Date:
November 13th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4843 76 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 3339)
---------------------------------------
Vector Time (GMT): 2007/311/14:08:18
812
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4126208
86 A = 6715934
35 meter
Y = 1831153
64 meter E =
0014289
Z = -4985354
73 I = 51
94485
XDOT = -802
617878 Wp = 113
45918
YDOT = 7373
232673 meter/sec RA = 83
75979 deg
ZDOT = 2042
967649 TA = 176
25596
MA = 176
24526
Ha = 187
513 n
mi
Hp = 180
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13537430
63 X = 4129644
62
Y = 6007721
91 feet Y = 1877314
46 meter
Z = -16356150
69 Z = -4965300
66
XDOT = -2633
260755 XDOT = -894
931490
YDOT = 24190
395909 feet/sec YDOT = 7363
741190 meter/sec
ZDOT = 6702
649767 ZDOT = 2038
844192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8765657
32 X = -2671772
35
Y = 12042248
11 feet Y = 3670477
22 meter
Z = -16279616
95 Z = -4962027
25
XDOT = -22192
911402 XDOT = -6764
399395
YDOT = -7109
027982 feet/sec YDOT = -2166
831729 meter/sec
ZDOT = 6687
794975 ZDOT = 2038
439908
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 07311
60150001
00020000 00000-0 20000-3 0 9004
2 25544 51
6396 84
4258 0002429 164
2874 195
8366 15
75947747 33406
Satellite: ISS
Catalog Number: 25544
Epoch time: 07311
60150001 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 84
4258 deg
Eccentricity:
0002429
Arg of perigee: 164
2874 deg
Mean anomaly: 195
8366 deg
Mean motion: 15
75947747 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3340
Checksum: 292
Coasting Arc #2 (Orbit 3355)
---------------------------------------
Vector Time (GMT): 2007/312/14:08:18
812
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 665334
13 A = 6724126
59 meter
Y = -6242599
82 meter E =
0007619
Z = -2402086
47 I = 51
96824
XDOT = 4833
320145 Wp = 143
81508
YDOT = 2590
504622 meter/sec RA = 78
66929 deg
ZDOT = -5408
171224 TA = 63
16554
MA = 63
08766
Ha = 187
457 n
mi
Hp = 180
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2182854
75 X = 746759
65
Y = -20480970
53 feet Y = -6234704
35 meter
Z = -7880861
14 Z = -2398656
51
XDOT = 15857
349557 XDOT = 4830
266277
YDOT = 8499
030912 feet/sec YDOT = 2644
536577 meter/sec
ZDOT = -17743
343910 ZDOT = -5384
697558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19649897
57 X = 5989288
78
Y = 6189597
88 feet Y = 1886589
43 meter
Z = -7868505
86 Z = -2398320
59
XDOT = -11004
288338 XDOT = -3354
107086
YDOT = 12553
888696 feet/sec YDOT = 3826
425275 meter/sec
ZDOT = -17653
711749 ZDOT = -5380
851341
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 07312
61608378
00020000 00000-0 20000-3 0 9012
2 25544 51
6398 79
2003 0002379 169
2901 190
8314 15
75949229 33560
Satellite: ISS
Catalog Number: 25544
Epoch time: 07312
61608378 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 79
2003 deg
Eccentricity:
0002379
Arg of perigee: 169
2901 deg
Mean anomaly: 190
8314 deg
Mean motion: 15
75949229 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3356
Checksum: 304
Coasting Arc #3 (Orbit 3371)
---------------------------------------
Vector Time (GMT): 2007/313/14:08:18
812
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4353744
96 A = 6718263
41 meter
Y = -2646857
44 meter E =
0009413
Z = 4371465
60 I = 51
94239
XDOT = 747
646383 Wp = 83
47855
YDOT = -6872
611601 meter/sec RA = 73
49604 deg
ZDOT = -3409
382235 TA = 40
73278
MA = 40
66243
Ha = 187
444 n
mi
Hp = 180
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14283940
15 X = -4345060
32
Y = -8683915
49 feet Y = -2695495
10 meter
Z = 14342078
72 Z = 4350335
38
XDOT = 2452
908081 XDOT = 841
004117
YDOT = -22547
938323 feet/sec YDOT = -6863
728871 meter/sec
ZDOT = -11185
637254 ZDOT = -3405
523545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11110712
42 X = 3386545
15
Y = -12581819
08 feet Y = -3834938
46 meter
Z = 14261362
30 Z = 4346863
23
XDOT = 20818
104902 XDOT = 6345
358374
YDOT = 5693
795076 feet/sec YDOT = 1735
468739 meter/sec
ZDOT = -11171
707533 ZDOT = -3405
136456
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 07313
63064702
00020000 00000-0 20000-3 0 9023
2 25544 51
6403 73
9749 0002180 170
3008 189
8199 15
75992923 33722
Satellite: ISS
Catalog Number: 25544
Epoch time: 07313
63064702 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 73
9749 deg
Eccentricity:
0002180
Arg of perigee: 170
3008 deg
Mean anomaly: 189
8199 deg
Mean motion: 15
75992923 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3372
Checksum: 297
Coasting Arc #4 (Orbit 3387)
---------------------------------------
Vector Time (GMT): 2007/314/14:08:18
812
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -696903
13 A = 6721070
48 meter
Y = 5689657
33 meter E =
0012728
Z = 3501130
78 I = 51
94303
XDOT = -5186
363744 Wp = 101
79105
YDOT = -3441
049370 meter/sec RA = 68
41676 deg
ZDOT = 4543
328660 TA = 299
66056
MA = 299
78724
Ha = 187
210 n
mi
Hp = 180
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2286427
60 X = -777482
37
Y = 18666854
77 feet Y = 5681413
42 meter
Z = 11486649
53 Z = 3497549
72
XDOT = -17015
629083 XDOT = -5169
571346
YDOT = -11289
532053 feet/sec YDOT = -3498
952607 meter/sec
ZDOT = 14905
933924 ZDOT = 4518
173051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18040900
37 X = -5498866
43
Y = -5338908
61 feet Y = -1627299
35 meter
Z = 11473635
17 Z = 3497164
00
XDOT = 13516
910944 XDOT = 4119
954456
YDOT = -13732
967599 feet/sec YDOT = -4185
808524 meter/sec
ZDOT = 14809
811336 ZDOT = 4514
030495
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 07314
64518904
00020000 00000-0 20000-3 0 9034
2 25544 51
6405 68
7493 0002175 176
1131 184
0050 15
76033305 33888
Satellite: ISS
Catalog Number: 25544
Epoch time: 07314
64518904 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 68
7493 deg
Eccentricity:
0002175
Arg of perigee: 176
1131 deg
Mean anomaly: 184
0050 deg
Mean motion: 15
76033305 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3388
Checksum: 274
Coasting Arc #5 (Orbit 3402)
---------------------------------------
Vector Time (GMT): 2007/315/14:08:18
812
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4714073
42 A = 6721163
60 meter
Y = 3307457
97 meter E =
0005548
Z = -3472433
91 I = 51
93134
XDOT = -926
519114 Wp = 114
25494
YDOT = 6120
150324 meter/sec RA = 63
23626 deg
ZDOT = 4575
030680 TA = 204
75620
MA = 204
78284
Ha = 187
104 n
mi
Hp = 180
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15466120
16 X = 4693607
55
Y = 10851240
06 feet Y = 3360059
25 meter
Z = -11392499
69 Z = -3449581
67
XDOT = -3039
760874 XDOT = -1017
112062
YDOT = 20079
233348 feet/sec YDOT = 6109
282571 meter/sec
ZDOT = 15009
943176 ZDOT = 4570
309936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12984524
67 X = -3957683
12
Y = 13796187
95 feet Y = 4205078
09 meter
Z = -11305160
34 Z = -3445812
87
XDOT = -18409
645846 XDOT = -5611
260054
YDOT = -5050
377552 feet/sec YDOT = -1539
355078 meter/sec
ZDOT = 14992
626038 ZDOT = 4569
752416
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 07315
59630525
00020000 00000-0 20000-3 0 9044
2 25544 51
6403 63
8513 0002047 179
2077 180
9091 15
76053996 34032
Satellite: ISS
Catalog Number: 25544
Epoch time: 07315
59630525 = yrday
fracday
Element set: 904
Inclination: 51
6403 deg
RA of node: 63
8513 deg
Eccentricity:
0002047
Arg of perigee: 179
2077 deg
Mean anomaly: 180
9091 deg
Mean motion: 15
76053996 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3403
Checksum: 288
Coasting Arc #6 (Orbit 3418)
---------------------------------------
Vector Time (GMT): 2007/316/14:08:18
812
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1000913
45 A = 6717822
56 meter
Y = -4962306
10 meter E =
0008839
Z = -4424442
51 I = 51
90552
XDOT = 5608
462966 Wp = 80
81418
YDOT = 4091
029006 meter/sec RA = 58
15445 deg
ZDOT = -3323
814337 TA = 155
92639
MA = 155
88505
Ha = 187
048 n
mi
Hp = 180
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3283836
77 X = 1077822
05
Y = -16280531
82 feet Y = -4950682
88 meter
Z = -14515887
51 Z = -4419393
59
XDOT = 18400
469050 XDOT = 5578
446565
YDOT = 13422
011173 feet/sec YDOT = 4153
578496 meter/sec
ZDOT = -10904
902680 ZDOT = -3296
640185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15717551
65 X = 4790709
74
Y = 5416674
29 feet Y = 1651002
33 meter
Z = -14497189
39 Z = -4418743
33
XDOT = -15274
321745 XDOT = -4655
613268
YDOT = 15450
694954 feet/sec YDOT = 4709
371822 meter/sec
ZDOT = -10801
028535 ZDOT = -3292
153497
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 07316
61080917
00020000 00000-0 20000-3 0 9053
2 25544 51
6398 58
6254 0001960 182
6697 177
4457 15
76059073 34194
Satellite: ISS
Catalog Number: 25544
Epoch time: 07316
61080917 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 58
6254 deg
Eccentricity:
0001960
Arg of perigee: 182
6697 deg
Mean anomaly: 177
4457 deg
Mean motion: 15
76059073 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3419
Checksum: 319
Coasting Arc #7 (Orbit 3434)
---------------------------------------
Vector Time (GMT): 2007/317/14:08:18
812
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5074278
65 A = 6723926
93 meter
Y = -3766121
03 meter E =
0014520
Z = 2275707
57 I = 51
91073
XDOT = 1423
145053 Wp = 114
35027
YDOT = -5237
535986 meter/sec RA = 52
97829 deg
ZDOT = -5473
174453 TA = 40
15041
MA = 40
04322
Ha = 186
937 n
mi
Hp = 180
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16647895
83 X = -5042843
42
Y = -12356040
12 feet Y = -3822688
96 meter
Z = 7466232
18 Z = 2251132
10
XDOT = 4669
111067 XDOT = 1508
194529
YDOT = -17183
517015 feet/sec YDOT = -5221
145476 meter/sec
ZDOT = -17956
609097 ZDOT = -5466
054593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14126096
20 X = 4305634
12
Y = -15220763
16 feet Y = -4639288
61 meter
Z = 7372283
30 Z = 2247071
95
XDOT = 15440
574806 XDOT = 4706
287201
YDOT = 5611
315729 feet/sec YDOT = 1710
329034 meter/sec
ZDOT = -17930
048732 ZDOT = -5465
078854
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 07317
62529185
00020000 00000-0 20000-3 0 9061
2 25544 51
6403 53
3996 0001692 184
7176 175
3973 15
76129786 34350
Satellite: ISS
Catalog Number: 25544
Epoch time: 07317
62529185 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 53
3996 deg
Eccentricity:
0001692
Arg of perigee: 184
7176 deg
Mean anomaly: 175
3973 deg
Mean motion: 15
76129786 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3435
Checksum: 323
Coasting Arc #8 (Orbit 3450)
---------------------------------------
Vector Time (GMT): 2007/318/14:08:18
812
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1551941
36 A = 6715062
86 meter
Y = 4169351
83 meter E =
0006406
Z = 5027632
74 I = 51
86248
XDOT = -5999
144255 Wp = 138
81761
YDOT = -4469
988136 meter/sec RA = 47
87936 deg
ZDOT = 1849
025339 TA = 293
38747
MA = 293
45484
Ha = 186
844 n
mi
Hp = 180
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5091671
14 X = -1622872
16
Y = 13678975
82 feet Y = 4151600
04 meter
Z = 16494858
06 Z = 5019921
39
XDOT = -19682
231807 XDOT = -5957
696709
YDOT = -14665
315406 feet/sec YDOT = -4536
842407 meter/sec
ZDOT = 6066
356100 ZDOT = 1819
981134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13134359
52 X = -4003352
78
Y = -6440620
26 feet Y = -1963101
05 meter
Z = 16465929
90 Z = 5018815
43
XDOT = 15974
615308 XDOT = 4869
062746
YDOT = -17300
991631 feet/sec YDOT = -5273
342249 meter/sec
ZDOT = 5955
318871 ZDOT = 1815
181192
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 07318
63975445
00020000 00000-0 20000-3 0 9078
2 25544 51
6401 48
1734 0001719 189
5790 170
5341 15
76152642 34516
Satellite: ISS
Catalog Number: 25544
Epoch time: 07318
63975445 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 48
1734 deg
Eccentricity:
0001719
Arg of perigee: 189
5790 deg
Mean anomaly: 170
5341 deg
Mean motion: 15
76152642 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3451
Checksum: 296
Coasting Arc #9 (Orbit 3465)
---------------------------------------
Vector Time (GMT): 2007/319/14:08:18
812
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5348078
61 A = 6725787
55 meter
Y = 3970283
61 meter E =
0008971
Z = -906470
84 I = 51
87742
XDOT = -2212
567875 Wp = 42
64046
YDOT = 4334
278021 meter/sec RA = 42
71998 deg
ZDOT = 5970
588110 TA = 307
48956
MA = 307
57110
Ha = 186
817 n
mi
Hp = 180
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17546189
65 X = 5307688
36
Y = 13025864
88 feet Y = 4029863
11 meter
Z = -2973985
69 Z = -880587
19
XDOT = -7259
080956 XDOT = -2289
874496
YDOT = 14220
072246 feet/sec YDOT = 4309
103038 meter/sec
ZDOT = 19588
543669 ZDOT = 5959
651898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14328687
89 X = -4367384
07
Y = 16516943
62 feet Y = 5034364
41 meter
Z = -2875029
54 Z = -876309
00
XDOT = -12411
478212 XDOT = -3783
018559
YDOT = -7388
625247 feet/sec YDOT = -2252
052975 meter/sec
ZDOT = 19547
350865 ZDOT = 5958
032544
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 07319
59079593
00020000 00000-0 20000-3 0 9084
2 25544 51
6396 43
2737 0001407 191
5247 168
5885 15
76128040 34663
Satellite: ISS
Catalog Number: 25544
Epoch time: 07319
59079593 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 43
2737 deg
Eccentricity:
0001407
Arg of perigee: 191
5247 deg
Mean anomaly: 168
5885 deg
Mean motion: 15
76128040 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3466
Checksum: 319
Coasting Arc #10 (Orbit 3481)
---------------------------------------
Vector Time (GMT): 2007/320/14:08:18
812
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2377373
92 A = 6713909
30 meter
Y = -3413124
77 meter E =
0014766
Z = -5282782
25 I = 51
81598
XDOT = 6179
747348 Wp = 94
10879
YDOT = 4579
712955 meter/sec RA = 37
59213 deg
ZDOT = -179
316804 TA = 174
20065
MA = 174
18353
Ha = 186
710 n
mi
Hp = 180
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7799783
22 X = 2441026
47
Y = -11197915
92 feet Y = -3386183
33 meter
Z = -17331962
77 Z = -5271078
45
XDOT = 20274
761642 XDOT = 6128
948112
YDOT = 15025
304971 feet/sec YDOT = 4648
534371 meter/sec
ZDOT = -588
309723 ZDOT = -149
418202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10710861
64 X = 3264670
63
Y = 8546226
78 feet Y = 2604889
92 meter
Z = -17287750
68 Z = -5269306
41
XDOT = -15575
872124 XDOT = -4747
525823
YDOT = 18571
915752 feet/sec YDOT = 5660
719921 meter/sec
ZDOT = -474
001145 ZDOT = -144
475549
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
60522033
00020000 00000-0 20000-3 0 9091
2 25544 51
6399 38
0467 0001478 193
2867 166
8259 15
76177886 34829
Satellite: ISS
Catalog Number: 25544
Epoch time: 07320
60522033 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 38
0467 deg
Eccentricity:
0001478
Arg of perigee: 193
2867 deg
Mean anomaly: 166
8259 deg
Mean motion: 15
76177886 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3482
Checksum: 322
Coasting Arc #11 (Orbit 3497)
---------------------------------------
Vector Time (GMT): 2007/321/14:08:18
812
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5377730
57 A = 6725633
10 meter
Y = -3983706
64 meter E =
0011688
Z = -604762
14 I = 51
83288
XDOT = 3277
927533 Wp = 144
48792
YDOT = -3521
476748 meter/sec RA = 32
45737 deg
ZDOT = -6018
576827 TA = 42
08510
MA = 41
99539
Ha = 186
603 n
mi
Hp = 180
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17643473
01 X = -5329846
61
Y = -13069903
69 feet Y = -4043575
71 meter
Z = -1984127
77 Z = -630771
44
XDOT = 10754
355423 XDOT = 3346
299159
YDOT = -11553
401404 feet/sec YDOT = -3484
438472 meter/sec
ZDOT = -19745
986965 ZDOT = -6002
486559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13798968
14 X = 4205925
49
Y = -17067469
21 feet Y = -5202164
61 meter
Z = -2083568
65 Z = -635071
72
XDOT = 9842
196762 XDOT = 2999
901573
YDOT = 10334
933348 feet/sec YDOT = 3150
087684 meter/sec
ZDOT = -19685
083208 ZDOT = -6000
013362
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
61962421
00020000 00000-0 20000-3 0 9104
2 25544 51
6404 32
8199 0001309 191
8670 168
2464 15
76241138 34982
Satellite: ISS
Catalog Number: 25544
Epoch time: 07321
61962421 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 32
8199 deg
Eccentricity:
0001309
Arg of perigee: 191
8670 deg
Mean anomaly: 168
2464 deg
Mean motion: 15
76241138 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3498
Checksum: 288
Coasting Arc #12 (Orbit 3513)
---------------------------------------
Vector Time (GMT): 2007/322/14:08:18
812
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3364909
14 A = 6714431
28 meter
Y = 2782819
89 meter E =
0003987
Z = 5097953
11 I = 51
76944
XDOT = -6064
357637 Wp = 65
34826
YDOT = -4498
849235 meter/sec RA = 27
29739 deg
ZDOT = -1544
428716 TA = 39
44570
MA = 39
41668
Ha = 186
628 n
mi
Hp = 180
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11039728
14 X = -3420542
29
Y = 9129986
53 feet Y = 2744880
31 meter
Z = 16725567
95 Z = 5081471
10
XDOT = -19896
186473 XDOT = -6006
097432
YDOT = -14760
004052 feet/sec YDOT = -4566
338508 meter/sec
ZDOT = -5067
023347 ZDOT = -1573
748491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8850897
18 X = -2697753
46
Y = -11356922
94 feet Y = -3461590
11 meter
Z = 16663096
80 Z = 5078911
91
XDOT = 14420
216356 XDOT = 4395
281945
YDOT = -18849
566310 feet/sec YDOT = -5745
347811 meter/sec
ZDOT = -5179
122013 ZDOT = -1578
596390
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
63400809
00020000 00000-0 20000-3 0 9115
2 25544 51
6396 27
5933 0001257 195
7796 164
3329 15
76279581 35142
Satellite: ISS
Catalog Number: 25544
Epoch time: 07322
63400809 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 27
5933 deg
Eccentricity:
0001257
Arg of perigee: 195
7796 deg
Mean anomaly: 164
3329 deg
Mean motion: 15
76279581 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3514
Checksum: 309
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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