Date:
December 25th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 95 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 3502)
---------------------------------------
Vector Time (GMT): 2009/352/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2755117
04 A = 6715446
41 meter
Y = -4114188
01 meter E =
0017542
Z = -4552966
53 I = 51
96304
XDOT = 3766
541698 Wp = 78
46616
YDOT = 5946
332655 meter/sec RA = 77
80709 deg
ZDOT = -3100
614102 TA = 160
78145
MA = 160
71519
Ha = 188
695 n
mi
Hp = 176
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9039097
90 X = 2823035
27
Y = -13497992
17 feet Y = -4082998
25 meter
Z = -14937554
23 Z = -4539417
83
XDOT = 12357
420268 XDOT = 3714
831006
YDOT = 19508
965405 feet/sec YDOT = 5988
163673 meter/sec
ZDOT = -10172
618446 ZDOT = -3082
441020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14050673
47 X = 4282645
27
Y = -8250823
69 feet Y = -2514851
06 meter
Z = -14884021
41 Z = -4536649
73
XDOT = 2200
986509 XDOT = 670
860688
YDOT = 21929
961840 feet/sec YDOT = 6684
252369 meter/sec
ZDOT = -10100
564271 ZDOT = -3078
651990
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 09352
70972962
00016717 00000-0 10270-3 0 9008
2 25544 51
6445 78
3879 0007695 90
3886 269
8160 15
76736880 35034
Satellite: ISS
Catalog Number: 25544
Epoch time: 09352
70972962 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 78
3879 deg
Eccentricity:
0007695
Arg of perigee: 90
3886 deg
Mean anomaly: 269
8160 deg
Mean motion: 15
76736880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3503
Checksum: 356
Coasting Arc #2 (Orbit 3518)
---------------------------------------
Vector Time (GMT): 2009/353/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3261542
49 A = 6722811
40 meter
Y = -5567450
16 meter E =
0021605
Z = 1855986
03 I = 51
97934
XDOT = 3430
332816 Wp = 106
32039
YDOT = -3920
459085 meter/sec RA = 72
63401 deg
ZDOT = -5683
997515 TA = 53
13747
MA = 52
93959
Ha = 188
682 n
mi
Hp = 176
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10700598
74 X = -3208059
89
Y = -18265912
61 feet Y = -5603623
86 meter
Z = 6089193
02 Z = 1840270
71
XDOT = 11254
372755 XDOT = 3501
528824
YDOT = -12862
398574 feet/sec YDOT = -3881
700252 meter/sec
ZDOT = -18648
285811 ZDOT = -5667
160618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2184071
19 X = -665704
90
Y = -21074422
21 feet Y = -6423483
89 meter
Z = 6026873
97 Z = 1836991
18
XDOT = 14141
159755 XDOT = 4310
225493
YDOT = -6825
190429 feet/sec YDOT = -2080
318043 meter/sec
ZDOT = -18581
728458 ZDOT = -5663
710834
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 09353
72378662
00016717 00000-0 10270-3 0 9019
2 25544 51
6432 73
1590 0007783 93
1764 267
0292 15
76779809 35198
Satellite: ISS
Catalog Number: 25544
Epoch time: 09353
72378662 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 73
1590 deg
Eccentricity:
0007783
Arg of perigee: 93
1764 deg
Mean anomaly: 267
0292 deg
Mean motion: 15
76779809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3519
Checksum: 341
Coasting Arc #3 (Orbit 3534)
---------------------------------------
Vector Time (GMT): 2009/354/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3287866
11 A = 6712490
11 meter
Y = 2686017
59 meter E =
0011201
Z = 5190555
27 I = 51
93408
XDOT = -3700
196553 Wp = 105
19960
YDOT = -6677
252440 meter/sec RA = 67
52593 deg
ZDOT = 1106
691300 TA = 334
27289
MA = 334
32857
Ha = 188
702 n
mi
Hp = 176
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10786962
31 X = -3342871
91
Y = 8812393
68 feet Y = 2648942
59 meter
Z = 17029380
81 Z = 5174449
60
XDOT = -12139
752472 XDOT = -3630
631414
YDOT = -21906
996195 feet/sec YDOT = -6718
241391 meter/sec
ZDOT = 3630
876968 ZDOT = 1088
884048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13500524
32 X = -4114959
81
Y = 3730675
10 feet Y = 1137109
77 meter
Z = 16965687
59 Z = 5171141
58
XDOT = -2125
915633 XDOT = -647
979085
YDOT = -23956
410511 feet/sec YDOT = -7301
913924 meter/sec
ZDOT = 3560
254906 ZDOT = 1085
165695
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 09354
73781993
00016717 00000-0 10270-3 0 9027
2 25544 51
6426 67
9300 0007714 96
6424 263
5619 15
76805906 35356
Satellite: ISS
Catalog Number: 25544
Epoch time: 09354
73781993 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 67
9300 deg
Eccentricity:
0007714
Arg of perigee: 96
6424 deg
Mean anomaly: 263
5619 deg
Mean motion: 15
76805906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3535
Checksum: 337
Coasting Arc #4 (Orbit 3549)
---------------------------------------
Vector Time (GMT): 2009/355/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3133463
17 A = 6723961
19 meter
Y = 5943697
69 meter E =
0017787
Z = -26987
35 I = 51
96114
XDOT = -4194
352093 Wp = 66
03626
YDOT = 2224
597967 meter/sec RA = 62
38226 deg
ZDOT = 6068
298581 TA = 293
67154
MA = 293
85812
Ha = 188
453 n
mi
Hp = 176
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10280390
98 X = 3066897
91
Y = 19500320
49 feet Y = 5978365
74 meter
Z = -88541
17 Z = -11926
16
XDOT = -13760
997680 XDOT = -4248
394762
YDOT = 7298
549762 feet/sec YDOT = 2177
391484 meter/sec
ZDOT = 19909
116081 ZDOT = 6047
791460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2013584
77 X = 613740
64
Y = 21952253
28 feet Y = 6691046
80 meter
Z = -28805
09 Z = -8779
79
XDOT = -14014
901511 XDOT = -4271
741981
YDOT = 1270
219771 feet/sec YDOT = 387
162986 meter/sec
ZDOT = 19827
988539 ZDOT = 6043
570907
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 09355
68845486
00016717 00000-0 10270-3 0 9031
2 25544 51
6428 63
0288 0007709 101
0283 259
1749 15
76890060 35505
Satellite: ISS
Catalog Number: 25544
Epoch time: 09355
68845486 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 63
0288 deg
Eccentricity:
0007709
Arg of perigee: 101
0283 deg
Mean anomaly: 259
1749 deg
Mean motion: 15
76890060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3550
Checksum: 330
Coasting Arc #5 (Orbit 3565)
---------------------------------------
Vector Time (GMT): 2009/356/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4089256
96 A = 6712400
85 meter
Y = -1189376
78 meter E =
0022004
Z = -5207511
47 I = 51
90588
XDOT = 3373
677546 Wp = 99
79746
YDOT = 6822
730983 meter/sec RA = 57
23586 deg
ZDOT = 1091
156540 TA = 180
58952
MA = 180
59211
Ha = 188
448 n
mi
Hp = 176
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13416197
37 X = 4127549
94
Y = -3902154
79 feet Y = -1143433
75 meter
Z = -17085011
38 Z = -5187552
99
XDOT = 11068
495886 XDOT = 3291
833203
YDOT = 22384
288002 feet/sec YDOT = 6859
999731 meter/sec
ZDOT = 3579
909907 ZDOT = 1107
347598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14004189
35 X = 4268476
91
Y = 1340256
68 feet Y = 408510
24 meter
Z = -17006033
36 Z = -5183438
97
XDOT = 2141
145629 XDOT = 652
621188
YDOT = 23857
071398 feet/sec YDOT = 7271
635362 meter/sec
ZDOT = 3644
132621 ZDOT = 1110
731623
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 09356
70244331
00016717 00000-0 10270-3 0 9048
2 25544 51
6421 57
7988 0007587 102
9033 257
2980 15
76851070 35663
Satellite: ISS
Catalog Number: 25544
Epoch time: 09356
70244331 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 57
7988 deg
Eccentricity:
0007587
Arg of perigee: 102
9033 deg
Mean anomaly: 257
2980 deg
Mean motion: 15
76851070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3566
Checksum: 325
Coasting Arc #6 (Orbit 3581)
---------------------------------------
Vector Time (GMT): 2009/357/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2663673
39 A = 6722285
80 meter
Y = -5865966
09 meter E =
0013967
Z = -1913111
32 I = 51
92218
XDOT = 5201
819425 Wp = 122
27717
YDOT = -529
616044 meter/sec RA = 52
12413 deg
ZDOT = -5655
796677 TA = 78
92345
MA = 78
76642
Ha = 188
365 n
mi
Hp = 176
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8739085
93 X = -2588587
60
Y = -19245295
58 feet Y = -5895332
89 meter
Z = -6276611
95 Z = -1925869
51
XDOT = 17066
336697 XDOT = 5234
829920
YDOT = -1737
585445 feet/sec YDOT = -471
261227 meter/sec
ZDOT = -18555
763375 ZDOT = -5630
446083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1379352
98 X = -420426
79
Y = -21076349
69 feet Y = -6424071
38 meter
Z = -6327223
07 Z = -1928537
59
XDOT = 15152
222582 XDOT = 4618
397443
YDOT = 4512
539600 feet/sec YDOT = 1375
422070 meter/sec
ZDOT = -18455
428769 ZDOT = -5625
214689
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 09357
71640905
00016717 00000-0 10270-3 0 9058
2 25544 51
6417 52
5687 0007662 105
9230 254
2780 15
76907665 35828
Satellite: ISS
Catalog Number: 25544
Epoch time: 09357
71640905 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 52
5687 deg
Eccentricity:
0007662
Arg of perigee: 105
9230 deg
Mean anomaly: 254
2780 deg
Mean motion: 15
76907665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3582
Checksum: 330
Coasting Arc #7 (Orbit 3597)
---------------------------------------
Vector Time (GMT): 2009/358/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4986691
09 A = 6715112
37 meter
Y = -186881
26 meter E =
0015460
Z = 4480796
46 I = 51
87845
XDOT = -2640
594737 Wp = 86
13877
YDOT = -6503
696065 meter/sec RA = 46
94388 deg
ZDOT = -3199
564860 TA = 35
73075
MA = 35
62739
Ha = 188
354 n
mi
Hp = 176
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16360535
09 X = -5005997
71
Y = -613127
51 feet Y = -242753
67 meter
Z = 14700775
80 Z = 4456524
11
XDOT = -8663
368561 XDOT = -2552
130043
YDOT = -21337
585515 feet/sec YDOT = -6532
729887 meter/sec
ZDOT = -10497
260040 ZDOT = -3212
178518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15287777
56 X = -4659714
60
Y = -6094466
89 feet Y = -1857593
51 meter
Z = 14604696
96 Z = 4451511
63
XDOT = -1389
555611 XDOT = -423
536550
YDOT = -21872
151820 feet/sec YDOT = -6666
631875 meter/sec
ZDOT = -10547
304269 ZDOT = -3214
818341
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 09358
73035129
00016717 00000-0 10270-3 0 9068
2 25544 51
6414 47
3392 0007467 109
2843 250
9130 15
76952374 35986
Satellite: ISS
Catalog Number: 25544
Epoch time: 09358
73035129 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 47
3392 deg
Eccentricity:
0007467
Arg of perigee: 109
2843 deg
Mean anomaly: 250
9130 deg
Mean motion: 15
76952374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3598
Checksum: 328
Coasting Arc #8 (Orbit 3613)
---------------------------------------
Vector Time (GMT): 2009/359/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1817140
50 A = 6718021
28 meter
Y = 5386718
49 meter E =
0019266
Z = 3566787
51 I = 51
86797
XDOT = -6225
836846 Wp = 100
98935
YDOT = -871
722157 meter/sec RA = 41
85266 deg
ZDOT = 4464
532101 TA = 301
51584
MA = 301
70391
Ha = 188
067 n
mi
Hp = 176
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5961747
06 X = 1739443
29
Y = 17672960
93 feet Y = 5406604
12 meter
Z = 11702058
77 Z = 3575426
95
XDOT = -20425
973903 XDOT = -6237
314417
YDOT = -2859
980829 feet/sec YDOT = -941
407674 meter/sec
ZDOT = 14647
415029 ZDOT = 4434
258819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -56737
91 X = -17293
72
Y = 18629791
57 feet Y = 5678360
47 meter
Z = 11736345
35 Z = 3577238
06
XDOT = -17167
007659 XDOT = -5232
503935
YDOT = -9253
380211 feet/sec YDOT = -2820
430288 meter/sec
ZDOT = 14527
573237 ZDOT = 4428
004323
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 09359
74427054
00016717 00000-0 10270-3 0 9073
2 25544 51
6418 42
1102 0007437 113
9815 246
2129 15
77015607 36145
Satellite: ISS
Catalog Number: 25544
Epoch time: 09359
74427054 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 42
1102 deg
Eccentricity:
0007437
Arg of perigee: 113
9815 deg
Mean anomaly: 246
2129 deg
Mean motion: 15
77015607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3614
Checksum: 302
Coasting Arc #9 (Orbit 3628)
---------------------------------------
Vector Time (GMT): 2009/360/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5813564
64 A = 6719447
40 meter
Y = 1251712
92 meter E =
0011395
Z = -3140343
74 I = 51
84916
XDOT = 1376
970411 Wp = 100
47049
YDOT = 5795
610036 meter/sec RA = 36
65878 deg
ZDOT = 4872
038076 TA = 223
10178
MA = 223
19106
Ha = 188
143 n
mi
Hp = 176
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19073374
81 X = 5814391
05
Y = 4106669
67 feet Y = 1316728
55 meter
Z = -10302965
03 Z = -3112099
05
XDOT = 4517
619460 XDOT = 1288
392840
YDOT = 19014
468622 feet/sec YDOT = 5810
512408 meter/sec
ZDOT = 15984
376889 ZDOT = 4878
512853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16991101
38 X = 5178887
70
Y = 9708368
07 feet Y = 2959110
59 meter
Z = -10191148
82 Z = -3106262
16
XDOT = -834
845412 XDOT = -254
460881
YDOT = 18222
641212 feet/sec YDOT = 5554
261042 meter/sec
ZDOT = 16010
093984 ZDOT = 4879
876646
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 09360
69480179
00016717 00000-0 10270-3 0 9087
2 25544 51
6419 37
2070 0007523 115
4475 244
7469 15
76997777 36292
Satellite: ISS
Catalog Number: 25544
Epoch time: 09360
69480179 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 37
2070 deg
Eccentricity:
0007523
Arg of perigee: 115
4475 deg
Mean anomaly: 244
7469 deg
Mean motion: 15
76997777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3629
Checksum: 353
Coasting Arc #10 (Orbit 3644)
---------------------------------------
Vector Time (GMT): 2009/361/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -457767
33 A = 6713555
64 meter
Y = -4700631
93 meter E =
0017664
Z = -4786542
51 I = 51
80559
XDOT = 6992
140458 Wp = 89
68506
YDOT = 1924
600611 meter/sec RA = 31
55799 deg
ZDOT = -2566
769022 TA = 155
23615
MA = 155
15127
Ha = 188
002 n
mi
Hp = 176
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1501861
33 X = -381917
63
Y = -15422020
76 feet Y = -4705326
29 meter
Z = -15703879
61 Z = -4788582
67
XDOT = 22940
093367 XDOT = 6982
568586
YDOT = 6314
306465 feet/sec YDOT = 2002
737636 meter/sec
ZDOT = -8421
158208 ZDOT = -2532
823881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3066612
85 X = 934703
60
Y = -15180067
71 feet Y = -4626884
64 meter
Z = -15712020
13 Z = -4789023
73
XDOT = 19110
388888 XDOT = 5824
846533
YDOT = 12410
578007 feet/sec YDOT = 3782
744176 meter/sec
ZDOT = -8286
770228 ZDOT = -2525
807566
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 09361
70867880
00016717 00000-0 10270-3 0 9099
2 25544 51
6425 31
9766 0007452 119
4294 240
7616 15
77040288 36451
Satellite: ISS
Catalog Number: 25544
Epoch time: 09361
70867880 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 31
9766 deg
Eccentricity:
0007452
Arg of perigee: 119
4294 deg
Mean anomaly: 240
7616 deg
Mean motion: 15
77040288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3645
Checksum: 334
Coasting Arc #11 (Orbit 3660)
---------------------------------------
Vector Time (GMT): 2009/362/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6279579
91 A = 6722783
92 meter
Y = -2012838
89 meter E =
0021303
Z = 1254606
93 I = 51
81083
XDOT = 404
014282 Wp = 121
61420
YDOT = -4967
126995 meter/sec RA = 26
37975 deg
ZDOT = -5885
214682 TA = 44
62912
MA = 44
45782
Ha = 187
901 n
mi
Hp = 176
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20602296
30 X = -6262699
98
Y = -6603802
13 feet Y = -2082966
66 meter
Z = 4116164
47 Z = 1224141
18
XDOT = 1325
506174 XDOT = 488
117089
YDOT = -16296
348409 feet/sec YDOT = -4962
137983 meter/sec
ZDOT = -19308
447119 ZDOT = -5883
048387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18078224
19 X = -5510242
73
Y = -11925646
20 feet Y = -3634936
96 meter
Z = 3995547
29 Z = 1217842
81
XDOT = 4914
152232 XDOT = 1497
833600
YDOT = -13985
455139 feet/sec YDOT = -4262
766726 meter/sec
ZDOT = -19299
933937 ZDOT = -5882
619864
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 09362
72253332
00016717 00000-0 10270-3 0 9105
2 25544 51
6428 26
7468 0007367 122
7453 237
4423 15
77080708 36612
Satellite: ISS
Catalog Number: 25544
Epoch time: 09362
72253332 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 26
7468 deg
Eccentricity:
0007367
Arg of perigee: 122
7453 deg
Mean anomaly: 237
4423 deg
Mean motion: 15
77080708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3661
Checksum: 311
Coasting Arc #12 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2009/363/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1221043
57 A = 6711200
04 meter
Y = 3975460
15 meter E =
0009540
Z = 5260455
94 I = 51
74512
XDOT = -7258
748810 Wp = 119
77931
YDOT = -2593
599075 meter/sec RA = 21
24564 deg
ZDOT = 270
149611 TA = 327
63501
MA = 327
69349
Ha = 187
772 n
mi
Hp = 176
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4006048
44 X = -1290961
56
Y = 13042848
25 feet Y = 3961413
91 meter
Z = 17258713
71 Z = 5254354
91
XDOT = -23814
792685 XDOT = -7230
519584
YDOT = -8509
183318 feet/sec YDOT = -2674
612897 meter/sec
ZDOT = 886
317621 ZDOT = 234
954593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7277031
14 X = -2218039
09
Y = 11577591
55 feet Y = 3528849
90 meter
Z = 17234607
78 Z = 5253108
45
XDOT = -20043
151630 XDOT = -6109
152617
YDOT = -13734
501892 feet/sec YDOT = -4186
276177 meter/sec
ZDOT = 746
970466 ZDOT = 227
676598
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 09363
73636510
00016717 00000-0 10270-3 0 9111
2 25544 51
6432 21
5175 0007274 126
6721 233
5113 15
77128497 36771
Satellite: ISS
Catalog Number: 25544
Epoch time: 09363
73636510 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 21
5175 deg
Eccentricity:
0007274
Arg of perigee: 126
6721 deg
Mean anomaly: 233
5113 deg
Mean motion: 15
77128497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3677
Checksum: 306
Coasting Arc #13 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2009/364/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6202417
21 A = 6722888
13 meter
Y = 2453575
26 meter E =
0016897
Z = 808636
67 I = 51
75602
XDOT = -2452
537949 Wp = 78
46710
YDOT = 4196
167751 meter/sec RA = 16
09985 deg
ZDOT = 5978
070923 TA = 290
34765
MA = 290
52912
Ha = 187
659 n
mi
Hp = 176
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20349137
84 X = 6170591
73
Y = 8049787
60 feet Y = 2522756
26 meter
Z = 2653007
46 Z = 838691
08
XDOT = -8046
384346 XDOT = -2528
318269
YDOT = 13766
954565 feet/sec YDOT = 4168
317253 meter/sec
ZDOT = 19613
093578 ZDOT = 5965
973194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17851042
42 X = 5440997
73
Y = 12632544
86 feet Y = 3850399
67 meter
Z = 2772009
17 Z = 844908
39
XDOT = -10265
925181 XDOT = -3129
053995
YDOT = 10143
655425 feet/sec YDOT = 3091
786174 meter/sec
ZDOT = 19565
246660 ZDOT = 5963
487182
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 09364
75017473
00016717 00000-0 10270-3 0 9126
2 25544 51
6429 16
2867 0007321 130
5841 229
5962 15
77161049 36931
Satellite: ISS
Catalog Number: 25544
Epoch time: 09364
75017473 = yrday
fracday
Element set: 912
Inclination: 51
6429 deg
RA of node: 16
2867 deg
Eccentricity:
0007321
Arg of perigee: 130
5841 deg
Mean anomaly: 229
5962 deg
Mean motion: 15
77161049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3693
Checksum: 321
Coasting Arc #14 (Orbit 3707)
---------------------------------------
Vector Time (GMT): 2009/365/16:31:20
798
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3066530
23 A = 6712608
59 meter
Y = -3381820
35 meter E =
0019306
Z = -4938856
64 I = 51
69252
XDOT = 6749
515077 Wp = 115
54772
YDOT = 3012
755999 meter/sec RA = 10
92045 deg
ZDOT = 2126
084495 TA = 175
08877
MA = 175
06981
Ha = 187
548 n
mi
Hp = 176
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10060794
73 X = 3128110
27
Y = -11095211
11 feet Y = -3347183
43 meter
Z = -16203597
91 Z = -4923810
59
XDOT = 22144
078335 XDOT = 6704
996239
YDOT = 9884
370074 feet/sec YDOT = 3087
983778 meter/sec
ZDOT = 6975
342832 ZDOT = 2158
765709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12346706
36 X = 3763276
10
Y = -8591148
23 feet Y = -2618581
98 meter
Z = -16144067
01 Z = -4920711
62
XDOT = 18762
090078 XDOT = 5718
685056
YDOT = 13602
157145 feet/sec YDOT = 4145
937498 meter/sec
ZDOT = 7104
756509 ZDOT = 2165
529784
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 09365
70060120
00016717 00000-0 10270-3 0 9130
2 25544 51
6434 11
3828 0007223 133
7150 226
4614 15
77180802 37084
Satellite: ISS
Catalog Number: 25544
Epoch time: 09365
70060120 = yrday
fracday
Element set: 913
Inclination: 51
6434 deg
RA of node: 11
3828 deg
Eccentricity:
0007223
Arg of perigee: 133
7150 deg
Mean anomaly: 226
4614 deg
Mean motion: 15
77180802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3708
Checksum: 278
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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