Date:
October 15th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 3229 17 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2931)
---------------------------------------
Vector Time (GMT): 2007/285/16:11:23
120
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -711547
63 A = 6719117
35 meter
Y = -4977989
59 meter E =
0011517
Z = 4448536
96 I = 51
43472
XDOT = 6752
490665 Wp = 105
37022
YDOT = 1899
382445 meter/sec RA = 217
00917 deg
ZDOT = 3195
647617 TA = 312
56081
MA = 312
65797
Ha = 188
687 n
mi
Hp = 180
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2334473
84 X = -677440
90
Y = -16331986
86 feet Y = -4985755
61 meter
Z = 14594937
52 Z = 4445163
25
XDOT = 22153
840765 XDOT = 6715
225318
YDOT = 6231
569702 feet/sec YDOT = 1974
684411 meter/sec
ZDOT = 10484
408192 ZDOT = 3228
361497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16505100
12 X = 5030754
52
Y = -397445
44 feet Y = -121141
37 meter
Z = 14581476
99 Z = 4444434
19
XDOT = -8920
419050 XDOT = -2718
943726
YDOT = 19961
050940 feet/sec YDOT = 6084
128326 meter/sec
ZDOT = 10608
914612 ZDOT = 3233
597174
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 07285
72786347
00020000 00000-0 20000-3 0 9005
2 25544 51
6378 217
6559 0002712 81
7456 278
4016 15
75562167 29329
Satellite: ISS
Catalog Number: 25544
Epoch time: 07285
72786347 = yrday
fracday
Element set: 900
Inclination: 51
6378 deg
RA of node: 217
6559 deg
Eccentricity:
0002712
Arg of perigee: 81
7456 deg
Mean anomaly: 278
4016 deg
Mean motion: 15
75562167 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2932
Checksum: 316
Coasting Arc #2 (Orbit 2946)
---------------------------------------
Vector Time (GMT): 2007/286/16:11:23
120
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6102969
09 A = 6725240
43 meter
Y = -1614378
53 meter E =
0007804
Z = -2316929
43 I = 51
47921
XDOT = -607
276550 Wp = 57
20706
YDOT = -5444
230167 meter/sec RA = 211
80375 deg
ZDOT = 5410
335801 TA = 276
66494
MA = 276
75376
Ha = 188
518 n
mi
Hp = 180
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20022864
46 X = -6073207
73
Y = -5296517
47 feet Y = -1682459
04 meter
Z = -7601474
52 Z = -2346506
16
XDOT = -1992
377133 XDOT = -572
636399
YDOT = -17861
647530 feet/sec YDOT = -5450
827233 meter/sec
ZDOT = 17750
445540 ZDOT = 5407
469873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7373297
45 X = 2247381
06
Y = -19310069
16 feet Y = -5885709
08 meter
Z = -7714034
43 Z = -2351237
69
XDOT = 16574
666618 XDOT = 5051
958385
YDOT = -735
173893 feet/sec YDOT = -224
081003 meter/sec
ZDOT = 17738
855204 ZDOT = 5406
803066
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 07286
67924469
00020000 00000-0 20000-3 0 9010
2 25544 51
6372 212
7580 0002485 83
7163 276
4284 15
75590278 29472
Satellite: ISS
Catalog Number: 25544
Epoch time: 07286
67924469 = yrday
fracday
Element set: 901
Inclination: 51
6372 deg
RA of node: 212
7580 deg
Eccentricity:
0002485
Arg of perigee: 83
7163 deg
Mean anomaly: 276
4284 deg
Mean motion: 15
75590278 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2947
Checksum: 324
Coasting Arc #3 (Orbit 2962)
---------------------------------------
Vector Time (GMT): 2007/287/16:11:23
120
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 281902
81 A = 6716937
96 meter
Y = 4549650
03 meter E =
0015156
Z = -4947151
54 I = 51
47545
XDOT = -7194
318570 Wp = 77
06403
YDOT = -1785
432609 meter/sec RA = 206
68150 deg
ZDOT = -2053
864198 TA = 172
99005
MA = 172
96883
Ha = 188
495 n
mi
Hp = 180
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 924877
98 X = 255040
03
Y = 14926673
33 feet Y = 4552652
18 meter
Z = -16230812
13 Z = -4945847
31
XDOT = -23603
407382 XDOT = -7163
841311
YDOT = -5857
718535 feet/sec YDOT = -1865
713165 meter/sec
ZDOT = -6738
399600 ZDOT = -2088
741128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14958183
19 X = -4559254
24
Y = -305855
02 feet Y = -93224
61 meter
Z = -16225271
85 Z = -4945462
86
XDOT = 7893
353935 XDOT = 2405
894279
YDOT = -21865
053669 feet/sec YDOT = -6664
468358 meter/sec
ZDOT = -6871
125113 ZDOT = -2094
318934
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 07287
69403977
00020000 00000-0 20000-3 0 9020
2 25544 51
6361 207
5332 0002449 88
2595 271
8849 15
75622068 29633
Satellite: ISS
Catalog Number: 25544
Epoch time: 07287
69403977 = yrday
fracday
Element set: 902
Inclination: 51
6361 deg
RA of node: 207
5332 deg
Eccentricity:
0002449
Arg of perigee: 88
2595 deg
Mean anomaly: 271
8849 deg
Mean motion: 15
75622068 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2963
Checksum: 325
Coasting Arc #4 (Orbit 2978)
---------------------------------------
Vector Time (GMT): 2007/288/16:11:23
120
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6437156
76 A = 6726792
39 meter
Y = 1467541
18 meter E =
0016226
Z = 1250299
43 I = 51
53567
XDOT = 6
822814 Wp = 116
94305
YDOT = 5005
215009 meter/sec RA = 201
49529 deg
ZDOT = -5859
107073 TA = 49
31006
MA = 49
16919
Ha = 188
475 n
mi
Hp = 180
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21119280
72 X = 6414194
18
Y = 4814767
66 feet Y = 1539396
71 meter
Z = 4102032
25 Z = 1281516
19
XDOT = 22
384561 XDOT = -20
683527
YDOT = 16421
309086 feet/sec YDOT = 5005
137551 meter/sec
ZDOT = -19222
792233 ZDOT = -5859
140706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6303622
79 X = -1921344
23
Y = 20699798
73 feet Y = 6309298
65 meter
Z = 4220822
96 Z = 1286506
84
XDOT = -14879
619036 XDOT = -4535
307882
YDOT = -578
587902 feet/sec YDOT = -176
353592 meter/sec
ZDOT = -19222
278035 ZDOT = -5858
950345
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 07288
70882266
00020000 00000-0 20000-3 0 9036
2 25544 51
6362 202
3092 0002525 92
2527 267
8926 15
75642548 29798
Satellite: ISS
Catalog Number: 25544
Epoch time: 07288
70882266 = yrday
fracday
Element set: 903
Inclination: 51
6362 deg
RA of node: 202
3092 deg
Eccentricity:
0002525
Arg of perigee: 92
2527 deg
Mean anomaly: 267
8926 deg
Mean motion: 15
75642548 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2979
Checksum: 316
Coasting Arc #5 (Orbit 2994)
---------------------------------------
Vector Time (GMT): 2007/289/16:11:23
120
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 299725
62 A = 6715686
25 meter
Y = -4224996
81 meter E =
0005687
Z = 5207199
82 I = 51
52431
XDOT = 7510
317437 Wp = 110
77047
YDOT = 1533
877316 meter/sec RA = 196
35793 deg
ZDOT = 809
563928 TA = 331
50401
MA = 331
53509
Ha = 188
488 n
mi
Hp = 180
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 983351
76 X = 321651
66
Y = -13861538
09 feet Y = -4221522
61 meter
Z = 17083988
89 Z = 5208709
10
XDOT = 24640
149070 XDOT = 7488
674395
YDOT = 5032
405894 feet/sec YDOT = 1617
740907 meter/sec
ZDOT = 2656
049634 ZDOT = 845
997362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13793510
01 X = 4204261
85
Y = 1634257
07 feet Y = 498121
56 meter
Z = 17089183
15 Z = 5208783
03
XDOT = -6235
299862 XDOT = -1900
519398
YDOT = 23311
379314 feet/sec YDOT = 7105
308415 meter/sec
ZDOT = 2794
683309 ZDOT = 851
819473
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 07289
72359273
00020000 00000-0 20000-3 0 9047
2 25544 51
6351 197
0838 0002501 96
9622 263
1827 15
75632844 29950
Satellite: ISS
Catalog Number: 25544
Epoch time: 07289
72359273 = yrday
fracday
Element set: 904
Inclination: 51
6351 deg
RA of node: 197
0838 deg
Eccentricity:
0002501
Arg of perigee: 96
9622 deg
Mean anomaly: 263
1827 deg
Mean motion: 15
75632844 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2995
Checksum: 319
Coasting Arc #6 (Orbit 3009)
---------------------------------------
Vector Time (GMT): 2007/290/16:11:23
120
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6614184
60 A = 6727424
71 meter
Y = -1191201
37 meter E =
0013352
Z = -145677
22 I = 51
59119
XDOT = 727
966158 Wp = 52
70285
YDOT = -4732
920547 meter/sec RA = 191
19413 deg
ZDOT = 6034
252298 TA = 305
71238
MA = 305
83654
Ha = 188
376 n
mi
Hp = 180
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21700080
71 X = -6599665
14
Y = -3908140
96 feet Y = -1265083
73 meter
Z = -477943
63 Z = -177774
33
XDOT = 2388
340412 XDOT = 751
522393
YDOT = -15527
954550 feet/sec YDOT = -4724
648448 meter/sec
ZDOT = 19797
415677 ZDOT = 6037
845938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4704000
93 X = 1433779
48
Y = -21538518
74 feet Y = -6564940
51 meter
Z = -600070
62 Z = -182901
52
XDOT = 13863
122022 XDOT = 4225
479592
YDOT = 2503
805101 feet/sec YDOT = 763
159795 meter/sec
ZDOT = 19810
466811 ZDOT = 6038
230284
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 07290
67492649
00020000 00000-0 20000-3 0 9059
2 25544 51
6339 192
1848 0002383 100
6585 259
4848 15
75665074 30103
Satellite: ISS
Catalog Number: 25544
Epoch time: 07290
67492649 = yrday
fracday
Element set: 905
Inclination: 51
6339 deg
RA of node: 192
1848 deg
Eccentricity:
0002383
Arg of perigee: 100
6585 deg
Mean anomaly: 259
4848 deg
Mean motion: 15
75665074 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3010
Checksum: 314
Coasting Arc #7 (Orbit 3025)
---------------------------------------
Vector Time (GMT): 2007/291/16:11:23
120
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1003802
86 A = 6715339
77 meter
Y = 4082541
20 meter E =
0017380
Z = -5251466
25 I = 51
57842
XDOT = -7578
419884 Wp = 95
78103
YDOT = -1207
870674 meter/sec RA = 186
03821 deg
ZDOT = 509
304340 TA = 179
06925
MA = 179
06601
Ha = 188
364 n
mi
Hp = 180
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3293316
48 X = -1023868
76
Y = 13394164
04 feet Y = 4071204
01 meter
Z = -17229219
99 Z = -5256391
47
XDOT = -24863
582295 XDOT = -7566
824193
YDOT = -3962
830296 feet/sec YDOT = -1292
552028 meter/sec
ZDOT = 1670
945999 ZDOT = 472
515919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13329001
25 X = -4062679
58
Y = -3458316
05 feet Y = -1054094
73 meter
Z = -17247416
07 Z = -5257012
42
XDOT = 4197
583387 XDOT = 1279
423416
YDOT = -23818
142769 feet/sec YDOT = -7259
769916 meter/sec
ZDOT = 1530
972589 ZDOT = 466
640445
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 07291
68967128
00020000 00000-0 20000-3 0 9061
2 25544 51
6329 186
9589 0002481 106
0672 254
0766 15
75699624 30266
Satellite: ISS
Catalog Number: 25544
Epoch time: 07291
68967128 = yrday
fracday
Element set: 906
Inclination: 51
6329 deg
RA of node: 186
9589 deg
Eccentricity:
0002481
Arg of perigee: 106
0672 deg
Mean anomaly: 254
0766 deg
Mean motion: 15
75699624 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3026
Checksum: 329
Coasting Arc #8 (Orbit 3041)
---------------------------------------
Vector Time (GMT): 2007/292/16:11:23
120
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6577130
50 A = 6726815
18 meter
Y = 924452
09 meter E =
0011915
Z = -1037288
94 I = 51
64676
XDOT = -1581
886204 Wp = 135
63803
YDOT = 4662
880109 meter/sec RA = 180
90227 deg
ZDOT = -5923
713582 TA = 55
71001
MA = 55
59727
Ha = 188
318 n
mi
Hp = 180
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21578512
13 X = 6571343
34
Y = 3032979
31 feet Y = 997968
94 meter
Z = -3403178
93 Z = -1005350
85
XDOT = -5189
915368 XDOT = -1605
132938
YDOT = 15298
163087 feet/sec YDOT = 4645
060620 meter/sec
ZDOT = -19434
755845 ZDOT = -5931
454928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3084964
53 X = -940297
19
Y = 21589962
06 feet Y = 6580620
44 meter
Z = -3281662
40 Z = -1000250
70
XDOT = -13711
623266 XDOT = -4179
302771
YDOT = -4892
295058 feet/sec YDOT = -1491
171534 meter/sec
ZDOT = -19463
582027 ZDOT = -5932
499802
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 07292
70440278
00020000 00000-0 20000-3 0 9078
2 25544 51
6334 181
7342 0002412 107
5250 252
6178 15
75732501 30425
Satellite: ISS
Catalog Number: 25544
Epoch time: 07292
70440278 = yrday
fracday
Element set: 907
Inclination: 51
6334 deg
RA of node: 181
7342 deg
Eccentricity:
0002412
Arg of perigee: 107
5250 deg
Mean anomaly: 252
6178 deg
Mean motion: 15
75732501 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3042
Checksum: 265
Coasting Arc #9 (Orbit 3057)
---------------------------------------
Vector Time (GMT): 2007/293/16:11:23
120
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1739932
86 A = 6716283
65 meter
Y = -4109501
71 meter E =
0006962
Z = 5014111
36 I = 51
63970
XDOT = 7431
915068 Wp = 73
23275
YDOT = 901
833367 meter/sec RA = 175
72821 deg
ZDOT = -1835
733080 TA = 34
47089
MA = 34
42575
Ha = 188
268 n
mi
Hp = 180
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5708441
15 X = 1761398
66
Y = -13482617
16 feet Y = -4089924
71 meter
Z = 16450496
60 Z = 5022616
25
XDOT = 24382
923452 XDOT = 7430
196044
YDOT = 2958
770888 feet/sec YDOT = 984
931613 meter/sec
ZDOT = -6022
746325 ZDOT = -1799
632574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13564310
20 X = 4134401
75
Y = 5415668
92 feet Y = 1650695
89 meter
Z = 16482297
26 Z = 5023804
21
XDOT = -2202
319915 XDOT = -671
267110
YDOT = 23468
413882 feet/sec YDOT = 7153
172551 meter/sec
ZDOT = -5885
397350 ZDOT = -1793
869112
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 07293
71912267
00020000 00000-0 20000-3 0 9083
2 25544 51
6329 176
5084 0002465 115
5634 244
5785 15
75713407 30582
Satellite: ISS
Catalog Number: 25544
Epoch time: 07293
71912267 = yrday
fracday
Element set: 908
Inclination: 51
6329 deg
RA of node: 176
5084 deg
Eccentricity:
0002465
Arg of perigee: 115
5634 deg
Mean anomaly: 244
5785 deg
Mean motion: 15
75713407 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3058
Checksum: 307
Coasting Arc #10 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2007/294/16:11:23
120
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6330229
08 A = 6725247
53 meter
Y = -673875
76 meter E =
0015841
Z = 2148818
66 I = 51
69864
XDOT = 2396
401872 Wp = 77
40777
YDOT = -4814
253649 meter/sec RA = 170
61495 deg
ZDOT = 5519
227523 TA = 306
64233
MA = 306
78787
Ha = 188
278 n
mi
Hp = 180
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20768468
12 X = -6332661
94
Y = -2210878
47 feet Y = -744677
49 meter
Z = 7049930
00 Z = 2118060
12
XDOT = 7862
210865 XDOT = 2423
245704
YDOT = -15794
795435 feet/sec YDOT = -4787
305444 meter/sec
ZDOT = 18107
701847 ZDOT = 5530
934769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1544094
57 X = 470640
03
Y = -20867901
85 feet Y = -6360536
48 meter
Z = 6932907
69 Z = 2113150
26
XDOT = 14513
358633 XDOT = 4423
671711
YDOT = 7138
280781 feet/sec YDOT = 2175
747982 meter/sec
ZDOT = 18151
586319 ZDOT = 5532
603510
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 07294
73382882
00020000 00000-0 20000-3 0 9091
2 25544 51
6327 171
2824 0002526 120
0128 240
1287 15
75756591 30749
Satellite: ISS
Catalog Number: 25544
Epoch time: 07294
73382882 = yrday
fracday
Element set: 909
Inclination: 51
6327 deg
RA of node: 171
2824 deg
Eccentricity:
0002526
Arg of perigee: 120
0128 deg
Mean anomaly: 240
1287 deg
Mean motion: 15
75756591 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3074
Checksum: 292
Coasting Arc #11 (Orbit 3088)
---------------------------------------
Vector Time (GMT): 2007/295/16:11:23
120
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2423588
75 A = 6718125
06 meter
Y = 4333044
04 meter E =
0012825
Z = -4538614
17 I = 51
70388
XDOT = -7013
197233 Wp = 113
28822
YDOT = -693
606093 meter/sec RA = 165
42781 deg
ZDOT = 3084
701572 TA = 187
42727
MA = 187
44629
Ha = 188
233 n
mi
Hp = 180
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7951406
66 X = -2449813
24
Y = 14216023
76 feet Y = 4305795
23 meter
Z = -14890466
43 Z = -4550452
09
XDOT = -23009
177274 XDOT = -7019
905158
YDOT = -2275
610541 feet/sec YDOT = -772
068974 meter/sec
ZDOT = 10120
411983 ZDOT = 3050
614643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14585822
87 X = -4445758
81
Y = -7158796
83 feet Y = -2182001
27 meter
Z = -14934911
75 Z = -4552161
10
XDOT = 616
507014 XDOT = 187
911338
YDOT = -22086
169583 feet/sec YDOT = -6731
864489 meter/sec
ZDOT = 9990
725367 ZDOT = 3045
173092
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 07295
68510508
00020000 00000-0 20000-3 0 9106
2 25544 51
6332 166
3833 0002661 123
2442 236
8977 15
75773157 30895
Satellite: ISS
Catalog Number: 25544
Epoch time: 07295
68510508 = yrday
fracday
Element set: 910
Inclination: 51
6332 deg
RA of node: 166
3833 deg
Eccentricity:
0002661
Arg of perigee: 123
2442 deg
Mean anomaly: 236
8977 deg
Mean motion: 15
75773157 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3089
Checksum: 303
Coasting Arc #12 (Orbit 3104)
---------------------------------------
Vector Time (GMT): 2007/296/16:11:23
120
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5876552
51 A = 6722619
44 meter
Y = 590799
72 meter E =
0007036
Z = -3214159
80 I = 51
74699
XDOT = -3135
482650 Wp = 109
01111
YDOT = 5138
596778 meter/sec RA = 160
33293 deg
ZDOT = -4798
920372 TA = 108
48465
MA = 108
40818
Ha = 188
198 n
mi
Hp = 180
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19280027
93 X = 5885123
49
Y = 1938319
29 feet Y = 656562
37 meter
Z = -10545143
71 Z = -3185590
11
XDOT = -10287
016568 XDOT = -3169
397375
YDOT = 16858
913313 feet/sec YDOT = 5103
344098 meter/sec
ZDOT = -15744
489409 ZDOT = -4814
235591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -650892
17 X = -198391
93
Y = 19425077
59 feet Y = 5920763
65 meter
Z = -10436441
65 Z = -3181027
42
XDOT = -16082
030196 XDOT = -4901
802804
YDOT = -9009
641931 feet/sec YDOT = -2746
138860 meter/sec
ZDOT = -15802
054470 ZDOT = -4816
466202
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 07296
69978663
00020000 00000-0 20000-3 0 9119
2 25544 51
6333 161
1582 0002608 124
0198 236
1214 15
75810705 31055
Satellite: ISS
Catalog Number: 25544
Epoch time: 07296
69978663 = yrday
fracday
Element set: 911
Inclination: 51
6333 deg
RA of node: 161
1582 deg
Eccentricity:
0002608
Arg of perigee: 124
0198 deg
Mean anomaly: 236
1214 deg
Mean motion: 15
75810705 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3105
Checksum: 286
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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