Date:
September 19th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 3798)
---------------------------------------
Vector Time (GMT): 2010/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1940484
26 A = 6739607
46 meter
Y = 6272705
15 meter E =
0014493
Z = -1484781
02 I = 51
96201
XDOT = -5033
874242 Wp = 20
54446
YDOT = -186
107694 meter/sec RA = 117
37977 deg
ZDOT = 5822
884982 TA = 323
19275
MA = 323
29216
Ha = 195
948 n
mi
Hp = 187
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6366418
18 X = -2003269
84
Y = 20579741
29 feet Y = 6250654
38 meter
Z = -4871328
81 Z = -1494360
56
XDOT = -16515
335440 XDOT = -5059
705356
YDOT = -610
589546 feet/sec YDOT = -242
543719 meter/sec
ZDOT = 19103
953352 ZDOT = 5798
367850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7920233
84 X = 2414087
28
Y = -20023786
22 feet Y = -6103250
04 meter
Z = -4909659
63 Z = -1496464
25
XDOT = 15070
264098 XDOT = 4593
416497
YDOT = 1325
050903 feet/sec YDOT = 403
875515 meter/sec
ZDOT = 19005
668055 ZDOT = 5792
927623
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 10260
50290982
00016717 00000-0 10270-3 0 9001
2 25544 51
6441 118
2813 0006952 359
8538
2620 15
71051715 37991
Satellite: ISS
Catalog Number: 25544
Epoch time: 10260
50290982 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 118
2813 deg
Eccentricity:
0006952
Arg of perigee: 359
8538 deg
Mean anomaly:
2620 deg
Mean motion: 15
71051715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3799
Checksum: 296
Coasting Arc #2 (Orbit 3814)
---------------------------------------
Vector Time (GMT): 2010/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4582624
29 A = 6730853
01 meter
Y = -1374153
31 meter E =
0015196
Z = -4748403
39 I = 51
94455
XDOT = -655
643970 Wp = 46
38124
YDOT = 7163
969725 meter/sec RA = 112
32268 deg
ZDOT = -2701
078713 TA = 197
07978
MA = 197
13098
Ha = 195
969 n
mi
Hp = 187
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15034856
61 X = 4620716
45
Y = -4508377
00 feet Y = -1322694
92 meter
Z = -15578751
28 Z = -4726048
58
XDOT = -2151
062894 XDOT = -722
582818
YDOT = 23503
837680 feet/sec YDOT = 7156
263503 meter/sec
ZDOT = -8861
806802 ZDOT = -2704
426778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15372753
85 X = -4685615
37
Y = 3582553
67 feet Y = 1091962
36 meter
Z = -15489145
11 Z = -4721091
43
XDOT = 3782
173112 XDOT = 1152
806365
YDOT = -22211
892377 feet/sec YDOT = -6770
184797 meter/sec
ZDOT = -8875
151768 ZDOT = -2705
146259
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 10261
52063588
00016717 00000-0 10270-3 0 9015
2 25544 51
6430 113
0774 0006895 3
2596 356
8610 15
71086343 38151
Satellite: ISS
Catalog Number: 25544
Epoch time: 10261
52063588 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 113
0774 deg
Eccentricity:
0006895
Arg of perigee: 3
2596 deg
Mean anomaly: 356
8610 deg
Mean motion: 15
71086343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3815
Checksum: 300
Coasting Arc #3 (Orbit 3830)
---------------------------------------
Vector Time (GMT): 2010/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -766729
64 A = 6735938
75 meter
Y = -5894500
94 meter E =
0014984
Z = 3163819
09 I = 51
97352
XDOT = 4989
850964 Wp = 66
09218
YDOT = -3270
477166 meter/sec RA = 107
18633 deg
ZDOT = -4860
027267 TA = 77
29093
MA = 77
12347
Ha = 195
968 n
mi
Hp = 187
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2515517
20 X = -716128
42
Y = -19338913
83 feet Y = -5902791
82 meter
Z = 10379983
88 Z = 3160217
67
XDOT = 16370
902114 XDOT = 5049
660159
YDOT = -10729
911962 feet/sec YDOT = -3214
343592 meter/sec
ZDOT = -15944
971349 ZDOT = -4835
641233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1733235
12 X = 528290
07
Y = 19432398
50 feet Y = 5922995
06 meter
Z = 10365484
31 Z = 3159399
62
XDOT = -15499
436479 XDOT = -4724
228239
YDOT = 9877
496758 feet/sec YDOT = 3010
661012 meter/sec
ZDOT = -15847
235796 ZDOT = -4830
237471
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 10262
53834242
00016717 00000-0 10270-3 0 9021
2 25544 51
6436 107
8734 0007037 6
1410 353
9837 15
71164056 38315
Satellite: ISS
Catalog Number: 25544
Epoch time: 10262
53834242 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 107
8734 deg
Eccentricity:
0007037
Arg of perigee: 6
1410 deg
Mean anomaly: 353
9837 deg
Mean motion: 15
71164056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3831
Checksum: 290
Coasting Arc #4 (Orbit 3846)
---------------------------------------
Vector Time (GMT): 2010/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3798553
49 A = 6734699
89 meter
Y = 4210762
88 meter E =
0014498
Z = 3615976
78 I = 51
97543
XDOT = -2282
094637 Wp = 65
64122
YDOT = -5872
393050 meter/sec RA = 102
14546 deg
ZDOT = 4433
038758 TA = 337
39808
MA = 337
46187
Ha = 196
146 n
mi
Hp = 187
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12462445
82 X = -3862922
38
Y = 13814838
85 feet Y = 4167925
59 meter
Z = 11863440
88 Z = 3597366
77
XDOT = -7487
187129 XDOT = -2237
793650
YDOT = -19266
381396 feet/sec YDOT = -5897
664713 meter/sec
ZDOT = 14544
090414 ZDOT = 4422
060516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12891828
77 X = 3929429
41
Y = -13480612
41 feet Y = -4108890
66 meter
Z = 11788867
54 Z = 3593246
83
XDOT = 6080
688945 XDOT = 1853
393990
YDOT = 18518
470556 feet/sec YDOT = 5644
429825 meter/sec
ZDOT = 14500
017858 ZDOT = 4419
605443
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 10263
55603287
00016717 00000-0 10270-3 0 9038
2 25544 51
6421 102
6686 0006910 10
0099 350
1199 15
71148360 38471
Satellite: ISS
Catalog Number: 25544
Epoch time: 10263
55603287 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 102
6686 deg
Eccentricity:
0006910
Arg of perigee: 10
0099 deg
Mean anomaly: 350
1199 deg
Mean motion: 15
71148360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3847
Checksum: 293
Coasting Arc #5 (Orbit 3861)
---------------------------------------
Vector Time (GMT): 2010/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3011900
40 A = 6731699
71 meter
Y = 4057525
42 meter E =
0011084
Z = -4454784
52 I = 51
96979
XDOT = -3344
782569 Wp = 72
80022
YDOT = 6089
624360 meter/sec RA = 97
00478 deg
ZDOT = 3295
049494 TA = 230
10838
MA = 230
20588
Ha = 196
136 n
mi
Hp = 187
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9881562
99 X = 2987945
07
Y = 13312091
26 feet Y = 4091071
91 meter
Z = -14615434
79 Z = -4440211
33
XDOT = -10973
696092 XDOT = -3428
636020
YDOT = 19979
082545 feet/sec YDOT = 6051
752474 meter/sec
ZDOT = 10810
529836 ZDOT = 3278
596266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9846321
35 X = -3001158
75
Y = -13401962
99 feet Y = -4084918
32 meter
Z = -14556968
74 Z = -4436964
07
XDOT = 10242
041314 XDOT = 3121
774193
YDOT = -19159
952741 feet/sec YDOT = -5839
953595 meter/sec
ZDOT = 10744
616085 ZDOT = 3274
958983
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 10264
51009967
00016717 00000-0 10270-3 0 9041
2 25544 51
6410 97
7887 0006847 14
6391 345
4968 15
71176314 38628
Satellite: ISS
Catalog Number: 25544
Epoch time: 10264
51009967 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 97
7887 deg
Eccentricity:
0006847
Arg of perigee: 14
6391 deg
Mean anomaly: 345
4968 deg
Mean motion: 15
71176314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3862
Checksum: 333
Coasting Arc #6 (Orbit 3877)
---------------------------------------
Vector Time (GMT): 2010/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1842659
74 A = 6738245
02 meter
Y = -6138734
77 meter E =
0006635
Z = -2088404
73 I = 51
99449
XDOT = 4247
933289 Wp = 75
31075
YDOT = 3166
004288 meter/sec RA = 91
95687 deg
ZDOT = -5571
205871 TA = 127
84178
MA = 127
78172
Ha = 196
152 n
mi
Hp = 186
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6045471
59 X = 1921312
38
Y = -20140205
94 feet Y = -6117689
50 meter
Z = -6851721
56 Z = -2079261
35
XDOT = 13936
789006 XDOT = 4239
278734
YDOT = 10387
153176 feet/sec YDOT = 3213
458233 meter/sec
ZDOT = -18278
234485 ZDOT = -5550
590710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5922977
20 X = -1805323
45
Y = 20188965
46 feet Y = 6153596
67 meter
Z = -6815110
04 Z = -2077245
54
XDOT = -12656
295573 XDOT = -3857
638891
YDOT = -9840
782893 feet/sec YDOT = -2999
470626 meter/sec
ZDOT = -18195
554626 ZDOT = -5546
005050
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 10265
52775215
00016717 00000-0 10270-3 0 9050
2 25544 51
6408 92
5846 0006969 18
2374 341
9036 15
71213081 38786
Satellite: ISS
Catalog Number: 25544
Epoch time: 10265
52775215 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 92
5846 deg
Eccentricity:
0006969
Arg of perigee: 18
2374 deg
Mean anomaly: 341
9036 deg
Mean motion: 15
71213081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3878
Checksum: 320
Coasting Arc #7 (Orbit 3893)
---------------------------------------
Vector Time (GMT): 2010/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4112216
93 A = 6728712
60 meter
Y = -1326596
36 meter E =
0010867
Z = 5154528
26 I = 51
96175
XDOT = 674
431125 Wp = 34
88469
YDOT = -7542
604764 meter/sec RA = 86
83509 deg
ZDOT = -1393
000233 TA = 68
45286
MA = 68
33707
Ha = 196
321 n
mi
Hp = 186
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13491525
36 X = -4122117
03
Y = -4352350
27 feet Y = -1372636
42 meter
Z = 16911181
95 Z = 5134527
05
XDOT = 2212
700540 XDOT = 765
490796
YDOT = -24746
078622 feet/sec YDOT = -7534
553883 meter/sec
ZDOT = -4570
210737 ZDOT = -1389
501797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13697303
78 X = 4174938
19
Y = 4006775
73 feet Y = 1221265
24 meter
Z = 16830980
42 Z = 5130082
83
XDOT = -1321
179702 XDOT = -402
695573
YDOT = 23796
117623 feet/sec YDOT = 7253
056652 meter/sec
ZDOT = -4556
233430 ZDOT = -1388
739950
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 10266
54538619
00016717 00000-0 10270-3 0 9069
2 25544 51
6404 87
3790 0006841 22
3867 337
7592 15
71206097 38941
Satellite: ISS
Catalog Number: 25544
Epoch time: 10266
54538619 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 87
3790 deg
Eccentricity:
0006841
Arg of perigee: 22
3867 deg
Mean anomaly: 337
7592 deg
Mean motion: 15
71206097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3894
Checksum: 334
Coasting Arc #8 (Orbit 3909)
---------------------------------------
Vector Time (GMT): 2010/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 722697
77 A = 6739964
14 meter
Y = 6683440
61 meter E =
0019331
Z = 310824
75 I = 51
99709
XDOT = -4750
826803 Wp = 40
60270
YDOT = 222
911435 meter/sec RA = 81
75799 deg
ZDOT = 6058
242069 TA = 322
75765
MA = 322
89156
Ha = 196
233 n
mi
Hp = 186
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2371055
68 X = 646398
64
Y = 21927298
58 feet Y = 6691095
67 meter
Z = 1019766
25 Z = 314149
62
XDOT = -15586
702110 XDOT = -4782
396557
YDOT = 731
336730 feet/sec YDOT = 169
608964 meter/sec
ZDOT = 19876
122273 ZDOT = 6035
085564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3294231
77 X = -1004081
84
Y = -21807084
41 feet Y = -6646799
33 meter
Z = 1033130
03 Z = 314898
03
XDOT = 14068
881722 XDOT = 4288
195149
YDOT = -1158
144509 feet/sec YDOT = -353
002446 meter/sec
ZDOT = 19783
280395 ZDOT = 6029
943864
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 10267
56299984
00016717 00000-0 10270-3 0 9072
2 25544 51
6403 82
1734 0006850 26
3746 333
7763 15
71255500 39109
Satellite: ISS
Catalog Number: 25544
Epoch time: 10267
56299984 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 82
1734 deg
Eccentricity:
0006850
Arg of perigee: 26
3746 deg
Mean anomaly: 333
7763 deg
Mean motion: 15
71255500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3910
Checksum: 315
Coasting Arc #9 (Orbit 3924)
---------------------------------------
Vector Time (GMT): 2010/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3851227
20 A = 6727958
31 meter
Y = -1659991
60 meter E =
0019685
Z = -5277304
89 I = 51
95202
XDOT = 2255
842891 Wp = 68
52115
YDOT = 7315
055219 meter/sec RA = 76
66927 deg
ZDOT = -649
619807 TA = 195
28497
MA = 195
34452
Ha = 196
261 n
mi
Hp = 186
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12635259
85 X = 3895139
90
Y = -5446166
66 feet Y = -1616679
83 meter
Z = -17313992
41 Z = -5258488
51
XDOT = 7401
059355 XDOT = 2177
032718
YDOT = 23999
524998 feet/sec YDOT = 7339
840697 meter/sec
ZDOT = -2131
298580 ZDOT = -638
852873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12390138
26 X = -3776514
14
Y = 6196894
57 feet Y = 1888813
47 meter
Z = -17238556
43 Z = -5254312
00
XDOT = -8380
203569 XDOT = -2554
286048
YDOT = -22610
946428 feet/sec YDOT = -6891
816471 meter/sec
ZDOT = -2088
107153 ZDOT = -636
455060
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 10268
51699476
00016717 00000-0 10270-3 0 9089
2 25544 51
6407 77
2942 0006894 31
2586 328
8984 15
71297323 39259
Satellite: ISS
Catalog Number: 25544
Epoch time: 10268
51699476 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 77
2942 deg
Eccentricity:
0006894
Arg of perigee: 31
2586 deg
Mean anomaly: 328
8984 deg
Mean motion: 15
71297323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3925
Checksum: 352
Coasting Arc #10 (Orbit 3940)
---------------------------------------
Vector Time (GMT): 2010/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3104575
59 A = 6738875
34 meter
Y = -5806669
35 meter E =
0015942
Z = 1417447
68 I = 51
98112
XDOT = 3677
027481 Wp = 93
56964
YDOT = -3404
815254 meter/sec RA = 71
55759 deg
ZDOT = -5839
351795 TA = 70
93666
MA = 70
76407
Ha = 196
214 n
mi
Hp = 186
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10185615
46 X = -3046299
43
Y = -19050752
46 feet Y = -5841060
63 meter
Z = 4650418
91 Z = 1402507
39
XDOT = 12063
738454 XDOT = 3743
194486
YDOT = -11170
653721 feet/sec YDOT = -3363
327011 meter/sec
ZDOT = -19157
978329 ZDOT = -5821
327499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11646280
20 X = 3549786
20
Y = 18209769
16 feet Y = 5550337
64 meter
Z = 4590511
11 Z = 1399187
79
XDOT = -9955
170458 XDOT = -3034
335955
YDOT = 11224
416484 feet/sec YDOT = 3421
202144 meter/sec
ZDOT = -19085
716870 ZDOT = -5817
326502
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 10269
53456812
00016717 00000-0 10270-3 0 9098
2 25544 51
6407 72
0884 0006935 32
6043 327
5546 15
71352334 39418
Satellite: ISS
Catalog Number: 25544
Epoch time: 10269
53456812 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 72
0884 deg
Eccentricity:
0006935
Arg of perigee: 32
6043 deg
Mean anomaly: 327
5546 deg
Mean motion: 15
71352334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3941
Checksum: 310
Coasting Arc #11 (Orbit 3956)
---------------------------------------
Vector Time (GMT): 2010/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2306016
59 A = 6729738
74 meter
Y = 4110111
06 meter E =
0010642
Z = 4794331
54 I = 51
94041
XDOT = -4627
973158 Wp = 79
97146
YDOT = -5597
387239 meter/sec RA = 66
49757 deg
ZDOT = 2569
576894 TA = 344
94999
MA = 344
98163
Ha = 196
329 n
mi
Hp = 186
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7565671
24 X = -2375095
64
Y = 13484616
34 feet Y = 4083937
83 meter
Z = 15729434
20 Z = 4782960
69
XDOT = -15183
638969 XDOT = -4577
520942
YDOT = -18364
131362 feet/sec YDOT = -5648
857775 meter/sec
ZDOT = 8430
370386 ZDOT = 2547
216662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6357953
50 X = 1937904
23
Y = -14145066
81 feet Y = -4311416
36 meter
Z = 15683841
10 Z = 4780434
77
XDOT = 15859
944032 XDOT = 4834
110941
YDOT = 16387
710748 feet/sec YDOT = 4994
974236 meter/sec
ZDOT = 8340
723876 ZDOT = 2542
252637
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 10270
55212350
00016717 00000-0 10270-3 0 9101
2 25544 51
6412 66
8832 0006850 37
5999 322
5641 15
71368926 39570
Satellite: ISS
Catalog Number: 25544
Epoch time: 10270
55212350 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 66
8832 deg
Eccentricity:
0006850
Arg of perigee: 37
5999 deg
Mean anomaly: 322
5641 deg
Mean motion: 15
71368926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3957
Checksum: 315
Coasting Arc #12 (Orbit 3971)
---------------------------------------
Vector Time (GMT): 2010/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4724308
00 A = 6735779
58 meter
Y = 3744268
06 meter E =
0011164
Z = -3004503
38 I = 51
94912
XDOT = -1346
743748 Wp = 52
69805
YDOT = 5692
833583 meter/sec RA = 61
36039 deg
ZDOT = 4996
112358 TA = 272
79738
MA = 272
92515
Ha = 196
362 n
mi
Hp = 185
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15499698
16 X = 4696683
36
Y = 12284344
02 feet Y = 3796943
53 meter
Z = -9857294
55 Z = -2981619
55
XDOT = -4418
450616 XDOT = -1434
572588
YDOT = 18677
275535 feet/sec YDOT = 5677
282600 meter/sec
ZDOT = 16391
444743 ZDOT = 4989
356209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16826020
14 X = -5128570
94
Y = -10480030
38 feet Y = -3194313
26 meter
Z = -9765552
52 Z = -2976540
41
XDOT = 1648
953397 XDOT = 502
600995
YDOT = -17836
807801 feet/sec YDOT = -5436
659018 meter/sec
ZDOT = 16364
341497 ZDOT = 4987
851288
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 10271
50606271
00016717 00000-0 10270-3 0 9117
2 25544 51
6427 62
0041 0006922 42
3836 317
7860 15
71386055 39729
Satellite: ISS
Catalog Number: 25544
Epoch time: 10271
50606271 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 62
0041 deg
Eccentricity:
0006922
Arg of perigee: 42
3836 deg
Mean anomaly: 317
7860 deg
Mean motion: 15
71386055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3972
Checksum: 290
Coasting Arc #13 (Orbit 3987)
---------------------------------------
Vector Time (GMT): 2010/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -62189
70 A = 6733103
93 meter
Y = -5533001
51 meter E =
0012969
Z = -3851181
29 I = 51
92532
XDOT = 5805
865164 Wp = 58
99301
YDOT = 2829
976277 meter/sec RA = 56
31546 deg
ZDOT = -4163
359466 TA = 167
53169
MA = 167
49957
Ha = 196
311 n
mi
Hp = 185
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -204034
45 X = 18394
57
Y = -18152892
09 feet Y = -5533246
48 meter
Z = -12635109
20 Z = -3851287
52
XDOT = 19048
114056 XDOT = 5794
013467
YDOT = 9284
699071 feet/sec YDOT = 2894
834572 meter/sec
ZDOT = -13659
315834 ZDOT = -4135
183046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2454288
76 X = 748067
22
Y = 17987090
00 feet Y = 5482465
03 meter
Z = -12635512
09 Z = -3851304
08
XDOT = -18849
224688 XDOT = -5745
243685
YDOT = -6935
381040 feet/sec YDOT = -2113
904141 meter/sec
ZDOT = -13546
352335 ZDOT = -4128
928192
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 10272
52357642
00016717 00000-0 10270-3 0 9126
2 25544 51
6430 56
7992 0006995 45
3728 314
8004 15
71423723 39880
Satellite: ISS
Catalog Number: 25544
Epoch time: 10272
52357642 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 56
7992 deg
Eccentricity:
0006995
Arg of perigee: 45
3728 deg
Mean anomaly: 314
8004 deg
Mean motion: 15
71423723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3988
Checksum: 320
Coasting Arc #14 (Orbit 4003)
---------------------------------------
Vector Time (GMT): 2010/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5134300
05 A = 6731977
36 meter
Y = -1131752
96 meter E =
0016848
Z = 4196286
89 I = 51
90344
XDOT = -1579
943867 Wp = 64
26336
YDOT = -6573
212871 meter/sec RA = 51
16797 deg
ZDOT = -3687
366305 TA = 63
30080
MA = 63
12841
Ha = 196
453 n
mi
Hp = 185
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16844816
44 X = -5141647
99
Y = -3713100
26 feet Y = -1189208
78 meter
Z = 13767345
42 Z = 4171326
38
XDOT = -5183
542871 XDOT = -1488
410822
YDOT = -21565
659025 feet/sec YDOT = -6590
369044 meter/sec
ZDOT = -12097
658480 ZDOT = -3694
819269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17285898
23 X = 5268741
78
Y = 1215842
43 feet Y = 370588
77 meter
Z = 13667267
61 Z = 4165783
17
XDOT = 8277
287709 XDOT = 2522
917294
YDOT = 19334
881864 feet/sec YDOT = 5893
271992 meter/sec
ZDOT = -12127
506992 ZDOT = -3696
464131
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 10273
54106973
00016717 00000-0 10270-3 0 9139
2 25544 51
6429 51
5936 0006965 49
6461 310
5308 15
71427468 40047
Satellite: ISS
Catalog Number: 25544
Epoch time: 10273
54106973 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 51
5936 deg
Eccentricity:
0006965
Arg of perigee: 49
6461 deg
Mean anomaly: 310
5308 deg
Mean motion: 15
71427468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 310
Coasting Arc #15 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2010/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2682879
85 A = 6736490
55 meter
Y = 5632388
51 meter E =
0020341
Z = 2513275
54 I = 51
90099
XDOT = -5555
226702 Wp = 68
03738
YDOT = 254
942555 meter/sec RA = 46
11710 deg
ZDOT = 5332
031176 TA = 320
31122
MA = 320
45990
Ha = 196
228 n
mi
Hp = 185
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8802099
26 X = 2607488
93
Y = 18478964
92 feet Y = 5661968
62 meter
Z = 8245654
66 Z = 2526125
77
XDOT = -18225
809390 XDOT = -5583
566841
YDOT = 836
425705 feet/sec YDOT = 192
662365 meter/sec
ZDOT = 17493
540605 ZDOT = 5304
974875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11634184
02 X = -3546099
29
Y = -16814964
73 feet Y = -5125201
25 meter
Z = 8297146
48 Z = 2528970
25
XDOT = 16724
712584 XDOT = 5097
692396
YDOT = -2950
269811 feet/sec YDOT = -899
242238 meter/sec
ZDOT = 17385
048454 ZDOT = 5298
962769
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 10274
55853863
00016717 00000-0 10270-3 0 9149
2 25544 51
6442 46
3887 0006913 53
0416 307
1378 15
71514537 40202
Satellite: ISS
Catalog Number: 25544
Epoch time: 10274
55853863 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node: 46
3887 deg
Eccentricity:
0006913
Arg of perigee: 53
0416 deg
Mean anomaly: 307
1378 deg
Mean motion: 15
71514537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 305
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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