
337205 XDOT = 614
274780
YDOT = 13898
480979 feet/sec YDOT = 4236
257003 meter/sec
ZDOT = 19796
370671 ZDOT = 6033
933780
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 10203
39704081
00016717 00000-0 10270-3 0 9083
2 25544 51
6459 50
3756 0007738 135
1954 224
9834 15
71266019 29013
Satellite: ISS
Catalog Number: 25544
Epoch time: 10203
39704081 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 50
3756 deg
Eccentricity:
0007738
Arg of perigee: 135
1954 deg
Mean anomaly: 224
9834 deg
Mean motion: 15
71266019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 310
Coasting Arc #10 (Orbit 2915)
---------------------------------------
Vector Time (GMT): 2010/204/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2154518
66 A = 6728060
39 meter
Y = -3658138
88 meter E =
0019972
Z = -5235702
59 I = 51
86792
XDOT = 5894
876241 Wp = 101
20220
YDOT = 4832
823334 meter/sec RA = 45
00638 deg
ZDOT = -957
738868 TA = 159
71856
MA = 159
63912
Ha = 196
691 n
mi
Hp = 185
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7068630
78 X = 2220698
19
Y = -12001767
99 feet Y = -3633674
94 meter
Z = -17177501
94 Z = -5225075
92
XDOT = 19340
145148 XDOT = 5845
049056
YDOT = 15855
719599 feet/sec YDOT = 4898
464908 meter/sec
ZDOT = -3142
187888 ZDOT = -929
222304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6862273
63 X = -2091621
00
Y = -12180993
36 feet Y = -3712766
78 meter
Z = -17134968
65 Z = -5222738
44
XDOT = 22483
673179 XDOT = 6853
023585
YDOT = -8438
359673 feet/sec YDOT = -2572
012028 meter/sec
ZDOT = -3028
201059 ZDOT = -922
995683
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 10204
35103004
00016717 00000-0 10270-3 0 9099
2 25544 51
6466 45
4964 0007710 138
7466 221
4280 15
71310892 29166
Satellite: ISS
Catalog Number: 25544
Epoch time: 10204
35103004 = yrday
fracday
Element set: 909
Inclination: 51
6466 deg
RA of node: 45
4964 deg
Eccentricity:
0007710
Arg of perigee: 138
7466 deg
Mean anomaly: 221
4280 deg
Mean motion: 15
71310892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2916
Checksum: 289
Coasting Arc #11 (Orbit 2931)
---------------------------------------
Vector Time (GMT): 2010/205/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5741058
24 A = 6738736
00 meter
Y = -3075242
54 meter E =
0021311
Z = 1684450
08 I = 51
88096
XDOT = 1001
237923 Wp = 125
30524
YDOT = -5036
302980 meter/sec RA = 39
88474 deg
ZDOT = -5743
516364 TA = 36
13611
MA = 35
99228
Ha = 196
715 n
mi
Hp = 185
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18835492
90 X = -5714426
22
Y = -10089378
41 feet Y = -3139293
81 meter
Z = 5526411
02 Z = 1656624
82
XDOT = 3284
901321 XDOT = 1085
380773
YDOT = -16523
303741 feet/sec YDOT = -5024
635254 meter/sec
ZDOT = -18843
557625 ZDOT = -5738
448784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17923818
79 X = -5463179
97
Y = 11684401
84 feet Y = 3561405
68 meter
Z = 5415167
77 Z = 1650543
13
XDOT = -11998
401050 XDOT = -3657
112640
YDOT = -9621
912385 feet/sec YDOT = -2932
758895 meter/sec
ZDOT = -18823
237970 ZDOT = -5737
322933
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 10205
36860723
00016717 00000-0 10270-3 0 9101
2 25544 51
6462 40
2920 0007765 142
9785 217
1914 15
71286555 29320
Satellite: ISS
Catalog Number: 25544
Epoch time: 10205
36860723 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 40
2920 deg
Eccentricity:
0007765
Arg of perigee: 142
9785 deg
Mean anomaly: 217
1914 deg
Mean motion: 15
71286555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2932
Checksum: 305
Coasting Arc #12 (Orbit 2947)
---------------------------------------
Vector Time (GMT): 2010/206/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 525538
52 A = 6730356
78 meter
Y = 4825123
91 meter E =
0015084
Z = 4657303
66 I = 51
82977
XDOT = -6854
901649 Wp = 130
68897
YDOT = -2029
267533 meter/sec RA = 34
82148 deg
ZDOT = 2860
260279 TA = 291
03393
MA = 291
19520
Ha = 196
472 n
mi
Hp = 186
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1724207
73 X = 448920
21
Y = 15830459
02 feet Y = 4830571
81 meter
Z = 15279867
65 Z = 4659671
17
XDOT = -22489
834808 XDOT = -6845
594855
YDOT = -6657
701879 feet/sec YDOT = -2105
871460 meter/sec
ZDOT = 9384
056035 ZDOT = 2826
982259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14767828
72 X = 4501234
19
Y = 5932934
44 feet Y = 1808358
42 meter
Z = 15289283
97 Z = 4660173
75
XDOT = -15965
069711 XDOT = -4866
153248
YDOT = 15766
881644 feet/sec YDOT = 4805
745525 meter/sec
ZDOT = 9250
992431 ZDOT = 2819
702493
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 10206
38616908
00016717 00000-0 10270-3 0 9119
2 25544 51
6465 35
0873 0007574 146
3716 213
7928 15
71331425 29483
Satellite: ISS
Catalog Number: 25544
Epoch time: 10206
38616908 = yrday
fracday
Element set: 911
Inclination: 51
6465 deg
RA of node: 35
0873 deg
Eccentricity:
0007574
Arg of perigee: 146
3716 deg
Mean anomaly: 213
7928 deg
Mean motion: 15
71331425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2948
Checksum: 316
Coasting Arc #13 (Orbit 2962)
---------------------------------------
Vector Time (GMT): 2010/207/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5900948
38 A = 6735283
42 meter
Y = 438488
84 meter E =
0009913
Z = -3230505
69 I = 51
82099
XDOT = 2204
361686 Wp = 124
48283
YDOT = 5591
279748 meter/sec RA = 29
67267 deg
ZDOT = 4790
392073 TA = 197
95742
MA = 197
99247
Ha = 196
293 n
mi
Hp = 186
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19360066
86 X = 5911299
39
Y = 1438611
67 feet Y = 504534
98 meter
Z = -10598771
95 Z = -3201814
36
XDOT = 7232
157764 XDOT = 2118
404833
YDOT = 18344
093661 feet/sec YDOT = 5615
449119 meter/sec
ZDOT = 15716
509426 ZDOT = 4800
892420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10039195
82 X = 3059946
89
Y = -16688779
15 feet Y = -5086739
88 meter
Z = -10484033
44 Z = -3195533
39
XDOT = 18376
185044 XDOT = 5601
061201
YDOT = 1164
895623 feet/sec YDOT = 355
060186 meter/sec
ZDOT = 15758
443479 ZDOT = 4803
173572
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 10207
34012103
00016717 00000-0 10270-3 0 9124
2 25544 51
6466 30
2076 0007377 150
6624 209
4954 15
71358105 29635
Satellite: ISS
Catalog Number: 25544
Epoch time: 10207
34012103 = yrday
fracday
Element set: 912
Inclination: 51
6466 deg
RA of node: 30
2076 deg
Eccentricity:
0007377
Arg of perigee: 150
6624 deg
Mean anomaly: 209
4954 deg
Mean motion: 15
71358105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2963
Checksum: 283
Coasting Arc #14 (Orbit 2978)
---------------------------------------
Vector Time (GMT): 2010/208/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3261651
17 A = 6733916
74 meter
Y = -4639996
10 meter E =
0010253
Z = -3632373
75 I = 51
78975
XDOT = 6237
600706 Wp = 123
10526
YDOT = -951
595545 meter/sec RA = 24
61919 deg
ZDOT = -4399
811296 TA = 100
23862
MA = 100
12299
Ha = 196
136 n
mi
Hp = 186
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10700955
28 X = -3191878
47
Y = -15223084
32 feet Y = -4676079
40 meter
Z = -11917236
71 Z = -3648049
41
XDOT = 20464
569246 XDOT = 6269
151025
YDOT = -3122
032629 feet/sec YDOT = -881
666182 meter/sec
ZDOT = -14435
076432 ZDOT = -4369
433174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18333015
39 X = -5587903
09
Y = 2942162
26 feet Y = 896771
06 meter
Z = -11979878
92 Z = -3651467
10
XDOT = 6350
075250 XDOT = 1935
502936
YDOT = -18522
487353 feet/sec YDOT = -5645
654145 meter/sec
ZDOT = -14313
578629 ZDOT = -4362
778766
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 10208
35765707
00016717 00000-0 10270-3 0 9132
2 25544 51
6465 25
0026 0007315 155
8284 204
3222 15
71360776 29798
Satellite: ISS
Catalog Number: 25544
Epoch time: 10208
35765707 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 25
0026 deg
Eccentricity:
0007315
Arg of perigee: 155
8284 deg
Mean anomaly: 204
3222 deg
Mean motion: 15
71360776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2979
Checksum: 304
Coasting Arc #15 (Orbit 2994)
---------------------------------------
Vector Time (GMT): 2010/209/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4695501
35 A = 6731240
84 meter
Y = 1999845
76 meter E =
0012076
Z = 4377019
39 I = 51
75361
XDOT = -5134
301213 Wp = 106
28771
YDOT = -4642
251345 meter/sec RA = 19
46326 deg
ZDOT = -3382
509912 TA = 17
72353
MA = 17
68144
Ha = 196
029 n
mi
Hp = 186
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15405188
15 X = -4738777
33
Y = 6561173
76 feet Y = 1947095
60 meter
Z = 14360299
84 Z = 4354104
14
XDOT = -16844
820252 XDOT = -5065
577844
YDOT = -15230
483414 feet/sec YDOT = -4699
281689 meter/sec
ZDOT = -11097
473464 ZDOT = -3407
285210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -547473
98 X = -166870
07
Y = 16813483
59 feet Y = 5124749
80 meter
Z = 14268639
61 Z = 4349081
35
XDOT = -19641
594366 XDOT = -5986
757963
YDOT = 8874
447338 feet/sec YDOT = 2704
931549 meter/sec
ZDOT = -11196
505782 ZDOT = -3412
694962
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 10209
37517851
00016717 00000-0 10270-3 0 9141
2 25544 51
6469 19
7977 0007131 158
9578 201
1879 15
71443141 29952
Satellite: ISS
Catalog Number: 25544
Epoch time: 10209
37517851 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 19
7977 deg
Eccentricity:
0007131
Arg of perigee: 158
9578 deg
Mean anomaly: 201
1879 deg
Mean motion: 15
71443141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2995
Checksum: 337
Coasting Arc #16 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2010/210/08:00:17
351
Vector Time (MET): N/A
Weight (LBS) : 828082
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5492752
97 A = 6737335
61 meter
Y = 3209109
84 meter E =
0015570
Z = 2209892
54 I = 51
74473
XDOT = -4200
399667 Wp = 98
62108
YDOT = 3387
512404 meter/sec RA = 14
39840 deg
ZDOT = 5485
951691 TA = 286
08011
MA = 286
25149
Ha = 195
830 n
mi
Hp = 186
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18020843
09 X = 5445724
82
Y = 10528575
58 feet Y = 3270270
02 meter
Z = 7250303
59 Z = 2236461
79
XDOT = -13780
838803 XDOT = -4264
616548
YDOT = 11113
885840 feet/sec YDOT = 3340
181681 meter/sec
ZDOT = 17998
529169 ZDOT = 5465
390712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16896134
75 X = 5149941
87
Y = -12188962
87 feet Y = -3715195
88 meter
Z = 7356521
34 Z = 2242267
70
XDOT = 3665
194139 XDOT = 1117
151174
YDOT = 15962
244856 feet/sec YDOT = 4865
292232 meter/sec
ZDOT = 17916
273716 ZDOT = 5460
880229
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 10210
39268798
00016717 00000-0 10270-3 0 9159
2 25544 51
6463 14
5922 0007129 163
3137 196
8260 15
71426863 30113
Satellite: ISS
Catalog Number: 25544
Epoch time: 10210
39268798 = yrday
fracday
Element set: 915
Inclination: 51
6463 deg
RA of node: 14
5922 deg
Eccentricity:
0007129
Arg of perigee: 163
3137 deg
Mean anomaly: 196
8260 deg
Mean motion: 15
71426863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3011
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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