Date:
October 2nd 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) : 88 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 19)
---------------------------------------
Vector Time (GMT): 2010/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2496548
50 A = 6735869
84 meter
Y = 5636953
72 meter E =
0019853
Z = 2687673
34 I = 51
90067
XDOT = -5667
371998 Wp = 69
35804
YDOT = 10
101100 meter/sec RA = 46
12403 deg
ZDOT = 5219
204419 TA = 321
16091
MA = 321
30341
Ha = 196
025 n
mi
Hp = 185
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8190775
90 X = 2420273
18
Y = 18493942
66 feet Y = 5664445
22 meter
Z = 8817825
93 Z = 2699616
22
XDOT = -18593
740150 XDOT = -5692
417844
YDOT = 33
140093 feet/sec YDOT = -53
414749 meter/sec
ZDOT = 17123
374078 ZDOT = 5191
611321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11030046
69 X = -3361958
23
Y = -16929458
87 feet Y = -5160099
06 meter
Z = 8865679
43 Z = 2702259
09
XDOT = 17207
532054 XDOT = 5244
855770
YDOT = -2260
977573 feet/sec YDOT = -689
145964 meter/sec
ZDOT = 17012
730997 ZDOT = 5185
480408
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 10274
55815304
00016717 00000-0 10270-3 0 9002
2 25544 51
6450 46
3970 0006738 51
3589 308
8176 15
71593687 204
Satellite: ISS
Catalog Number: 25544
Epoch time: 10274
55815304 = yrday
fracday
Element set: 900
Inclination: 51
6450 deg
RA of node: 46
3970 deg
Eccentricity:
0006738
Arg of perigee: 51
3589 deg
Mean anomaly: 308
8176 deg
Mean motion: 15
71593687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 20
Checksum: 310
Coasting Arc #2 (Orbit 34)
---------------------------------------
Vector Time (GMT): 2010/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4438318
43 A = 6728669
52 meter
Y = -1255923
23 meter E =
0017326
Z = -4913486
23 I = 51
85459
XDOT = 4207
124917 Wp = 87
99699
YDOT = 6016
647746 meter/sec RA = 40
98416 deg
ZDOT = 2269
813846 TA = 204
02278
MA = 204
10371
Ha = 196
109 n
mi
Hp = 185
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14561412
19 X = 4475901
44
Y = -4120483
05 feet Y = -1206081
37 meter
Z = -16120361
66 Z = -4891833
47
XDOT = 13802
903271 XDOT = 4128
506584
YDOT = 19739
657958 feet/sec YDOT = 6063
254864 meter/sec
ZDOT = 7446
895819 ZDOT = 2290
060894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13681528
55 X = -4170129
90
Y = 6679888
23 feet Y = 2036029
93 meter
Z = -16033528
47 Z = -4887019
48
XDOT = -16584
914661 XDOT = -5055
081989
YDOT = -15958
305149 feet/sec YDOT = -4864
091409 meter/sec
ZDOT = 7528
043801 ZDOT = 2294
547750
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 10275
51196437
00016717 00000-0 10270-3 0 9019
2 25544 51
6450 41
5177 0006864 54
0011 306
1786 15
71607135 358
Satellite: ISS
Catalog Number: 25544
Epoch time: 10275
51196437 = yrday
fracday
Element set: 901
Inclination: 51
6450 deg
RA of node: 41
5177 deg
Eccentricity:
0006864
Arg of perigee: 54
0011 deg
Mean anomaly: 306
1786 deg
Mean motion: 15
71607135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 35
Checksum: 281
Coasting Arc #3 (Orbit 50)
---------------------------------------
Vector Time (GMT): 2010/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4712862
45 A = 6738143
17 meter
Y = -4644638
60 meter E =
0011737
Z = -1270577
88 I = 51
86360
XDOT = 4191
960733 Wp = 106
20565
YDOT = -2659
447558 meter/sec RA = 35
91133 deg
ZDOT = -5875
072744 TA = 87
66618
MA = 87
53179
Ha = 196
068 n
mi
Hp = 185
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15462147
15 X = -4654402
72
Y = -15238315
63 feet Y = -4697013
88 meter
Z = -4168562
60 Z = -1293330
70
XDOT = 13753
152010 XDOT = 4249
927715
YDOT = -8725
221647 feet/sec YDOT = -2612
246820 meter/sec
ZDOT = -19275
173045 ZDOT = -5854
567176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18124833
05 X = 5524449
11
Y = 11916626
46 feet Y = 3632187
75 meter
Z = -4259766
74 Z = -1298376
90
XDOT = -11018
734761 XDOT = -3358
510355
YDOT = 9953
279073 feet/sec YDOT = 3033
759462 meter/sec
ZDOT = -19192
930234 ZDOT = -5850
005135
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 10276
52933841
00016717 00000-0 10270-3 0 9020
2 25544 51
6453 36
3107 0006926 57
1302 303
0526 15
71647165 515
Satellite: ISS
Catalog Number: 25544
Epoch time: 10276
52933841 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 36
3107 deg
Eccentricity:
0006926
Arg of perigee: 57
1302 deg
Mean anomaly: 303
0526 deg
Mean motion: 15
71647165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 51
Checksum: 279
Coasting Arc #4 (Orbit 66)
---------------------------------------
Vector Time (GMT): 2010/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2674238
40 A = 6726796
80 meter
Y = 3222316
21 meter E =
0009852
Z = 5257542
43 I = 51
80149
XDOT = -6353
961928 Wp = 60
67863
YDOT = -4317
661511 meter/sec RA = 30
79038 deg
ZDOT = -580
120393 TA = 34
85204
MA = 34
78756
Ha = 196
145 n
mi
Hp = 185
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8773748
04 X = -2735612
46
Y = 10571903
57 feet Y = 3192068
59 meter
Z = 17249154
94 Z = 5244401
56
XDOT = -20846
331784 XDOT = -6302
390665
YDOT = -14165
556140 feet/sec YDOT = -4388
427035 meter/sec
ZDOT = -1903
282129 ZDOT = -610
862380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6421977
89 X = 1957418
86
Y = -12219564
89 feet Y = -3724523
38 meter
Z = 17196440
90 Z = 5241475
19
XDOT = 22481
519943 XDOT = 6852
367279
YDOT = 8937
578400 feet/sec YDOT = 2724
173896 meter/sec
ZDOT = -2026
520737 ZDOT = -617
683521
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 10277
54668799
00016717 00000-0 10270-3 0 9031
2 25544 51
6463 31
1049 0006959 59
6962 300
4887 15
71693428 670
Satellite: ISS
Catalog Number: 25544
Epoch time: 10277
54668799 = yrday
fracday
Element set: 903
Inclination: 51
6463 deg
RA of node: 31
1049 deg
Eccentricity:
0006959
Arg of perigee: 59
6962 deg
Mean anomaly: 300
4887 deg
Mean motion: 15
71693428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 67
Checksum: 345
Coasting Arc #5 (Orbit 81)
---------------------------------------
Vector Time (GMT): 2010/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6147288
67 A = 6738714
23 meter
Y = 2729810
61 meter E =
0018596
Z = -260157
85 I = 51
81560
XDOT = -1729
986616 Wp = 50
27481
YDOT = 4443
695629 meter/sec RA = 25
68765 deg
ZDOT = 6045
169793 TA = 306
90676
MA = 307
07701
Ha = 196
130 n
mi
Hp = 184
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20168269
92 X = 6117570
35
Y = 8956071
56 feet Y = 2798387
10 meter
Z = -853536
26 Z = -230366
59
XDOT = -5675
809109 XDOT = -1808
914832
YDOT = 14579
053901 feet/sec YDOT = 4423
909234 meter/sec
ZDOT = 19833
234230 ZDOT = 6036
573249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21690560
92 X = -6611282
97
Y = -4084055
67 feet Y = -1244820
17 meter
Z = -734104
91 Z = -223755
18
XDOT = 1992
614712 XDOT = 607
348964
YDOT = -13938
765423 feet/sec YDOT = -4248
535701 meter/sec
ZDOT = 19798
734046 ZDOT = 6034
654137
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 10278
50043178
00016717 00000-0 10270-3 0 9047
2 25544 51
6469 26
2247 0007062 62
8119 297
3762 15
71697765 828
Satellite: ISS
Catalog Number: 25544
Epoch time: 10278
50043178 = yrday
fracday
Element set: 904
Inclination: 51
6469 deg
RA of node: 26
2247 deg
Eccentricity:
0007062
Arg of perigee: 62
8119 deg
Mean anomaly: 297
3762 deg
Mean motion: 15
71697765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 82
Checksum: 319
Coasting Arc #6 (Orbit 97)
---------------------------------------
Vector Time (GMT): 2010/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 278165
49 A = 6726941
10 meter
Y = -4277306
25 meter E =
0021220
Z = -5202977
89 I = 51
74888
XDOT = 7375
749705 Wp = 76
25599
YDOT = 1834
271430 meter/sec RA = 20
59178 deg
ZDOT = -1112
456637 TA = 183
11015
MA = 183
12337
Ha = 196
027 n
mi
Hp = 184
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 912616
44 X = 351249
91
Y = -14033157
00 feet Y = -4273787
60 meter
Z = -17070137
44 Z = -5201448
53
XDOT = 24198
653889 XDOT = 7360
094541
YDOT = 6017
950886 feet/sec YDOT = 1916
663836 meter/sec
ZDOT = -3649
792116 ZDOT = -1076
663014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2474582
00 X = 754252
59
Y = 13850964
65 feet Y = 4221774
03 meter
Z = -17063973
11 Z = -5201099
00
XDOT = -23945
921232 XDOT = -7298
716791
YDOT = -46
171374 feet/sec YDOT = -14
073035 meter/sec
ZDOT = -3506
296939 ZDOT = -1068
719307
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 10279
51773423
00016717 00000-0 10270-3 0 9053
2 25544 51
6473 21
0191 0006959 66
1020 294
0871 15
71738168 981
Satellite: ISS
Catalog Number: 25544
Epoch time: 10279
51773423 = yrday
fracday
Element set: 905
Inclination: 51
6473 deg
RA of node: 21
0191 deg
Eccentricity:
0006959
Arg of perigee: 66
1020 deg
Mean anomaly: 294
0871 deg
Mean motion: 15
71738168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 98
Checksum: 308
Coasting Arc #7 (Orbit 113)
---------------------------------------
Vector Time (GMT): 2010/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6508151
77 A = 6737394
00 meter
Y = -443010
44 meter E =
0019668
Z = 1658985
45 I = 51
75522
XDOT = -1135
507643 Wp = 101
13499
YDOT = -5006
339549 meter/sec RA = 15
45754 deg
ZDOT = -5737
980138 TA = 60
57476
MA = 60
37860
Ha = 196
081 n
mi
Hp = 184
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21352203
96 X = -6510773
44
Y = -1453446
33 feet Y = -515802
99 meter
Z = 5442865
65 Z = 1627361
93
XDOT = -3725
418776 XDOT = -1051
566825
YDOT = -16424
998521 feet/sec YDOT = -5018
568741 meter/sec
ZDOT = -18825
394153 ZDOT = -5743
292118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21013585
87 X = 6404940
97
Y = -4221649
96 feet Y = -1286758
91 meter
Z = 5316087
56 Z = 1620343
49
XDOT = 7498
306857 XDOT = 2285
483930
YDOT = 13364
732448 feet/sec YDOT = 4073
570450 meter/sec
ZDOT = -18846
647568 ZDOT = -5744
458179
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 10280
53501282
00016717 00000-0 10270-3 0 9060
2 25544 51
6470 15
8132 0007094 70
5706 289
6222 15
71770942 1140
Satellite: ISS
Catalog Number: 25544
Epoch time: 10280
53501282 = yrday
fracday
Element set: 906
Inclination: 51
6470 deg
RA of node: 15
8132 deg
Eccentricity:
0007094
Arg of perigee: 70
5706 deg
Mean anomaly: 289
6222 deg
Mean motion: 15
71770942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 114
Checksum: 284
Coasting Arc #8 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2010/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2249982
61 A = 6728511
57 meter
Y = 4210669
77 meter E =
0013420
Z = 4730573
48 I = 51
69737
XDOT = -7180
525610 Wp = 96
33981
YDOT = 828
488486 meter/sec RA = 10
38063 deg
ZDOT = 2669
904714 TA = 327
41699
MA = 327
49974
Ha = 195
895 n
mi
Hp = 184
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7381832
72 X = 2179750
09
Y = 13814533
38 feet Y = 4235438
13 meter
Z = 15520254
19 Z = 4741333
20
XDOT = -23558
154889 XDOT = -7202
226462
YDOT = 2718
138076 feet/sec YDOT = 748
070418 meter/sec
ZDOT = 8759
529900 ZDOT = 2634
968126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10860892
44 X = -3310400
02
Y = -11226500
12 feet Y = -3421837
24 meter
Z = 15563347
57 Z = 4743708
34
XDOT = 21089
903061 XDOT = 6428
202453
YDOT = -8418
030726 feet/sec YDOT = -2565
815765 meter/sec
ZDOT = 8619
464824 ZDOT = 2627
212878
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 10281
55226442
00016717 00000-0 10270-3 0 9076
2 25544 51
6477 10
6067 0007060 73
3035 286
8901 15
71850068 1305
Satellite: ISS
Catalog Number: 25544
Epoch time: 10281
55226442 = yrday
fracday
Element set: 907
Inclination: 51
6477 deg
RA of node: 10
6067 deg
Eccentricity:
0007060
Arg of perigee: 73
3035 deg
Mean anomaly: 286
8901 deg
Mean motion: 15
71850068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 130
Checksum: 285
Coasting Arc #9 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2010/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5780640
44 A = 6734628
25 meter
Y = -1810388
55 meter E =
0011617
Z = -2947746
14 I = 51
68729
XDOT = 3903
547101 Wp = 71
18160
YDOT = 4334
072159 meter/sec RA = 5
22253 deg
ZDOT = 5012
909470 TA = 254
92370
MA = 255
05227
Ha = 195
997 n
mi
Hp = 184
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18965355
76 X = 5814774
88
Y = -5939594
98 feet Y = -1745555
26 meter
Z = -9671083
15 Z = -2919580
08
XDOT = 12806
913062 XDOT = 3830
440165
YDOT = 14219
396846 feet/sec YDOT = 4377
315485 meter/sec
ZDOT = 16446
553379 ZDOT = 5031
695548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16411551
07 X = -5002240
77
Y = 11304692
56 feet Y = 3445670
29 meter
Z = -9558152
26 Z = -2913324
81
XDOT = -15524
497165 XDOT = -4731
866736
YDOT = -8623
750380 feet/sec YDOT = -2628
519116 meter/sec
ZDOT = 16521
813825 ZDOT = 5035
848854
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 10282
50591766
00016717 00000-0 10270-3 0 9087
2 25544 51
6473 5
7267 0007075 75
3222 284
8724 15
71845905 1455
Satellite: ISS
Catalog Number: 25544
Epoch time: 10282
50591766 = yrday
fracday
Element set: 908
Inclination: 51
6473 deg
RA of node: 5
7267 deg
Eccentricity:
0007075
Arg of perigee: 75
3222 deg
Mean anomaly: 284
8724 deg
Mean motion: 15
71845905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 145
Checksum: 316
Coasting Arc #10 (Orbit 160)
---------------------------------------
Vector Time (GMT): 2010/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4420189
23 A = 6731247
44 meter
Y = -3164576
51 meter E =
0014252
Z = -3984094
04 I = 51
64530
XDOT = 5798
577764 Wp = 75
11417
YDOT = -3120
299025 meter/sec RA =
15472 deg
ZDOT = -3963
012308 TA = 153
80719
MA = 153
73504
Ha = 195
926 n
mi
Hp = 184
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14501933
17 X = -4365119
36
Y = -10382468
88 feet Y = -3213697
94 meter
Z = -13071174
68 Z = -4005433
96
XDOT = 19024
205261 XDOT = 5852
290607
YDOT = -10237
201524 feet/sec YDOT = -3055
155646 meter/sec
ZDOT = -13002
008885 ZDOT = -3934
711586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16945826
13 X = 5165087
80
Y = 5357057
06 feet Y = 1632830
99 meter
Z = -13156680
79 Z = -4010156
31
XDOT = -14556
079461 XDOT = -4436
693020
YDOT = 14456
786654 feet/sec YDOT = 4406
428572 meter/sec
ZDOT = -12888
521474 ZDOT = -3928
421345
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 10283
52312299
00016717 00000-0 10270-3 0 9093
2 25544 51
6464
5199 0007140 79
4887 280
7079 15
71883444 1613
Satellite: ISS
Catalog Number: 25544
Epoch time: 10283
52312299 = yrday
fracday
Element set: 909
Inclination: 51
6464 deg
RA of node:
5199 deg
Eccentricity:
0007140
Arg of perigee: 79
4887 deg
Mean anomaly: 280
7079 deg
Mean motion: 15
71883444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 161
Checksum: 320
Coasting Arc #11 (Orbit 176)
---------------------------------------
Vector Time (GMT): 2010/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4181410
15 A = 6731329
76 meter
Y = 3497066
96 meter E =
0018335
Z = 3936233
32 I = 51
61608
XDOT = -6016
687282 Wp = 80
02316
YDOT = -2659
983606 meter/sec RA = 354
98329 deg
ZDOT = -4009
338660 TA = 51
65876
MA = 51
49411
Ha = 195
911 n
mi
Hp = 184
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13718537
23 X = -4239326
12
Y = 11473316
81 feet Y = 3449984
16 meter
Z = 12914151
30 Z = 3915778
88
XDOT = -19739
787671 XDOT = -5967
018637
YDOT = -8726
980335 feet/sec YDOT = -2726
988165 meter/sec
ZDOT = -13153
998229 ZDOT = -4038
447630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9257011
89 X = 2821537
22
Y = -15370597
31 feet Y = -4684958
06 meter
Z = 12832109
55 Z = 3911226
99
XDOT = 20316
723764 XDOT = 6192
537403
YDOT = 1104
759619 feet/sec YDOT = 336
730732 meter/sec
ZDOT = -13270
651954 ZDOT = -4044
894716
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 10284
54030207
00016717 00000-0 10270-3 0 9104
2 25544 51
6468 355
3127 0007180 81
3966 278
8009 15
71964595 1778
Satellite: ISS
Catalog Number: 25544
Epoch time: 10284
54030207 = yrday
fracday
Element set: 910
Inclination: 51
6468 deg
RA of node: 355
3127 deg
Eccentricity:
0007180
Arg of perigee: 81
3966 deg
Mean anomaly: 278
8009 deg
Mean motion: 15
71964595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 177
Checksum: 316
Coasting Arc #12 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2010/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5885512
07 A = 6734026
15 meter
Y = 1340160
65 meter E =
0020502
Z = 2964953
20 I = 51
59489
XDOT = -3584
686411 Wp = 83
74486
YDOT = 4652
208950 meter/sec RA = 349
91125 deg
ZDOT = 4985
689396 TA = 310
49160
MA = 310
67009
Ha = 195
778 n
mi
Hp = 184
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19309422
81 X = 5855685
28
Y = 4396852
52 feet Y = 1405809
23 meter
Z = 9727536
74 Z = 2993473
02
XDOT = -11760
782189 XDOT = -3660
661820
YDOT = 15263
152722 feet/sec YDOT = 4611
698071 meter/sec
ZDOT = 16357
248675 ZDOT = 4968
090123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19586659
81 X = -5970013
91
Y = 2512350
47 feet Y = 765764
42 meter
Z = 9841846
61 Z = 2999794
85
XDOT = 6048
902347 XDOT = 1843
705435
YDOT = -16988
518406 feet/sec YDOT = -5178
100410 meter/sec
ZDOT = 16286
634413 ZDOT = 4964
166169
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 10285
55745742
00016717 00000-0 10270-3 0 9114
2 25544 51
6462 350
1058 0007261 85
7102 274
4889 15
71981252 1933
Satellite: ISS
Catalog Number: 25544
Epoch time: 10285
55745742 = yrday
fracday
Element set: 911
Inclination: 51
6462 deg
RA of node: 350
1058 deg
Eccentricity:
0007261
Arg of perigee: 85
7102 deg
Mean anomaly: 274
4889 deg
Mean motion: 15
71981252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 193
Checksum: 311
Coasting Arc #13 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2010/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2002785
61 A = 6728365
61 meter
Y = -4406872
81 meter E =
0017987
Z = -4689889
45 I = 51
54560
XDOT = 7162
426168 Wp = 100
29072
YDOT = 320
640425 meter/sec RA = 344
74105 deg
ZDOT = 2763
197137 TA = 197
01618
MA = 197
07657
Ha = 195
836 n
mi
Hp = 184
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6570818
94 X = 2074698
14
Y = -14458244
13 feet Y = -4384074
42 meter
Z = -15386776
42 Z = -4679985
08
XDOT = 23498
773516 XDOT = 7144
885096
YDOT = 1051
969899 feet/sec YDOT = 400
636927 meter/sec
ZDOT = 9065
607406 ZDOT = 2797
950022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -993332
57 X = -302767
77
Y = 15888734
55 feet Y = 4842886
29 meter
Z = -15347012
02 Z = -4677769
26
XDOT = -21084
890669 XDOT = -6426
674676
YDOT = 7554
394514 feet/sec YDOT = 2302
579448 meter/sec
ZDOT = 9204
919064 ZDOT = 2805
659331
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 10286
51101801
00016717 00000-0 10270-3 0 9124
2 25544 51
6456 345
2239 0007370 87
8610 272
3396 15
72016707 2082
Satellite: ISS
Catalog Number: 25544
Epoch time: 10286
51101801 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 345
2239 deg
Eccentricity:
0007370
Arg of perigee: 87
8610 deg
Mean anomaly: 272
3396 deg
Mean motion: 15
72016707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 290
Coasting Arc #14 (Orbit 223)
---------------------------------------
Vector Time (GMT): 2010/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6422595
98 A = 6736137
46 meter
Y = 803960
01 meter E =
0013161
Z = -1862888
08 I = 51
54388
XDOT = 981
536771 Wp = 114
97976
YDOT = -5140
448527 meter/sec RA = 339
65202 deg
ZDOT = -5638
946868 TA = 85
70291
MA = 85
55253
Ha = 195
763 n
mi
Hp = 184
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21071509
13 X = -6422059
01
Y = 2637664
07 feet Y = 732141
65 meter
Z = -6111837
53 Z = -1894088
05
XDOT = 3220
264997 XDOT = 1066
338510
YDOT = -16864
988607 feet/sec YDOT = -5128
998353 meter/sec
ZDOT = -18500
481849 ZDOT = -5633
972430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18488665
68 X = 5635345
30
Y = -10372577
95 feet Y = -3161561
76 meter
Z = -6236921
92 Z = -1901013
80
XDOT = 2517
247749 XDOT = 767
257114
YDOT = 15528
434126 feet/sec YDOT = 4733
066722 meter/sec
ZDOT = -18480
472304 ZDOT = -5632
847958
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 10287
52812485
00016717 00000-0 10270-3 0 9134
2 25544 51
6460 340
0159 0007450 91
2029 268
9987 15
72057176 2243
Satellite: ISS
Catalog Number: 25544
Epoch time: 10287
52812485 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 340
0159 deg
Eccentricity:
0007450
Arg of perigee: 91
2029 deg
Mean anomaly: 268
9987 deg
Mean motion: 15
72057176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 224
Checksum: 311
Coasting Arc #15 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2010/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 299202
54 A = 6726195
21 meter
Y = 4359053
67 meter E =
0011289
Z = 5104739
92 I = 51
48247
XDOT = -7247
159424 Wp = 78
72276
YDOT = 2188
521561 meter/sec RA = 334
49346 deg
ZDOT = -1439
197916 TA = 25
11452
MA = 25
05966
Ha = 195
653 n
mi
Hp = 184
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 981635
63 X = 225638
46
Y = 14301357
17 feet Y = 4361988
39 meter
Z = 16747834
39 Z = 5106014
62
XDOT = -23776
769763 XDOT = -7264
101830
YDOT = 7180
188850 feet/sec YDOT = 2107
384690 meter/sec
ZDOT = -4721
777939 ZDOT = -1474
446116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6429847
49 X = -1959817
52
Y = -12805472
72 feet Y = -3903108
08 meter
Z = 16752889
66 Z = 5106280
77
XDOT = 18084
443470 XDOT = 5512
138370
YDOT = -15463
550231 feet/sec YDOT = -4713
290110 meter/sec
ZDOT = -4863
106773 ZDOT = -1482
274945
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 10288
54520489
00016717 00000-0 10270-3 0 9148
2 25544 51
6458 334
8085 0007320 94
7220 265
4778 15
72114278 2401
Satellite: ISS
Catalog Number: 25544
Epoch time: 10288
54520489 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 334
8085 deg
Eccentricity:
0007320
Arg of perigee: 94
7220 deg
Mean anomaly: 265
4778 deg
Mean motion: 15
72114278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 313
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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