Date:
January 22nd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
022/09:06:27
023 1
5 3
3 3
3
N/A 2
7 0
0 185
4
000/00:00:54
046 1
1 0
0 179
6
024/09:03:00
612 -4
8 9
2 9
2
N/A -7
6 0
0 187
9
000/00:02:31
224 -2
1 0
1 183
7
Coasting Arc #1 (Orbit 20)
---------------------------------------
Vector Time (GMT): 2010/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 36380
37 A = 6722037
12 meter
Y = 6709774
11 meter E =
0015446
Z = -178707
83 I = 51
32893
XDOT = -4821
135540 Wp = 162
38628
YDOT = -130
144281 meter/sec RA = 268
46797 deg
ZDOT = -6017
490859 TA = 19
56793
MA = 19
50871
Ha = 184
949 n
mi
Hp = 179
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 119358
17 X = -37784
10
Y = 22013694
57 feet Y = 6709766
26 meter
Z = -586311
78 Z = -178711
09
XDOT = -15817
373819 XDOT = -4790
090515
YDOT = -426
982550 feet/sec YDOT = -183
883354 meter/sec
ZDOT = -19742
424079 ZDOT = -6040
836154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19196278
39 X = -5851025
65
Y = 10775903
33 feet Y = 3284495
33 meter
Z = -586140
01 Z = -178655
48
XDOT = -6449
596234 XDOT = -1965
836932
YDOT = -12541
542093 feet/sec YDOT = -3822
662030 meter/sec
ZDOT = -19834
885298 ZDOT = -6045
673039
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 10020
53135479
00016717 00000-0 10270-3 0 9007
2 25544 51
6448 269
0797 0007063 210
3784 149
6973 15
77566722 211
Satellite: ISS
Catalog Number: 25544
Epoch time: 10020
53135479 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 269
0797 deg
Eccentricity:
0007063
Arg of perigee: 210
3784 deg
Mean anomaly: 149
6973 deg
Mean motion: 15
77566722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 21
Checksum: 312
Coasting Arc #2 (Orbit 36)
---------------------------------------
Vector Time (GMT): 2010/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4227828
48 A = 6710457
89 meter
Y = 1268427
86 meter E =
0002731
Z = 5053854
18 I = 51
29295
XDOT = -381
201770 Wp = 182
59516
YDOT = 7535
307438 meter/sec RA = 263
26587 deg
ZDOT = -1575
060337 TA = 282
57067
MA = 282
60122
Ha = 184
452 n
mi
Hp = 179
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13870828
33 X = 4188780
06
Y = 4161508
72 feet Y = 1315487
49 meter
Z = 16580886
41 Z = 5074297
90
XDOT = -1250
661974 XDOT = -457
783313
YDOT = 24722
137263 feet/sec YDOT = 7530
616460 meter/sec
ZDOT = -5167
520791 ZDOT = -1577
098034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3275928
19 X = 998502
91
Y = 14010478
91 feet Y = 4270393
97 meter
Z = 16661890
74 Z = 5078544
30
XDOT = -21003
545209 XDOT = -6401
880580
YDOT = 11055
242744 feet/sec YDOT = 3369
637988 meter/sec
ZDOT = -5175
375585 ZDOT = -1577
454478
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 10021
54485120
00016717 00000-0 10270-3 0 9011
2 25544 51
6448 263
8470 0006916 216
3721 143
6975 15
77674615 378
Satellite: ISS
Catalog Number: 25544
Epoch time: 10021
54485120 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 263
8470 deg
Eccentricity:
0006916
Arg of perigee: 216
3721 deg
Mean anomaly: 143
6975 deg
Mean motion: 15
77674615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 37
Checksum: 303
Coasting Arc #3 (Orbit 50)
---------------------------------------
Vector Time (GMT): 2010/022/09:06:54
046
Vector Time (MET): N/A
Weight (LBS) : 751544
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3193827
94 A = 6713517
85 meter
Y = -3492211
46 meter E =
0009013
Z = 4761227
31 I = 51
29977
XDOT = 3336
341644 Wp = 151
18470
YDOT = 6479
014940 meter/sec RA = 258
73492 deg
ZDOT = 2504
372732 TA = 274
15430
MA = 274
25731
Ha = 185
402 n
mi
Hp = 179
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10478438
12 X = 3209512
13
Y = -11457386
70 feet Y = -3456408
63 meter
Z = 15620824
49 Z = 4776780
77
XDOT = 10946
002769 XDOT = 3251
478517
YDOT = 21256
610695 feet/sec YDOT = 6515
849320 meter/sec
ZDOT = 8216
445970 ZDOT = 2520
374582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8951924
41 X = 2728546
56
Y = 12609809
67 feet Y = 3843469
99 meter
Z = 15682323
89 Z = 4779972
32
XDOT = -22185
103472 XDOT = -6762
019538
YDOT = 5412
371838 feet/sec YDOT = 1649
690936 meter/sec
ZDOT = 8280
013606 ZDOT = 2523
748147
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 10022
43167375
00016717 00000-0 10270-3 0 9020
2 25544 51
6432 259
2679 0004677 204
6412 155
4530 15
77054905 518
Satellite: ISS
Catalog Number: 25544
Epoch time: 10022
43167375 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 259
2679 deg
Eccentricity:
0004677
Arg of perigee: 204
6412 deg
Mean anomaly: 155
4530 deg
Mean motion: 15
77054905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 51
Checksum: 292
Coasting Arc #4 (Orbit 65)
---------------------------------------
Vector Time (GMT): 2010/023/09:06:54
046
Vector Time (MET): N/A
Weight (LBS) : 751544
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2785389
64 A = 6722809
39 meter
Y = -5995399
72 meter E =
0004710
Z = -1212802
18 I = 51
33866
XDOT = 3985
408641 Wp = 45
44038
YDOT = -3031
857645 meter/sec RA = 253
52097 deg
ZDOT = 5851
845543 TA = 301
19851
MA = 301
24467
Ha = 185
294 n
mi
Hp = 179
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9138417
46 X = -2712249
48
Y = -19669946
59 feet Y = -6026138
60 meter
Z = -3979009
77 Z = -1226156
09
XDOT = 13075
487666 XDOT = 3990
588211
YDOT = -9947
039519 feet/sec YDOT = -2987
261731 meter/sec
ZDOT = 19198
968316 ZDOT = 5871
218966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21087847
74 X = 6427575
99
Y = -5029412
09 feet Y = -1532964
80 meter
Z = -4032081
75 Z = -1228978
52
XDOT = 6809
077050 XDOT = 2075
406685
YDOT = 13141
167298 feet/sec YDOT = 4005
427792 meter/sec
ZDOT = 19275
612542 ZDOT = 5875
206703
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 10023
38217115
00016717 00000-0 10270-3 0 9034
2 25544 51
6435 254
3646 0004567 209
2993 150
7916 15
77062590 665
Satellite: ISS
Catalog Number: 25544
Epoch time: 10023
38217115 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 254
3646 deg
Eccentricity:
0004567
Arg of perigee: 209
2993 deg
Mean anomaly: 150
7916 deg
Mean motion: 15
77062590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 66
Checksum: 303
Coasting Arc #5 (Orbit 81)
---------------------------------------
Vector Time (GMT): 2010/024/09:04:16
224
Vector Time (MET): N/A
Weight (LBS) : 750804
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3289545
91 A = 6716676
40 meter
Y = 2838752
85 meter E =
0005769
Z = -5125222
36 I = 51
31234
XDOT = -3725
228599 Wp = 127
24738
YDOT = -6617
273103 meter/sec RA = 248
37156 deg
ZDOT = -1278
617894 TA = 130
49613
MA = 130
44585
Ha = 187
939 n
mi
Hp = 183
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10792473
47 X = -3296147
64
Y = 9313493
61 feet Y = 2801930
59 meter
Z = -16815033
98 Z = -5141218
72
XDOT = -12221
878606 XDOT = -3644
744965
YDOT = -21710
213594 feet/sec YDOT = -6658
480731 meter/sec
ZDOT = -4194
940596 ZDOT = -1296
519825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7075380
26 X = -2156575
90
Y = -12289248
14 feet Y = -3745762
83 meter
Z = -16878311
20 Z = -5144509
25
XDOT = 22759
219365 XDOT = 6937
010062
YDOT = -7264
138328 feet/sec YDOT = -2214
109362 meter/sec
ZDOT = -4266
052795 ZDOT = -1300
292892
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 10024
39602317
00016717 00000-0 10270-3 0 9049
2 25544 51
6441 249
1346 0011095 237
7769 122
2320 15
75394779 828
Satellite: ISS
Catalog Number: 25544
Epoch time: 10024
39602317 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 249
1346 deg
Eccentricity:
0011095
Arg of perigee: 237
7769 deg
Mean anomaly: 122
2320 deg
Mean motion: 15
75394779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 82
Checksum: 301
Coasting Arc #6 (Orbit 97)
---------------------------------------
Vector Time (GMT): 2010/025/09:04:16
224
Vector Time (MET): N/A
Weight (LBS) : 750804
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3468912
79 A = 6728085
57 meter
Y = 5717772
40 meter E =
0013629
Z = 646449
20 I = 51
36273
XDOT = -3834
492086 Wp = 177
18686
YDOT = 3000
924014 meter/sec RA = 243
18673 deg
ZDOT = -5974
669091 TA = 355
73782
MA = 355
74942
Ha = 187
806 n
mi
Hp = 183
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11380947
48 X = 3401577
53
Y = 18759095
81 feet Y = 5756187
30 meter
Z = 2120896
34 Z = 663137
93
XDOT = -12580
354612 XDOT = -3838
740361
YDOT = 9845
551226 feet/sec YDOT = 2958
021175 meter/sec
ZDOT = -19601
932714 ZDOT = -5993
306968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20467079
14 X = -6238365
72
Y = 7889406
80 feet Y = 2404691
19 meter
Z = 2187184
07 Z = 666653
70
XDOT = -6922
334459 XDOT = -2109
927543
YDOT = -12510
703677 feet/sec YDOT = -3813
262481 meter/sec
ZDOT = -19675
673784 ZDOT = -5997
145369
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 10025
41096082
00016717 00000-0 10270-3 0 9050
2 25544 51
6440 243
9122 0011191 241
4001 118
6037 15
75372107 981
Satellite: ISS
Catalog Number: 25544
Epoch time: 10025
41096082 = yrday
fracday
Element set: 905
Inclination: 51
6440 deg
RA of node: 243
9122 deg
Eccentricity:
0011191
Arg of perigee: 241
4001 deg
Mean anomaly: 118
6037 deg
Mean motion: 15
75372107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 98
Checksum: 265
Coasting Arc #7 (Orbit 113)
---------------------------------------
Vector Time (GMT): 2010/026/09:04:16
224
Vector Time (MET): N/A
Weight (LBS) : 750804
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3450916
47 A = 6715982
89 meter
Y = -2397805
77 meter E =
0009304
Z = 5245813
72 I = 51
33729
XDOT = 4197
742715 Wp = 237
88479
YDOT = 6449
933986 meter/sec RA = 238
02796 deg
ZDOT = 182
104436 TA = 210
35212
MA = 210
40602
Ha = 187
364 n
mi
Hp = 183
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11321904
43 X = 3451989
79
Y = -7866816
84 feet Y = -2359210
09 meter
Z = 17210674
94 Z = 5262580
43
XDOT = 13772
121767 XDOT = 4124
421809
YDOT = 21161
200740 feet/sec YDOT = 6496
465652 meter/sec
ZDOT = 597
455498 ZDOT = 202
319337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5981810
14 X = 1823255
73
Y = 12328905
02 feet Y = 3757850
25 meter
Z = 17277028
31 Z = 5266038
23
XDOT = -22182
492249 XDOT = -6761
223638
YDOT = 9791
620880 feet/sec YDOT = 2984
486044 meter/sec
ZDOT = 677
747448 ZDOT = 206
577422
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 10026
42587984
00016717 00000-0 10270-3 0 9069
2 25544 51
6439 238
6894 0011225 246
2696 113
7291 15
75450096 1148
Satellite: ISS
Catalog Number: 25544
Epoch time: 10026
42587984 = yrday
fracday
Element set: 906
Inclination: 51
6439 deg
RA of node: 238
6894 deg
Eccentricity:
0011225
Arg of perigee: 246
2696 deg
Mean anomaly: 113
7291 deg
Mean motion: 15
75450096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 114
Checksum: 321
Coasting Arc #8 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2010/027/09:04:16
224
Vector Time (MET): N/A
Weight (LBS) : 750804
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3832965
56 A = 6727991
88 meter
Y = -5514871
82 meter E =
0004891
Z = 342940
79 I = 51
39474
XDOT = 4125
111354 Wp = 349
09981
YDOT = -2494
786896 meter/sec RA = 232
86316 deg
ZDOT = 6005
056604 TA = 14
64183
MA = 14
62767
Ha = 187
086 n
mi
Hp = 184
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12575346
31 X = -3772678
32
Y = -18093411
48 feet Y = -5557397
26 meter
Z = 1125133
83 Z = 324466
45
XDOT = 13533
829901 XDOT = 4123
530986
YDOT = -8184
996379 feet/sec YDOT = -2448
666923 meter/sec
ZDOT = 19701
629278 ZDOT = 6025
091921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19696914
22 X = 6003619
45
Y = -9884441
65 feet Y = -3012777
82 meter
Z = 1051752
54 Z = 320574
17
XDOT = 5475
036046 XDOT = 1668
790987
YDOT = 13008
027387 feet/sec YDOT = 3964
846747 meter/sec
ZDOT = 19780
937728 ZDOT = 6029
229820
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 10027
44078468
00016717 00000-0 10270-3 0 9075
2 25544 51
6438 233
4662 0011197 250
7271 109
2682 15
75456045 1302
Satellite: ISS
Catalog Number: 25544
Epoch time: 10027
44078468 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 233
4662 deg
Eccentricity:
0011197
Arg of perigee: 250
7271 deg
Mean anomaly: 109
2682 deg
Mean motion: 15
75456045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 130
Checksum: 301
Coasting Arc #9 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2010/028/09:04:16
224
Vector Time (MET): N/A
Weight (LBS) : 750804
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3791129
93 A = 6716132
89 meter
Y = 1984306
06 meter E =
0006046
Z = -5180320
56 I = 51
37399
XDOT = -4543
789893 Wp = 143
00380
YDOT = -6141
117607 meter/sec RA = 227
68665 deg
ZDOT = 968
784508 TA = 136
28722
MA = 136
23933
Ha = 186
611 n
mi
Hp = 184
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12438090
33 X = -3787872
61
Y = 6510190
49 feet Y = 1941930
12 meter
Z = -16995802
36 Z = -5198729
30
XDOT = -14907
447154 XDOT = -4479
487187
YDOT = -20148
023644 feet/sec YDOT = -6191
569512 meter/sec
ZDOT = 3178
426865 ZDOT = 946
866930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4916719
81 X = -1498616
20
Y = -13054948
12 feet Y = -3979148
19 meter
Z = -17068689
61 Z = -5202536
59
XDOT = 20903
410071 XDOT = 6371
359390
YDOT = -11932
218210 feet/sec YDOT = -3636
940110 meter/sec
ZDOT = 3091
361615 ZDOT = 942
247020
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 10028
39224237
00016717 00000-0 10270-3 0 9088
2 25544 51
6434 228
5696 0011226 254
7546 105
2377 15
75494221 1453
Satellite: ISS
Catalog Number: 25544
Epoch time: 10028
39224237 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 228
5696 deg
Eccentricity:
0011226
Arg of perigee: 254
7546 deg
Mean anomaly: 105
2377 deg
Mean motion: 15
75494221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 145
Checksum: 305
Coasting Arc #10 (Orbit 160)
---------------------------------------
Vector Time (GMT): 2010/029/09:04:16
224
Vector Time (MET): N/A
Weight (LBS) : 750804
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4060575
07 A = 6727255
65 meter
Y = 5182829
69 meter E =
0011034
Z = -1345504
84 I = 51
43210
XDOT = -4595
253612 Wp = 211
58078
YDOT = 2085
246226 meter/sec RA = 222
54436 deg
ZDOT = -5823
430425 TA = 343
25668
MA = 343
29308
Ha = 186
434 n
mi
Hp = 184
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13322096
69 X = 4008853
98
Y = 17004034
43 feet Y = 5227948
36 meter
Z = -4414385
95 Z = -1325904
42
XDOT = -15076
291378 XDOT = -4589
941378
YDOT = 6841
359009 feet/sec YDOT = 2033
889504 meter/sec
ZDOT = -19105
742864 ZDOT = -5845
740426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18344811
45 X = -5591498
53
Y = 11435242
27 feet Y = 3485461
84 meter
Z = -4336516
75 Z = -1321770
31
XDOT = -4352
567062 XDOT = -1326
662441
YDOT = -14276
874898 feet/sec YDOT = -4351
591469 meter/sec
ZDOT = -19194
095502 ZDOT = -5850
360309
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 10029
40711556
00016717 00000-0 10270-3 0 9097
2 25544 51
6432 223
3468 0011356 258
1582 101
8308 15
75463615 1610
Satellite: ISS
Catalog Number: 25544
Epoch time: 10029
40711556 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 223
3468 deg
Eccentricity:
0011356
Arg of perigee: 258
1582 deg
Mean anomaly: 101
8308 deg
Mean motion: 15
75463615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 161
Checksum: 291
Coasting Arc #11 (Orbit 176)
---------------------------------------
Vector Time (GMT): 2010/030/09:04:16
224
Vector Time (MET): N/A
Weight (LBS) : 750804
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4256658
15 A = 6717089
73 meter
Y = -1688357
97 meter E =
0006501
Z = 4920188
64 I = 51
42192
XDOT = 4707
736916 Wp = 288
78303
YDOT = 5712
972487 meter/sec RA = 217
35156 deg
ZDOT = -2112
667368 TA = 181
76702
MA = 181
76932
Ha = 185
759 n
mi
Hp = 183
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13965413
87 X = 4251320
71
Y = -5539232
17 feet Y = -1640787
53 meter
Z = 16142351
18 Z = 4940853
77
XDOT = 15445
331089 XDOT = 4653
766175
YDOT = 18743
348054 feet/sec YDOT = 5765
315503 meter/sec
ZDOT = -6931
323386 ZDOT = -2089
928814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4256851
89 X = 1297488
46
Y = 14315927
34 feet Y = 4363494
65 meter
Z = 16224204
63 Z = 4945137
57
XDOT = -19027
614268 XDOT = -5799
616829
YDOT = 13409
956715 feet/sec YDOT = 4087
354807 meter/sec
ZDOT = -6840
976471 ZDOT = -2085
129628
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 10030
42196955
00016717 00000-0 10270-3 0 9103
2 25544 51
6431 218
1228 0011356 263
3794 96
6078 15
75561550 1777
Satellite: ISS
Catalog Number: 25544
Epoch time: 10030
42196955 = yrday
fracday
Element set: 910
Inclination: 51
6431 deg
RA of node: 218
1228 deg
Eccentricity:
0011356
Arg of perigee: 263
3794 deg
Mean anomaly: 96
6078 deg
Mean motion: 15
75561550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 177
Checksum: 304
Coasting Arc #12 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2010/031/09:04:16
224
Vector Time (MET): N/A
Weight (LBS) : 750804
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4102919
24 A = 6725415
90 meter
Y = -4785497
91 meter E =
0004127
Z = 2336450
85 I = 51
47389
XDOT = 5186
423314 Wp = 29
29203
YDOT = -1810
945824 meter/sec RA = 212
22732 deg
ZDOT = 5397
978600 TA = 357
08348
MA = 357
08588
Ha = 185
570 n
mi
Hp = 183
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13461021
12 X = -4060451
71
Y = -15700452
45 feet Y = -4831141
74 meter
Z = 7665521
16 Z = 2316622
63
XDOT = 17015
824520 XDOT = 5180
066597
YDOT = -5941
423306 feet/sec YDOT = -1752
983732 meter/sec
ZDOT = 17709
903544 ZDOT = 5423
157994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16652127
17 X = 5075568
36
Y = -12313070
54 feet Y = -3753023
90 meter
Z = 7586729
60 Z = 2312435
18
XDOT = 3781
727444 XDOT = 1152
670525
YDOT = 16088
799630 feet/sec YDOT = 4903
866127 meter/sec
ZDOT = 17809
652778 ZDOT = 5428
382167
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 10031
43680931
00016717 00000-0 10270-3 0 9118
2 25544 51
6425 212
8982 0011384 267
6265 92
3596 15
75558816 1936
Satellite: ISS
Catalog Number: 25544
Epoch time: 10031
43680931 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 212
8982 deg
Eccentricity:
0011384
Arg of perigee: 267
6265 deg
Mean anomaly: 92
3596 deg
Mean motion: 15
75558816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 193
Checksum: 318
Coasting Arc #13 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2010/032/09:04:16
224
Vector Time (MET): N/A
Weight (LBS) : 750804
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4803090
39 A = 6718934
42 meter
Y = 1522122
58 meter E =
0003896
Z = -4444717
98 I = 51
47836
XDOT = -4640
224704 Wp = 215
55124
YDOT = -5239
977653 meter/sec RA = 207
02317 deg
ZDOT = 3215
368050 TA = 86
71776
MA = 86
67320
Ha = 185
353 n
mi
Hp = 183
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15758170
56 X = -4798163
01
Y = 4993840
49 feet Y = 1468439
05 meter
Z = -14582408
08 Z = -4468038
81
XDOT = -15223
834331 XDOT = -4596
904724
YDOT = -17191
527734 feet/sec YDOT = -5291
625122 meter/sec
ZDOT = 10549
107777 ZDOT = 3192
931779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4100541
46 X = -1249845
04
Y = -15929239
08 feet Y = -4855232
07 meter
Z = -14674805
27 Z = -4472880
65
XDOT = 16865
409712 XDOT = 5140
576880
YDOT = -13991
353472 feet/sec YDOT = -4264
564538 meter/sec
ZDOT = 10459
945725 ZDOT = 3188
191457
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 10032
38820569
00016717 00000-0 10270-3 0 9127
2 25544 51
6421 208
0003 0011397 271
2668 88
7191 15
75589384 2086
Satellite: ISS
Catalog Number: 25544
Epoch time: 10032
38820569 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 208
0003 deg
Eccentricity:
0011397
Arg of perigee: 271
2668 deg
Mean anomaly: 88
7191 deg
Mean motion: 15
75589384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 307
Coasting Arc #14 (Orbit 223)
---------------------------------------
Vector Time (GMT): 2010/033/09:04:16
224
Vector Time (MET): N/A
Weight (LBS) : 750804
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3936725
57 A = 6723097
09 meter
Y = 4369744
71 meter E =
0006835
Z = -3251610
65 I = 51
51922
XDOT = -5825
719185 Wp = 274
16037
YDOT = 1715
959453 meter/sec RA = 201
91507 deg
ZDOT = -4738
155499 TA = 304
01471
MA = 304
07961
Ha = 185
700 n
mi
Hp = 183
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12915766
30 X = 3903365
11
Y = 14336432
76 feet Y = 4413580
89 meter
Z = -10668013
96 Z = -3232567
61
XDOT = -19113
251919 XDOT = -5821
457773
YDOT = 5629
788231 feet/sec YDOT = 1650
836511 meter/sec
ZDOT = -15545
129590 ZDOT = -4766
445909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14834969
62 X = -4521698
74
Y = 12404960
13 feet Y = 3781031
85 meter
Z = -10592331
46 Z = -3228542
63
XDOT = -3973
207517 XDOT = -1211
033651
YDOT = -18146
330625 feet/sec YDOT = -5531
001575 meter/sec
ZDOT = -15657
227162 ZDOT = -4772
322839
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 10033
40301231
00016717 00000-0 10270-3 0 9132
2 25544 51
6417 202
7772 0011453 275
3342 84
6515 15
75595706 2240
Satellite: ISS
Catalog Number: 25544
Epoch time: 10033
40301231 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 202
7772 deg
Eccentricity:
0011453
Arg of perigee: 275
3342 deg
Mean anomaly: 84
6515 deg
Mean motion: 15
75595706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 224
Checksum: 276
Coasting Arc #15 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2010/034/09:04:16
224
Vector Time (MET): N/A
Weight (LBS) : 750804
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5356749
61 A = 6721148
52 meter
Y = -1516895
71 meter E =
0003506
Z = 3768296
60 I = 51
54276
XDOT = 4318
703355 Wp =
39759
YDOT = 4786
453801 meter/sec RA = 196
70750 deg
ZDOT = -4208
951955 TA = 133
89329
MA = 133
86433
Ha = 185
952 n
mi
Hp = 183
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17574637
83 X = 5355008
30
Y = -4976691
97 feet Y = -1457003
03 meter
Z = 12363177
83 Z = 3794315
04
XDOT = 14168
974263 XDOT = 4285
305379
YDOT = 15703
588587 feet/sec YDOT = 4834
561281 meter/sec
ZDOT = -13808
897489 ZDOT = -4188
053277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4588535
18 X = 1398585
52
Y = 17607404
23 feet Y = 5366736
81 meter
Z = 12466281
93 Z = 3799722
73
XDOT = -14730
280404 XDOT = -4489
789467
YDOT = 13564
823805 feet/sec YDOT = 4134
558296 meter/sec
ZDOT = -13725
833785 ZDOT = -4183
634138
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 10034
41780036
00016717 00000-0 10270-3 0 9149
2 25544 51
6423 197
5527 0011570 279
7707 80
2150 15
75667534 2403
Satellite: ISS
Catalog Number: 25544
Epoch time: 10034
41780036 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 197
5527 deg
Eccentricity:
0011570
Arg of perigee: 279
7707 deg
Mean anomaly: 80
2150 deg
Mean motion: 15
75667534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 296
Coasting Arc #16 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2010/035/09:04:16
224
Vector Time (MET): N/A
Weight (LBS) : 750804
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3541814
31 A = 6720387
97 meter
Y = -4016677
71 meter E =
0000770
Z = 4060606
20 I = 51
56766
XDOT = 6431
167685 Wp = 294
41139
YDOT = -1789
900074 meter/sec RA = 191
60437 deg
ZDOT = 3839
853257 TA = 116
06045
MA = 116
05252
Ha = 186
383 n
mi
Hp = 183
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11620125
68 X = -3516361
28
Y = -13178076
48 feet Y = -4056142
04 meter
Z = 13322198
82 Z = 4043462
16
XDOT = 21099
631511 XDOT = 6432
051642
YDOT = -5872
375570 feet/sec YDOT = -1717
977985 meter/sec
ZDOT = 12597
943757 ZDOT = 3871
097573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13234821
19 X = 4033973
50
Y = -11633557
86 feet Y = -3545908
44 meter
Z = 13254049
99 Z = 4039834
44
XDOT = 4920
824807 XDOT = 1499
867401
YDOT = 20088
663283 feet/sec YDOT = 6123
024569 meter/sec
ZDOT = 12721
767775 ZDOT = 3877
594818
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 10035
43257410
00016717 00000-0 10270-3 0 9158
2 25544 51
6410 192
3277 0011504 283
7328 76
2555 15
75645293 2564
Satellite: ISS
Catalog Number: 25544
Epoch time: 10035
43257410 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 192
3277 deg
Eccentricity:
0011504
Arg of perigee: 283
7328 deg
Mean anomaly: 76
2555 deg
Mean motion: 15
75645293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 296
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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