Date:
October 30th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6113 9 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 1451)
---------------------------------------
Vector Time (GMT): 2006/303/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4250166
98 A = 6712112
69 meter
Y = -1997044
83 meter E =
0013398
Z = 4783437
85 I = 51
46688
XDOT = 5196
681502 Wp = 123
44061
YDOT = 5139
749067 meter/sec RA = 209
04710 deg
ZDOT = -2473
866953 TA = 350
74207
MA = 350
76674
Ha = 188
301 n
mi
Hp = 175
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13944117
40 X = 4248944
98
Y = -6551984
35 feet Y = -1949524
02 meter
Z = 15693693
74 Z = 4804082
40
XDOT = 17049
479992 XDOT = 5150
839624
YDOT = 16862
693788 feet/sec YDOT = 5197
604971 meter/sec
ZDOT = -8116
361394 ZDOT = -2448
732432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3112470
74 X = -948681
08
Y = 15008848
66 feet Y = 4574697
07 meter
Z = 15770412
80 Z = 4806821
82
XDOT = -22661
543094 XDOT = -6907
238335
YDOT = 3721
503756 feet/sec YDOT = 1134
314345 meter/sec
ZDOT = -8021
902989 ZDOT = -2445
076031
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 06303
58500863
00020000 00000-0 20000-3 0 9006
2 25544 51
6344 209
7903 0012088 154
7685 205
4073 15
77497190 14523
Satellite: ISS
Catalog Number: 25544
Epoch time: 06303
58500863 = yrday
fracday
Element set: 900
Inclination: 51
6344 deg
RA of node: 209
7903 deg
Eccentricity:
0012088
Arg of perigee: 154
7685 deg
Mean anomaly: 205
4073 deg
Mean motion: 15
77497190 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1452
Checksum: 291
Coasting Arc #2 (Orbit 1467)
---------------------------------------
Vector Time (GMT): 2006/304/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3902438
68 A = 6718028
96 meter
Y = -4469005
09 meter E =
0020313
Z = 3148155
74 I = 51
51241
XDOT = 5783
315691 Wp = 120
63954
YDOT = -1629
522071 meter/sec RA = 203
91835 deg
ZDOT = 4822
570514 TA = 276
14540
MA = 276
37680
Ha = 188
376 n
mi
Hp = 175
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12803276
49 X = -3867468
97
Y = -14662090
20 feet Y = -4512448
78 meter
Z = 10328594
94 Z = 3129282
42
XDOT = 18974
132843 XDOT = 5777
679923
YDOT = -5346
201021 feet/sec YDOT = -1564
881308 meter/sec
ZDOT = 15822
081738 ZDOT = 4850
652546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19422087
15 X = 5919852
16
Y = -1773524
14 feet Y = -540570
16 meter
Z = 10257572
54 Z = 3126508
11
XDOT = -6916
897499 XDOT = -2108
270358
YDOT = 17001
380000 feet/sec YDOT = 5182
020624 meter/sec
ZDOT = 15926
597574 ZDOT = 4854
426941
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 06304
59860050
00020000 00000-0 20000-3 0 9016
2 25544 51
6348 204
5570 0012107 158
3593 201
8085 15
77482840 14686
Satellite: ISS
Catalog Number: 25544
Epoch time: 06304
59860050 = yrday
fracday
Element set: 901
Inclination: 51
6348 deg
RA of node: 204
5570 deg
Eccentricity:
0012107
Arg of perigee: 158
3593 deg
Mean anomaly: 201
8085 deg
Mean motion: 15
77482840 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1468
Checksum: 284
Coasting Arc #3 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2006/305/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5736618
76 A = 6717040
99 meter
Y = 905182
09 meter E =
0014427
Z = -3394171
68 I = 51
53669
XDOT = -3523
340216 Wp = 144
15960
YDOT = -5054
547913 meter/sec RA = 198
69629 deg
ZDOT = 4605
303971 TA = 175
71853
MA = 175
70617
Ha = 188
120 n
mi
Hp = 175
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18820927
68 X = -5729825
72
Y = 2969757
50 feet Y = 841069
93 meter
Z = -11135733
85 Z = -3422024
16
XDOT = -11559
515145 XDOT = -3488
929801
YDOT = -16583
162445 feet/sec YDOT = -5093
755341 meter/sec
ZDOT = 15109
264996 ZDOT = 4588
271016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8342135
46 X = 2542682
89
Y = -17062642
05 feet Y = -5200693
30 meter
Z = -11239500
38 Z = -3425799
72
XDOT = 19018
075754 XDOT = 5796
709490
YDOT = -615
801174 feet/sec YDOT = -187
696198 meter/sec
ZDOT = 15045
017993 ZDOT = 4585
721484
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 06305
54881996
00020000 00000-0 20000-3 0 9025
2 25544 51
6351 199
6508 0012010 162
8109 197
3465 15
77528115 14835
Satellite: ISS
Catalog Number: 25544
Epoch time: 06305
54881996 = yrday
fracday
Element set: 902
Inclination: 51
6351 deg
RA of node: 199
6508 deg
Eccentricity:
0012010
Arg of perigee: 162
8109 deg
Mean anomaly: 197
3465 deg
Mean motion: 15
77528115 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1483
Checksum: 302
Coasting Arc #4 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2006/306/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2083193
98 A = 6712482
17 meter
Y = 4334520
06 meter E =
0015357
Z = -4690569
35 I = 51
54866
XDOT = -7179
026455 Wp = 121
76549
YDOT = 503
193463 meter/sec RA = 193
57347 deg
ZDOT = -2737
861365 TA = 121
30669
MA = 121
15624
Ha = 187
929 n
mi
Hp = 176
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6834625
90 X = 2057356
38
Y = 14220866
33 feet Y = 4357670
87 meter
Z = -15389007
06 Z = -4680511
88
XDOT = -23553
236402 XDOT = -7170
819340
YDOT = 1650
897189 feet/sec YDOT = 422
959404 meter/sec
ZDOT = -8982
484794 ZDOT = -2772
717926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15656580
55 X = -4772125
75
Y = -2233540
10 feet Y = -680783
02 meter
Z = -15350878
57 Z = -4678947
79
XDOT = 11634
445050 XDOT = 3546
178851
YDOT = -19253
209839 feet/sec YDOT = -5868
378359 meter/sec
ZDOT = -9112
440024 ZDOT = -2777
471719
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 06306
56236600
00020000 00000-0 20000-3 0 9035
2 25544 51
6349 194
4173 0011946 167
1846 192
9624 15
77569898 14994
Satellite: ISS
Catalog Number: 25544
Epoch time: 06306
56236600 = yrday
fracday
Element set: 903
Inclination: 51
6349 deg
RA of node: 194
4173 deg
Eccentricity:
0011946
Arg of perigee: 167
1846 deg
Mean anomaly: 192
9624 deg
Mean motion: 15
77569898 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1499
Checksum: 331
Coasting Arc #5 (Orbit 1514)
---------------------------------------
Vector Time (GMT): 2006/307/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6586958
96 A = 6721322
17 meter
Y = -39909
63 meter E =
0023695
Z = 1260270
43 I = 51
60666
XDOT = 1159
839991 Wp = 144
06530
YDOT = 4873
215230 meter/sec RA = 188
37285 deg
ZDOT = -5871
250328 TA = 22
06228
MA = 21
96046
Ha = 187
838 n
mi
Hp = 176
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21610757
74 X = 6580793
34
Y = -130937
12 feet Y = 33714
95 meter
Z = 4134745
51 Z = 1292255
80
XDOT = 3805
249314 XDOT = 1133
783095
YDOT = 15988
238942 feet/sec YDOT = 4886
039378 meter/sec
ZDOT = -19262
632310 ZDOT = -5865
679073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11672810
71 X = -3557872
70
Y = 18160026
71 feet Y = 5535176
14 meter
Z = 4254061
03 Z = 1296637
80
XDOT = -14207
633026 XDOT = -4330
486546
YDOT = -4597
743259 feet/sec YDOT = -1401
392145 meter/sec
ZDOT = -19241
164004 ZDOT = -5864
706788
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 06307
57589143
00020000 00000-0 20000-3 0 9041
2 25544 51
6350 189
1845 0012109 170
5638 189
5756 15
77567611 15150
Satellite: ISS
Catalog Number: 25544
Epoch time: 06307
57589143 = yrday
fracday
Element set: 904
Inclination: 51
6350 deg
RA of node: 189
1845 deg
Eccentricity:
0012109
Arg of perigee: 170
5638 deg
Mean anomaly: 189
5756 deg
Mean motion: 15
77567611 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1515
Checksum: 313
Coasting Arc #6 (Orbit 1530)
---------------------------------------
Vector Time (GMT): 2006/308/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 135405
72 A = 6709766
79 meter
Y = -4165314
38 meter E =
0012638
Z = 5255859
48 I = 51
59598
XDOT = 7700
749983 Wp = 164
59885
YDOT = 368
457731 meter/sec RA = 183
21996 deg
ZDOT = 81
580505 TA = 284
55743
MA = 284
69758
Ha = 187
615 n
mi
Hp = 176
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 444244
47 X = 156439
92
Y = -13665729
58 feet Y = -4163682
60 meter
Z = 17243633
45 Z = 5256568
38
XDOT = 25264
927766 XDOT = 7695
661179
YDOT = 1208
850822 feet/sec YDOT = 454
543336 meter/sec
ZDOT = 267
652577 ZDOT = 118
979618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11392031
51 X = 3472291
21
Y = 7556452
08 feet Y = 2303206
59 meter
Z = 17245696
94 Z = 5256488
43
XDOT = -13895
564622 XDOT = -4235
368097
YDOT = 19929
331499 feet/sec YDOT = 6074
460241 meter/sec
ZDOT = 407
229163 ZDOT = 124
123449
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 06308
58939162
00020000 00000-0 20000-3 0 9054
2 25544 51
6343 183
9508 0011941 175
0752 185
0533 15
77632922 15310
Satellite: ISS
Catalog Number: 25544
Epoch time: 06308
58939162 = yrday
fracday
Element set: 905
Inclination: 51
6343 deg
RA of node: 183
9508 deg
Eccentricity:
0011941
Arg of perigee: 175
0752 deg
Mean anomaly: 185
0533 deg
Mean motion: 15
77632922 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1531
Checksum: 296
Coasting Arc #7 (Orbit 1546)
---------------------------------------
Vector Time (GMT): 2006/309/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6588835
87 A = 6721148
16 meter
Y = -683266
26 meter E =
0012532
Z = 1144851
21 I = 51
66214
XDOT = 1522
731649 Wp = 110
97066
YDOT = -4714
927051 meter/sec RA = 178
06478 deg
ZDOT = 5893
605283 TA = 261
56950
MA = 261
71157
Ha = 187
365 n
mi
Hp = 176
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21616915
58 X = -6586267
46
Y = -2241687
20 feet Y = -756931
96 meter
Z = 3756073
52 Z = 1112847
75
XDOT = 4995
838742 XDOT = 1546
710388
YDOT = -15468
920772 feet/sec YDOT = -4697
765166 meter/sec
ZDOT = 19335
975339 ZDOT = 5901
061042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13098430
90 X = 3992401
74
Y = -17367519
34 feet Y = -5293619
89 meter
Z = 3636573
80 Z = 1108427
70
XDOT = 9452
152482 XDOT = 2881
016077
YDOT = 11222
941618 feet/sec YDOT = 3420
752605 meter/sec
ZDOT = 19363
141108 ZDOT = 5901
885410
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 06309
60286927
00020000 00000-0 20000-3 0 9063
2 25544 51
6330 178
7162 0011948 179
7088 180
4086 15
77695756 15477
Satellite: ISS
Catalog Number: 25544
Epoch time: 06309
60286927 = yrday
fracday
Element set: 906
Inclination: 51
6330 deg
RA of node: 178
7162 deg
Eccentricity:
0011948
Arg of perigee: 179
7088 deg
Mean anomaly: 180
4086 deg
Mean motion: 15
77695756 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1547
Checksum: 332
Coasting Arc #8 (Orbit 1561)
---------------------------------------
Vector Time (GMT): 2006/310/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2487461
62 A = 6711854
46 meter
Y = 4080153
81 meter E =
0018526
Z = -4728336
82 I = 51
65811
XDOT = -7111
349161 Wp = 147
13715
YDOT = -1234
804050 meter/sec RA = 172
86953 deg
ZDOT = 2665
158344 TA = 149
12611
MA = 149
01704
Ha = 187
166 n
mi
Hp = 176
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8160963
31 X = -2509931
44
Y = 13386331
38 feet Y = 4052212
33 meter
Z = -15512916
08 Z = -4740475
60
XDOT = -23331
198034 XDOT = -7109
960153
YDOT = -4051
194389 feet/sec YDOT = -1314
319519 meter/sec
ZDOT = 8743
957823 ZDOT = 2630
613569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7526129
34 X = -2293964
22
Y = -13702648
61 feet Y = -4176567
30 meter
Z = -15557652
57 Z = -4741972
50
XDOT = 14237
845119 XDOT = 4339
695192
YDOT = -17639
906182 feet/sec YDOT = -5376
643404 meter/sec
ZDOT = 8614
888049 ZDOT = 2625
817877
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 06310
55298648
00020000 00000-0 20000-3 0 9073
2 25544 51
6317 173
8082 0011868 183
3745 176
7342 15
77708020 15620
Satellite: ISS
Catalog Number: 25544
Epoch time: 06310
55298648 = yrday
fracday
Element set: 907
Inclination: 51
6317 deg
RA of node: 173
8082 deg
Eccentricity:
0011868
Arg of perigee: 183
3745 deg
Mean anomaly: 176
7342 deg
Mean motion: 15
77708020 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1562
Checksum: 305
Coasting Arc #9 (Orbit 1577)
---------------------------------------
Vector Time (GMT): 2006/311/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5596272
55 A = 6716675
13 meter
Y = 1517414
48 meter E =
0012279
Z = -3380733
40 I = 51
70149
XDOT = -4051
641551 Wp = 164
88745
YDOT = 4631
605184 meter/sec RA = 167
75522 deg
ZDOT = -4643
388582 TA = 55
03962
MA = 54
92436
Ha = 187
071 n
mi
Hp = 177
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18360474
25 X = 5595312
13
Y = 4978393
97 feet Y = 1579990
05 meter
Z = -11091645
02 Z = -3353548
14
XDOT = -13292
787240 XDOT = -4080
574305
YDOT = 15195
555065 feet/sec YDOT = 4586
136144 meter/sec
ZDOT = -15234
214508 ZDOT = -4663
141856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13317923
97 X = -4059303
23
Y = 13666349
25 feet Y = 4165503
25 meter
Z = -10989986
79 Z = -3349747
98
XDOT = -5845
031114 XDOT = -1781
565484
YDOT = -17964
611863 feet/sec YDOT = -5475
613696 meter/sec
ZDOT = -15307
303302 ZDOT = -4665
666046
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 06311
56642239
00020000 00000-0 20000-3 0 9085
2 25544 51
6307 168
5744 0011832 187
5751 172
5237 15
77729196 15780
Satellite: ISS
Catalog Number: 25544
Epoch time: 06311
56642239 = yrday
fracday
Element set: 908
Inclination: 51
6307 deg
RA of node: 168
5744 deg
Eccentricity:
0011832
Arg of perigee: 187
5751 deg
Mean anomaly: 172
5237 deg
Mean motion: 15
77729196 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1578
Checksum: 317
Coasting Arc #10 (Orbit 1593)
---------------------------------------
Vector Time (GMT): 2006/312/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4402985
95 A = 6717013
80 meter
Y = -3973177
62 meter E =
0016211
Z = 3130489
89 I = 51
73165
XDOT = 5529
422576 Wp = 139
97213
YDOT = 2288
850677 meter/sec RA = 162
54485 deg
ZDOT = -4870
413546 TA = 3
54578
MA = 3
53431
Ha = 186
618 n
mi
Hp = 177
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14445491
95 X = 4431879
64
Y = -13035359
64 feet Y = -3923779
76 meter
Z = 10270636
12 Z = 3151949
84
XDOT = 18141
150183 XDOT = 5527
077477
YDOT = 7509
352615 feet/sec YDOT = 2350
671136 meter/sec
ZDOT = -15979
047068 ZDOT = -4843
556475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4704836
27 X = 1434034
09
Y = 18836579
46 feet Y = 5741389
42 meter
Z = 10350197
81 Z = 3154740
29
XDOT = -13848
145410 XDOT = -4220
914721
YDOT = 12186
638830 feet/sec YDOT = 3714
487515 meter/sec
ZDOT = -15878
497008 ZDOT = -4839
765888
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 06312
57983467
00020000 00000-0 20000-3 0 9099
2 25544 51
6311 163
3393 0011734 192
2865 167
8016 15
77805942 15942
Satellite: ISS
Catalog Number: 25544
Epoch time: 06312
57983467 = yrday
fracday
Element set: 909
Inclination: 51
6311 deg
RA of node: 163
3393 deg
Eccentricity:
0011734
Arg of perigee: 192
2865 deg
Mean anomaly: 167
8016 deg
Mean motion: 15
77805942 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1594
Checksum: 313
Coasting Arc #11 (Orbit 1609)
---------------------------------------
Vector Time (GMT): 2006/313/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3870510
22 A = 6711262
63 meter
Y = -2542654
92 meter E =
0015162
Z = 4860488
36 I = 51
73718
XDOT = 5857
650955 Wp = 169
67813
YDOT = -4427
202411 meter/sec RA = 157
43001 deg
ZDOT = 2332
821100 TA = 257
55325
MA = 257
72295
Ha = 186
682 n
mi
Hp = 177
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12698524
35 X = -3865402
00
Y = -8342043
70 feet Y = -2585909
04 meter
Z = 15946484
11 Z = 4841697
26
XDOT = 19218
014944 XDOT = 5895
388583
YDOT = -14524
942294 feet/sec YDOT = -4361
488143 meter/sec
ZDOT = 7653
612532 ZDOT = 2361
369267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13259817
77 X = 4041592
46
Y = -7567200
49 feet Y = -2306482
71 meter
Z = 15875996
93 Z = 4839003
86
XDOT = 3616
043956 XDOT = 1102
170198
YDOT = 22724
884673 feet/sec YDOT = 6926
544848 meter/sec
ZDOT = 7759
585634 ZDOT = 2365
121701
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 06313
59322885
00020000 00000-0 20000-3 0 9105
2 25544 51
6299 158
1039 0011722 195
2938 164
7874 15
77765183 16106
Satellite: ISS
Catalog Number: 25544
Epoch time: 06313
59322885 = yrday
fracday
Element set: 910
Inclination: 51
6299 deg
RA of node: 158
1039 deg
Eccentricity:
0011722
Arg of perigee: 195
2938 deg
Mean anomaly: 164
7874 deg
Mean motion: 15
77765183 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1610
Checksum: 313
Coasting Arc #12 (Orbit 1624)
---------------------------------------
Vector Time (GMT): 2006/314/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5590064
33 A = 6720984
92 meter
Y = 3649769
00 meter E =
0004143
Z = -796369
23 I = 51
79626
XDOT = -3217
324634 Wp = 140
67227
YDOT = -3625
777417 meter/sec RA = 152
24638 deg
ZDOT = 5980
567503 TA = 210
65838
MA = 210
68259
Ha = 186
402 n
mi
Hp = 177
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18340106
07 X = -5626592
42
Y = 11974307
75 feet Y = 3587053
63 meter
Z = -2612759
93 Z = -823614
51
XDOT = -10555
527016 XDOT = -3205
594444
YDOT = -11895
595199 feet/sec YDOT = -3661
690263 meter/sec
ZDOT = 19621
284460 ZDOT = 5964
965719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2660798
27 X = -811011
31
Y = -21728425
56 feet Y = -6622824
11 meter
Z = -2713987
20 Z = -827223
30
XDOT = 13795
746020 XDOT = 4204
943387
YDOT = -4127
426061 feet/sec YDOT = -1258
039463 meter/sec
ZDOT = 19562
550380 ZDOT = 5962
665356
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 06314
54326187
00020000 00000-0 20000-3 0 9111
2 25544 51
6295 153
1953 0011869 199
0256 161
0467 15
77831586 16254
Satellite: ISS
Catalog Number: 25544
Epoch time: 06314
54326187 = yrday
fracday
Element set: 911
Inclination: 51
6295 deg
RA of node: 153
1953 deg
Eccentricity:
0011869
Arg of perigee: 199
0256 deg
Mean anomaly: 161
0467 deg
Mean motion: 15
77831586 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1625
Checksum: 307
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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