Date:
May 6th 2010
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) : 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 1643)
---------------------------------------
Vector Time (GMT): 2010/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -524992
63 A = 6731686
01 meter
Y = -6414385
56 meter E =
0005850
Z = 1960450
77 I = 51
98980
XDOT = 4799
778498 Wp = 148
71505
YDOT = -2116
188337 meter/sec RA = 99
09416 deg
ZDOT = -5636
029939 TA = 9
57935
MA = 9
56820
Ha = 188
109 n
mi
Hp = 187
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1722416
77 X = -462750
36
Y = -21044572
04 feet Y = -6419908
47 meter
Z = 6431925
09 Z = 1958051
04
XDOT = 15747
304783 XDOT = 4850
464311
YDOT = -6942
875122 feet/sec YDOT = -2062
230529 meter/sec
ZDOT = -18490
911874 ZDOT = -5612
589544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15007404
53 X = -4574256
90
Y = -14857417
18 feet Y = -4528540
76 meter
Z = 6422254
76 Z = 1957503
25
XDOT = 6462
477894 XDOT = 1969
763262
YDOT = -14483
905206 feet/sec YDOT = -4414
694307 meter/sec
ZDOT = -18397
611532 ZDOT = -5607
591995
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 10123
53559400
00016717 00000-0 10270-3 0 9005
2 25544 51
6419 99
7457 0010024 272
0194 87
9821 15
73587184 16440
Satellite: ISS
Catalog Number: 25544
Epoch time: 10123
53559400 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 99
7457 deg
Eccentricity:
0010024
Arg of perigee: 272
0194 deg
Mean anomaly: 87
9821 deg
Mean motion: 15
73587184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1644
Checksum: 309
Coasting Arc #2 (Orbit 1659)
---------------------------------------
Vector Time (GMT): 2010/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3990322
76 A = 6723005
71 meter
Y = 2351855
91 meter E =
0005011
Z = 4877466
38 I = 51
96485
XDOT = -1349
323501 Wp = 238
22081
YDOT = -7198
010430 meter/sec RA = 94
02247 deg
ZDOT = 2366
080252 TA = 188
79967
MA = 188
80846
Ha = 188
596 n
mi
Hp = 187
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13091610
12 X = -4040018
98
Y = 7716062
70 feet Y = 2306955
57 meter
Z = 16002186
28 Z = 4857960
78
XDOT = -4426
914373 XDOT = -1280
227788
YDOT = -23615
519784 feet/sec YDOT = -7212
713183 meter/sec
ZDOT = 7762
730485 ZDOT = 2359
692601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4764421
69 X = -1452195
73
Y = 14515744
06 feet Y = 4424398
79 meter
Z = 15924550
40 Z = 4853802
96
XDOT = -17937
154367 XDOT = -5467
244651
YDOT = -14378
449191 feet/sec YDOT = -4382
551313 meter/sec
ZDOT = 7737
172033 ZDOT = 2358
290036
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 10124
55168929
00016717 00000-0 10270-3 0 9011
2 25544 51
6423 94
5314 0010124 275
4495 84
5513 15
73626415 16602
Satellite: ISS
Catalog Number: 25544
Epoch time: 10124
55168929 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 94
5314 deg
Eccentricity:
0010124
Arg of perigee: 275
4495 deg
Mean anomaly: 84
5513 deg
Mean motion: 15
73626415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1660
Checksum: 297
Coasting Arc #3 (Orbit 1674)
---------------------------------------
Vector Time (GMT): 2010/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1812868
34 A = 6731185
88 meter
Y = 6103876
63 meter E =
0008466
Z = -2166112
13 I = 51
99335
XDOT = -4264
838763 Wp = 318
07552
YDOT = 3234
013137 meter/sec RA = 88
87575 deg
ZDOT = 5537
586141 TA = 17
79879
MA = 17
76916
Ha = 189
019 n
mi
Hp = 187
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5947730
76 X = 1755001
55
Y = 20025841
96 feet Y = 6123825
75 meter
Z = -7106667
11 Z = -2157445
48
XDOT = -13992
253161 XDOT = -4327
585749
YDOT = 10610
279321 feet/sec YDOT = 3185
970075 meter/sec
ZDOT = 18167
933533 ZDOT = 5516
715253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17940850
44 X = 5468371
21
Y = 10725040
02 feet Y = 3268992
20 meter
Z = -7072055
34 Z = -2155562
47
XDOT = -2451
103761 XDOT = -747
096426
YDOT = 16038
750543 feet/sec YDOT = 4888
611165 meter/sec
ZDOT = 18084
868226 ZDOT = 5512
267835
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 10125
50425757
00016717 00000-0 10270-3 0 9023
2 25544 51
6422 89
6423 0009968 279
4068 80
5968 15
73637784 16758
Satellite: ISS
Catalog Number: 25544
Epoch time: 10125
50425757 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 89
6423 deg
Eccentricity:
0009968
Arg of perigee: 279
4068 deg
Mean anomaly: 80
5968 deg
Mean motion: 15
73637784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1675
Checksum: 345
Coasting Arc #4 (Orbit 1690)
---------------------------------------
Vector Time (GMT): 2010/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3418734
22 A = 6723176
89 meter
Y = -3251210
16 meter E =
0006074
Z = -4793333
91 I = 51
96579
XDOT = 2756
792527 Wp = 11
83094
YDOT = 6707
926390 meter/sec RA = 83
80587 deg
ZDOT = -2578
377601 TA = 232
97169
MA = 233
02728
Ha = 189
243 n
mi
Hp = 187
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11216319
60 X = 3478120
96
Y = -10666700
00 feet Y = -3212647
64 meter
Z = -15726161
11 Z = -4776581
50
XDOT = 9044
594905 XDOT = 2694
103724
YDOT = 22007
632512 feet/sec YDOT = 6738
404056 meter/sec
ZDOT = -8459
244097 ZDOT = -2565
137120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 870326
06 X = 265275
38
Y = -15521574
82 feet Y = -4730976
01 meter
Z = -15659492
50 Z = -4773013
31
XDOT = 20607
558299 XDOT = 6281
183770
YDOT = 9654
030081 feet/sec YDOT = 2942
548369 meter/sec
ZDOT = -8406
411896 ZDOT = -2562
274346
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 10126
52030645
00016717 00000-0 10270-3 0 9035
2 25544 51
6429 84
4272 0010054 283
3795 76
6247 15
73683357 16910
Satellite: ISS
Catalog Number: 25544
Epoch time: 10126
52030645 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 84
4272 deg
Eccentricity:
0010054
Arg of perigee: 283
3795 deg
Mean anomaly: 76
6247 deg
Mean motion: 15
73683357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1691
Checksum: 309
Coasting Arc #5 (Orbit 1706)
---------------------------------------
Vector Time (GMT): 2010/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2972263
32 A = 6730652
48 meter
Y = -5570509
41 meter E =
0003884
Z = 2326543
01 I = 51
98716
XDOT = 3511
000345 Wp = 106
86718
YDOT = -4151
714322 meter/sec RA = 78
65650 deg
ZDOT = -5448
776757 TA = 47
10251
MA = 47
06991
Ha = 189
500 n
mi
Hp = 187
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9751520
09 X = -2921053
96
Y = -18275949
50 feet Y = -5603460
75 meter
Z = 7633015
12 Z = 2312227
95
XDOT = 11519
030003 XDOT = 3583
633929
YDOT = -13621
109979 feet/sec YDOT = -4112
045995 meter/sec
ZDOT = -17876
564163 ZDOT = -5431
543885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19791347
77 X = -6032402
80
Y = -6186542
52 feet Y = -1885658
16 meter
Z = 7575924
97 Z = 2309141
93
XDOT = -1691
710681 XDOT = -515
633416
YDOT = -16421
021077 feet/sec YDOT = -5005
127224 meter/sec
ZDOT = -17807
990309 ZDOT = -5427
875446
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 10127
53633105
00016717 00000-0 10270-3 0 9048
2 25544 51
6432 79
2123 0010095 287
4842 72
5217 15
73721190 17072
Satellite: ISS
Catalog Number: 25544
Epoch time: 10127
53633105 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 79
2123 deg
Eccentricity:
0010095
Arg of perigee: 287
4842 deg
Mean anomaly: 72
5217 deg
Mean motion: 15
73721190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1707
Checksum: 284
Coasting Arc #6 (Orbit 1722)
---------------------------------------
Vector Time (GMT): 2010/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2693995
43 A = 6723111
95 meter
Y = 3950242
23 meter E =
0002770
Z = 4728742
59 I = 51
95601
XDOT = -3991
511338 Wp = 267
66449
YDOT = -5989
210482 meter/sec RA = 73
58781 deg
ZDOT = 2730
461408 TA = 155
57326
MA = 155
56014
Ha = 189
691 n
mi
Hp = 187
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8838567
69 X = -2760939
11
Y = 12960112
31 feet Y = 3919742
00 meter
Z = 15514247
34 Z = 4715492
50
XDOT = -13095
509638 XDOT = -3937
506452
YDOT = -19649
640689 feet/sec YDOT = -6033
544023 meter/sec
ZDOT = 8958
206719 ZDOT = 2711
201564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2967398
51 X = 904463
07
Y = 15456790
02 feet Y = 4711229
60 meter
Z = 15461528
03 Z = 4712673
74
XDOT = -22098
369744 XDOT = -6735
583098
YDOT = -4637
565998 feet/sec YDOT = -1413
530116 meter/sec
ZDOT = 8881
424008 ZDOT = 2707
058037
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 10128
55232947
00016717 00000-0 10270-3 0 9051
2 25544 51
6439 73
9973 0010208 290
4565 69
5502 15
73792605 17235
Satellite: ISS
Catalog Number: 25544
Epoch time: 10128
55232947 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 73
9973 deg
Eccentricity:
0010208
Arg of perigee: 290
4565 deg
Mean anomaly: 69
5502 deg
Mean motion: 15
73792605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1723
Checksum: 320
Coasting Arc #7 (Orbit 1737)
---------------------------------------
Vector Time (GMT): 2010/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3967601
41 A = 6730262
52 meter
Y = 4849911
99 meter E =
0009620
Z = -2438491
28 I = 51
96996
XDOT = -2613
838630 Wp = 326
93939
YDOT = 4847
380500 meter/sec RA = 68
43463 deg
ZDOT = 5386
035722 TA = 5
64661
MA = 5
63577
Ha = 190
008 n
mi
Hp = 186
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13017064
99 X = 3924919
84
Y = 15911784
74 feet Y = 4894041
46 meter
Z = -8000299
46 Z = -2419320
02
XDOT = -8575
586055 XDOT = -2694
013366
YDOT = 15903
479332 feet/sec YDOT = 4817
702636 meter/sec
ZDOT = 17670
720874 ZDOT = 5373
142860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20532413
40 X = 6258279
60
Y = 1505193
84 feet Y = 458783
08 meter
Z = -7923891
59 Z = -2415202
16
XDOT = 5647
378854 XDOT = 1721
321075
YDOT = 15754
019147 feet/sec YDOT = 4801
825036 meter/sec
ZDOT = 17619
429570 ZDOT = 5370
402133
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 10129
50480830
00016717 00000-0 10270-3 0 9064
2 25544 51
6436 69
1075 0010226 295
0178 64
9923 15
73780398 17381
Satellite: ISS
Catalog Number: 25544
Epoch time: 10129
50480830 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 69
1075 deg
Eccentricity:
0010226
Arg of perigee: 295
0178 deg
Mean anomaly: 64
9923 deg
Mean motion: 15
73780398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1738
Checksum: 319
Coasting Arc #8 (Orbit 1753)
---------------------------------------
Vector Time (GMT): 2010/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1861892
42 A = 6723145
66 meter
Y = -4460078
65 meter E =
0008657
Z = -4678567
46 I = 51
93555
XDOT = 5033
837218 Wp = 9
22343
YDOT = 5083
892633 meter/sec RA = 63
36509 deg
ZDOT = -2835
561448 TA = 232
83335
MA = 232
91244
Ha = 190
054 n
mi
Hp = 186
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6108570
93 X = 1934355
46
Y = -14632803
96 feet Y = -4438852
59 meter
Z = -15349630
79 Z = -4669346
32
XDOT = 16515
213970 XDOT = 4990
388963
YDOT = 16679
437772 feet/sec YDOT = 5139
941131 meter/sec
ZDOT = -9303
023125 ZDOT = -2811
212076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6576988
06 X = -2004665
96
Y = -14467256
27 feet Y = -4409619
71 meter
Z = -15312951
38 Z = -4667387
58
XDOT = 22438
105556 XDOT = 6839
134573
YDOT = -429
902708 feet/sec YDOT = -131
034345 meter/sec
ZDOT = -9205
999497 ZDOT = -2805
988647
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 10130
52076062
00016717 00000-0 10270-3 0 9077
2 25544 51
6447 63
8918 0010164 298
9949 61
0195 15
73847775 17549
Satellite: ISS
Catalog Number: 25544
Epoch time: 10130
52076062 = yrday
fracday
Element set: 907
Inclination: 51
6447 deg
RA of node: 63
8918 deg
Eccentricity:
0010164
Arg of perigee: 298
9949 deg
Mean anomaly: 61
0195 deg
Mean motion: 15
73847775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1754
Checksum: 330
Coasting Arc #9 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2010/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4790117
86 A = 6729871
62 meter
Y = -4009817
21 meter E =
0005174
Z = 2502481
61 I = 51
94429
XDOT = 1636
858693 Wp = 67
78406
YDOT = -5294
904148 meter/sec RA = 58
20951 deg
ZDOT = -5340
379227 TA = 84
03452
MA = 83
97556
Ha = 190
211 n
mi
Hp = 186
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15715609
78 X = -4757080
20
Y = -13155568
27 feet Y = -4063198
53 meter
Z = 8210241
50 Z = 2479290
84
XDOT = 5370
271303 XDOT = 1721
888732
YDOT = -17371
732770 feet/sec YDOT = -5276
124187 meter/sec
ZDOT = -17520
929223 ZDOT = -5332
220866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20303955
12 X = -6188645
52
Y = 3050791
62 feet Y = 929881
28 meter
Z = 8117851
31 Z = 2474321
08
XDOT = -9132
093187 XDOT = -2783
462003
YDOT = -14147
755058 feet/sec YDOT = -4312
235742 meter/sec
ZDOT = -17488
481162 ZDOT = -5330
489058
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 10131
53668836
00016717 00000-0 10270-3 0 9086
2 25544 51
6452 58
6764 0010206 302
6272 57
3906 15
73875088 17709
Satellite: ISS
Catalog Number: 25544
Epoch time: 10131
53668836 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 58
6764 deg
Eccentricity:
0010206
Arg of perigee: 302
6272 deg
Mean anomaly: 57
3906 deg
Mean motion: 15
73875088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 319
Coasting Arc #10 (Orbit 1785)
---------------------------------------
Vector Time (GMT): 2010/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1003339
27 A = 6722995
53 meter
Y = 4745445
69 meter E =
0002572
Z = 4655218
86 I = 51
90507
XDOT = -5870
860897 Wp = 335
70987
YDOT = -4064
874072 meter/sec RA = 53
13811 deg
ZDOT = 2881
165302 TA = 85
91627
MA = 85
88687
Ha = 190
364 n
mi
Hp = 185
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3291795
49 X = -1078943
84
Y = 15569047
53 feet Y = 4733802
74 meter
Z = 15273027
77 Z = 4650161
17
XDOT = -19261
354650 XDOT = -5838
966897
YDOT = -13336
201023 feet/sec YDOT = -4130
347379 meter/sec
ZDOT = 9452
642067 ZDOT = 2852
721243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9615565
01 X = 2930824
22
Y = 12703781
00 feet Y = 3872112
45 meter
Z = 15252914
26 Z = 4649088
27
XDOT = -21772
469256 XDOT = -6636
248629
YDOT = 5277
595557 feet/sec YDOT = 1608
611126 meter/sec
ZDOT = 9339
338738 ZDOT = 2846
630447
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 10132
55259090
00016717 00000-0 10270-3 0 9098
2 25544 51
6455 53
4606 0010199 306
0275 53
9943 15
73921703 17868
Satellite: ISS
Catalog Number: 25544
Epoch time: 10132
55259090 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 53
4606 deg
Eccentricity:
0010199
Arg of perigee: 306
0275 deg
Mean anomaly: 53
9943 deg
Mean motion: 15
73921703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1786
Checksum: 310
Coasting Arc #11 (Orbit 1800)
---------------------------------------
Vector Time (GMT): 2010/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5424983
36 A = 6729611
69 meter
Y = 3062478
09 meter E =
0010751
Z = -2526243
71 I = 51
90892
XDOT = -640
755529 Wp = 338
70901
YDOT = 5527
934771 meter/sec RA = 47
97907 deg
ZDOT = 5328
104734 TA = 352
76993
MA = 352
78542
Ha = 190
586 n
mi
Hp = 185
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17798501
84 X = 5402607
29
Y = 10047500
30 feet Y = 3123018
59 meter
Z = -8288201
15 Z = -2499942
63
XDOT = -2102
216301 XDOT = -728
405824
YDOT = 18136
268935 feet/sec YDOT = 5520
278923 meter/sec
ZDOT = 17480
658575 ZDOT = 5324
779442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19122496
72 X = 5828537
00
Y = -7334478
46 feet Y = -2235549
04 meter
Z = -8183443
84 Z = -2494313
68
XDOT = 12025
434440 XDOT = 3665
352417
YDOT = 11873
766571 feet/sec YDOT = 3619
124051 meter/sec
ZDOT = 17467
437424 ZDOT = 5324
074927
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 10133
50497813
00016717 00000-0 10270-3 0 9103
2 25544 51
6461 48
5708 0010264 309
8484 50
1776 15
73949117 18019
Satellite: ISS
Catalog Number: 25544
Epoch time: 10133
50497813 = yrday
fracday
Element set: 910
Inclination: 51
6461 deg
RA of node: 48
5708 deg
Eccentricity:
0010264
Arg of perigee: 309
8484 deg
Mean anomaly: 50
1776 deg
Mean motion: 15
73949117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1801
Checksum: 306
Coasting Arc #12 (Orbit 1816)
---------------------------------------
Vector Time (GMT): 2010/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 135402
77 A = 6722770
85 meter
Y = -4859189
26 meter E =
0011114
Z = -4651219
05 I = 51
86628
XDOT = 6496
160601 Wp = 14
33021
YDOT = 2948
599132 meter/sec RA = 42
90521 deg
ZDOT = -2882
248578 TA = 227
18292
MA = 227
27639
Ha = 190
612 n
mi
Hp = 185
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 444234
80 X = 212324
28
Y = -15942221
99 feet Y = -4857244
50 meter
Z = -15259905
02 Z = -4650374
94
XDOT = 21312
862863 XDOT = 6476
707753
YDOT = 9673
881666 feet/sec YDOT = 3021
134619 meter/sec
ZDOT = -9456
196122 ZDOT = -2850
736492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12116858
03 X = -3693218
33
Y = -10374768
81 feet Y = -3162229
53 meter
Z = -15256553
06 Z = -4650197
37
XDOT = 20144
449044 XDOT = 6140
028068
YDOT = -9762
017712 feet/sec YDOT = -2975
462999 meter/sec
ZDOT = -9330
689097 ZDOT = -2843
994037
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 10134
52083332
00016717 00000-0 10270-3 0 9114
2 25544 51
6469 43
3552 0010270 314
0917 45
9400 15
74005356 18175
Satellite: ISS
Catalog Number: 25544
Epoch time: 10134
52083332 = yrday
fracday
Element set: 911
Inclination: 51
6469 deg
RA of node: 43
3552 deg
Eccentricity:
0010270
Arg of perigee: 314
0917 deg
Mean anomaly: 45
9400 deg
Mean motion: 15
74005356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1817
Checksum: 273
Coasting Arc #13 (Orbit 1832)
---------------------------------------
Vector Time (GMT): 2010/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5892442
14 A = 6729524
18 meter
Y = -2083286
28 meter E =
0007569
Z = 2495933
34 I = 51
86548
XDOT = -309
258537 Wp = 58
35867
YDOT = -5536
961299 meter/sec RA = 37
74294 deg
ZDOT = -5335
974381 TA = 93
50868
MA = 93
42211
Ha = 190
771 n
mi
Hp = 185
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19332159
24 X = -5880833
51
Y = -6834928
75 feet Y = -2149114
49 meter
Z = 8188757
69 Z = 2467335
29
XDOT = -1014
627745 XDOT = -221
398616
YDOT = -18165
883528 feet/sec YDOT = -5539
927666 meter/sec
ZDOT = -17506
477628 ZDOT = -5337
264091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17252665
24 X = -5258612
36
Y = 11164524
40 feet Y = 3402947
04 meter
Z = 8074857
37 Z = 2461216
53
XDOT = -14123
006579 XDOT = -4304
692405
YDOT = -9121
261022 feet/sec YDOT = -2780
160359 meter/sec
ZDOT = -17511
616053 ZDOT = -5337
540573
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 10135
53666482
00016717 00000-0 10270-3 0 9120
2 25544 51
6465 38
1391 0010236 317
4602 42
5768 15
74007185 18334
Satellite: ISS
Catalog Number: 25544
Epoch time: 10135
53666482 = yrday
fracday
Element set: 912
Inclination: 51
6465 deg
RA of node: 38
1391 deg
Eccentricity:
0010236
Arg of perigee: 317
4602 deg
Mean anomaly: 42
5768 deg
Mean motion: 15
74007185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1833
Checksum: 298
Coasting Arc #14 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2010/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 654192
71 A = 6722487
72 meter
Y = 4785215
27 meter E =
0004453
Z = 4673615
74 I = 51
81827
XDOT = -6934
020264 Wp = 6
87892
YDOT = -1806
820130 meter/sec RA = 32
66396 deg
ZDOT = 2824
614518 TA = 55
33186
MA = 55
28989
Ha = 190
911 n
mi
Hp = 184
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2146301
55 X = 577931
10
Y = 15699525
18 feet Y = 4792103
79 meter
Z = 15333384
98 Z = 4676609
28
XDOT = -22749
410316 XDOT = -6927
022349
YDOT = -5927
887564 feet/sec YDOT = -1884
321738 meter/sec
ZDOT = 9267
108000 ZDOT = 2790
945385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13819101
63 X = 4212062
18
Y = 7729714
09 feet Y = 2356016
86 meter
Z = 15345303
72 Z = 4677248
57
XDOT = -17812
034657 XDOT = -5429
108164
YDOT = 13739
391524 feet/sec YDOT = 4187
766537 meter/sec
ZDOT = 9133
007168 ZDOT = 2783
740585
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 10136
55247062
00016717 00000-0 10270-3 0 9133
2 25544 51
6469 32
9224 0010328 321
4402 38
6023 15
74057228 18490
Satellite: ISS
Catalog Number: 25544
Epoch time: 10136
55247062 = yrday
fracday
Element set: 913
Inclination: 51
6469 deg
RA of node: 32
9224 deg
Eccentricity:
0010328
Arg of perigee: 321
4402 deg
Mean anomaly: 38
6023 deg
Mean motion: 15
74057228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1849
Checksum: 287
Coasting Arc #15 (Orbit 1863)
---------------------------------------
Vector Time (GMT): 2010/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6175634
65 A = 6729370
00 meter
Y = 1057154
07 meter E =
0012498
Z = -2433244
68 I = 51
81588
XDOT = 1193
005072 Wp = 350
41459
YDOT = 5388
598419 meter/sec RA = 27
49808 deg
ZDOT = 5377
160555 TA = 342
16188
MA = 342
20572
Ha = 191
095 n
mi
Hp = 184
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20261268
53 X = 6175174
71
Y = 3468353
25 feet Y = 1126211
46 meter
Z = -7983086
23 Z = -2403244
22
XDOT = 3914
058635 XDOT = 1106
538680
YDOT = 17679
128670 feet/sec YDOT = 5401
455107 meter/sec
ZDOT = 17641
602871 ZDOT = 5382
746932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14665716
30 X = 4470110
33
Y = -14469237
00 feet Y = -4410223
44 meter
Z = -7863592
62 Z = -2396823
03
XDOT = 15526
137572 XDOT = 4732
366732
YDOT = 6151
936581 feet/sec YDOT = 1875
110270 meter/sec
ZDOT = 17663
844990 ZDOT = 5383
939953
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 10137
50476626
00016717 00000-0 10270-3 0 9140
2 25544 51
6472 28
0318 0010447 324
6378 35
4091 15
74106583 18649
Satellite: ISS
Catalog Number: 25544
Epoch time: 10137
50476626 = yrday
fracday
Element set: 914
Inclination: 51
6472 deg
RA of node: 28
0318 deg
Eccentricity:
0010447
Arg of perigee: 324
6378 deg
Mean anomaly: 35
4091 deg
Mean motion: 15
74106583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1864
Checksum: 303
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:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
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