Date:
November 17th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 3480)
---------------------------------------
Vector Time (GMT): 2007/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5024624
84 A = 6717217
58 meter
Y = 485967
12 meter E =
0008465
Z = 4425384
25 I = 51
83273
XDOT = -3494
900875 Wp = 77
95383
YDOT = -6025
831770 meter/sec RA = 38
03017 deg
ZDOT = -3299
423999 TA = 45
06821
MA = 44
99957
Ha = 186
644 n
mi
Hp = 180
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16484989
63 X = -5051183
58
Y = 1594380
32 feet Y = 429630
08 meter
Z = 14518977
19 Z = 4400909
79
XDOT = -11466
210219 XDOT = -3411
231128
YDOT = -19769
789273 feet/sec YDOT = -6064
445651 meter/sec
ZDOT = -10824
881886 ZDOT = -3316
199709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8337135
52 X = 2541158
91
Y = -14404336
74 feet Y = -4390441
84 meter
Z = 14425840
88 Z = 4396996
30
XDOT = 21665
143671 XDOT = 6603
535791
YDOT = 1610
854620 feet/sec YDOT = 490
988488 meter/sec
ZDOT = -10889
373261 ZDOT = -3319
080970
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 07320
54170354
00020000 00000-0 20000-3 0 9000
2 25544 51
6423 38
3795 0001636 194
9949 165
1167 15
76293326 34816
Satellite: ISS
Catalog Number: 25544
Epoch time: 07320
54170354 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 38
3795 deg
Eccentricity:
0001636
Arg of perigee: 194
9949 deg
Mean anomaly: 165
1167 deg
Mean motion: 15
76293326 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3481
Checksum: 298
Coasting Arc #2 (Orbit 3496)
---------------------------------------
Vector Time (GMT): 2007/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2741795
06 A = 6720225
62 meter
Y = 5043131
43 meter E =
0011964
Z = 3486244
77 I = 51
81939
XDOT = -6219
304236 Wp = 99
59337
YDOT = 228
975122 meter/sec RA = 32
94029 deg
ZDOT = 4544
912135 TA = 301
73489
MA = 301
85144
Ha = 186
416 n
mi
Hp = 180
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8995390
63 X = 2668262
45
Y = 16545706
79 feet Y = 5073380
38 meter
Z = 11437810
92 Z = 3499386
28
XDOT = -20404
541456 XDOT = -6243
481103
YDOT = 751
230716 feet/sec YDOT = 159
291888 meter/sec
ZDOT = 14911
129053 ZDOT = 4514
639622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18691583
12 X = -5697194
53
Y = -2035476
82 feet Y = -620413
34 meter
Z = 11488365
36 Z = 3501653
76
XDOT = 10859
373015 XDOT = 3309
936895
YDOT = -15933
271690 feet/sec YDOT = -4856
461211 meter/sec
ZDOT = 14795
887802 ZDOT = 4509
786602
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 07321
55606002
00020000 00000-0 20000-3 0 9017
2 25544 51
6420 33
1528 0001659 197
8190 162
2917 15
76325242 34976
Satellite: ISS
Catalog Number: 25544
Epoch time: 07321
55606002 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 33
1528 deg
Eccentricity:
0001659
Arg of perigee: 197
8190 deg
Mean anomaly: 162
2917 deg
Mean motion: 15
76325242 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3497
Checksum: 275
Coasting Arc #3 (Orbit 3511)
---------------------------------------
Vector Time (GMT): 2007/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5801009
91 A = 6720521
55 meter
Y = 29685
53 meter E =
0004562
Z = -3398148
35 I = 51
79485
XDOT = 2683
359900 Wp = 107
06550
YDOT = 5531
860197 meter/sec RA = 27
74789 deg
ZDOT = 4632
889031 TA = 212
90207
MA = 212
93047
Ha = 186
382 n
mi
Hp = 180
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19032184
75 X = 5816754
66
Y = 97393
47 feet Y = 94643
88 meter
Z = -11148780
69 Z = -3369928
36
XDOT = 8803
674211 XDOT = 2598
796282
YDOT = 18149
147628 feet/sec YDOT = 5561
394039 meter/sec
ZDOT = 15199
767161 ZDOT = 4645
719813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10644657
58 X = -3244491
63
Y = 15852734
73 feet Y = 4831913
55 meter
Z = -11041327
78 Z = -3365396
71
XDOT = -18785
758828 XDOT = -5725
899291
YDOT = -2001
849398 feet/sec YDOT = -610
163697 meter/sec
ZDOT = 15249
188686 ZDOT = 4647
952712
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 07322
50699593
00020000 00000-0 20000-3 0 9021
2 25544 51
6413 28
2530 0001512 199
0755 161
0353 15
76363056 35129
Satellite: ISS
Catalog Number: 25544
Epoch time: 07322
50699593 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 28
2530 deg
Eccentricity:
0001512
Arg of perigee: 199
0755 deg
Mean anomaly: 161
0353 deg
Mean motion: 15
76363056 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3512
Checksum: 272
Coasting Arc #4 (Orbit 3527)
---------------------------------------
Vector Time (GMT): 2007/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1841460
73 A = 6716512
86 meter
Y = -4626021
43 meter E =
0009184
Z = -4516617
30 I = 51
75525
XDOT = 7026
282669 Wp = 75
64769
YDOT = 257
665372 meter/sec RA = 22
65241 deg
ZDOT = -3131
627607 TA = 163
16548
MA = 163
13499
Ha = 186
317 n
mi
Hp = 180
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6041537
84 X = -1767653
67
Y = -15177235
67 feet Y = -4646200
89 meter
Z = -14818298
21 Z = -4525384
13
XDOT = 23052
108493 XDOT = 7038
092374
YDOT = 845
358831 feet/sec YDOT = 336
303362 meter/sec
ZDOT = -10274
368790 ZDOT = -3097
464583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15995893
68 X = 4875548
39
Y = 3158416
59 feet Y = 962685
38 meter
Z = -14852151
83 Z = -4526935
88
XDOT = -12933
451493 XDOT = -3942
116015
YDOT = 17846
348974 feet/sec YDOT = 5439
567167 meter/sec
ZDOT = -10144
265740 ZDOT = -3091
972198
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 07323
52130164
00020000 00000-0 20000-3 0 9039
2 25544 51
6412 23
0255 0001403 202
8332 157
2770 15
76371196 35289
Satellite: ISS
Catalog Number: 25544
Epoch time: 07323
52130164 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 23
0255 deg
Eccentricity:
0001403
Arg of perigee: 202
8332 deg
Mean anomaly: 157
2770 deg
Mean motion: 15
76371196 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3528
Checksum: 250
Coasting Arc #5 (Orbit 3543)
---------------------------------------
Vector Time (GMT): 2007/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6402215
85 A = 6723519
10 meter
Y = -363793
64 meter E =
0014030
Z = 1997461
86 I = 51
75291
XDOT = -1465
604478 Wp = 116
32508
YDOT = -5088
983655 meter/sec RA = 17
46571 deg
ZDOT = -5600
334289 TA = 41
42273
MA = 41
31645
Ha = 186
203 n
mi
Hp = 180
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21004645
18 X = -6407375
57
Y = -1193548
68 feet Y = -435415
74 meter
Z = 6553352
55 Z = 1966346
61
XDOT = -4808
413641 XDOT = -1381
383701
YDOT = -16696
140602 feet/sec YDOT = -5104
901843 meter/sec
ZDOT = -18373
800160 ZDOT = -5607
249907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12046947
95 X = 3671909
73
Y = -17292481
22 feet Y = -5270748
28 meter
Z = 6434846
18 Z = 1961341
11
XDOT = 15423
379854 XDOT = 4701
046180
YDOT = 3867
728167 feet/sec YDOT = 1178
883545 meter/sec
ZDOT = -18400
649440 ZDOT = -5608
517949
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 07324
53557971
00020000 00000-0 20000-3 0 9041
2 25544 51
6420 17
7982 0001138 209
6471 150
4629 15
76458073 35445
Satellite: ISS
Catalog Number: 25544
Epoch time: 07324
53557971 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 17
7982 deg
Eccentricity:
0001138
Arg of perigee: 209
6471 deg
Mean anomaly: 150
4629 deg
Mean motion: 15
76458073 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3544
Checksum: 298
Coasting Arc #6 (Orbit 3559)
---------------------------------------
Vector Time (GMT): 2007/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 646937
42 A = 6713640
20 meter
Y = 4286108
17 meter E =
0004636
Z = 5124892
86 I = 51
69156
XDOT = -7561
580473 Wp = 139
35253
YDOT = -528
949538 meter/sec RA = 12
34754 deg
ZDOT = 1392
751003 TA = 297
30909
MA = 297
35628
Ha = 186
113 n
mi
Hp = 180
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2122498
10 X = 574064
90
Y = 14062034
68 feet Y = 4292934
96 meter
Z = 16813952
95 Z = 5127858
91
XDOT = -24808
334886 XDOT = -7561
869611
YDOT = -1735
398748 feet/sec YDOT = -613
509082 meter/sec
ZDOT = 4569
393055 ZDOT = 1356
015052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13132992
27 X = -4002936
04
Y = -5419952
58 feet Y = -1652001
55 meter
Z = 16825678
58 Z = 5128466
83
XDOT = 13751
004469 XDOT = 4191
306162
YDOT = -19526
669453 feet/sec YDOT = -5951
728849 meter/sec
ZDOT = 4429
473173 ZDOT = 1350
103423
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 07325
54983281
00020000 00000-0 20000-3 0 9051
2 25544 51
6416 12
5710 0001151 209
1559 150
9541 15
76480547 35606
Satellite: ISS
Catalog Number: 25544
Epoch time: 07325
54983281 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 12
5710 deg
Eccentricity:
0001151
Arg of perigee: 209
1559 deg
Mean anomaly: 150
9541 deg
Mean motion: 15
76480547 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3560
Checksum: 279
Coasting Arc #7 (Orbit 3574)
---------------------------------------
Vector Time (GMT): 2007/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6687675
29 A = 6725100
57 meter
Y = 534746
77 meter E =
0010684
Z = -386906
54 I = 51
70134
XDOT = -40
528735 Wp = 42
47679
YDOT = 4794
833628 meter/sec RA = 7
18194 deg
ZDOT = 6030
383828 TA = 313
31609
MA = 313
40511
Ha = 186
165 n
mi
Hp = 180
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21941191
90 X = 6683078
21
Y = 1754418
54 feet Y = 609506
47 meter
Z = -1269378
41 Z = -354427
87
XDOT = -132
968292 XDOT = -123
437760
YDOT = 15731
081457 feet/sec YDOT = 4793
916473 meter/sec
ZDOT = 19784
723844 ZDOT = 6029
985835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12380948
36 X = -3773713
06
Y = 18207272
41 feet Y = 5549576
63 meter
Z = -1145668
85 Z = -349199
87
XDOT = -12223
264905 XDOT = -3725
651143
YDOT = -7090
734857 feet/sec YDOT = -2161
255984 meter/sec
ZDOT = 19783
686539 ZDOT = 6030
067657
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 07326
50067216
00020000 00000-0 20000-3 0 9060
2 25544 51
6415 7
6700 0000860 215
3158 144
7950 15
76469777 35752
Satellite: ISS
Catalog Number: 25544
Epoch time: 07326
50067216 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 7
6700 deg
Eccentricity:
0000860
Arg of perigee: 215
3158 deg
Mean anomaly: 144
7950 deg
Mean motion: 15
76469777 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3575
Checksum: 294
Coasting Arc #8 (Orbit 3590)
---------------------------------------
Vector Time (GMT): 2007/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 758135
52 A = 6713021
78 meter
Y = -4131243
29 meter E =
0014432
Z = -5249075
19 I = 51
63276
XDOT = 7642
541115 Wp = 97
43562
YDOT = 705
006581 meter/sec RA = 2
02769 deg
ZDOT = 548
408268 TA = 177
78313
MA = 177
77673
Ha = 186
041 n
mi
Hp = 180
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2487321
25 X = 829775
28
Y = -13553947
80 feet Y = -4122364
31 meter
Z = -17221375
31 Z = -5245218
43
XDOT = 25073
953789 XDOT = 7631
425450
YDOT = 2313
013716 feet/sec YDOT = 790
407600 meter/sec
ZDOT = 1799
239725 ZDOT = 585
510061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10653845
59 X = 3247292
14
Y = 8768319
21 feet Y = 2672583
70 meter
Z = -17207097
02 Z = -5244723
17
XDOT = -13410
864449 XDOT = -4087
631484
YDOT = 20106
471841 feet/sec YDOT = 6128
452617 meter/sec
ZDOT = 1940
568822 ZDOT = 591
485377
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 07327
51487526
00020000 00000-0 20000-3 0 9073
2 25544 51
6421 2
4419 0000956 215
4413 144
6688 15
76528001 35911
Satellite: ISS
Catalog Number: 25544
Epoch time: 07327
51487526 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 2
4419 deg
Eccentricity:
0000956
Arg of perigee: 215
4413 deg
Mean anomaly: 144
6688 deg
Mean motion: 15
76528001 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3591
Checksum: 286
Coasting Arc #9 (Orbit 3606)
---------------------------------------
Vector Time (GMT): 2007/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6545579
04 A = 6723986
72 meter
Y = -710067
01 meter E =
0009038
Z = -1344549
80 I = 51
64117
XDOT = 1707
166303 Wp = 147
42271
YDOT = -4723
150966 meter/sec RA = 356
89030 deg
ZDOT = -5842
132666 TA = 47
36072
MA = 47
28456
Ha = 185
941 n
mi
Hp = 179
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21474996
83 X = -6530620
69
Y = -2329616
16 feet Y = -783179
56 meter
Z = -4411252
64 Z = -1376312
97
XDOT = 5600
939313 XDOT = 1788
235301
YDOT = -15495
902119 feet/sec YDOT = -4703
606400 meter/sec
ZDOT = -19167
101923 ZDOT = -5833
642710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12025334
19 X = 3665321
86
Y = -17914008
62 feet Y = -5460189
83 meter
Z = -4532260
27 Z = -1381432
93
XDOT = 9765
412751 XDOT = 2976
497806
YDOT = 11375
897846 feet/sec YDOT = 3467
373663 meter/sec
ZDOT = -19135
233661 ZDOT = -5832
419220
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 07328
52905230
00020000 00000-0 20000-3 0 9083
2 25544 51
6419 357
2136 0000839 213
2116 146
8996 15
76588972 36078
Satellite: ISS
Catalog Number: 25544
Epoch time: 07328
52905230 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 357
2136 deg
Eccentricity:
0000839
Arg of perigee: 213
2116 deg
Mean anomaly: 146
8996 deg
Mean motion: 15
76588972 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3607
Checksum: 313
Coasting Arc #10 (Orbit 3622)
---------------------------------------
Vector Time (GMT): 2007/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2191128
04 A = 6714678
74 meter
Y = 4159448
33 meter E =
0006594
Z = 4790452
32 I = 51
58006
XDOT = -7234
513146 Wp = 62
11430
YDOT = -938
963481 meter/sec RA = 351
70006 deg
ZDOT = -2488
118135 TA = 52
24702
MA = 52
18729
Ha = 185
937 n
mi
Hp = 179
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7188740
27 X = -2260748
48
Y = 13646484
03 feet Y = 4134555
87 meter
Z = 15716707
07 Z = 4779639
10
XDOT = -23735
279349 XDOT = -7211
388706
YDOT = -3080
588849 feet/sec YDOT = -1019
734214 meter/sec
ZDOT = -8163
117240 ZDOT = -2523
208234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8924070
97 X = -2720056
83
Y = -12631132
78 feet Y = -3849969
27 meter
Z = 15675931
76 Z = 4778024
00
XDOT = 12470
965220 XDOT = 3801
150199
YDOT = -19130
701171 feet/sec YDOT = -5831
037717 meter/sec
ZDOT = -8296
822185 ZDOT = -2528
871402
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 07329
54320336
00020000 00000-0 20000-3 0 9095
2 25544 51
6407 351
9853 0000735 217
3896 142
7218 15
76648070 36233
Satellite: ISS
Catalog Number: 25544
Epoch time: 07329
54320336 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 351
9853 deg
Eccentricity:
0000735
Arg of perigee: 217
3896 deg
Mean anomaly: 142
7218 deg
Mean motion: 15
76648070 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3623
Checksum: 300
Coasting Arc #11 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2007/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5957150
18 A = 6720782
27 meter
Y = 977994
94 meter E =
0012892
Z = 2941223
10 I = 51
57221
XDOT = -3276
889467 Wp = 84
57494
YDOT = 4862
112130 meter/sec RA = 346
58373 deg
ZDOT = 5002
781662 TA = 309
41824
MA = 309
53230
Ha = 185
840 n
mi
Hp = 179
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19544455
99 X = 5931483
18
Y = 3208644
80 feet Y = 1044467
17 meter
Z = 9649682
08 Z = 2970101
23
XDOT = -10750
949696 XDOT = -3355
317802
YDOT = 15951
811449 feet/sec YDOT = 4825
028761 meter/sec
ZDOT = 16413
325662 ZDOT = 4986
672558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11343982
26 X = -3457645
79
Y = 16169692
89 feet Y = 4928522
39 meter
Z = 9759745
06 Z = 2974770
29
XDOT = -8491
499895 XDOT = -2588
209168
YDOT = -15861
619555 feet/sec YDOT = -4834
621640 meter/sec
ZDOT = 16352
445693 ZDOT = 4984
225447
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 07330
55733058
00020000 00000-0 20000-3 0 9109
2 25544 51
6406 346
7564 0000598 218
5120 141
6002 15
76653669 36399
Satellite: ISS
Catalog Number: 25544
Epoch time: 07330
55733058 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 346
7564 deg
Eccentricity:
0000598
Arg of perigee: 218
5120 deg
Mean anomaly: 141
6002 deg
Mean motion: 15
76653669 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3639
Checksum: 290
Coasting Arc #12 (Orbit 3653)
---------------------------------------
Vector Time (GMT): 2007/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3459009
13 A = 6718317
43 meter
Y = -4342663
28 meter E =
0005790
Z = -3789395
51 I = 51
53701
XDOT = 6312
963553 Wp = 108
47771
YDOT = 1379
893551 meter/sec RA = 341
37139 deg
ZDOT = 4184
593108 TA = 205
47019
MA = 205
49874
Ha = 185
808 n
mi
Hp = 179
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11348455
14 X = 3525720
74
Y = -14247582
92 feet Y = -4303609
09 meter
Z = -12432399
97 Z = -3772430
09
XDOT = 20711
822679 XDOT = 6276
735983
YDOT = 4527
209812 feet/sec YDOT = 1450
285487 meter/sec
ZDOT = 13728
980014 ZDOT = 4215
174007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8167709
71 X = 2489517
92
Y = 16329777
21 feet Y = 4977316
09 meter
Z = -12368205
87 Z = -3769829
15
XDOT = -11549
631585 XDOT = -3520
327707
YDOT = 16254
978276 feet/sec YDOT = 4954
517378 meter/sec
ZDOT = 13845
574299 ZDOT = 4220
131046
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 07331
50804970
00020000 00000-0 20000-3 0 9118
2 25544 51
6414 341
8548 0000613 229
1590 130
9522 15
76696248 36548
Satellite: ISS
Catalog Number: 25544
Epoch time: 07331
50804970 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 341
8548 deg
Eccentricity:
0000613
Arg of perigee: 229
1590 deg
Mean anomaly: 130
9522 deg
Mean motion: 15
76696248 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3654
Checksum: 288
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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