Date:
August 26th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4467 02 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 ET - UTC (sec) : 65 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 2078)
---------------------------------------
Vector Time (GMT): 2007/231/15:10:06
062
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2000175
83 A = 6714490
41 meter
Y = 3760718
47 meter E =
0006347
Z = -5195709
82 I = 51
83941
XDOT = -5998
328696 Wp = 117
45977
YDOT = 4702
933916 meter/sec RA = 135
43193 deg
ZDOT = 1093
029938 TA = 162
95166
MA = 162
93032
Ha = 185
116 n
mi
Hp = 184
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6562256
66 X = 1983214
04
Y = 12338315
20 feet Y = 3782990
88 meter
Z = -17046292
05 Z = -5186034
07
XDOT = -19679
556088 XDOT = -6055
781525
YDOT = 15429
573216 feet/sec YDOT = 4635
535956 meter/sec
ZDOT = 3586
056227 ZDOT = 1063
750689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9512936
68 X = -2899543
10
Y = -10298902
40 feet Y = -3139105
45 meter
Z = -17009113
80 Z = -5184377
89
XDOT = 14500
359207 XDOT = 4419
709486
YDOT = -19143
956493 feet/sec YDOT = -5835
077939 meter/sec
ZDOT = 3475
610971 ZDOT = 1059
366224
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 07231
64608892
00020000 00000-0 20000-3 0 9005
2 25544 51
6328 136
2877 0008731 264
4902 95
5266 15
76100517 20791
Satellite: ISS
Catalog Number: 25544
Epoch time: 07231
64608892 = yrday
fracday
Element set: 900
Inclination: 51
6328 deg
RA of node: 136
2877 deg
Eccentricity:
0008731
Arg of perigee: 264
4902 deg
Mean anomaly: 95
5266 deg
Mean motion: 15
76100517 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2079
Checksum: 298
Coasting Arc #2 (Orbit 2094)
---------------------------------------
Vector Time (GMT): 2007/232/15:10:06
062
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5116518
69 A = 6725127
82 meter
Y = -4033715
95 meter E =
0007788
Z = -1645932
10 I = 51
89443
XDOT = 1892
089178 Wp = 211
11789
YDOT = 4752
992480 meter/sec RA = 130
32159 deg
ZDOT = -5761
027605 TA = 347
01781
MA = 347
03785
Ha = 184
970 n
mi
Hp = 184
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16786478
63 X = 5169239
66
Y = -13233976
20 feet Y = -3976205
30 meter
Z = -5400039
69 Z = -1620948
21
XDOT = 6207
641661 XDOT = 1866
785881
YDOT = 15593
807348 feet/sec YDOT = 4774
009674 meter/sec
ZDOT = -18901
009203 ZDOT = -5751
897091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12709699
99 X = -3873916
56
Y = 17216171
33 feet Y = 5247489
02 meter
Z = -5305788
40 Z = -1617204
30
XDOT = -8963
821754 XDOT = -2732
172871
YDOT = -12437
302084 feet/sec YDOT = -3790
889675 meter/sec
ZDOT = -18865
774398 ZDOT = -5750
288036
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 07232
66057145
00020000 00000-0 20000-3 0 9018
2 25544 51
6326 131
0616 0008835 267
8601 92
1551 15
76079443 20952
Satellite: ISS
Catalog Number: 25544
Epoch time: 07232
66057145 = yrday
fracday
Element set: 901
Inclination: 51
6326 deg
RA of node: 131
0616 deg
Eccentricity:
0008835
Arg of perigee: 267
8601 deg
Mean anomaly: 92
1551 deg
Mean motion: 15
76079443 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2095
Checksum: 282
Coasting Arc #3 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2007/233/15:10:06
062
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1354590
94 A = 6716290
55 meter
Y = -4552393
51 meter E =
0004594
Z = 4752236
80 I = 51
88297
XDOT = 5687
519934 Wp = 329
87799
YDOT = -4463
516462 meter/sec RA = 125
15064 deg
ZDOT = -2651
836584 TA = 146
09353
MA = 146
06415
Ha = 184
713 n
mi
Hp = 184
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4444196
00 X = -1326670
17
Y = -14935674
25 feet Y = -4567385
49 meter
Z = 15591328
09 Z = 4745723
76
XDOT = 18659
842304 XDOT = 5749
891039
YDOT = -14644
082881 feet/sec YDOT = -4399
566512 meter/sec
ZDOT = -8700
251261 ZDOT = -2624
055455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8552415
28 X = 2606776
18
Y = 13056379
86 feet Y = 3979584
58 meter
Z = 15566049
37 Z = 4744531
85
XDOT = -12878
070725 XDOT = -3925
235957
YDOT = 18694
178495 feet/sec YDOT = 5697
985605 meter/sec
ZDOT = -8595
431015 ZDOT = -2619
887373
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 07233
67503923
00020000 00000-0 20000-3 0 9021
2 25544 51
6326 125
8336 0008890 272
2550 87
7596 15
76138287 21116
Satellite: ISS
Catalog Number: 25544
Epoch time: 07233
67503923 = yrday
fracday
Element set: 902
Inclination: 51
6326 deg
RA of node: 125
8336 deg
Eccentricity:
0008890
Arg of perigee: 272
2550 deg
Mean anomaly: 87
7596 deg
Mean motion: 15
76138287 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2111
Checksum: 299
Coasting Arc #4 (Orbit 2126)
---------------------------------------
Vector Time (GMT): 2007/234/15:10:06
062
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4793073
56 A = 6722313
02 meter
Y = 3674005
77 meter E =
0005114
Z = 2945443
00 I = 51
91797
XDOT = -1265
477268 Wp = 58
54472
YDOT = -5691
155839 meter/sec RA = 120
06048 deg
ZDOT = 5035
831986 TA = 335
29792
MA = 335
32241
Ha = 185
093 n
mi
Hp = 184
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15725306
95 X = -4848108
96
Y = 12053824
71 feet Y = 3620098
99 meter
Z = 9663526
90 Z = 2922024
95
XDOT = -4151
828306 XDOT = -1226
206895
YDOT = -18671
771124 feet/sec YDOT = -5705
087907 meter/sec
ZDOT = 16521
758484 ZDOT = 5029
779311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11471489
26 X = 3496509
93
Y = -16207567
11 feet Y = -4940066
45 meter
Z = 9575146
14 Z = 2918504
54
XDOT = 8432
881951 XDOT = 2570
342419
YDOT = 15722
798935 feet/sec YDOT = 4792
309115 meter/sec
ZDOT = 16498
085530 ZDOT = 5028
616469
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 07234
68949462
00020000 00000-0 20000-3 0 9036
2 25544 51
6316 120
6055 0008951 275
7131 84
3012 15
76165750 21275
Satellite: ISS
Catalog Number: 25544
Epoch time: 07234
68949462 = yrday
fracday
Element set: 903
Inclination: 51
6316 deg
RA of node: 120
6055 deg
Eccentricity:
0008951
Arg of perigee: 275
7131 deg
Mean anomaly: 84
3012 deg
Mean motion: 15
76165750 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2127
Checksum: 283
Coasting Arc #5 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2007/235/15:10:06
062
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 918201
20 A = 6719256
59 meter
Y = 5362275
29 meter E =
0002237
Z = -3942168
26 I = 51
92050
XDOT = -5288
336060 Wp = 253
53810
YDOT = 3878
164920 meter/sec RA = 114
87721 deg
ZDOT = 4040
970256 TA = 58
26621
MA = 58
24441
Ha = 185
256 n
mi
Hp = 184
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3012471
13 X = 877321
36
Y = 17592766
70 feet Y = 5372314
85 meter
Z = -12933622
90 Z = -3937806
58
XDOT = -17350
183923 XDOT = -5350
939358
YDOT = 12723
638188 feet/sec YDOT = 3818
677434 meter/sec
ZDOT = 13257
776429 ZDOT = 4015
127978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8458309
74 X = -2578092
81
Y = -15731574
28 feet Y = -4794983
84 meter
Z = -12916407
81 Z = -3936921
10
XDOT = 11394
980355 XDOT = 3473
190012
YDOT = -16938
605537 feet/sec YDOT = -5162
886968 meter/sec
ZDOT = 13160
212289 ZDOT = 4011
232706
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 07235
64053589
00020000 00000-0 20000-3 0 9040
2 25544 51
6309 115
7040 0008808 279
2320 80
7848 15
76166569 21429
Satellite: ISS
Catalog Number: 25544
Epoch time: 07235
64053589 = yrday
fracday
Element set: 904
Inclination: 51
6309 deg
RA of node: 115
7040 deg
Eccentricity:
0008808
Arg of perigee: 279
2320 deg
Mean anomaly: 80
7848 deg
Mean motion: 15
76166569 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2142
Checksum: 301
Coasting Arc #6 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2007/236/15:10:06
062
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4447022
09 A = 6718906
83 meter
Y = -3008492
06 meter E =
0004662
Z = -4041156
16 I = 51
93018
XDOT = 888
857612 Wp = 339
63899
YDOT = 6574
424578 meter/sec RA = 109
79725 deg
ZDOT = -3910
671966 TA = 250
16771
MA = 250
21797
Ha = 185
418 n
mi
Hp = 184
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14589967
48 X = 4499963
92
Y = -9870380
77 feet Y = -2958466
67 meter
Z = -13258386
34 Z = -4019424
42
XDOT = 2916
199513 XDOT = 834
272440
YDOT = 21569
634442 feet/sec YDOT = 6584
059343 meter/sec
ZDOT = -12830
288602 ZDOT = -3906
486104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10576612
93 X = -3223751
62
Y = 14163217
76 feet Y = 4316948
77 meter
Z = -13176300
60 Z = -4016136
42
XDOT = -8918
191315 XDOT = -2718
264713
YDOT = -18597
772385 feet/sec YDOT = -5668
601023 meter/sec
ZDOT = -12813
590249 ZDOT = -3905
582308
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 07236
65496630
00020000 00000-0 20000-3 0 9051
2 25544 51
6307 110
4773 0008742 283
7322 76
2869 15
76195505 21583
Satellite: ISS
Catalog Number: 25544
Epoch time: 07236
65496630 = yrday
fracday
Element set: 905
Inclination: 51
6307 deg
RA of node: 110
4773 deg
Eccentricity:
0008742
Arg of perigee: 283
7322 deg
Mean anomaly: 76
2869 deg
Mean motion: 15
76195505 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2158
Checksum: 306
Coasting Arc #7 (Orbit 2173)
---------------------------------------
Vector Time (GMT): 2007/237/15:10:06
062
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -688233
78 A = 6722414
94 meter
Y = -6067660
94 meter E =
0004761
Z = 2807253
28 I = 51
95135
XDOT = 4924
519007 Wp = 85
66915
YDOT = -2940
411000 meter/sec RA = 104
61635 deg
ZDOT = -5140
392098 TA = 62
29793
MA = 62
24964
Ha = 185
559 n
mi
Hp = 183
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2257984
85 X = -633970
04
Y = -19907024
09 feet Y = -6075053
89 meter
Z = 9210148
57 Z = 2804041
42
XDOT = 16156
558423 XDOT = 4982
003788
YDOT = -9647
017716 feet/sec YDOT = -2885
020592 meter/sec
ZDOT = -16864
803472 ZDOT = -5116
329706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9069701
16 X = 2764444
91
Y = 17870837
48 feet Y = 5447031
26 meter
Z = 9197207
68 Z = 2803308
90
XDOT = -10594
083493 XDOT = -3229
076649
YDOT = 14022
433423 feet/sec YDOT = 4274
037707 meter/sec
ZDOT = -16773
857726 ZDOT = -5112
671835
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 07237
66938201
00020000 00000-0 20000-3 0 9069
2 25544 51
6311 105
2493 0009000 287
2931 72
7248 15
76230319 21745
Satellite: ISS
Catalog Number: 25544
Epoch time: 07237
66938201 = yrday
fracday
Element set: 906
Inclination: 51
6311 deg
RA of node: 105
2493 deg
Eccentricity:
0009000
Arg of perigee: 287
2931 deg
Mean anomaly: 72
7248 deg
Mean motion: 15
76230319 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2174
Checksum: 276
Coasting Arc #8 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2007/238/15:10:06
062
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4185094
18 A = 6715799
77 meter
Y = 2053437
81 meter E =
0002188
Z = 4836284
76 I = 51
93396
XDOT = -729
363711 Wp = 258
14794
YDOT = -7264
583431 meter/sec RA = 99
52695 deg
ZDOT = 2453
799072 TA = 167
98596
MA = 167
98074
Ha = 185
858 n
mi
Hp = 183
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13730623
96 X = -4231238
33
Y = 6737000
69 feet Y = 2006379
62 meter
Z = 15867075
99 Z = 4815841
93
XDOT = -2392
925562 XDOT = -659
995735
YDOT = -23833
935141 feet/sec YDOT = -7272
351783 meter/sec
ZDOT = 8050
521890 ZDOT = 2450
424231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10433065
23 X = 3179998
28
Y = -11292308
98 feet Y = -3441895
78 meter
Z = 15789750
50 Z = 4812715
95
XDOT = 10096
911253 XDOT = 3077
538550
YDOT = 20564
050574 feet/sec YDOT = 6267
922615 meter/sec
ZDOT = 8036
811311 ZDOT = 2449
620088
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 07238
68378781
00020000 00000-0 20000-3 0 9074
2 25544 51
6303 100
0209 0008800 291
2220 68
8004 15
76209256 21907
Satellite: ISS
Catalog Number: 25544
Epoch time: 07238
68378781 = yrday
fracday
Element set: 907
Inclination: 51
6303 deg
RA of node: 100
0209 deg
Eccentricity:
0008800
Arg of perigee: 291
2220 deg
Mean anomaly: 68
8004 deg
Mean motion: 15
76209256 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2190
Checksum: 273
Coasting Arc #9 (Orbit 2204)
---------------------------------------
Vector Time (GMT): 2007/239/15:10:06
062
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 621392
15 A = 6724914
36 meter
Y = 6534758
31 meter E =
0010727
Z = -1427697
61 I = 51
96884
XDOT = -4717
119886 Wp = 345
31346
YDOT = 1725
536836 meter/sec RA = 94
36270 deg
ZDOT = 5845
580252 TA = 359
03321
MA = 359
03529
Ha = 185
875 n
mi
Hp = 183
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2038688
17 X = 555208
70
Y = 21439495
77 feet Y = 6541337
00 meter
Z = -4684047
28 Z = -1424839
77
XDOT = -15476
115110 XDOT = -4764
460750
YDOT = 5661
210093 feet/sec YDOT = 1672
522700 meter/sec
ZDOT = 19178
412901 ZDOT = 5822
549910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10033125
44 X = -3058096
63
Y = -19059216
23 feet Y = -5809249
11 meter
Z = -4672386
77 Z = -1424143
49
XDOT = 10887
596181 XDOT = 3318
539316
YDOT = -10411
137551 feet/sec YDOT = -3173
314725 meter/sec
ZDOT = 19091
223349 ZDOT = 5819
004877
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 07239
63477882
00020000 00000-0 20000-3 0 9083
2 25544 51
6305 95
1194 0008662 294
0797 65
9460 15
76243481 22051
Satellite: ISS
Catalog Number: 25544
Epoch time: 07239
63477882 = yrday
fracday
Element set: 908
Inclination: 51
6305 deg
RA of node: 95
1194 deg
Eccentricity:
0008662
Arg of perigee: 294
0797 deg
Mean anomaly: 65
9460 deg
Mean motion: 15
76243481 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2205
Checksum: 316
Coasting Arc #10 (Orbit 2220)
---------------------------------------
Vector Time (GMT): 2007/240/15:10:06
062
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4097133
06 A = 6713809
59 meter
Y = -914708
44 meter E =
0009095
Z = -5246198
66 I = 51
93265
XDOT = 705
845217 Wp = 51
99937
YDOT = 7627
581422 meter/sec RA = 89
25237 deg
ZDOT = -774
099054 TA = 210
63688
MA = 210
69001
Ha = 186
036 n
mi
Hp = 183
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13442037
59 X = 4132541
65
Y = -3001011
95 feet Y = -868694
20 meter
Z = -17211937
86 Z = -5226209
06
XDOT = 2315
765146 XDOT = 624
260382
YDOT = 25024
873432 feet/sec YDOT = 7635
018390 meter/sec
ZDOT = -2539
695059 ZDOT = -770
868557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11254858
07 X = -3430480
74
Y = 8100898
36 feet Y = 2469153
82 meter
Z = -17136185
92 Z = -5223109
47
XDOT = -11427
411832 XDOT = -3483
075126
YDOT = -21252
758714 feet/sec YDOT = -6477
840856 meter/sec
ZDOT = -2526
482354 ZDOT = -770
071821
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 07240
64915679
00020000 00000-0 20000-3 0 9098
2 25544 51
6306 89
8921 0008538 298
4691 61
5613 15
76279509 22213
Satellite: ISS
Catalog Number: 25544
Epoch time: 07240
64915679 = yrday
fracday
Element set: 909
Inclination: 51
6306 deg
RA of node: 89
8921 deg
Eccentricity:
0008538
Arg of perigee: 298
4691 deg
Mean anomaly: 61
5613 deg
Mean motion: 15
76279509 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2221
Checksum: 323
Coasting Arc #11 (Orbit 2236)
---------------------------------------
Vector Time (GMT): 2007/241/15:10:06
062
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -610238
12 A = 6725561
92 meter
Y = -6694471
65 meter E =
0003976
Z = -101602
98 I = 51
97048
XDOT = 4733
782841 Wp = 164
80664
YDOT = -340
319665 meter/sec RA = 84
11424 deg
ZDOT = -6065
249775 TA = 16
29271
MA = 16
27993
Ha = 186
177 n
mi
Hp = 182
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2002093
58 X = -534840
63
Y = -21963489
68 feet Y = -6700874
12 meter
Z = -333343
11 Z = -104383
99
XDOT = 15530
783599 XDOT = 4766
700123
YDOT = -1116
534335 feet/sec YDOT = -287
200107 meter/sec
ZDOT = -19899
113436 ZDOT = -6042
173312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10838769
91 X = 3303657
07
Y = 19207201
81 feet Y = 5854355
11 meter
Z = -344732
28 Z = -105074
40
XDOT = -12405
150585 XDOT = -3781
089898
YDOT = 6647
976403 feet/sec YDOT = 2026
303208 meter/sec
ZDOT = -19811
573964 ZDOT = -6038
567744
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 07241
66351945
00020000 00000-0 20000-3 0 9103
2 25544 51
6301 84
6628 0008808 303
0837 56
9481 15
76325427 22379
Satellite: ISS
Catalog Number: 25544
Epoch time: 07241
66351945 = yrday
fracday
Element set: 910
Inclination: 51
6301 deg
RA of node: 84
6628 deg
Eccentricity:
0008808
Arg of perigee: 303
0837 deg
Mean anomaly: 56
9481 deg
Mean motion: 15
76325427 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2237
Checksum: 294
Coasting Arc #12 (Orbit 2252)
---------------------------------------
Vector Time (GMT): 2007/242/15:10:06
062
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4223454
60 A = 6714004
92 meter
Y = -321180
62 meter E =
0008013
Z = 5213602
82 I = 51
92690
XDOT = -676
048346 Wp = 331
55872
YDOT = -7604
804081 meter/sec RA = 78
97250 deg
ZDOT = -1009
881816 TA = 128
06615
MA = 127
99383
Ha = 186
443 n
mi
Hp = 182
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13856478
33 X = -4244875
87
Y = -1053742
20 feet Y = -368529
16 meter
Z = 17104996
14 Z = 5193033
34
XDOT = -2218
006383 XDOT = -586
054242
YDOT = -24950
144624 feet/sec YDOT = -7611
860909 meter/sec
ZDOT = -3313
260551 ZDOT = -1012
947031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13071553
11 X = 3984209
39
Y = -4991270
43 feet Y = -1521339
23 meter
Z = 17026889
79 Z = 5189796
01
XDOT = 12256
293484 XDOT = 3735
718254
YDOT = 20681
842431 feet/sec YDOT = 6303
825573 meter/sec
ZDOT = -3325
836643 ZDOT = -1013
715009
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 07242
67787257
00020000 00000-0 20000-3 0 9115
2 25544 51
6304 79
4342 0008532 306
6830 53
3549 15
76263004 22539
Satellite: ISS
Catalog Number: 25544
Epoch time: 07242
67787257 = yrday
fracday
Element set: 911
Inclination: 51
6304 deg
RA of node: 79
4342 deg
Eccentricity:
0008532
Arg of perigee: 306
6830 deg
Mean anomaly: 53
3549 deg
Mean motion: 15
76263004 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2253
Checksum: 286
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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