Date:
October 28th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 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
303/01:14:42
395 1
2 1
8 1
9
N/A -0
7 -0
3 191
5
000/00:03:24
790 -1
2 -0
1 187
9
Coasting Arc #1 (Orbit 935)
---------------------------------------
Vector Time (GMT): 2008/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 511211
40 A = 6731225
48 meter
Y = 5774592
46 meter E =
0008759
Z = 3412851
53 I = 51
92278
XDOT = -5729
981471 Wp = 86
69801
YDOT = -2236
017398 meter/sec RA = 57
47447 deg
ZDOT = 4632
018544 TA = 313
42884
MA = 313
50170
Ha = 191
012 n
mi
Hp = 187
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1677202
76 X = 430021
47
Y = 18945513
32 feet Y = 5779855
29 meter
Z = 11197019
46 Z = 3415137
64
XDOT = -18799
151808 XDOT = -5727
054270
YDOT = -7336
015086 feet/sec YDOT = -2300
076824 meter/sec
ZDOT = 15196
911232 ZDOT = 4604
188663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12305445
32 X = -3750699
73
Y = -14495251
98 feet Y = -4418152
80 meter
Z = 11206355
98 Z = 3415697
30
XDOT = 18581
630683 XDOT = 5663
681032
YDOT = -4084
755003 feet/sec YDOT = -1245
033325 meter/sec
ZDOT = 15088
868990 ZDOT = 4599
087268
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 08301
55642898
00020000 00000-0 20000-3 0 9008
2 25544 51
6423 57
7740 0003778 279
3107 80
7629 15
72557207 9368
Satellite: ISS
Catalog Number: 25544
Epoch time: 08301
55642898 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 57
7740 deg
Eccentricity:
0003778
Arg of perigee: 279
3107 deg
Mean anomaly: 80
7629 deg
Mean motion: 15
72557207 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 936
Checksum: 308
Coasting Arc #2 (Orbit 950)
---------------------------------------
Vector Time (GMT): 2008/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5054321
65 A = 6728274
51 meter
Y = 980607
70 meter E =
0004953
Z = -4336590
66 I = 51
89600
XDOT = 1691
706260 Wp = 114
53903
YDOT = 6650
978106 meter/sec RA = 52
32045 deg
ZDOT = 3476
719077 TA = 190
50734
MA = 190
51770
Ha = 191
120 n
mi
Hp = 187
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16582420
11 X = 5064047
74
Y = 3217216
86 feet Y = 1037182
34 meter
Z = -14227659
65 Z = -4312012
37
XDOT = 5550
217387 XDOT = 1600
318389
YDOT = 21820
794310 feet/sec YDOT = 6669
384831 meter/sec
ZDOT = 11406
558651 ZDOT = 3484
715540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15315505
13 X = -4668165
96
Y = 7312052
86 feet Y = 2228713
71 meter
Z = -14132325
56 Z = -4307532
83
XDOT = -16842
365700 XDOT = -5133
553065
YDOT = -13177
277235 feet/sec YDOT = -4016
434101 meter/sec
ZDOT = 11438
086433 ZDOT = 3486
328745
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 08302
50966293
00020000 00000-0 20000-3 0 9013
2 25544 51
6426 52
8906 0003820 285
2366 74
8374 15
72543930 9518
Satellite: ISS
Catalog Number: 25544
Epoch time: 08302
50966293 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 52
8906 deg
Eccentricity:
0003820
Arg of perigee: 285
2366 deg
Mean anomaly: 74
8374 deg
Mean motion: 15
72543930 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 951
Checksum: 293
Coasting Arc #3 (Orbit 959)
---------------------------------------
Vector Time (GMT): 2008/303/01:16:24
790
Vector Time (MET): N/A
Weight (LBS) : 626561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3162721
94 A = 6736100
41 meter
Y = -5708124
12 meter E =
0006017
Z = -1655641
41 I = 51
90869
XDOT = 4991
331394 Wp = 170
66310
YDOT = -1098
957068 meter/sec RA = 49
53937 deg
ZDOT = -5754
640111 TA = 27
54464
MA = 27
51277
Ha = 191
490 n
mi
Hp = 187
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10376384
33 X = -3090614
64
Y = -18727441
32 feet Y = -5743088
34 meter
Z = -5431894
38 Z = -1670831
23
XDOT = 16375
759166 XDOT = 5031
205070
YDOT = -3605
502193 feet/sec YDOT = -1042
918212 meter/sec
ZDOT = -18880
052856 ZDOT = -5730
294554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21313830
01 X = -6496455
39
Y = -1859853
65 feet Y = -566883
39 meter
Z = -5491218
60 Z = -1673723
43
XDOT = 6066
328197 XDOT = 1849
016834
YDOT = -14138
174301 feet/sec YDOT = -4309
315527 meter/sec
ZDOT = -18785
787538 ZDOT = -5725
908042
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 08303
08160403
00020000 00000-0 20000-3 0 9027
2 25544 51
6424 49
9631 0003810 273
5263 86
5463 15
72195854 9600
Satellite: ISS
Catalog Number: 25544
Epoch time: 08303
08160403 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 49
9631 deg
Eccentricity:
0003810
Arg of perigee: 273
5263 deg
Mean anomaly: 86
5463 deg
Mean motion: 15
72195854 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 960
Checksum: 279
Coasting Arc #4 (Orbit 975)
---------------------------------------
Vector Time (GMT): 2008/304/01:16:24
790
Vector Time (MET): N/A
Weight (LBS) : 626561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3840108
25 A = 6725587
36 meter
Y = 1927884
02 meter E =
0003085
Z = 5174932
02 I = 51
85373
XDOT = -4691
168903 Wp = 351
90324
YDOT = -5972
989821 meter/sec RA = 44
40883 deg
ZDOT = -1253
033023 TA = 110
05915
MA = 110
02594
Ha = 191
519 n
mi
Hp = 187
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12598780
36 X = -3886520
48
Y = 6325078
82 feet Y = 1884682
14 meter
Z = 16978123
43 Z = 5156163
44
XDOT = -15390
974091 XDOT = -4617
942088
YDOT = -19596
423298 feet/sec YDOT = -6025
039733 meter/sec
ZDOT = -4111
000731 ZDOT = -1275
645690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1589723
66 X = -484547
77
Y = 14094972
76 feet Y = 4296147
70 meter
Z = 16905534
17 Z = 5152806
81
XDOT = -23773
478111 XDOT = -7246
156128
YDOT = 2366
541120 feet/sec YDOT = 721
321734 meter/sec
ZDOT = -4199
103687 ZDOT = -1279
886804
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 08304
09858655
00020000 00000-0 20000-3 0 9033
2 25544 51
6423 44
7546 0003911 279
6712 80
4008 15
72266668 9762
Satellite: ISS
Catalog Number: 25544
Epoch time: 08304
09858655 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 44
7546 deg
Eccentricity:
0003911
Arg of perigee: 279
6712 deg
Mean anomaly: 80
4008 deg
Mean motion: 15
72266668 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 976
Checksum: 307
Coasting Arc #5 (Orbit 991)
---------------------------------------
Vector Time (GMT): 2008/305/01:16:24
790
Vector Time (MET): N/A
Weight (LBS) : 626561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4918067
56 A = 6737060
49 meter
Y = 4564107
10 meter E =
0011363
Z = 528419
96 I = 51
87087
XDOT = -3594
826704 Wp = 34
62142
YDOT = 3169
707670 meter/sec RA = 39
31807 deg
ZDOT = 6026
061529 TA = 331
10683
MA = 331
16970
Ha = 191
551 n
mi
Hp = 187
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16135392
24 X = 4864098
39
Y = 14974104
67 feet Y = 4618802
00 meter
Z = 1733661
30 Z = 552181
75
XDOT = -11794
050865 XDOT = -3659
278163
YDOT = 10399
303380 feet/sec YDOT = 3129
147677 meter/sec
ZDOT = 19770
543074 ZDOT = 6008
440849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21236993
40 X = 6473035
59
Y = -5765044
42 feet Y = -1757185
54 meter
Z = 1826102
20 Z = 556595
95
XDOT = 2107
435065 XDOT = 642
346208
YDOT = 14057
186418 feet/sec YDOT = 4284
630420 meter/sec
ZDOT = 19702
492743 ZDOT = 6005
319788
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 08305
11555959
00020000 00000-0 20000-3 0 9049
2 25544 51
6428 39
5455 0003847 285
0614 75
0122 15
72241442 9926
Satellite: ISS
Catalog Number: 25544
Epoch time: 08305
11555959 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 39
5455 deg
Eccentricity:
0003847
Arg of perigee: 285
0614 deg
Mean anomaly: 75
0122 deg
Mean motion: 15
72241442 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 992
Checksum: 287
Coasting Arc #6 (Orbit 1006)
---------------------------------------
Vector Time (GMT): 2008/306/01:16:24
790
Vector Time (MET): N/A
Weight (LBS) : 626561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2309940
07 A = 6724990
44 meter
Y = -3463250
82 meter E =
0011447
Z = -5291364
21 I = 51
80756
XDOT = 6373
977498 Wp = 83
37761
YDOT = 4302
118583 meter/sec RA = 34
20493 deg
ZDOT = -31
992991 TA = 186
31187
MA = 186
32631
Ha = 191
528 n
mi
Hp = 187
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7578543
54 X = 2374200
27
Y = -11362371
46 feet Y = -3437060
19 meter
Z = -17360118
81 Z = -5279986
27
XDOT = 20911
999664 XDOT = 6325
552196
YDOT = 14114
562281 feet/sec YDOT = 4373
125323 meter/sec
ZDOT = -104
963880 ZDOT = -1
144723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5796699
99 X = -1766834
16
Y = -12428043
32 feet Y = -3788067
60 meter
Z = -17316279
65 Z = -5278002
04
XDOT = 21952
912766 XDOT = 6691
247811
YDOT = -10254
436301 feet/sec YDOT = -3125
552185 meter/sec
ZDOT = 14
919114 ZDOT = 4
547346
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 08306
06895860
00020000 00000-0 20000-3 0 9053
2 25544 51
6432 34
6624 0003874 289
0003 71
0739 15
72286267 10073
Satellite: ISS
Catalog Number: 25544
Epoch time: 08306
06895860 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 34
6624 deg
Eccentricity:
0003874
Arg of perigee: 289
0003 deg
Mean anomaly: 71
0739 deg
Mean motion: 15
72286267 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1007
Checksum: 288
Coasting Arc #7 (Orbit 1022)
---------------------------------------
Vector Time (GMT): 2008/307/01:16:24
790
Vector Time (MET): N/A
Weight (LBS) : 626561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6067951
68 A = 6737035
44 meter
Y = -2857783
14 meter E =
0009606
Z = 575871
87 I = 51
82269
XDOT = 1563
405115 Wp = 136
11660
YDOT = -4542
282195 meter/sec RA = 29
08963 deg
ZDOT = -6014
910072 TA = 37
63610
MA = 37
56893
Ha = 191
635 n
mi
Hp = 187
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19907977
95 X = -6038342
05
Y = -9375928
94 feet Y = -2925472
96 meter
Z = 1889343
40 Z = 546464
75
XDOT = 5129
281874 XDOT = 1643
301562
YDOT = -14902
500639 feet/sec YDOT = -4524
352229 meter/sec
ZDOT = -19733
956930 ZDOT = -6007
121037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18070435
63 X = -5507868
78
Y = 12574316
43 feet Y = 3832651
65 meter
Z = 1775153
58 Z = 541066
81
XDOT = -9376
110217 XDOT = -2857
838394
YDOT = -10666
635732 feet/sec YDOT = -3251
190571 meter/sec
ZDOT = -19704
102428 ZDOT = -6005
810420
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 08307
08590759
00020000 00000-0 20000-3 0 9066
2 25544 51
6432 29
4536 0003826 291
2615 68
8138 15
72250596 10239
Satellite: ISS
Catalog Number: 25544
Epoch time: 08307
08590759 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 29
4536 deg
Eccentricity:
0003826
Arg of perigee: 291
2615 deg
Mean anomaly: 68
8138 deg
Mean motion: 15
72250596 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1023
Checksum: 297
Coasting Arc #8 (Orbit 1038)
---------------------------------------
Vector Time (GMT): 2008/308/01:16:24
790
Vector Time (MET): N/A
Weight (LBS) : 626561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -350709
85 A = 6725436
79 meter
Y = 4296926
50 meter E =
0000520
Z = 5162048
06 I = 51
75811
XDOT = -7284
151927 Wp = 190
44724
YDOT = -2135
793010 meter/sec RA = 23
99350 deg
ZDOT = 1282
482772 TA = 247
30407
MA = 247
30956
Ha = 191
713 n
mi
Hp = 187
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1150622
88 X = -423809
58
Y = 14097527
90 feet Y = 4292595
63 meter
Z = 16935853
21 Z = 5160166
96
XDOT = -23898
136245 XDOT = -7265
957975
YDOT = -7007
194915 feet/sec YDOT = -2217
146953 meter/sec
ZDOT = 4207
620644 ZDOT = 1247
139622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11728567
92 X = 3574867
50
Y = 7920934
53 feet Y = 2414300
85 meter
Z = 16928875
94 Z = 5159921
39
XDOT = -17140
981615 XDOT = -5224
571196
YDOT = 16677
815090 feet/sec YDOT = 5083
398039 meter/sec
ZDOT = 4070
473900 ZDOT = 1240
680445
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 08308
10284226
00020000 00000-0 20000-3 0 9070
2 25544 51
6433 24
2442 0003929 298
1158 61
9607 15
72307220 10390
Satellite: ISS
Catalog Number: 25544
Epoch time: 08308
10284226 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 24
2442 deg
Eccentricity:
0003929
Arg of perigee: 298
1158 deg
Mean anomaly: 61
9607 deg
Mean motion: 15
72307220 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1039
Checksum: 272
Coasting Arc #9 (Orbit 1053)
---------------------------------------
Vector Time (GMT): 2008/309/01:16:24
790
Vector Time (MET): N/A
Weight (LBS) : 626561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6471485
87 A = 6735812
44 meter
Y = 836198
86 meter E =
0008652
Z = -1649829
72 I = 51
76549
XDOT = 807
907425 Wp = 8
92230
YDOT = 5059
662409 meter/sec RA = 18
85328 deg
ZDOT = 5745
839196 TA = 332
89392
MA = 332
93907
Ha = 191
809 n
mi
Hp = 187
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21231909
01 X = 6469669
11
Y = 2743434
59 feet Y = 908556
69 meter
Z = -5412827
17 Z = -1618394
99
XDOT = 2650
614910 XDOT = 723
356611
YDOT = 16599
942288 feet/sec YDOT = 5068
223835 meter/sec
ZDOT = 18851
178464 ZDOT = 5749
558986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12401300
34 X = 3779916
34
Y = -17488081
36 feet Y = -5330367
20 meter
Z = -5290921
62 Z = -1612672
91
XDOT = 14576
331604 XDOT = 4442
865873
YDOT = 4641
265425 feet/sec YDOT = 1414
657702 meter/sec
ZDOT = 18865
964468 ZDOT = 5750
345970
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 08309
05620825
00020000 00000-0 20000-3 0 9085
2 25544 51
6430 19
3602 0004094 302
5057 57
5709 15
72326203 10545
Satellite: ISS
Catalog Number: 25544
Epoch time: 08309
05620825 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 19
3602 deg
Eccentricity:
0004094
Arg of perigee: 302
5057 deg
Mean anomaly: 57
5709 deg
Mean motion: 15
72326203 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1054
Checksum: 262
Coasting Arc #10 (Orbit 1069)
---------------------------------------
Vector Time (GMT): 2008/310/01:16:24
790
Vector Time (MET): N/A
Weight (LBS) : 626561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1745997
17 A = 6726733
26 meter
Y = -4354403
87 meter E =
0010105
Z = -4829969
20 I = 51
70638
XDOT = 7287
373208 Wp = 52
67003
YDOT = -203
961646 meter/sec RA = 13
77120 deg
ZDOT = -2447
939683 TA = 193
38907
MA = 193
41590
Ha = 191
804 n
mi
Hp = 187
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5728337
19 X = -1673712
22
Y = -14286101
94 feet Y = -4373524
25 meter
Z = -15846355
65 Z = -4838276
01
XDOT = 23908
704750 XDOT = 7301
004181
YDOT = -669
165504 feet/sec YDOT = -122
393706 meter/sec
ZDOT = -8031
298173 ZDOT = -2412
503894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15288287
63 X = -4659870
07
Y = -1463993
12 feet Y = -446225
10 meter
Z = -15878870
51 Z = -4839879
73
XDOT = 10173
544465 XDOT = 3100
896353
YDOT = -20531
789625 feet/sec YDOT = -6258
089478 meter/sec
ZDOT = -7893
957345 ZDOT = -2406
078199
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 08310
07312040
00020000 00000-0 20000-3 0 9097
2 25544 51
6423 14
1505 0004195 306
3844 53
6931 15
72348575 10708
Satellite: ISS
Catalog Number: 25544
Epoch time: 08310
07312040 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 14
1505 deg
Eccentricity:
0004195
Arg of perigee: 306
3844 deg
Mean anomaly: 53
6931 deg
Mean motion: 15
72348575 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1070
Checksum: 257
Coasting Arc #11 (Orbit 1085)
---------------------------------------
Vector Time (GMT): 2008/311/01:16:24
790
Vector Time (MET): N/A
Weight (LBS) : 626561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6095048
78 A = 6733917
11 meter
Y = 1159948
59 meter E =
0010291
Z = 2608054
10 I = 51
70228
XDOT = -3142
987570 Wp = 91
74616
YDOT = -4669
793569 meter/sec RA = 8
61191 deg
ZDOT = -5250
821187 TA = 58
66536
MA = 58
56467
Ha = 191
945 n
mi
Hp = 187
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19996879
20 X = -6120236
18
Y = 3805605
62 feet Y = 1091649
33 meter
Z = 8556607
94 Z = 2578382
70
XDOT = -10311
639008 XDOT = -3065
027612
YDOT = -15320
845042 feet/sec YDOT = -4704
504228 meter/sec
ZDOT = -17227
103633 ZDOT = -5265
900843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5373245
82 X = -1637765
32
Y = 19683485
92 feet Y = 5999526
51 meter
Z = 8441680
08 Z = 2573024
09
XDOT = -16812
746292 XDOT = -5124
525070
YDOT = 2848
728655 feet/sec YDOT = 868
292494 meter/sec
ZDOT = -17285
894953 ZDOT = -5268
740782
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 08311
09002128
00020000 00000-0 20000-3 0 9105
2 25544 51
6427 8
9412 0004178 311
9681 48
1125 15
72381923 10867
Satellite: ISS
Catalog Number: 25544
Epoch time: 08311
09002128 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 8
9412 deg
Eccentricity:
0004178
Arg of perigee: 311
9681 deg
Mean anomaly: 48
1125 deg
Mean motion: 15
72381923 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1086
Checksum: 264
Coasting Arc #12 (Orbit 1101)
---------------------------------------
Vector Time (GMT): 2008/312/01:16:24
790
Vector Time (MET): N/A
Weight (LBS) : 626561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3674614
54 A = 6728770
04 meter
Y = 3636407
45 meter E =
0006217
Z = 4301676
17 I = 51
65477
XDOT = -6440
229732 Wp = 90
41438
YDOT = 2370
439463 meter/sec RA = 3
53709 deg
ZDOT = 3493
211619 TA = 324
22659
MA = 324
26822
Ha = 192
023 n
mi
Hp = 187
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12055822
00 X = 3612781
40
Y = 11930470
64 feet Y = 3677153
34 meter
Z = 14113110
78 Z = 4319377
61
XDOT = -21129
362637 XDOT = -6483
227408
YDOT = 7777
032360 feet/sec YDOT = 2298
180640 meter/sec
ZDOT = 11460
668040 ZDOT = 3461
820010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15876780
15 X = 4839242
59
Y = -5801542
11 feet Y = -1768310
04 meter
Z = 14181989
66 Z = 4322670
45
XDOT = -2344
772946 XDOT = -714
686794
YDOT = 21336
902119 feet/sec YDOT = 6503
487766 meter/sec
ZDOT = 11339
162110 ZDOT = 3456
176611
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 08312
10691161
00020000 00000-0 20000-3 0 9110
2 25544 51
6418 3
7307 0004212 316
2640 43
8188 15
72347293 11027
Satellite: ISS
Catalog Number: 25544
Epoch time: 08312
10691161 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 3
7307 deg
Eccentricity:
0004212
Arg of perigee: 316
2640 deg
Mean anomaly: 43
8188 deg
Mean motion: 15
72347293 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1102
Checksum: 249
Coasting Arc #13 (Orbit 1116)
---------------------------------------
Vector Time (GMT): 2008/313/01:16:24
790
Vector Time (MET): N/A
Weight (LBS) : 626561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4999364
50 A = 6731617
48 meter
Y = -2885026
33 meter E =
0003627
Z = -3462669
81 I = 51
63442
XDOT = 5148
032011 Wp = 35
70346
YDOT = 3460
195305 meter/sec RA = 358
36370 deg
ZDOT = 4554
987509 TA = 283
29285
MA = 283
33330
Ha = 192
114 n
mi
Hp = 187
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16402114
50 X = 5048075
13
Y = -9465309
48 feet Y = -2828848
20 meter
Z = -11360465
26 Z = -3438264
07
XDOT = 16889
868803 XDOT = 5086
829171
YDOT = 11352
346802 feet/sec YDOT = 3517
421390 meter/sec
ZDOT = 14944
184742 ZDOT = 4579
848480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1933756
53 X = -589408
99
Y = -18894911
63 feet Y = -5759169
06 meter
Z = -11266078
06 Z = -3433900
59
XDOT = 15836
695123 XDOT = 4827
024674
YDOT = -10578
421508 feet/sec YDOT = -3224
302876 meter/sec
ZDOT = 15040
800480 ZDOT = 4584
435986
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 08313
06023319
00020000 00000-0 20000-3 0 9121
2 25544 51
6410 358
8461 0004223 317
6274 42
4562 15
72398550 11173
Satellite: ISS
Catalog Number: 25544
Epoch time: 08313
06023319 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 358
8461 deg
Eccentricity:
0004223
Arg of perigee: 317
6274 deg
Mean anomaly: 42
4562 deg
Mean motion: 15
72398550 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1117
Checksum: 266
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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