Date:
August 20th 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
There are no maneuvers
Coasting Arc #1 (Orbit 3342)
---------------------------------------
Vector Time (GMT): 2010/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1952372
11 A = 6738796
72 meter
Y = -6168588
80 meter E =
0006353
Z = -1868762
29 I = 51
32160
XDOT = 4282
869812 Wp = 324
75792
YDOT = -3057
940306 meter/sec RA = 265
80593 deg
ZDOT = 5615
067263 TA = 14
42129
MA = 14
40317
Ha = 191
998 n
mi
Hp = 191
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6405420
31 X = -1874170
74
Y = -20238152
24 feet Y = -6189984
05 meter
Z = -6131109
89 Z = -1878057
18
XDOT = 14051
410143 XDOT = 4289
469370
YDOT = -10032
612551 feet/sec YDOT = -3010
010107 meter/sec
ZDOT = 18422
136690 ZDOT = 5635
888997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5698092
45 X = -1736778
58
Y = 20437378
49 feet Y = 6229312
96 meter
Z = -6168308
27 Z = -1880100
36
XDOT = -15666
931486 XDOT = -4775
280717
YDOT = 1221
467484 feet/sec YDOT = 372
303289 meter/sec
ZDOT = 18505
399623 ZDOT = 5640
445805
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 10231
50368847
00016717 00000-0 10270-3 0 9005
2 25544 51
6453 266
5994 0008141 267
3761 92
6469 15
71138994 33430
Satellite: ISS
Catalog Number: 25544
Epoch time: 10231
50368847 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 266
5994 deg
Eccentricity:
0008141
Arg of perigee: 267
3761 deg
Mean anomaly: 92
6469 deg
Mean motion: 15
71138994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 329
Coasting Arc #2 (Orbit 3358)
---------------------------------------
Vector Time (GMT): 2010/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3006436
53 A = 6731430
97 meter
Y = 3996405
01 meter E =
0003923
Z = -4508836
59 I = 51
30043
XDOT = -3502
882692 Wp = 19
40946
YDOT = -6116
143981 meter/sec RA = 260
70911 deg
ZDOT = -3082
483489 TA = 219
68372
MA = 219
71244
Ha = 191
740 n
mi
Hp = 191
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9863636
92 X = -3028998
91
Y = 13111564
98 feet Y = 3962659
29 meter
Z = -14792770
96 Z = -4523496
21
XDOT = -11492
397285 XDOT = -3419
256633
YDOT = -20066
089175 feet/sec YDOT = -6154
847592 meter/sec
ZDOT = -10113
134807 ZDOT = -3099
297339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15244581
01 X = 4646548
29
Y = -5921967
46 feet Y = -1805015
68 meter
Z = -14851383
56 Z = -4526701
71
XDOT = -1395
259119 XDOT = -425
274979
YDOT = 21962
781729 feet/sec YDOT = 6694
255871 meter/sec
ZDOT = -10180
419076 ZDOT = -3102
991734
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 10232
52137641
00016717 00000-0 10270-3 0 9015
2 25544 51
6454 261
3959 0008094 271
6238 88
3997 15
71147088 33598
Satellite: ISS
Catalog Number: 25544
Epoch time: 10232
52137641 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 261
3959 deg
Eccentricity:
0008094
Arg of perigee: 271
6238 deg
Mean anomaly: 88
3997 deg
Mean motion: 15
71147088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3359
Checksum: 327
Coasting Arc #3 (Orbit 3374)
---------------------------------------
Vector Time (GMT): 2010/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3939130
95 A = 6734989
15 meter
Y = 4242437
89 meter E =
0004520
Z = 3439083
35 I = 51
31737
XDOT = -2261
214978 Wp = 74
76774
YDOT = 5785
609631 meter/sec RA = 255
52335 deg
ZDOT = -4540
964494 TA = 64
36860
MA = 64
32191
Ha = 192
433 n
mi
Hp = 191
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12923657
97 X = 3874692
36
Y = 13918759
48 feet Y = 4286127
21 meter
Z = 11283081
85 Z = 3458062
86
XDOT = -7418
684311 XDOT = -2303
683934
YDOT = 18981
658894 feet/sec YDOT = 5760
086047 meter/sec
ZDOT = -14898
177475 ZDOT = -4552
052239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3826623
49 X = -1166354
84
Y = -18557750
56 feet Y = -5656402
37 meter
Z = 11359030
92 Z = 3462232
62
XDOT = 14722
674664 XDOT = 4487
471237
YDOT = -12194
233817 feet/sec YDOT = -3716
802467 meter/sec
ZDOT = -14942
486524 ZDOT = -4554
469893
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 10233
53904860
00016717 00000-0 10270-3 0 9023
2 25544 51
6439 256
1921 0008059 276
5799 83
4445 15
71190976 33755
Satellite: ISS
Catalog Number: 25544
Epoch time: 10233
53904860 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 256
1921 deg
Eccentricity:
0008059
Arg of perigee: 276
5799 deg
Mean anomaly: 83
4445 deg
Mean motion: 15
71190976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3375
Checksum: 332
Coasting Arc #4 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2010/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 758181
85 A = 6735421
60 meter
Y = -5806662
07 meter E =
0005090
Z = 3321786
71 I = 51
32680
XDOT = 5140
268154 Wp = 70
46977
YDOT = 3336
826253 meter/sec RA = 250
43736 deg
ZDOT = 4655
590287 TA = 328
72613
MA = 328
75640
Ha = 192
664 n
mi
Hp = 191
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2487473
26 X = 806920
36
Y = -19050728
59 feet Y = -5797911
15 meter
Z = 10898250
36 Z = 3325588
21
XDOT = 16864
396832 XDOT = 5079
957578
YDOT = 10947
592692 feet/sec YDOT = 3393
970551 meter/sec
ZDOT = 15274
246348 ZDOT = 4680
414721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11647625
42 X = -3550196
23
Y = 15268270
17 feet Y = 4653768
75 meter
Z = 10913404
22 Z = 3326405
61
XDOT = -7910
615691 XDOT = -2411
155663
YDOT = -17033
056919 feet/sec YDOT = -5191
675749 meter/sec
ZDOT = 15373
581230 ZDOT = 4685
867559
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 10234
55670707
00016717 00000-0 10270-3 0 9037
2 25544 51
6433 250
9877 0008004 280
8814 79
1447 15
71179206 33912
Satellite: ISS
Catalog Number: 25544
Epoch time: 10234
55670707 = yrday
fracday
Element set: 903
Inclination: 51
6433 deg
RA of node: 250
9877 deg
Eccentricity:
0008004
Arg of perigee: 280
8814 deg
Mean anomaly: 79
1447 deg
Mean motion: 15
71179206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 313
Coasting Arc #5 (Orbit 3405)
---------------------------------------
Vector Time (GMT): 2010/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4712065
45 A = 6730964
49 meter
Y = -1463537
71 meter E =
0002522
Z = -4580719
66 I = 51
32385
XDOT = -665
690218 Wp = 127
76397
YDOT = -7076
164266 meter/sec RA = 245
25369 deg
ZDOT = 2945
192360 TA = 171
60221
MA = 171
59799
Ha = 192
828 n
mi
Hp = 191
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15459532
31 X = -4673097
83
Y = -4801632
91 feet Y = -1516013
02 meter
Z = -15028607
82 Z = -4603515
75
XDOT = -2184
023024 XDOT = -600
820698
YDOT = -23215
762026 feet/sec YDOT = -7083
245676 meter/sec
ZDOT = 9662
704593 ZDOT = 2942
116143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11093565
30 X = 3381318
70
Y = 11672006
59 feet Y = 3557627
61 meter
Z = -15119819
51 Z = -4608520
99
XDOT = -8482
927651 XDOT = -2585
596348
YDOT = 20565
234473 feet/sec YDOT = 6268
283467 meter/sec
ZDOT = 9650
320019 ZDOT = 2941
417542
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 10235
51074606
00016717 00000-0 10270-3 0 9041
2 25544 51
6438 246
1092 0008157 284
4977 75
5279 15
71195693 34060
Satellite: ISS
Catalog Number: 25544
Epoch time: 10235
51074606 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 246
1092 deg
Eccentricity:
0008157
Arg of perigee: 284
4977 deg
Mean anomaly: 75
5279 deg
Mean motion: 15
71195693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3406
Checksum: 325
Coasting Arc #6 (Orbit 3421)
---------------------------------------
Vector Time (GMT): 2010/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1931257
37 A = 6738740
39 meter
Y = 6206165
07 meter E =
0004572
Z = -1768024
01 I = 51
36264
XDOT = -5211
775609 Wp = 221
71367
YDOT = 7
890839 meter/sec RA = 240
15612 deg
ZDOT = -5660
220320 TA = 337
92157
MA = 337
94126
Ha = 193
119 n
mi
Hp = 191
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6336146
23 X = 1870303
95
Y = 20361433
95 feet Y = 6227420
69 meter
Z = -5800603
69 Z = -1758790
36
XDOT = -17099
001342 XDOT = -5183
980660
YDOT = 25
888580 feet/sec YDOT = -50
235111 meter/sec
ZDOT = -18570
276640 ZDOT = -5685
471158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3978015
38 X = 1212499
09
Y = -20960397
09 feet Y = -6388729
03 meter
Z = -5763583
30 Z = -1756740
19
XDOT = 13466
876447 XDOT = 4104
703941
YDOT = 7694
551077 feet/sec YDOT = 2345
299168 meter/sec
ZDOT = -18671
296980 ZDOT = -5691
011319
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 10236
52837364
00016717 00000-0 10270-3 0 9052
2 25544 51
6425 240
9044 0008057 288
2282 71
8003 15
71227210 34228
Satellite: ISS
Catalog Number: 25544
Epoch time: 10236
52837364 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 240
9044 deg
Eccentricity:
0008057
Arg of perigee: 288
2282 deg
Mean anomaly: 71
8003 deg
Mean motion: 15
71227210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3422
Checksum: 284
Coasting Arc #7 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2010/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4064240
95 A = 6728261
24 meter
Y = -1415037
79 meter E =
0006780
Z = 5176565
09 I = 51
34343
XDOT = 3662
017985 Wp = 319
01253
YDOT = 6684
365334 meter/sec RA = 234
99554 deg
ZDOT = -1043
663779 TA = 141
01667
MA = 140
96777
Ha = 193
254 n
mi
Hp = 190
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13334123
85 X = 4054615
64
Y = -4642512
45 feet Y = -1369642
61 meter
Z = 16983481
27 Z = 5196285
57
XDOT = 12014
494701 XDOT = 3592
069873
YDOT = 21930
332459 feet/sec YDOT = 6724
925067 meter/sec
ZDOT = -3424
093764 ZDOT = -1026
044145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13893895
65 X = -4234859
39
Y = -1904197
34 feet Y = -580399
35 meter
Z = 17062359
53 Z = 5200607
19
XDOT = -847
195164 XDOT = -258
225086
YDOT = -23992
125525 feet/sec YDOT = -7312
799860 meter/sec
ZDOT = -3353
504313 ZDOT = -1022
148114
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 10237
54598459
00016717 00000-0 10270-3 0 9065
2 25544 51
6420 235
6994 0008152 292
6349 67
3950 15
71262410 34386
Satellite: ISS
Catalog Number: 25544
Epoch time: 10237
54598459 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 235
6994 deg
Eccentricity:
0008152
Arg of perigee: 292
6349 deg
Mean anomaly: 67
3950 deg
Mean motion: 15
71262410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 325
Coasting Arc #8 (Orbit 3452)
---------------------------------------
Vector Time (GMT): 2010/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4315813
49 A = 6739768
66 meter
Y = -5165991
72 meter E =
0012134
Z = 37133
78 I = 51
40135
XDOT = 3708
401758 Wp = 7
25599
YDOT = -3053
397965 meter/sec RA = 229
87138 deg
ZDOT = 6017
373503 TA = 353
14842
MA = 353
16500
Ha = 193
279 n
mi
Hp = 190
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14159493
09 X = -4257906
05
Y = -16948791
72 feet Y = -5213929
95 meter
Z = 121829
99 Z = 16308
71
XDOT = 12166
672435 XDOT = 3713
038780
YDOT = -10017
709860 feet/sec YDOT = -3011
902146 meter/sec
ZDOT = 19742
039052 ZDOT = 6035
400160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5241525
30 X = 1597616
91
Y = 21454429
93 feet Y = 6539310
24 meter
Z = 38428
16 Z = 11712
90
XDOT = -13666
273457 XDOT = -4165
480150
YDOT = 3299
553250 feet/sec YDOT = 1005
703831 meter/sec
ZDOT = 19814
115959 ZDOT = 6039
342544
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 10238
56357775
00016717 00000-0 10270-3 0 9073
2 25544 51
6422 230
4953 0008040 295
5747 64
4583 15
71337949 34533
Satellite: ISS
Catalog Number: 25544
Epoch time: 10238
56357775 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 230
4953 deg
Eccentricity:
0008040
Arg of perigee: 295
5747 deg
Mean anomaly: 64
4583 deg
Mean motion: 15
71337949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3453
Checksum: 330
Coasting Arc #9 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2010/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2164302
70 A = 6728124
42 meter
Y = 3697525
84 meter E =
0009567
Z = -5194869
03 I = 51
38186
XDOT = -5926
924840 Wp = 50
74644
YDOT = -4808
171022 meter/sec RA = 224
74608 deg
ZDOT = -948
199986 TA = 210
14680
MA = 210
20189
Ha = 193
630 n
mi
Hp = 190
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7100730
65 X = -2180252
67
Y = 12130990
28 feet Y = 3673233
83 meter
Z = -17043533
57 Z = -5205422
10
XDOT = -19445
291471 XDOT = -5868
112328
YDOT = -15774
839311 feet/sec YDOT = -4874
120664 meter/sec
ZDOT = -3110
892343 ZDOT = -976
849688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11493102
66 X = 3503097
69
Y = -8003179
71 feet Y = -2439369
17 meter
Z = -17085697
04 Z = -5207720
46
XDOT = 10292
074989 XDOT = 3137
024457
YDOT = 21699
827003 feet/sec YDOT = 6614
107270 meter/sec
ZDOT = -3225
604045 ZDOT = -983
164113
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 10239
51756045
00016717 00000-0 10270-3 0 9083
2 25544 51
6418 225
6152 0008169 300
7917 59
2440 15
71301406 34695
Satellite: ISS
Catalog Number: 25544
Epoch time: 10239
51756045 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 225
6152 deg
Eccentricity:
0008169
Arg of perigee: 300
7917 deg
Mean anomaly: 59
2440 deg
Mean motion: 15
71301406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 302
Coasting Arc #10 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2010/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5770502
82 A = 6738456
66 meter
Y = 3051939
19 meter E =
0006017
Z = 1663013
11 I = 51
43985
XDOT = -1024
789495 Wp = 102
57951
YDOT = 5056
321056 meter/sec RA = 219
59082 deg
ZDOT = -5707
295216 TA = 59
01680
MA = 58
95770
Ha = 193
828 n
mi
Hp = 189
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18932095
88 X = 5727868
00
Y = 10012923
87 feet Y = 3116230
12 meter
Z = 5456079
75 Z = 1690942
43
XDOT = -3362
170258 XDOT = -1053
529083
YDOT = 16588
979843 feet/sec YDOT = 5044
700253 meter/sec
ZDOT = -18724
721837 ZDOT = -5712
343708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13140703
50 X = -4005286
43
Y = -16875196
23 feet Y = -5143559
81 meter
Z = 5567887
25 Z = 1697092
03
XDOT = 8529
300064 XDOT = 2599
730660
YDOT = -12843
573546 feet/sec YDOT = -3914
721217 meter/sec
ZDOT = -18744
836077 ZDOT = -5713
426036
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 10240
53512282
00016717 00000-0 10270-3 0 9091
2 25544 51
6420 220
4103 0008353 305
4264 54
6117 15
71358129 34851
Satellite: ISS
Catalog Number: 25544
Epoch time: 10240
53512282 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 220
4103 deg
Eccentricity:
0008353
Arg of perigee: 305
4264 deg
Mean anomaly: 54
6117 deg
Mean motion: 15
71358129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 276
Coasting Arc #11 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2010/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -476095
18 A = 6730234
16 meter
Y = -4833272
57 meter E =
0001668
Z = 4658057
23 I = 51
43643
XDOT = 6879
240362 Wp = 21
04477
YDOT = 2019
397278 meter/sec RA = 214
49875 deg
ZDOT = 2799
700567 TA = 41
23816
MA = 41
22556
Ha = 193
904 n
mi
Hp = 189
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1561992
08 X = -444641
28
Y = -15857193
48 feet Y = -4838420
49 meter
Z = 15282339
99 Z = 4655820
96
XDOT = 22569
686226 XDOT = 6842
547353
YDOT = 6625
319152 feet/sec YDOT = 2096
120022 meter/sec
ZDOT = 9185
369315 ZDOT = 2833
030738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4725438
13 X = -1440313
54
Y = 15226182
66 feet Y = 4640940
47 meter
Z = 15273307
30 Z = 4655304
07
XDOT = -16976
006861 XDOT = -5174
286891
YDOT = -14612
089141 feet/sec YDOT = -4453
764770 meter/sec
ZDOT = 9318
778409 ZDOT = 2840
363659
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 10241
55266843
00016717 00000-0 10270-3 0 9105
2 25544 51
6421 215
2058 0008397 308
2283 51
8122 15
71382770 35016
Satellite: ISS
Catalog Number: 25544
Epoch time: 10241
55266843 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 215
2058 deg
Eccentricity:
0008397
Arg of perigee: 308
2283 deg
Mean anomaly: 51
8122 deg
Mean motion: 15
71382770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 285
Coasting Arc #12 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2010/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5922372
13 A = 6735208
18 meter
Y = -432802
90 meter E =
0006584
Z = -3169626
66 I = 51
47895
XDOT = -2162
477647 Wp = 346
69013
YDOT = -5606
806566 meter/sec RA = 209
32415 deg
ZDOT = 4810
452782 TA = 336
30603
MA = 336
33633
Ha = 194
037 n
mi
Hp = 189
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19430354
76 X = -5901694
77
Y = -1419957
01 feet Y = -498914
88 meter
Z = -10399037
61 Z = -3198347
38
XDOT = -7094
742936 XDOT = -2122
988958
YDOT = -18395
034664 feet/sec YDOT = -5630
767768 meter/sec
ZDOT = 15782
325399 ZDOT = 4800
043502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17395086
12 X = 5302022
25
Y = 8634934
52 feet Y = 2631928
04 meter
Z = -10513982
70 Z = -3204661
93
XDOT = 332
762632 XDOT = 101
426050
YDOT = 18478
447920 feet/sec YDOT = 5632
230926 meter/sec
ZDOT = 15740
570611 ZDOT = 4797
725922
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 10242
50660243
00016717 00000-0 10270-3 0 9114
2 25544 51
6421 210
3262 0008339 313
0191 47
0272 15
71372022 35165
Satellite: ISS
Catalog Number: 25544
Epoch time: 10242
50660243 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 210
3262 deg
Eccentricity:
0008339
Arg of perigee: 313
0191 deg
Mean anomaly: 47
0272 deg
Mean motion: 15
71372022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 253
Coasting Arc #13 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2010/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3231730
11 A = 6733782
73 meter
Y = 4645131
39 meter E =
0007078
Z = -3656157
64 I = 51
50199
XDOT = -6280
297254 Wp = 358
41014
YDOT = 952
166269 meter/sec RA = 204
24870 deg
ZDOT = -4334
366071 TA = 225
49102
MA = 225
54888
Ha = 194
258 n
mi
Hp = 189
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10602789
08 X = 3197308
21
Y = 15239932
37 feet Y = 4681078
03 meter
Z = -11995267
84 Z = -3640541
51
XDOT = -20604
649785 XDOT = -6269
422166
YDOT = 3123
905083 feet/sec YDOT = 881
996987 meter/sec
ZDOT = -14220
361125 ZDOT = -4364
849421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4433975
29 X = -1351475
67
Y = -18069642
20 feet Y = -5507626
94 meter
Z = -11932687
02 Z = -3637083
00
XDOT = 18941
544782 XDOT = 5773
382849
YDOT = 4838
945456 feet/sec YDOT = 1474
910575 meter/sec
ZDOT = -14342
347299 ZDOT = -4371
547457
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 10243
52411398
00016717 00000-0 10270-3 0 9123
2 25544 51
6427 205
1211 0008392 316
9372 43
1133 15
71426858 35327
Satellite: ISS
Catalog Number: 25544
Epoch time: 10243
52411398 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 205
1211 deg
Eccentricity:
0008392
Arg of perigee: 316
9372 deg
Mean anomaly: 43
1133 deg
Mean motion: 15
71426858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 284
Coasting Arc #14 (Orbit 3547)
---------------------------------------
Vector Time (GMT): 2010/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4772572
70 A = 6731258
55 meter
Y = -1980064
30 meter E =
0010317
Z = 4316767
23 I = 51
52206
XDOT = 5062
576879 Wp = 20
88232
YDOT = 4652
724740 meter/sec RA = 199
07431 deg
ZDOT = -3450
958993 TA = 104
13434
MA = 104
01967
Ha = 194
328 n
mi
Hp = 189
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15658046
93 X = 4773389
35
Y = -6496273
95 feet Y = -1926689
99 meter
Z = 14162622
13 Z = 4339954
37
XDOT = 16609
504197 XDOT = 5026
937136
YDOT = 15264
844948 feet/sec YDOT = 4709
138253 meter/sec
ZDOT = -11322
043941 ZDOT = -3426
451531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16859344
70 X = -5138728
26
Y = 708490
10 feet Y = 215947
78 meter
Z = 14255399
42 Z = 4345045
74
XDOT = -10316
019891 XDOT = -3144
322863
YDOT = -18860
787546 feet/sec YDOT = -5748
768044 meter/sec
ZDOT = -11223
866678 ZDOT = -3421
034563
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 10244
54160719
00016717 00000-0 10270-3 0 9135
2 25544 51
6426 199
9164 0008481 320
2857 39
7683 15
71452625 35487
Satellite: ISS
Catalog Number: 25544
Epoch time: 10244
54160719 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 199
9164 deg
Eccentricity:
0008481
Arg of perigee: 320
2857 deg
Mean anomaly: 39
7683 deg
Mean motion: 15
71452625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3548
Checksum: 326
Coasting Arc #15 (Orbit 3563)
---------------------------------------
Vector Time (GMT): 2010/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5424531
10 A = 6737087
25 meter
Y = -3240981
23 meter E =
0013807
Z = 2310000
67 I = 51
57096
XDOT = 4318
008771 Wp = 37
49235
YDOT = -3357
785508 meter/sec RA = 193
99627 deg
ZDOT = 5422
686870 TA = 348
50214
MA = 348
53364
Ha = 194
493 n
mi
Hp = 188
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17797018
04 X = -5399108
22
Y = -10633140
52 feet Y = -3301499
47 meter
Z = 7578742
35 Z = 2283710
08
XDOT = 14166
695444 XDOT = 4328
892865
YDOT = -11016
356655 feet/sec YDOT = -3309
438163 meter/sec
ZDOT = 17790
967422 ZDOT = 5443
690088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13338801
06 X = 4065666
56
Y = 15920394
56 feet Y = 4852536
26 meter
Z = 7473438
78 Z = 2277904
14
XDOT = -15745
580853 XDOT = -4799
253044
YDOT = 4791
729503 feet/sec YDOT = 1460
519152 meter/sec
ZDOT = 17874
989301 ZDOT = 5448
296739
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 10245
55908156
00016717 00000-0 10270-3 0 9143
2 25544 51
6428 194
7111 0008415 323
8051 36
2541 15
71488247 35648
Satellite: ISS
Catalog Number: 25544
Epoch time: 10245
55908156 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 194
7111 deg
Eccentricity:
0008415
Arg of perigee: 323
8051 deg
Mean anomaly: 36
2541 deg
Mean motion: 15
71488247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3564
Checksum: 305
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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