Date:
March 17th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 29062 56 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
There are no maneuvers
Coasting Arc #1 (Orbit 871)
---------------------------------------
Vector Time (GMT): 2010/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6538189
47 A = 6731013
51 meter
Y = -248415
83 meter E =
0010652
Z = -1586131
66 I = 51
61275
XDOT = 1572
175199 Wp = 96
13892
YDOT = -4859
805074 meter/sec RA = 351
10333 deg
ZDOT = -5753
640391 TA = 101
35291
MA = 101
23323
Ha = 192
604 n
mi
Hp = 181
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21450752
85 X = -6527220
65
Y = -815012
57 feet Y = -321468
61 meter
Z = -5203844
04 Z = -1617867
16
XDOT = 5158
055114 XDOT = 1654
351398
YDOT = -15944
242368 feet/sec YDOT = -4841
765280 meter/sec
ZDOT = -18876
772936 ZDOT = -5745
802676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21111703
12 X = -6434847
11
Y = -3710425
48 feet Y = -1130937
69 meter
Z = -5329894
04 Z = -1624551
70
XDOT = 7110
633445 XDOT = 2167
321074
YDOT = -13544
031516 feet/sec YDOT = -4128
220806 meter/sec
ZDOT = -18845
747513 ZDOT = -5744
183842
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 10074
52864055
00016717 00000-0 10270-3 0 9004
2 25544 51
6478 351
4487 0007679 48
5410 311
6411 15
74002968 8722
Satellite: ISS
Catalog Number: 25544
Epoch time: 10074
52864055 = yrday
fracday
Element set: 900
Inclination: 51
6478 deg
RA of node: 351
4487 deg
Eccentricity:
0007679
Arg of perigee: 48
5410 deg
Mean anomaly: 311
6411 deg
Mean motion: 15
74002968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 872
Checksum: 310
Coasting Arc #2 (Orbit 887)
---------------------------------------
Vector Time (GMT): 2010/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1028214
08 A = 6721021
09 meter
Y = 4356193
85 meter E =
0013285
Z = 5007004
20 I = 51
54961
XDOT = -7474
727582 Wp = 52
51457
YDOT = 365
374795 meter/sec RA = 345
93386 deg
ZDOT = -1841
573458 TA = 55
31314
MA = 55
18803
Ha = 192
551 n
mi
Hp = 181
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3373405
77 X = -1101172
37
Y = 14291974
58 feet Y = 4344288
41 meter
Z = 16427179
12 Z = 5001831
43
XDOT = -24523
384455 XDOT = -7469
311752
YDOT = 1198
736203 feet/sec YDOT = 281
818011 meter/sec
ZDOT = -6041
907671 ZDOT = -1877
872338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5138564
62 X = -1566234
50
Y = 13780675
03 feet Y = 4200349
75 meter
Z = 16406729
32 Z = 5000771
10
XDOT = -23452
093006 XDOT = -7148
197948
YDOT = -1335
852370 feet/sec YDOT = -407
167802 meter/sec
ZDOT = -6186
060103 ZDOT = -1885
511119
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 10075
54444932
00016717 00000-0 10270-3 0 9016
2 25544 51
6473 346
2329 0007653 51
3781 308
8066 15
74087993 8881
Satellite: ISS
Catalog Number: 25544
Epoch time: 10075
54444932 = yrday
fracday
Element set: 901
Inclination: 51
6473 deg
RA of node: 346
2329 deg
Eccentricity:
0007653
Arg of perigee: 51
3781 deg
Mean anomaly: 308
8066 deg
Mean motion: 15
74087993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 888
Checksum: 331
Coasting Arc #3 (Orbit 903)
---------------------------------------
Vector Time (GMT): 2010/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6459316
57 A = 6730699
38 meter
Y = -872271
98 meter E =
0021759
Z = 1634952
34 I = 51
55376
XDOT = -775
996719 Wp = 60
51689
YDOT = 5090
745285 meter/sec RA = 340
82246 deg
ZDOT = 5735
349922 TA = 317
58171
MA = 317
74969
Ha = 192
526 n
mi
Hp = 181
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21191983
51 X = 6460648
11
Y = -2861784
71 feet Y = -800032
43 meter
Z = 5364016
87 Z = 1666334
97
XDOT = -2545
920994 XDOT = -860
725912
YDOT = 16701
920228 feet/sec YDOT = 5081
594518 meter/sec
ZDOT = 18816
764837 ZDOT = 5731
373768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21341148
72 X = 6504782
13
Y = -702142
23 feet Y = -214012
95 meter
Z = 5488626
53 Z = 1672933
37
XDOT = -4387
009501 XDOT = -1337
160496
YDOT = 14790
843212 feet/sec YDOT = 4508
249011 meter/sec
ZDOT = 18801
083583 ZDOT = 5730
570276
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 10076
56022854
00016717 00000-0 10270-3 0 9025
2 25544 51
6476 341
0163 0007705 55
4003 304
7886 15
74094633 9046
Satellite: ISS
Catalog Number: 25544
Epoch time: 10076
56022854 = yrday
fracday
Element set: 902
Inclination: 51
6476 deg
RA of node: 341
0163 deg
Eccentricity:
0007705
Arg of perigee: 55
4003 deg
Mean anomaly: 304
7886 deg
Mean motion: 15
74094633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 904
Checksum: 295
Coasting Arc #4 (Orbit 918)
---------------------------------------
Vector Time (GMT): 2010/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 348724
44 A = 6720952
39 meter
Y = -4511735
65 meter E =
0019028
Z = -4985402
46 I = 51
49366
XDOT = 7265
035566 Wp = 87
70601
YDOT = -1585
400143 meter/sec RA = 335
64640 deg
ZDOT = 1950
099712 TA = 201
16961
MA = 201
24845
Ha = 192
449 n
mi
Hp = 181
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1144109
07 X = 423367
78
Y = -14802282
31 feet Y = -4507419
13 meter
Z = -16356307
28 Z = -4983526
61
XDOT = 23835
418525 XDOT = 7272
750590
YDOT = -5201
444039 feet/sec YDOT = -1504
114873 meter/sec
ZDOT = 6397
964934 ZDOT = 1985
412196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2482736
65 X = 756738
13
Y = -14645581
69 feet Y = -4463973
30 meter
Z = -16348953
81 Z = -4983161
12
XDOT = 23082
948166 XDOT = 7035
682601
YDOT = -3359
352286 feet/sec YDOT = -1023
930577 meter/sec
ZDOT = 6538
159561 ZDOT = 1992
831034
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 10077
51249022
00016717 00000-0 10270-3 0 9030
2 25544 51
6480 336
1258 0007575 58
6158 301
5746 15
74161219 9193
Satellite: ISS
Catalog Number: 25544
Epoch time: 10077
51249022 = yrday
fracday
Element set: 903
Inclination: 51
6480 deg
RA of node: 336
1258 deg
Eccentricity:
0007575
Arg of perigee: 58
6158 deg
Mean anomaly: 301
5746 deg
Mean motion: 15
74161219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 919
Checksum: 307
Coasting Arc #5 (Orbit 934)
---------------------------------------
Vector Time (GMT): 2010/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6212128
02 A = 6730191
90 meter
Y = 1863347
25 meter E =
0011326
Z = -1802256
82 I = 51
49814
XDOT = 69
721999 Wp = 101
39891
YDOT = -5211
414613 meter/sec RA = 330
53214 deg
ZDOT = -5660
575571 TA = 98
60740
MA = 98
47905
Ha = 192
376 n
mi
Hp = 180
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20380997
44 X = -6223747
53
Y = 6113343
99 feet Y = 1793814
44 meter
Z = -5912916
07 Z = -1832463
80
XDOT = 228
746716 XDOT = 155
489935
YDOT = -17097
816973 feet/sec YDOT = -5210
155816 meter/sec
ZDOT = -18571
442162 ZDOT = -5660
028134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20710111
46 X = -6312441
97
Y = 4734647
22 feet Y = 1443120
47 meter
Z = -6032827
43 Z = -1838805
80
XDOT = 1829
404698 XDOT = 557
602552
YDOT = -15526
862439 feet/sec YDOT = -4732
587671 meter/sec
ZDOT = -18569
377044 ZDOT = -5659
946123
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 10078
52820620
00016717 00000-0 10270-3 0 9042
2 25544 51
6479 330
9086 0007391 62
8496 297
3420 15
74178379 9354
Satellite: ISS
Catalog Number: 25544
Epoch time: 10078
52820620 = yrday
fracday
Element set: 904
Inclination: 51
6479 deg
RA of node: 330
9086 deg
Eccentricity:
0007391
Arg of perigee: 62
8496 deg
Mean anomaly: 297
3420 deg
Mean motion: 15
74178379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 935
Checksum: 330
Coasting Arc #6 (Orbit 950)
---------------------------------------
Vector Time (GMT): 2010/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 237656
17 A = 6720835
50 meter
Y = 4584365
28 meter E =
0013792
Z = 4900704
77 I = 51
44174
XDOT = -6898
517042 Wp = 60
85175
YDOT = 2676
814137 meter/sec RA = 325
34838 deg
ZDOT = -2158
307766 TA = 50
19119
MA = 50
06986
Ha = 192
224 n
mi
Hp = 180
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 779711
85 X = 162568
50
Y = 15040568
52 feet Y = 4586603
33 meter
Z = 16078427
72 Z = 4901676
67
XDOT = -22632
929927 XDOT = -6917
452235
YDOT = 8782
198612 feet/sec YDOT = 2599
564829 meter/sec
ZDOT = -7081
062224 ZDOT = -2191
867011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -66370
11 X = -20229
61
Y = 15056396
98 feet Y = 4589189
80 meter
Z = 16082381
50 Z = 4901909
88
XDOT = -21903
091771 XDOT = -6676
062372
YDOT = 7648
485805 feet/sec YDOT = 2331
258473 meter/sec
ZDOT = -7214
267374 ZDOT = -2198
908696
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 10079
54388788
00016717 00000-0 10270-3 0 9050
2 25544 51
6477 325
6912 0007399 64
8418 295
3512 15
74301686 9512
Satellite: ISS
Catalog Number: 25544
Epoch time: 10079
54388788 = yrday
fracday
Element set: 905
Inclination: 51
6477 deg
RA of node: 325
6912 deg
Eccentricity:
0007399
Arg of perigee: 64
8418 deg
Mean anomaly: 295
3512 deg
Mean motion: 15
74301686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 951
Checksum: 346
Coasting Arc #7 (Orbit 966)
---------------------------------------
Vector Time (GMT): 2010/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5792654
23 A = 6729588
99 meter
Y = -2776996
74 meter E =
0021534
Z = 1971131
44 I = 51
44699
XDOT = 615
861542 Wp = 68
09258
YDOT = 5277
112675 meter/sec RA = 320
23242 deg
ZDOT = 5584
031522 TA = 313
93823
MA = 314
11573
Ha = 192
219 n
mi
Hp = 180
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19004771
10 X = 5813701
17
Y = -9110881
69 feet Y = -2712102
09 meter
Z = 6466966
66 Z = 1999323
41
XDOT = 2020
543116 XDOT = 529
679903
YDOT = 17313
361795 feet/sec YDOT = 5283
517941 meter/sec
ZDOT = 18320
313393 ZDOT = 5586
813853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19254346
93 X = 5868724
94
Y = -8485275
48 feet Y = -2586311
97 meter
Z = 6578857
96 Z = 2005235
91
XDOT = 726
467890 XDOT = 221
427413
YDOT = 15963
062008 feet/sec YDOT = 4865
541300 meter/sec
ZDOT = 18331
470114 ZDOT = 5587
432091
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 10080
55954052
00016717 00000-0 10270-3 0 9067
2 25544 51
6475 320
4734 0007424 68
4763 291
7192 15
74297484 9678
Satellite: ISS
Catalog Number: 25544
Epoch time: 10080
55954052 = yrday
fracday
Element set: 906
Inclination: 51
6475 deg
RA of node: 320
4734 deg
Eccentricity:
0007424
Arg of perigee: 68
4763 deg
Mean anomaly: 291
7192 deg
Mean motion: 15
74297484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 967
Checksum: 329
Coasting Arc #8 (Orbit 981)
---------------------------------------
Vector Time (GMT): 2010/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -818369
63 A = 6721028
93 meter
Y = -4625185
16 meter E =
0018336
Z = -4823510
16 I = 51
39603
XDOT = 6341
534142 Wp = 93
86773
YDOT = -3621
151744 meter/sec RA = 315
04112 deg
ZDOT = 2402
977111 TA = 199
67340
MA = 199
74423
Ha = 192
120 n
mi
Hp = 180
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2684939
72 X = -743157
47
Y = -15174491
98 feet Y = -4633916
24 meter
Z = -15825164
56 Z = -4827302
98
XDOT = 20805
558208 XDOT = 6369
881989
YDOT = -11880
419106 feet/sec YDOT = -3550
078380 meter/sec
ZDOT = 7883
783173 ZDOT = 2433
853151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2355937
93 X = -718089
88
Y = -15213273
57 feet Y = -4637005
78 meter
Z = -15840322
14 Z = -4828130
19
XDOT = 19831
363753 XDOT = 6044
599672
YDOT = -11384
768519 feet/sec YDOT = -3470
077444 meter/sec
ZDOT = 8006
317418 ZDOT = 2440
325549
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 10081
51168314
00016717 00000-0 10270-3 0 9073
2 25544 51
6473 315
5815 0007261 71
8269 288
3685 15
74364897 9828
Satellite: ISS
Catalog Number: 25544
Epoch time: 10081
51168314 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 315
5815 deg
Eccentricity:
0007261
Arg of perigee: 71
8269 deg
Mean anomaly: 288
3685 deg
Mean motion: 15
74364897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 982
Checksum: 335
Coasting Arc #9 (Orbit 997)
---------------------------------------
Vector Time (GMT): 2010/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5282970
55 A = 6728818
06 meter
Y = 3507614
99 meter E =
0011272
Z = -2255301
41 I = 51
40183
XDOT = -1215
086819 Wp = 102
57334
YDOT = -5308
906774 meter/sec RA = 309
92532 deg
ZDOT = -5435
755895 TA = 102
81506
MA = 102
68909
Ha = 192
043 n
mi
Hp = 180
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17332580
56 X = -5310844
92
Y = 11507923
19 feet Y = 3448381
77 meter
Z = -7399282
85 Z = -2281033
69
XDOT = -3986
505313 XDOT = -1129
225634
YDOT = -17417
673144 feet/sec YDOT = -5322
014645 meter/sec
ZDOT = -17833
844801 ZDOT = -5441
450069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17269406
28 X = -5263715
03
Y = 11536755
04 feet Y = 3516402
94 meter
Z = -7501394
63 Z = -2286425
08
XDOT = -3069
488888 XDOT = -935
580213
YDOT = -16152
253909 feet/sec YDOT = -4923
206991 meter/sec
ZDOT = -17856
571263 ZDOT = -5442
682921
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 10082
52727163
00016717 00000-0 10270-3 0 9089
2 25544 51
6470 310
3638 0007104 76
1147 284
0806 15
74379215 9985
Satellite: ISS
Catalog Number: 25544
Epoch time: 10082
52727163 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 310
3638 deg
Eccentricity:
0007104
Arg of perigee: 76
1147 deg
Mean anomaly: 284
0806 deg
Mean motion: 15
74379215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 998
Checksum: 308
Coasting Arc #10 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2010/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1320907
34 A = 6721240
65 meter
Y = 4643501
13 meter E =
0014821
Z = 4666636
81 I = 51
35879
XDOT = -5711
094574 Wp = 69
73705
YDOT = 4392
088314 meter/sec RA = 304
72616 deg
ZDOT = -2741
678419 TA = 47
41286
MA = 47
28791
Ha = 191
848 n
mi
Hp = 180
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4333685
50 X = 1246215
28
Y = 15234583
77 feet Y = 4657854
83 meter
Z = 15310488
21 Z = 4672872
13
XDOT = -18737
186922 XDOT = -5746
464800
YDOT = 14409
738564 feet/sec YDOT = 4328
025607 meter/sec
ZDOT = -8995
007936 ZDOT = -2769
508657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4530415
73 X = 1380870
71
Y = 15152116
11 feet Y = 4618364
99 meter
Z = 15335355
63 Z = 4674216
40
XDOT = -17303
650603 XDOT = -5274
152704
YDOT = 14429
343390 feet/sec YDOT = 4398
063865 meter/sec
ZDOT = -9105
431125 ZDOT = -2775
335407
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 10083
54282547
00016717 00000-0 10270-3 0 9095
2 25544 51
6470 305
1452 0007058 78
3758 281
8197 15
74493209 10149
Satellite: ISS
Catalog Number: 25544
Epoch time: 10083
54282547 = yrday
fracday
Element set: 909
Inclination: 51
6470 deg
RA of node: 305
1452 deg
Eccentricity:
0007058
Arg of perigee: 78
3758 deg
Mean anomaly: 281
8197 deg
Mean motion: 15
74493209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1014
Checksum: 318
Coasting Arc #11 (Orbit 1029)
---------------------------------------
Vector Time (GMT): 2010/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4667862
44 A = 6727855
68 meter
Y = -4115155
82 meter E =
0020756
Z = 2533384
83 I = 51
36398
XDOT = 1817
443549 Wp = 78
20981
YDOT = 5324
526598 meter/sec RA = 299
61024 deg
ZDOT = 5268
146628 TA = 310
65308
MA = 310
83335
Ha = 191
776 n
mi
Hp = 180
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15314509
31 X = 4701225
37
Y = -13501167
38 feet Y = -4062770
33 meter
Z = 8311630
01 Z = 2556142
23
XDOT = 5962
741301 XDOT = 1732
177318
YDOT = 17468
919285 feet/sec YDOT = 5344
373857 meter/sec
ZDOT = 17283
945629 ZDOT = 5276
768258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14768351
17 X = 4501393
44
Y = -14042884
96 feet Y = -4280271
34 meter
Z = 8401910
18 Z = 2560902
22
XDOT = 5463
323713 XDOT = 1665
221068
YDOT = 16169
596860 feet/sec YDOT = 4928
493123 meter/sec
ZDOT = 17318
314216 ZDOT = 5278
622173
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 10084
55834852
00016717 00000-0 10270-3 0 9101
2 25544 51
6458 299
9264 0006980 82
3488 277
8468 15
74517572 10308
Satellite: ISS
Catalog Number: 25544
Epoch time: 10084
55834852 = yrday
fracday
Element set: 910
Inclination: 51
6458 deg
RA of node: 299
9264 deg
Eccentricity:
0006980
Arg of perigee: 82
3488 deg
Mean anomaly: 277
8468 deg
Mean motion: 15
74517572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1030
Checksum: 343
Coasting Arc #12 (Orbit 1044)
---------------------------------------
Vector Time (GMT): 2010/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1843198
03 A = 6721748
26 meter
Y = -4655125
14 meter E =
0016551
Z = -4500457
14 I = 51
32872
XDOT = 4981
354422 Wp = 100
18967
YDOT = -4966
701106 meter/sec RA = 294
40363 deg
ZDOT = 3104
044787 TA = 200
91343
MA = 200
98120
Ha = 191
762 n
mi
Hp = 180
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6047237
64 X = -1769144
51
Y = -15272720
26 feet Y = -4675323
17 meter
Z = -14765279
34 Z = -4509231
03
XDOT = 16343
026318 XDOT = 5021
444063
YDOT = -16294
951136 feet/sec YDOT = -4910
772245 meter/sec
ZDOT = 10183
873972 ZDOT = 3128
341617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6765245
83 X = -2062046
93
Y = -14933945
82 feet Y = -4551866
69 meter
Z = -14800245
01 Z = -4511114
68
XDOT = 14302
850883 XDOT = 4359
508949
YDOT = -16645
480249 feet/sec YDOT = -5073
542380 meter/sec
ZDOT = 10280
240313 ZDOT = 3133
417247
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 10085
51037087
00016717 00000-0 10270-3 0 9114
2 25544 51
6446 295
0331 0006983 85
9771 274
2190 15
74561343 10458
Satellite: ISS
Catalog Number: 25544
Epoch time: 10085
51037087 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 295
0331 deg
Eccentricity:
0006983
Arg of perigee: 85
9771 deg
Mean anomaly: 274
2190 deg
Mean motion: 15
74561343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1045
Checksum: 306
Coasting Arc #13 (Orbit 1060)
---------------------------------------
Vector Time (GMT): 2010/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4050819
78 A = 6726703
88 meter
Y = 4515700
82 meter E =
0011242
Z = -2913946
23 I = 51
33362
XDOT = -2371
009727 Wp = 98
48108
YDOT = -5343
402893 meter/sec RA = 289
28934 deg
ZDOT = -5002
623319 TA = 115
19803
MA = 115
08142
Ha = 191
658 n
mi
Hp = 180
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13290091
14 X = -4086858
83
Y = 14815291
39 feet Y = 4470200
34 meter
Z = -9560191
03 Z = -2933712
87
XDOT = -7778
903304 XDOT = -2286
781068
YDOT = -17530
849388 feet/sec YDOT = -5369
446494 meter/sec
ZDOT = -16412
806165 ZDOT = -5013
936416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12157332
00 X = -3705554
79
Y = 15710311
35 feet Y = 4788502
90 meter
Z = -9638569
92 Z = -2937836
11
XDOT = -7752
219588 XDOT = -2362
876530
YDOT = -16060
121322 feet/sec YDOT = -4895
124979 meter/sec
ZDOT = -16457
882708 ZDOT = -5016
362649
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 10086
52582866
00016717 00000-0 10270-3 0 9127
2 25544 51
6436 289
8144 0006914 89
4472 270
7483 15
74602780 10616
Satellite: ISS
Catalog Number: 25544
Epoch time: 10086
52582866 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 289
8144 deg
Eccentricity:
0006914
Arg of perigee: 89
4472 deg
Mean anomaly: 270
7483 deg
Mean motion: 15
74602780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1061
Checksum: 327
Coasting Arc #14 (Orbit 1076)
---------------------------------------
Vector Time (GMT): 2010/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2321178
07 A = 6722409
19 meter
Y = 4669929
68 meter E =
0016473
Z = 4229656
53 I = 51
31088
XDOT = -4270
318074 Wp = 80
83713
YDOT = 5348
806178 meter/sec RA = 284
07637 deg
ZDOT = -3547
754024 TA = 45
35722
MA = 45
22303
Ha = 191
458 n
mi
Hp = 180
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7615413
62 X = 2248238
80
Y = 15321291
59 feet Y = 4695479
14 meter
Z = 13876825
87 Z = 4240755
02
XDOT = -14010
229900 XDOT = -4312
577768
YDOT = 17548
576698 feet/sec YDOT = 5300
816242 meter/sec
ZDOT = -11639
612938 ZDOT = -3568
602352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8846514
00 X = 2696417
47
Y = 14602969
04 feet Y = 4450984
96 meter
Z = 13921037
40 Z = 4243132
20
XDOT = -11286
230145 XDOT = -3440
042948
YDOT = 18056
742072 feet/sec YDOT = 5503
694983 meter/sec
ZDOT = -11722
256379 ZDOT = -3572
943744
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 10087
54125163
00016717 00000-0 10270-3 0 9134
2 25544 51
6436 284
5942 0006758 93
2055 266
9882 15
74672601 10776
Satellite: ISS
Catalog Number: 25544
Epoch time: 10087
54125163 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 284
5942 deg
Eccentricity:
0006758
Arg of perigee: 93
2055 deg
Mean anomaly: 266
9882 deg
Mean motion: 15
74672601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1077
Checksum: 324
Coasting Arc #15 (Orbit 1092)
---------------------------------------
Vector Time (GMT): 2010/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3407674
48 A = 6725372
56 meter
Y = -4773526
40 meter E =
0019424
Z = 3275026
36 I = 51
31402
XDOT = 2960
503134 Wp = 91
59471
YDOT = 5349
829499 meter/sec RA = 278
96179 deg
ZDOT = 4692
773805 TA = 307
05674
MA = 307
23421
Ha = 191
362 n
mi
Hp = 180
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11180034
38 X = 3444890
16
Y = -15661175
87 feet Y = -4735211
29 meter
Z = 10744837
12 Z = 3291671
78
XDOT = 9712
936791 XDOT = 2877
663715
YDOT = 17551
934052 feet/sec YDOT = 5382
472976 meter/sec
ZDOT = 15396
239519 ZDOT = 4706
954075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9415824
11 X = 2869943
19
Y = -16738756
80 feet Y = -5101973
07 meter
Z = 10810800
16 Z = 3295131
89
XDOT = 10186
405638 XDOT = 3104
816438
YDOT = 15761
772390 feet/sec YDOT = 4804
188224 meter/sec
ZDOT = 15452
713536 ZDOT = 4709
987086
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 10088
55664121
00016717 00000-0 10270-3 0 9149
2 25544 51
6423 279
3737 0006743 97
8248 262
3681 15
74730469 10936
Satellite: ISS
Catalog Number: 25544
Epoch time: 10088
55664121 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 279
3737 deg
Eccentricity:
0006743
Arg of perigee: 97
8248 deg
Mean anomaly: 262
3681 deg
Mean motion: 15
74730469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1093
Checksum: 329
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
http://www aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list