Date:
December 4th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8180 57 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 3749)
---------------------------------------
Vector Time (GMT): 2007/337/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4199807
50 A = 6712331
10 meter
Y = 1304948
93 meter E =
0003865
Z = 5069131
87 I = 51
37266
XDOT = -3871
832251 Wp = 134
07505
YDOT = 6485
367622 meter/sec RA = 310
18292 deg
ZDOT = 1534
931364 TA = 301
13747
MA = 301
17537
Ha = 184
984 n
mi
Hp = 179
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13778896
00 X = 4160277
92
Y = 4281328
51 feet Y = 1351692
21 meter
Z = 16631010
08 Z = 5089438
91
XDOT = -12702
861717 XDOT = -3951
521384
YDOT = 21277
452829 feet/sec YDOT = 6441
624934 meter/sec
ZDOT = 5035
864054 ZDOT = 1515
928570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5170136
53 X = -1575857
61
Y = 13374396
14 feet Y = 4076515
94 meter
Z = 16708484
70 Z = 5092746
14
XDOT = -19420
846923 XDOT = -5919
474142
YDOT = -13722
920935 feet/sec YDOT = -4182
746301 meter/sec
ZDOT = 4964
137260 ZDOT = 1513
069037
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 07337
59176302
00020000 00000-0 20000-3 0 9002
2 25544 51
6378 310
4881 0001085 273
7372 86
3668 15
76995862 37502
Satellite: ISS
Catalog Number: 25544
Epoch time: 07337
59176302 = yrday
fracday
Element set: 900
Inclination: 51
6378 deg
RA of node: 310
4881 deg
Eccentricity:
0001085
Arg of perigee: 273
7372 deg
Mean anomaly: 86
3668 deg
Mean motion: 15
76995862 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3750
Checksum: 316
Coasting Arc #2 (Orbit 3764)
---------------------------------------
Vector Time (GMT): 2007/338/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3616795
75 A = 6723546
93 meter
Y = -5650689
97 meter E =
0011037
Z = -347105
29 I = 51
39265
XDOT = 4219
757255 Wp = 38
27923
YDOT = 2338
572531 meter/sec RA = 304
98946 deg
ZDOT = 6008
851276 TA = 317
92970
MA = 318
01439
Ha = 185
119 n
mi
Hp = 179
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11866127
80 X = 3681400
02
Y = -18539009
08 feet Y = -5609883
66 meter
Z = -1138796
88 Z = -329378
06
XDOT = 13844
347950 XDOT = 4164
102901
YDOT = 7672
482056 feet/sec YDOT = 2385
448618 meter/sec
ZDOT = 19714
078991 ZDOT = 6029
216231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17942023
10 X = 5468728
64
Y = 12756631
99 feet Y = 3888221
43 meter
Z = -1071845
36 Z = -326698
46
XDOT = -7398
585577 XDOT = -2255
088884
YDOT = 12036
694468 feet/sec YDOT = 3668
784474 meter/sec
ZDOT = 19791
877868 ZDOT = 6032
564374
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 07338
54229552
00020000 00000-0 20000-3 0 9015
2 25544 51
6375 305
5844 0000960 275
2370 84
8685 15
77019881 37656
Satellite: ISS
Catalog Number: 25544
Epoch time: 07338
54229552 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 305
5844 deg
Eccentricity:
0000960
Arg of perigee: 275
2370 deg
Mean anomaly: 84
8685 deg
Mean motion: 15
77019881 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3765
Checksum: 313
Coasting Arc #3 (Orbit 3780)
---------------------------------------
Vector Time (GMT): 2007/339/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3177721
96 A = 6711661
00 meter
Y = -2827913
71 meter E =
0013697
Z = -5203344
13 I = 51
33783
XDOT = 4335
811486 Wp = 95
45911
YDOT = -6310
009706 meter/sec RA = 299
80721 deg
ZDOT = 781
930519 TA = 182
01466
MA = 182
02019
Ha = 185
059 n
mi
Hp = 179
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10425596
98 X = -3120586
18
Y = -9277932
10 feet Y = -2863128
86 meter
Z = -17071339
02 Z = -5218643
31
XDOT = 14225
103300 XDOT = 4402
250165
YDOT = -20702
131581 feet/sec YDOT = -6261
152798 meter/sec
ZDOT = 2565
388841 ZDOT = 803
155147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9596292
51 X = 2924949
96
Y = -10034024
05 feet Y = -3058370
53 meter
Z = -17129893
28 Z = -5221191
47
XDOT = 19516
083704 XDOT = 5948
502313
YDOT = 14150
864016 feet/sec YDOT = 4313
183352 meter/sec
ZDOT = 2645
596374 ZDOT = 806
377775
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 07339
55617320
00020000 00000-0 20000-3 0 9022
2 25544 51
6383 300
3535 0001052 283
6070 76
4978 15
77041844 37812
Satellite: ISS
Catalog Number: 25544
Epoch time: 07339
55617320 = yrday
fracday
Element set: 902
Inclination: 51
6383 deg
RA of node: 300
3535 deg
Eccentricity:
0001052
Arg of perigee: 283
6070 deg
Mean anomaly: 76
4978 deg
Mean motion: 15
77041844 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3781
Checksum: 286
Coasting Arc #4 (Orbit 3796)
---------------------------------------
Vector Time (GMT): 2007/340/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3885771
09 A = 6722105
08 meter
Y = 5211937
08 meter E =
0006805
Z = -1698584
66 I = 51
36100
XDOT = -3099
127226 Wp = 147
02689
YDOT = -4161
106195 meter/sec RA = 294
65045 deg
ZDOT = -5694
515069 TA = 51
85622
MA = 51
79492
Ha = 184
979 n
mi
Hp = 179
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12748592
83 X = -3935511
36
Y = 17099531
10 feet Y = 5168206
26 meter
Z = -5572784
32 Z = -1717582
40
XDOT = -10167
740243 XDOT = -3024
703231
YDOT = -13651
923211 feet/sec YDOT = -4195
345637 meter/sec
ZDOT = -18682
792220 ZDOT = -5709
390646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16918990
95 X = -5156908
44
Y = -12956175
47 feet Y = -3949042
28 meter
Z = -5644623
14 Z = -1720481
13
XDOT = 12847
303131 XDOT = 3915
857994
YDOT = -8635
417387 feet/sec YDOT = -2632
075220 meter/sec
ZDOT = -18739
867338 ZDOT = -5711
911565
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 07340
57002699
00020000 00000-0 20000-3 0 9034
2 25544 51
6390 295
1230 0001043 288
6698 71
4353 15
77089929 37979
Satellite: ISS
Catalog Number: 25544
Epoch time: 07340
57002699 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 295
1230 deg
Eccentricity:
0001043
Arg of perigee: 288
6698 deg
Mean anomaly: 71
4353 deg
Mean motion: 15
77089929 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3797
Checksum: 315
Coasting Arc #5 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2007/341/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2286856
79 A = 6714322
02 meter
Y = 4399975
94 meter E =
0007956
Z = 4522877
22 I = 51
32426
XDOT = -4505
051230 Wp = 60
59635
YDOT = 5468
919349 meter/sec RA = 289
43126 deg
ZDOT = -3034
611003 TA = 59
72715
MA = 59
64843
Ha = 184
907 n
mi
Hp = 179
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7502810
99 X = 2215513
83
Y = 14435616
59 feet Y = 4425149
38 meter
Z = 14838836
04 Z = 4533814
29
XDOT = -14780
351805 XDOT = -4551
128779
YDOT = 17942
648783 feet/sec YDOT = 5418
284076 meter/sec
ZDOT = -9956
072844 ZDOT = -3056
608232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14412267
07 X = -4392859
00
Y = 7464220
53 feet Y = 2275094
42 meter
Z = 14880934
91 Z = 4535708
96
XDOT = -17444
460972 XDOT = -5317
071704
YDOT = -13616
606208 feet/sec YDOT = -4150
341572 meter/sec
ZDOT = -10039
315395 ZDOT = -3059
983332
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 07341
58385712
00020000 00000-0 20000-3 0 9047
2 25544 51
6392 289
8928 0001019 291
0457 69
0599 15
77120801 38138
Satellite: ISS
Catalog Number: 25544
Epoch time: 07341
58385712 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 289
8928 deg
Eccentricity:
0001019
Arg of perigee: 291
0457 deg
Mean anomaly: 69
0599 deg
Mean motion: 15
77120801 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3813
Checksum: 307
Coasting Arc #6 (Orbit 3828)
---------------------------------------
Vector Time (GMT): 2007/342/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3944377
70 A = 6717805
68 meter
Y = -4160571
92 meter E =
0011322
Z = 3491849
11 I = 51
32822
XDOT = 2208
437438 Wp = 90
52282
YDOT = 5868
091147 meter/sec RA = 284
29807 deg
ZDOT = 4484
641654 TA = 311
25665
MA = 311
35413
Ha = 184
844 n
mi
Hp = 179
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12940871
71 X = 3973645
59
Y = -13650170
35 feet Y = -4116300
53 meter
Z = 11456197
88 Z = 3511081
75
XDOT = 7245
529652 XDOT = 2120
869414
YDOT = 19252
267543 feet/sec YDOT = 5892
296863 meter/sec
ZDOT = 14713
391252 ZDOT = 4495
158617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13909223
24 X = 4239531
24
Y = 12595729
39 feet Y = 3839178
32 meter
Z = 11529045
54 Z = 3514053
08
XDOT = -18184
121676 XDOT = -5542
520287
YDOT = 6538
191092 feet/sec YDOT = 1992
840645 meter/sec
ZDOT = 14754
038512 ZDOT = 4497
030939
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 07342
59766292
00020000 00000-0 20000-3 0 9056
2 25544 51
6394 284
6618 0001021 294
1200 65
9858 15
77162118 38299
Satellite: ISS
Catalog Number: 25544
Epoch time: 07342
59766292 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 284
6618 deg
Eccentricity:
0001021
Arg of perigee: 294
1200 deg
Mean anomaly: 65
9858 deg
Mean motion: 15
77162118 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3829
Checksum: 307
Coasting Arc #7 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2007/343/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1614561
48 A = 6718821
76 meter
Y = -5728188
60 meter E =
0003792
Z = -3119513
03 I = 51
32628
XDOT = 4543
192055 Wp = 66
61508
YDOT = -3910
601309 meter/sec RA = 279
06450 deg
ZDOT = 4835
534520 TA = 256
89711
MA = 256
93943
Ha = 184
843 n
mi
Hp = 179
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5297117
72 X = -1535233
74
Y = -18793269
69 feet Y = -5745799
49 meter
Z = -10234622
79 Z = -3127164
93
XDOT = 14905
485745 XDOT = 4563
092807
YDOT = -12830
056789 feet/sec YDOT = -3859
686277 meter/sec
ZDOT = 15864
614567 ZDOT = 4857
653407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18583384
97 X = 5664215
74
Y = -5940956
20 feet Y = -1810803
45 meter
Z = -10264345
47 Z = -3128572
50
XDOT = 12943
870654 XDOT = 3945
291775
YDOT = 12968
599921 feet/sec YDOT = 3952
829256 meter/sec
ZDOT = 15948
487770 ZDOT = 4861
099072
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 07343
54808450
00020000 00000-0 20000-3 0 9066
2 25544 51
6396 279
7578 0001076 298
0564 62
0492 15
77195777 38443
Satellite: ISS
Catalog Number: 25544
Epoch time: 07343
54808450 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 279
7578 deg
Eccentricity:
0001076
Arg of perigee: 298
0564 deg
Mean anomaly: 62
0492 deg
Mean motion: 15
77195777 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3844
Checksum: 331
Coasting Arc #8 (Orbit 3859)
---------------------------------------
Vector Time (GMT): 2007/344/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4003960
81 A = 6712930
63 meter
Y = 2523826
09 meter E =
0011215
Z = -4771067
52 I = 51
30432
XDOT = -1515
351553 Wp = 67
85894
YDOT = -7121
688168 meter/sec RA = 273
92616 deg
ZDOT = -2496
073128 TA = 177
59297
MA = 177
58757
Ha = 184
819 n
mi
Hp = 178
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13136354
36 X = -4008707
78
Y = 8280269
33 feet Y = 2479025
81 meter
Z = -15653108
67 Z = -4790530
09
XDOT = -4971
625830 XDOT = -1423
477520
YDOT = -23365
118661 feet/sec YDOT = -7138
119568 meter/sec
ZDOT = -8189
216299 ZDOT = -2503
212843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8981791
71 X = -2737650
11
Y = -12575180
20 feet Y = -3832914
92 meter
Z = -15727006
63 Z = -4793591
62
XDOT = 22143
624619 XDOT = 6749
376784
YDOT = -5541
454052 feet/sec YDOT = -1689
035195 meter/sec
ZDOT = -8217
132458 ZDOT = -2504
581973
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 07344
56184449
00020000 00000-0 20000-3 0 9075
2 25544 51
6403 274
5268 0001019 305
4454 54
6615 15
77250101 38604
Satellite: ISS
Catalog Number: 25544
Epoch time: 07344
56184449 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 274
5268 deg
Eccentricity:
0001019
Arg of perigee: 305
4454 deg
Mean anomaly: 54
6615 deg
Mean motion: 15
77250101 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3860
Checksum: 281
Coasting Arc #9 (Orbit 3875)
---------------------------------------
Vector Time (GMT): 2007/345/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1054754
48 A = 6722365
02 meter
Y = 6535192
94 meter E =
0012865
Z = 1134297
83 I = 51
33539
XDOT = -4661
482562 Wp = 122
54431
YDOT = 1779
137830 meter/sec RA = 268
71203 deg
ZDOT = -5874
359120 TA = 44
96401
MA = 44
85991
Ha = 184
799 n
mi
Hp = 179
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3460480
59 X = 976088
32
Y = 21440921
73 feet Y = 6546547
77 meter
Z = 3721449
56 Z = 1139231
89
XDOT = -15293
577958 XDOT = -4652
493931
YDOT = 5837
066373 feet/sec YDOT = 1727
061751 meter/sec
ZDOT = -19272
831760 ZDOT = -5896
982627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21138214
82 X = -6442927
88
Y = 4971790
53 feet Y = 1515401
75 meter
Z = 3740910
36 Z = 1140229
48
XDOT = -6550
938162 XDOT = -1996
725952
YDOT = -13184
247512 feet/sec YDOT = -4018
558642 meter/sec
ZDOT = -19358
854388 ZDOT = -5900
578817
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 07345
57558144
00020000 00000-0 20000-3 0 9085
2 25544 51
6402 269
2958 0001011 303
8427 56
2642 15
77255971 38769
Satellite: ISS
Catalog Number: 25544
Epoch time: 07345
57558144 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 269
2958 deg
Eccentricity:
0001011
Arg of perigee: 303
8427 deg
Mean anomaly: 56
2642 deg
Mean motion: 15
77255971 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3876
Checksum: 306
Coasting Arc #10 (Orbit 3891)
---------------------------------------
Vector Time (GMT): 2007/346/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4162404
55 A = 6710584
91 meter
Y = -526225
96 meter E =
0001505
Z = 5236102
81 I = 51
29819
XDOT = 906
420728 Wp = 68
49604
YDOT = 7654
505829 meter/sec RA = 263
54002 deg
ZDOT = 49
254959 TA = 21
03791
MA = 21
03172
Ha = 184
502 n
mi
Hp = 178
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13656182
89 X = 4142543
42
Y = -1726463
12 feet Y = -479791
49 meter
Z = 17178815
01 Z = 5256275
51
XDOT = 2973
821285 XDOT = 820
520241
YDOT = 25113
208099 feet/sec YDOT = 7664
161637 meter/sec
ZDOT = 161
597635 ZDOT = 53
450946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2926763
43 X = 892077
49
Y = 13351437
36 feet Y = 4069518
11 meter
Z = 17255632
92 Z = 5259516
91
XDOT = -23775
202830 XDOT = -7246
681823
YDOT = 4983
478292 feet/sec YDOT = 1518
964183 meter/sec
ZDOT = 178
369087 ZDOT = 54
366898
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 07346
58929277
00020000 00000-0 20000-3 0 9097
2 25544 51
6399 264
0646 0001174 304
7301 55
3753 15
77342930 38925
Satellite: ISS
Catalog Number: 25544
Epoch time: 07346
58929277 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 264
0646 deg
Eccentricity:
0001174
Arg of perigee: 304
7301 deg
Mean anomaly: 55
3753 deg
Mean motion: 15
77342930 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3892
Checksum: 314
Coasting Arc #11 (Orbit 3907)
---------------------------------------
Vector Time (GMT): 2007/347/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -494580
49 A = 6722236
99 meter
Y = -6612338
37 meter E =
0013632
Z = 1061354
13 I = 51
34200
XDOT = 4933
809423 Wp = 51
69748
YDOT = 583
838716 meter/sec RA = 258
36592 deg
ZDOT = 5893
769071 TA = 319
97988
MA = 320
08025
Ha = 184
705 n
mi
Hp = 178
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1622639
39 X = -425759
42
Y = -21694023
53 feet Y = -6617484
41 meter
Z = 3482132
98 Z = 1059117
67
XDOT = 16187
038788 XDOT = 4898
283304
YDOT = 1915
481353 feet/sec YDOT = 638
811882 meter/sec
ZDOT = 19336
512701 ZDOT = 5917
651306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21397124
52 X = 6521843
55
Y = -3935824
69 feet Y = -1199639
37 meter
Z = 3472925
55 Z = 1058547
71
XDOT = -485
024906 XDOT = -147
835591
YDOT = 14629
804911 feet/sec YDOT = 4459
164537 meter/sec
ZDOT = 19427
588945 ZDOT = 5921
529111
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 07347
60298442
00020000 00000-0 20000-3 0 9106
2 25544 51
6400 258
8329 0001166 315
3263 44
7808 15
77330873 39087
Satellite: ISS
Catalog Number: 25544
Epoch time: 07347
60298442 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 258
8329 deg
Eccentricity:
0001166
Arg of perigee: 315
3263 deg
Mean anomaly: 44
7808 deg
Mean motion: 15
77330873 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3908
Checksum: 295
Coasting Arc #12 (Orbit 3922)
---------------------------------------
Vector Time (GMT): 2007/348/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4464480
87 A = 6712472
11 meter
Y = -1515022
97 meter E =
0010862
Z = -4788220
26 I = 51
31690
XDOT = -155
346449 Wp = 104
83347
YDOT = -7294
202669 meter/sec RA = 253
15246 deg
ZDOT = 2454
666466 TA = 189
26723
MA = 189
28729
Ha = 184
610 n
mi
Hp = 178
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14647246
96 X = -4423947
58
Y = -4970547
81 feet Y = -1564720
11 meter
Z = -15709384
04 Z = -4809810
40
XDOT = -509
666828 XDOT = -85
694327
YDOT = -23931
111118 feet/sec YDOT = -7295
550698 meter/sec
ZDOT = 8053
367670 ZDOT = 2454
080081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3138509
42 X = 956617
67
Y = -15059906
64 feet Y = -4590259
54 meter
Z = -15791830
38 Z = -4813349
90
XDOT = 22582
083950 XDOT = 6883
019188
YDOT = -3729
004202 feet/sec YDOT = -1136
600481 meter/sec
ZDOT = 8050
367371 ZDOT = 2453
751975
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 07348
55329704
00020000 00000-0 20000-3 0 9118
2 25544 51
6401 253
9282 0001215 314
7063 45
4003 15
77380849 39238
Satellite: ISS
Catalog Number: 25544
Epoch time: 07348
55329704 = yrday
fracday
Element set: 911
Inclination: 51
6401 deg
RA of node: 253
9282 deg
Eccentricity:
0001215
Arg of perigee: 314
7063 deg
Mean anomaly: 45
4003 deg
Mean motion: 15
77380849 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3923
Checksum: 278
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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