Date:
June 30th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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 2532)
---------------------------------------
Vector Time (GMT): 2010/179/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -877721
67 A = 6726269
00 meter
Y = 4288004
96 meter E =
0017964
Z = -5120428
09 I = 51
68468
XDOT = -7535
116766 Wp = 69
54419
YDOT = 237
073727 meter/sec RA = 169
14881 deg
ZDOT = 1500
553564 TA = 214
80367
MA = 214
92129
Ha = 195
700 n
mi
Hp = 184
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2879664
27 X = -900731
93
Y = 14068257
74 feet Y = 4278061
95 meter
Z = -16799304
76 Z = -5124747
18
XDOT = -24721
511701 XDOT = -7544
497054
YDOT = 777
800941 feet/sec YDOT = 152
758861 meter/sec
ZDOT = 4923
075999 ZDOT = 1463
925739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14172480
13 X = -4319771
94
Y = -2184322
11 feet Y = -665781
38 meter
Z = -16816495
67 Z = -5125667
88
XDOT = -1980
775263 XDOT = -603
740300
YDOT = -23661
843017 feet/sec YDOT = -7212
129752 meter/sec
ZDOT = 4776
850218 ZDOT = 1455
983947
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 10180
00297908
00016717 00000-0 10270-3 0 9002
2 25544 51
6415 170
1307 0009592 18
9367 341
2150 15
72082592 25332
Satellite: ISS
Catalog Number: 25544
Epoch time: 10180
00297908 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 170
1307 deg
Eccentricity:
0009592
Arg of perigee: 18
9367 deg
Mean anomaly: 341
2150 deg
Mean motion: 15
72082592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2533
Checksum: 288
Coasting Arc #2 (Orbit 2548)
---------------------------------------
Vector Time (GMT): 2010/180/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6575657
34 A = 6737237
57 meter
Y = -1279589
00 meter E =
0010552
Z = -731167
25 I = 51
75205
XDOT = 281
646666 Wp = 85
31038
YDOT = 4823
929999 meter/sec RA = 164
05248 deg
ZDOT = -5982
224728 TA = 102
63093
MA = 102
51292
Ha = 195
761 n
mi
Hp = 184
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21573678
95 X = 6593029
05
Y = -4198126
66 feet Y = -1205958
85 meter
Z = -2398842
68 Z = -699181
15
XDOT = 924
037619 XDOT = 256
743821
YDOT = 15826
541990 feet/sec YDOT = 4826
941179 meter/sec
ZDOT = -19626
721547 ZDOT = -5980
916287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5472453
58 X = 1668003
85
Y = 21300152
12 feet Y = 6492286
37 meter
Z = -2271146
90 Z = -692245
58
XDOT = -14183
002404 XDOT = -4322
979133
YDOT = 1578
727574 feet/sec YDOT = 481
196164 meter/sec
ZDOT = -19621
436749 ZDOT = -5980
613921
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 10181
02004490
00016717 00000-0 10270-3 0 9018
2 25544 51
6419 164
9222 0009823 21
9897 338
1685 15
72147345 25495
Satellite: ISS
Catalog Number: 25544
Epoch time: 10181
02004490 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 164
9222 deg
Eccentricity:
0009823
Arg of perigee: 21
9897 deg
Mean anomaly: 338
1685 deg
Mean motion: 15
72147345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 307
Coasting Arc #3 (Orbit 2564)
---------------------------------------
Vector Time (GMT): 2010/181/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1351284
49 A = 6725581
07 meter
Y = -3938244
68 meter E =
0011102
Z = 5276130
20 I = 51
74079
XDOT = 7224
796734 Wp = 38
07324
YDOT = -2670
131581 meter/sec RA = 158
93084 deg
ZDOT = -133
971298 TA = 53
24676
MA = 53
14488
Ha = 195
952 n
mi
Hp = 184
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4433348
06 X = -1332776
05
Y = -12920750
27 feet Y = -3953252
75 meter
Z = 17310138
46 Z = 5269610
19
XDOT = 23703
401359 XDOT = 7254
768467
YDOT = -8760
274217 feet/sec YDOT = -2589
171996 meter/sec
ZDOT = -439
538379 ZDOT = -98
801221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12535170
61 X = 3820720
00
Y = -5511103
49 feet Y = -1679784
35 meter
Z = 17284053
12 Z = 5268179
39
XDOT = 10146
965480 XDOT = 3092
795078
YDOT = 22051
532091 feet/sec YDOT = 6721
306981 meter/sec
ZDOT = -299
134189 ZDOT = -91
176101
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 10182
03710272
00016717 00000-0 10270-3 0 9023
2 25544 51
6418 159
7136 0009659 27
3150 332
8518 15
72076187 25658
Satellite: ISS
Catalog Number: 25544
Epoch time: 10182
03710272 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 159
7136 deg
Eccentricity:
0009659
Arg of perigee: 27
3150 deg
Mean anomaly: 332
8518 deg
Mean motion: 15
72076187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2565
Checksum: 305
Coasting Arc #4 (Orbit 2579)
---------------------------------------
Vector Time (GMT): 2010/182/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5833963
81 A = 6737352
10 meter
Y = 3311179
92 meter E =
0020520
Z = -504788
24 I = 51
81016
XDOT = -2742
832502 Wp = 36
72753
YDOT = -3935
200932 meter/sec RA = 153
81565 deg
ZDOT = 6027
787125 TA = 317
79397
MA = 317
95176
Ha = 195
834 n
mi
Hp = 184
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19140301
23 X = -5868104
29
Y = 10863451
20 feet Y = 3245750
23 meter
Z = -1656129
39 Z = -533211
89
XDOT = -8998
794297 XDOT = -2727
906122
YDOT = -12910
764214 feet/sec YDOT = -3965
790168 meter/sec
ZDOT = 19776
204479 ZDOT = 6014
498372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12607593
70 X = -3842794
56
Y = -18028465
79 feet Y = -5495076
37 meter
Z = -1769595
98 Z = -539372
85
XDOT = 10684
827999 XDOT = 3256
735574
YDOT = -9365
416319 feet/sec YDOT = -2854
578894 meter/sec
ZDOT = 19723
086423 ZDOT = 6011
596742
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 10182
99057931
00016717 00000-0 10270-3 0 9035
2 25544 51
6431 154
8313 0009542 30
9716 329
2007 15
72139579 25800
Satellite: ISS
Catalog Number: 25544
Epoch time: 10182
99057931 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node: 154
8313 deg
Eccentricity:
0009542
Arg of perigee: 30
9716 deg
Mean anomaly: 329
2007 deg
Mean motion: 15
72139579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2580
Checksum: 309
Coasting Arc #5 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2010/183/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3300368
70 A = 6725860
81 meter
Y = 2768395
54 meter E =
0022047
Z = -5183921
07 I = 51
79868
XDOT = -5921
720851 Wp = 62
54703
YDOT = 4734
916851 meter/sec RA = 148
72269 deg
ZDOT = -1235
543363 TA = 195
60886
MA = 195
67694
Ha = 195
922 n
mi
Hp = 184
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10827981
29 X = 3294349
09
Y = 9082662
54 feet Y = 2805269
15 meter
Z = -17007615
07 Z = -5167902
30
XDOT = -19428
218015 XDOT = -5968
225428
YDOT = 15534
504105 feet/sec YDOT = 4668
436751 meter/sec
ZDOT = -4053
619957 ZDOT = -1264
423333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7815521
74 X = -2382171
03
Y = 11867213
12 feet Y = 3617126
56 meter
Z = -16943605
90 Z = -5164411
08
XDOT = -16723
019758 XDOT = -5097
176422
YDOT = -16993
598910 feet/sec YDOT = -5179
648948 meter/sec
ZDOT = -4168
901306 ZDOT = -1270
681118
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 10184
00761044
00016717 00000-0 10270-3 0 9047
2 25544 51
6435 149
6240 0009624 35
0463 325
1331 15
72172742 25962
Satellite: ISS
Catalog Number: 25544
Epoch time: 10184
00761044 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 149
6240 deg
Eccentricity:
0009624
Arg of perigee: 35
0463 deg
Mean anomaly: 325
1331 deg
Mean motion: 15
72172742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 283
Coasting Arc #6 (Orbit 2611)
---------------------------------------
Vector Time (GMT): 2010/184/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4390894
05 A = 6736179
82 meter
Y = -4835049
61 meter E =
0018580
Z = 1635927
13 I = 51
85809
XDOT = 4605
794041 Wp = 86
40076
YDOT = 2216
799755 meter/sec RA = 143
58749 deg
ZDOT = -5753
315300 TA = 75
60437
MA = 75
39821
Ha = 195
924 n
mi
Hp = 183
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14405820
37 X = 4436687
10
Y = -15863023
65 feet Y = -4785692
15 meter
Z = 5367215
00 Z = 1657368
73
XDOT = 15110
872838 XDOT = 4608
611550
YDOT = 7272
965077 feet/sec YDOT = 2268
320886 meter/sec
ZDOT = -18875
706365 ZDOT = -5730
933326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17570524
56 X = 5355495
89
Y = 12227585
20 feet Y = 3726967
97 meter
Z = 5452797
78 Z = 1662012
76
XDOT = -4374
654182 XDOT = -1333
394595
YDOT = 14745
848263 feet/sec YDOT = 4494
534551 meter/sec
ZDOT = -18786
286024 ZDOT = -5726
059980
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 10185
02462863
00016717 00000-0 10270-3 0 9058
2 25544 51
6428 144
4143 0009517 38
2999 321
8838 15
72175065 26124
Satellite: ISS
Catalog Number: 25544
Epoch time: 10185
02462863 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 144
4143 deg
Eccentricity:
0009517
Arg of perigee: 38
2999 deg
Mean anomaly: 321
8838 deg
Mean motion: 15
72175065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2612
Checksum: 316
Coasting Arc #7 (Orbit 2627)
---------------------------------------
Vector Time (GMT): 2010/185/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4590697
45 A = 6727275
76 meter
Y = -980280
08 meter E =
0013051
Z = 4806703
63 I = 51
85320
XDOT = 3944
396285 Wp = 75
10529
YDOT = -6125
149752 meter/sec RA = 138
51628 deg
ZDOT = 2515
625586 TA = 350
36113
MA = 350
38615
Ha = 196
017 n
mi
Hp = 183
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15061343
34 X = -4602744
69
Y = -3216142
01 feet Y = -1031683
93 meter
Z = 15770025
02 Z = 4784372
63
XDOT = 12940
932693 XDOT = 4000
375209
YDOT = -20095
635668 feet/sec YDOT = -6080
728463 meter/sec
ZDOT = 8253
364782 ZDOT = 2534
922714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 985766
25 X = 300461
55
Y = -15460322
01 feet Y = -4712306
15 meter
Z = 15680817
25 Z = 4779513
10
XDOT = 20623
979893 XDOT = 6286
189071
YDOT = 9772
062278 feet/sec YDOT = 2978
524582 meter/sec
ZDOT = 8330
379769 ZDOT = 2539
099754
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 10186
04163345
00016717 00000-0 10270-3 0 9065
2 25544 51
6438 139
2061 0009442 41
9111 318
2772 15
72227619 26287
Satellite: ISS
Catalog Number: 25544
Epoch time: 10186
04163345 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 139
2061 deg
Eccentricity:
0009442
Arg of perigee: 41
9111 deg
Mean anomaly: 318
2772 deg
Mean motion: 15
72227619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2628
Checksum: 296
Coasting Arc #8 (Orbit 2642)
---------------------------------------
Vector Time (GMT): 2010/186/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2409551
99 A = 6734015
89 meter
Y = 5664413
79 meter E =
0014301
Z = -2726745
50 I = 51
89839
XDOT = -5675
457953 Wp = 50
09690
YDOT = 74
270331 meter/sec RA = 133
36959 deg
ZDOT = 5196
372617 TA = 278
92694
MA = 279
08881
Ha = 196
007 n
mi
Hp = 183
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7905354
31 X = -2459467
35
Y = 18584034
73 feet Y = 5637190
01 meter
Z = -8946015
42 Z = -2738571
62
XDOT = -18620
268876 XDOT = -5701
109737
YDOT = 243
669064 feet/sec YDOT = 10
659856 meter/sec
ZDOT = 17048
466592 ZDOT = 5168
738877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19609871
82 X = -5977088
93
Y = -4739974
06 feet Y = -1444744
09 meter
Z = -8993205
14 Z = -2741128
93
XDOT = -3617
583884 XDOT = -1102
639568
YDOT = -17004
229011 feet/sec YDOT = -5182
889003 meter/sec
ZDOT = 16938
080055 ZDOT = 5162
726801
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 10186
99506573
00016717 00000-0 10270-3 0 9074
2 25544 51
6445 134
3239 0009579 45
6736 314
5210 15
72207091 26438
Satellite: ISS
Catalog Number: 25544
Epoch time: 10186
99506573 = yrday
fracday
Element set: 907
Inclination: 51
6445 deg
RA of node: 134
3239 deg
Eccentricity:
0009579
Arg of perigee: 45
6736 deg
Mean anomaly: 314
5210 deg
Mean motion: 15
72207091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2643
Checksum: 316
Coasting Arc #9 (Orbit 2658)
---------------------------------------
Vector Time (GMT): 2010/187/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5120359
48 A = 6729571
79 meter
Y = -1119119
64 meter E =
0017376
Z = -4239490
61 I = 51
90347
XDOT = -1569
370453 Wp = 59
04025
YDOT = 6583
780387 meter/sec RA = 128
31356 deg
ZDOT = -3635
623438 TA = 174
00676
MA = 173
98595
Ha = 196
015 n
mi
Hp = 183
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16799079
65 X = 5153087
85
Y = -3671652
37 feet Y = -1061677
09 meter
Z = -13909089
94 Z = -4214536
51
XDOT = -5148
853191 XDOT = -1625
213593
YDOT = 21600
329353 feet/sec YDOT = 6565
919067 meter/sec
ZDOT = -11927
898418 ZDOT = -3643
382105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6632121
31 X = 2021470
58
Y = 15952057
88 feet Y = 4862187
24 meter
Z = -13809406
49 Z = -4209107
10
XDOT = -20996
669275 XDOT = -6399
784795
YDOT = -1616
767960 feet/sec YDOT = -492
790874 meter/sec
ZDOT = -11958
844900 ZDOT = -3645
055926
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 10188
01204653
00016717 00000-0 10270-3 0 9084
2 25544 51
6446 129
1152 0009493 49
4084 310
7903 15
72225230 26597
Satellite: ISS
Catalog Number: 25544
Epoch time: 10188
01204653 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 129
1152 deg
Eccentricity:
0009493
Arg of perigee: 49
4084 deg
Mean anomaly: 310
7903 deg
Mean motion: 15
72225230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2659
Checksum: 295
Coasting Arc #10 (Orbit 2674)
---------------------------------------
Vector Time (GMT): 2010/188/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 328379
69 A = 6731553
94 meter
Y = -5667340
82 meter E =
0020743
Z = 3606661
90 I = 51
92863
XDOT = 5781
099717 Wp = 71
89265
YDOT = -2502
195124 meter/sec RA = 123
16072 deg
ZDOT = -4431
176978 TA = 65
17152
MA = 64
95594
Ha = 196
083 n
mi
Hp = 183
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1077361
19 X = 374207
99
Y = -18593637
85 feet Y = -5663413
06 meter
Z = 11832880
26 Z = 3608367
51
XDOT = 18966
862588 XDOT = 5830
175935
YDOT = -8209
301588 feet/sec YDOT = -2437
272253 meter/sec
ZDOT = -14537
982210 ZDOT = -4402
973576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18430729
05 X = 5617686
22
Y = -2651747
84 feet Y = -808252
74 meter
Z = 11839661
78 Z = 3608728
91
XDOT = 11587
119847 XDOT = 3531
754129
YDOT = 15732
833245 feet/sec YDOT = 4795
367573 meter/sec
ZDOT = -14425
312415 ZDOT = -4396
835224
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 10189
02901505
00016717 00000-0 10270-3 0 9097
2 25544 51
6450 123
9068 0009560 53
8169 306
3876 15
72234586 26750
Satellite: ISS
Catalog Number: 25544
Epoch time: 10189
02901505 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 123
9068 deg
Eccentricity:
0009560
Arg of perigee: 53
8169 deg
Mean anomaly: 306
3876 deg
Mean motion: 15
72234586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2675
Checksum: 321
Coasting Arc #11 (Orbit 2690)
---------------------------------------
Vector Time (GMT): 2010/189/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4783099
37 A = 6731915
45 meter
Y = 3222199
04 meter E =
0021060
Z = 3450087
04 I = 51
94700
XDOT = -803
091873 Wp = 76
40984
YDOT = -6134
483916 meter/sec RA = 118
11079 deg
ZDOT = 4597
471081 TA = 324
27929
MA = 324
42000
Ha = 196
100 n
mi
Hp = 183
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15692583
23 X = -4835534
95
Y = 10571519
15 feet Y = 3168417
73 meter
Z = 11319183
21 Z = 3426724
04
XDOT = -2634
815857 XDOT = -756
768905
YDOT = -20126
259566 feet/sec YDOT = -6143
206438 meter/sec
ZDOT = 15083
566539 ZDOT = 4593
681018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13680495
71 X = -4169815
09
Y = -13151525
35 feet Y = -4008584
93 meter
Z = 11225841
27 Z = 3421636
42
XDOT = 18127
599071 XDOT = 5525
292197
YDOT = -5942
634329 feet/sec YDOT = -1811
314944 meter/sec
ZDOT = 15068
395600 ZDOT = 4592
846979
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 10190
04596813
00016717 00000-0 10270-3 0 9105
2 25544 51
6461 118
6983 0009532 57
2683 302
9396 15
72305371 26915
Satellite: ISS
Catalog Number: 25544
Epoch time: 10190
04596813 = yrday
fracday
Element set: 910
Inclination: 51
6461 deg
RA of node: 118
6983 deg
Eccentricity:
0009532
Arg of perigee: 57
2683 deg
Mean anomaly: 302
9396 deg
Mean motion: 15
72305371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 314
Coasting Arc #12 (Orbit 2705)
---------------------------------------
Vector Time (GMT): 2010/190/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1649821
92 A = 6728800
19 meter
Y = 4860965
24 meter E =
0016770
Z = -4363757
16 I = 51
95023
XDOT = -4949
654036 Wp = 84
79624
YDOT = 4764
036332 meter/sec RA = 112
96186 deg
ZDOT = 3448
292799 TA = 219
86948
MA = 219
99278
Ha = 196
057 n
mi
Hp = 183
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5412801
57 X = 1616541
29
Y = 15948048
68 feet Y = 4879229
32 meter
Z = -14316788
58 Z = -4355822
25
XDOT = -16239
022427 XDOT = -5019
309543
YDOT = 15630
040459 feet/sec YDOT = 4708
296198 meter/sec
ZDOT = 11313
296584 ZDOT = 3424
079306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14261494
23 X = -4346903
44
Y = 9008654
97 feet Y = 2745838
03 meter
Z = -14285063
21 Z = -4354087
27
XDOT = -18296
761983 XDOT = -5576
853052
YDOT = -11245
868913 feet/sec YDOT = -3427
740845 meter/sec
ZDOT = 11216
544555 ZDOT = 3418
802780
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 10190
99935285
00016717 00000-0 10270-3 0 9110
2 25544 51
6465 113
8164 0009554 60
2349 299
9763 15
72302838 27069
Satellite: ISS
Catalog Number: 25544
Epoch time: 10190
99935285 = yrday
fracday
Element set: 911
Inclination: 51
6465 deg
RA of node: 113
8164 deg
Eccentricity:
0009554
Arg of perigee: 60
2349 deg
Mean anomaly: 299
9763 deg
Mean motion: 15
72302838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2706
Checksum: 333
Coasting Arc #13 (Orbit 2721)
---------------------------------------
Vector Time (GMT): 2010/191/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3728152
73 A = 6734144
06 meter
Y = -4987801
58 meter E =
0012671
Z = -2575663
88 I = 51
97934
XDOT = 2797
762842 Wp = 85
94998
YDOT = 4816
643260 meter/sec RA = 107
90807 deg
ZDOT = -5299
225296 TA = 123
07388
MA = 122
95215
Ha = 196
079 n
mi
Hp = 183
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12231472
22 X = 3796162
09
Y = -16364178
40 feet Y = -4945730
39 meter
Z = -8450340
82 Z = -2557388
53
XDOT = 9179
011948 XDOT = 2769
436653
YDOT = 15802
635368 feet/sec YDOT = 4847
772163 meter/sec
ZDOT = -17385
909765 ZDOT = -5285
701811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18883374
73 X = 5755652
62
Y = 7876699
49 feet Y = 2400818
01 meter
Z = -8377306
94 Z = -2553403
15
XDOT = -12457
780113 XDOT = -3797
131378
YDOT = 11507
772736 feet/sec YDOT = 3507
569130 meter/sec
ZDOT = -17331
848029 ZDOT = -5282
747279
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 10192
01628296
00016717 00000-0 10270-3 0 9127
2 25544 51
6468 108
6077 0009573 64
2053 296
0096 15
72314729 27221
Satellite: ISS
Catalog Number: 25544
Epoch time: 10192
01628296 = yrday
fracday
Element set: 912
Inclination: 51
6468 deg
RA of node: 108
6077 deg
Eccentricity:
0009573
Arg of perigee: 64
2053 deg
Mean anomaly: 296
0096 deg
Mean motion: 15
72314729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2722
Checksum: 312
Coasting Arc #14 (Orbit 2737)
---------------------------------------
Vector Time (GMT): 2010/192/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3128896
01 A = 6726629
29 meter
Y = -3417830
38 meter E =
0016427
Z = 4866161
21 I = 51
96309
XDOT = 3382
147356 Wp = 63
56340
YDOT = -6502
612094 meter/sec RA = 102
76867 deg
ZDOT = -2379
235237 TA = 49
58744
MA = 49
44423
Ha = 196
146 n
mi
Hp = 182
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10265406
86 X = -3114083
15
Y = -11213354
25 feet Y = -3452737
59 meter
Z = 15965095
84 Z = 4850996
70
XDOT = 11096
283976 XDOT = 3466
167055
YDOT = -21334
029180 feet/sec YDOT = -6464
320706 meter/sec
ZDOT = -7805
889884 ZDOT = -2362
602135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8097365
09 X = 2468076
88
Y = -12941506
65 feet Y = -3944571
23 meter
Z = 15904472
99 Z = 4847683
37
XDOT = 22568
398798 XDOT = 6878
847954
YDOT = 4555
645535 feet/sec YDOT = 1388
560759 meter/sec
ZDOT = -7739
412092 ZDOT = -2358
972806
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 10193
03319967
00016717 00000-0 10270-3 0 9133
2 25544 51
6473 103
3992 0009642 67
1020 293
1159 15
72355948 27381
Satellite: ISS
Catalog Number: 25544
Epoch time: 10193
03319967 = yrday
fracday
Element set: 913
Inclination: 51
6473 deg
RA of node: 103
3992 deg
Eccentricity:
0009642
Arg of perigee: 67
1020 deg
Mean anomaly: 293
1159 deg
Mean motion: 15
72355948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2738
Checksum: 318
Coasting Arc #15 (Orbit 2753)
---------------------------------------
Vector Time (GMT): 2010/193/23:44:56
394
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2064682
61 A = 6735851
88 meter
Y = 6209189
05 meter E =
0023659
Z = 1553452
15 I = 51
99953
XDOT = -4187
236202 Wp = 65
86170
YDOT = -2858
610696 meter/sec RA = 97
70365 deg
ZDOT = 5801
415349 TA = 311
18351
MA = 311
38731
Ha = 196
115 n
mi
Hp = 182
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6773893
09 X = -2141507
67
Y = 20371355
16 feet Y = 6185670
76 meter
Z = 5096627
78 Z = 1543236
45
XDOT = -13737
651580 XDOT = -4183
141103
YDOT = -9378
644015 feet/sec YDOT = -2905
412834 meter/sec
ZDOT = 19033
514926 ZDOT = 5781
083717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21461123
87 X = -6541350
55
Y = -844058
50 feet Y = -257269
03 meter
Z = 5055796
78 Z = 1541006
86
XDOT = 5075
453779 XDOT = 1546
998312
YDOT = -14352
970998 feet/sec YDOT = -4374
785560 meter/sec
ZDOT = 18952
231497 ZDOT = 5776
640160
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 10194
05010446
00016717 00000-0 10270-3 0 9147
2 25544 51
6472 98
1911 0009656 71
0523 289
1685 15
72351325 27541
Satellite: ISS
Catalog Number: 25544
Epoch time: 10194
05010446 = yrday
fracday
Element set: 914
Inclination: 51
6472 deg
RA of node: 98
1911 deg
Eccentricity:
0009656
Arg of perigee: 71
0523 deg
Mean anomaly: 289
1685 deg
Mean motion: 15
72351325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2754
Checksum: 302
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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