Date:
October 16th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4574 66 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 2976)
---------------------------------------
Vector Time (GMT): 2007/288/12:57:44
867
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4711972
13 A = 6718854
74 meter
Y = -1862051
26 meter E =
0011642
Z = 4405000
93 I = 51
50628
XDOT = 5000
907183 Wp = 74
08116
YDOT = 4859
788873 meter/sec RA = 202
17986 deg
ZDOT = -3284
801661 TA = 48
95750
MA = 48
85694
Ha = 188
397 n
mi
Hp = 180
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15459226
15 X = 4711044
39
Y = -6109092
06 feet Y = -1809364
53 meter
Z = 14452102
78 Z = 4427890
03
XDOT = 16407
175796 XDOT = 4962
150010
YDOT = 15944
189217 feet/sec YDOT = 4915
495161 meter/sec
ZDOT = -10776
908336 ZDOT = -3260
600727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8511196
43 X = -2594212
67
Y = 14189927
26 feet Y = 4325089
83 meter
Z = 14538825
72 Z = 4431434
08
XDOT = -21730
431092 XDOT = -6623
435397
YDOT = -2052
546914 feet/sec YDOT = -625
616299 meter/sec
ZDOT = -10684
338936 ZDOT = -3256
586508
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
58195589
00020000 00000-0 20000-3 0 9004
2 25544 51
6369 202
9651 0002664 92
1784 267
9685 15
75671407 29777
Satellite: ISS
Catalog Number: 25544
Epoch time: 07288
58195589 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 202
9651 deg
Eccentricity:
0002664
Arg of perigee: 92
1784 deg
Mean anomaly: 267
9685 deg
Mean motion: 15
75671407 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2977
Checksum: 343
Coasting Arc #2 (Orbit 2992)
---------------------------------------
Vector Time (GMT): 2007/289/12:57:44
867
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4208427
90 A = 6722685
09 meter
Y = -4048429
36 meter E =
0015395
Z = 3317571
54 I = 51
54658
XDOT = 5745
213067 Wp = 90
15445
YDOT = -2122
576048 meter/sec RA = 197
07249 deg
ZDOT = 4679
116208 TA = 308
95279
MA = 309
08988
Ha = 188
544 n
mi
Hp = 180
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13807178
15 X = -4178961
52
Y = -13282248
54 feet Y = -4095325
68 meter
Z = 10884421
06 Z = 3297198
01
XDOT = 18849
124236 XDOT = 5745
790188
YDOT = -6963
832177 feet/sec YDOT = -2058
326681 meter/sec
ZDOT = 15351
431128 ZDOT = 4707
028483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19117542
59 X = 5827026
98
Y = 1807278
08 feet Y = 550858
36 meter
Z = 10806490
09 Z = 3293818
18
XDOT = -10257
543452 XDOT = -3126
499244
YDOT = 15711
104252 feet/sec YDOT = 4788
744576 meter/sec
ZDOT = 15457
217079 ZDOT = 4711
359766
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
59670986
00020000 00000-0 20000-3 0 9016
2 25544 51
6372 197
7402 0002668 95
9600 264
1868 15
75677226 29933
Satellite: ISS
Catalog Number: 25544
Epoch time: 07289
59670986 = yrday
fracday
Element set: 901
Inclination: 51
6372 deg
RA of node: 197
7402 deg
Eccentricity:
0002668
Arg of perigee: 95
9600 deg
Mean anomaly: 264
1868 deg
Mean motion: 15
75677226 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2993
Checksum: 341
Coasting Arc #3 (Orbit 3007)
---------------------------------------
Vector Time (GMT): 2007/290/12:57:44
867
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5297844
18 A = 6721267
62 meter
Y = 1880570
50 meter E =
0008425
Z = -3692587
17 I = 51
57067
XDOT = -4573
463280 Wp = 101
98525
YDOT = -4449
103953 meter/sec RA = 191
86649 deg
ZDOT = 4302
333370 TA = 213
52214
MA = 213
57548
Ha = 188
347 n
mi
Hp = 180
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17381378
53 X = -5300540
96
Y = 6169850
72 feet Y = 1821312
01 meter
Z = -12114787
30 Z = -3718331
13
XDOT = -15004
800788 XDOT = -4544
273203
YDOT = -14596
797747 feet/sec YDOT = -4500
083896 meter/sec
ZDOT = 14115
266963 ZDOT = 4280
185834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9476083
88 X = 2888310
37
Y = -15748305
79 feet Y = -4800083
61 meter
Z = -12212376
84 Z = -3722332
46
XDOT = 19771
073770 XDOT = 6026
223285
YDOT = 1032
845909 feet/sec YDOT = 314
811433 meter/sec
ZDOT = 14030
534764 ZDOT = 4276
506996
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
54802385
00020000 00000-0 20000-3 0 9024
2 25544 51
6373 192
8421 0002508 99
2589 260
8858 15
75714901 30089
Satellite: ISS
Catalog Number: 25544
Epoch time: 07290
54802385 = yrday
fracday
Element set: 902
Inclination: 51
6373 deg
RA of node: 192
8421 deg
Eccentricity:
0002508
Arg of perigee: 99
2589 deg
Mean anomaly: 260
8858 deg
Mean motion: 15
75714901 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3008
Checksum: 305
Coasting Arc #4 (Orbit 3023)
---------------------------------------
Vector Time (GMT): 2007/291/12:57:44
867
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3713104
93 A = 6719774
03 meter
Y = 3761144
78 meter E =
0009912
Z = -4159622
16 I = 51
59413
XDOT = -6374
717328 Wp = 78
14495
YDOT = 2201
651473 meter/sec RA = 186
76493 deg
ZDOT = -3705
095506 TA = 153
96834
MA = 153
91846
Ha = 188
281 n
mi
Hp = 180
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12182102
78 X = 3690978
31
Y = 12339713
85 feet Y = 3802543
19 meter
Z = -13647054
34 Z = -4141637
27
XDOT = -20914
426930 XDOT = -6380
863754
YDOT = 7223
265989 feet/sec YDOT = 2130
331484 meter/sec
ZDOT = -12155
825152 ZDOT = -3736
079290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17331466
43 X = -5282630
97
Y = -1471892
13 feet Y = -448632
72 meter
Z = -13578220
18 Z = -4138641
51
XDOT = 11107
577374 XDOT = 3385
589584
YDOT = -17734
718127 feet/sec YDOT = -5405
542085 meter/sec
ZDOT = -12273
298952 ZDOT = -3740
901521
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
56274154
00020000 00000-0 20000-3 0 9035
2 25544 51
6373 187
6170 0002369 103
6891 256
4537 15
75741180 30245
Satellite: ISS
Catalog Number: 25544
Epoch time: 07291
56274154 = yrday
fracday
Element set: 903
Inclination: 51
6373 deg
RA of node: 187
6170 deg
Eccentricity:
0002369
Arg of perigee: 103
6891 deg
Mean anomaly: 256
4537 deg
Mean motion: 15
75741180 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3024
Checksum: 292
Coasting Arc #5 (Orbit 3039)
---------------------------------------
Vector Time (GMT): 2007/292/12:57:44
867
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5796443
77 A = 6723811
91 meter
Y = -2007470
83 meter E =
0016085
Z = 2735315
12 I = 51
63713
XDOT = 3898
102333 Wp = 101
56819
YDOT = 4193
097487 meter/sec RA = 181
56571 deg
ZDOT = -5160
881940 TA = 47
14005
MA = 47
00505
Ha = 188
215 n
mi
Hp = 180
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19017203
96 X = 5805172
95
Y = -6586190
38 feet Y = -1942602
93 meter
Z = 8974130
97 Z = 2763495
82
XDOT = 12789
049650 XDOT = 3875
995751
YDOT = 13756
881518 feet/sec YDOT = 4236
564711 meter/sec
ZDOT = -16932
027363 ZDOT = -5141
998358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9895692
75 X = -3016207
15
Y = 17469341
90 feet Y = 5324655
41 meter
Z = 9080987
59 Z = 2767885
02
XDOT = -17485
773534 XDOT = -5329
663773
YDOT = -1103
344675 feet/sec YDOT = -336
299457 meter/sec
ZDOT = -16859
712859 ZDOT = -5138
840479
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
57744221
00020000 00000-0 20000-3 0 9045
2 25544 51
6372 182
3921 0002515 106
1995 253
9446 15
75769355 30409
Satellite: ISS
Catalog Number: 25544
Epoch time: 07292
57744221 = yrday
fracday
Element set: 904
Inclination: 51
6372 deg
RA of node: 182
3921 deg
Eccentricity:
0002515
Arg of perigee: 106
1995 deg
Mean anomaly: 253
9446 deg
Mean motion: 15
75769355 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3040
Checksum: 296
Coasting Arc #6 (Orbit 3055)
---------------------------------------
Vector Time (GMT): 2007/293/12:57:44
867
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3046595
97 A = 6717212
90 meter
Y = -3599648
04 meter E =
0009769
Z = 4777834
66 I = 51
64380
XDOT = 6860
972465 Wp = 117
40589
YDOT = -2433
149358 meter/sec RA = 176
45941 deg
ZDOT = 2533
406208 TA = 307
76947
MA = 307
85792
Ha = 188
283 n
mi
Hp = 180
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9995393
61 X = -3029327
88
Y = -11809868
91 feet Y = -3633620
21 meter
Z = 15675310
56 Z = 4763076
09
XDOT = 22509
752183 XDOT = 6875
363399
YDOT = -7982
773483 feet/sec YDOT = -2356
345592 meter/sec
ZDOT = 8311
700158 ZDOT = 2566
772209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15406482
45 X = 4695895
85
Y = 1947149
56 feet Y = 593491
19 meter
Z = 15618744
04 Z = 4760593
18
XDOT = -11097
397248 XDOT = -3382
486681
YDOT = 19899
637978 feet/sec YDOT = 6065
409656 meter/sec
ZDOT = 8438
222730 ZDOT = 2571
970288
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
59212390
00020000 00000-0 20000-3 0 9056
2 25544 51
6373 177
1666 0002417 109
4573 250
6852 15
75784062 30561
Satellite: ISS
Catalog Number: 25544
Epoch time: 07293
59212390 = yrday
fracday
Element set: 905
Inclination: 51
6373 deg
RA of node: 177
1666 deg
Eccentricity:
0002417
Arg of perigee: 109
4573 deg
Mean anomaly: 250
6852 deg
Mean motion: 15
75784062 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3056
Checksum: 299
Coasting Arc #7 (Orbit 3070)
---------------------------------------
Vector Time (GMT): 2007/294/12:57:44
867
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6120196
59 A = 6725775
00 meter
Y = 2249809
29 meter E =
0008604
Z = -1640536
40 I = 51
70168
XDOT = -3048
664719 Wp = 52
22973
YDOT = -4122
486296 meter/sec RA = 171
27636 deg
ZDOT = 5745
414308 TA = 289
65710
MA = 289
74993
Ha = 188
028 n
mi
Hp = 180
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20079385
13 X = -6136929
89
Y = 7381264
08 feet Y = 2181276
18 meter
Z = -5382337
28 Z = -1670309
42
XDOT = -10002
180835 XDOT = -3030
250424
YDOT = -13525
217507 feet/sec YDOT = -4156
475050 meter/sec
ZDOT = 18849
784475 ZDOT = 5730
648561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9531591
00 X = 2905228
94
Y = -19120290
34 feet Y = -5827864
50 meter
Z = -5495233
55 Z = -1674947
19
XDOT = 15237
614621 XDOT = 4644
424936
YDOT = 2218
460266 feet/sec YDOT = 676
186689 meter/sec
ZDOT = 18793
116575 ZDOT = 5728
141932
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
54337078
00020000 00000-0 20000-3 0 9064
2 25544 51
6369 172
2675 0002188 113
2192 246
9203 15
75819389 30713
Satellite: ISS
Catalog Number: 25544
Epoch time: 07294
54337078 = yrday
fracday
Element set: 906
Inclination: 51
6369 deg
RA of node: 172
2675 deg
Eccentricity:
0002188
Arg of perigee: 113
2192 deg
Mean anomaly: 246
9203 deg
Mean motion: 15
75819389 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3071
Checksum: 309
Coasting Arc #8 (Orbit 3086)
---------------------------------------
Vector Time (GMT): 2007/295/12:57:44
867
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2239781
41 A = 6715278
82 meter
Y = 3661144
71 meter E =
0016075
Z = -5178650
26 I = 51
69403
XDOT = -7107
304959 Wp = 85
75369
YDOT = 2700
624983 meter/sec RA = 166
15584 deg
ZDOT = -1166
601025 TA = 173
11360
MA = 173
09148
Ha = 187
954 n
mi
Hp = 180
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7348364
19 X = 2223832
82
Y = 12011629
62 feet Y = 3686101
77 meter
Z = -16990322
37 Z = -5167808
16
XDOT = -23317
929655 XDOT = -7131
308293
YDOT = 8860
318186 feet/sec YDOT = 2621
012804 meter/sec
ZDOT = -3827
431186 ZDOT = -1201
187308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13715337
67 X = -4180434
92
Y = -3403279
94 feet Y = -1037319
73 meter
Z = -16948626
94 Z = -5165941
49
XDOT = 10245
489980 XDOT = 3122
825346
YDOT = -21607
229402 feet/sec YDOT = -6585
883522 meter/sec
ZDOT = -3958
575240 ZDOT = -1206
573733
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
55801741
00020000 00000-0 20000-3 0 9070
2 25544 51
6360 167
0415 0002152 117
8009 242
3374 15
75864209 30873
Satellite: ISS
Catalog Number: 25544
Epoch time: 07295
55801741 = yrday
fracday
Element set: 907
Inclination: 51
6360 deg
RA of node: 167
0415 deg
Eccentricity:
0002152
Arg of perigee: 117
8009 deg
Mean anomaly: 242
3374 deg
Mean motion: 15
75864209 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3087
Checksum: 285
Coasting Arc #9 (Orbit 3102)
---------------------------------------
Vector Time (GMT): 2007/296/12:57:44
867
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6240277
01 A = 6726811
75 meter
Y = -2463791
70 meter E =
0015206
Z = 377912
27 I = 51
76097
XDOT = 2078
408768 Wp = 130
00975
YDOT = 4315
345537 meter/sec RA = 160
99897 deg
ZDOT = -6036
492035 TA = 45
88418
MA = 45
75918
Ha = 187
960 n
mi
Hp = 180
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20473349
76 X = 6265527
83
Y = -8083306
09 feet Y = -2393868
17 meter
Z = 1239869
64 Z = 408289
66
XDOT = 6818
926404 XDOT = 2059
324259
YDOT = 14157
957799 feet/sec YDOT = 4338
480388 meter/sec
ZDOT = -19804
763895 ZDOT = -6026
441547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8663287
32 X = -2640569
97
Y = 20227369
10 feet Y = 6165302
10 meter
Z = 1355048
52 Z = 413018
79
XDOT = -13459
989395 XDOT = -4102
604768
YDOT = -4410
659824 feet/sec YDOT = -1344
369114 meter/sec
ZDOT = -19765
991892 ZDOT = -6024
674329
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
57264725
00020000 00000-0 20000-3 0 9089
2 25544 51
6362 161
8165 0002214 123
3914 236
7462 15
75862982 31035
Satellite: ISS
Catalog Number: 25544
Epoch time: 07296
57264725 = yrday
fracday
Element set: 908
Inclination: 51
6362 deg
RA of node: 161
8165 deg
Eccentricity:
0002214
Arg of perigee: 123
3914 deg
Mean anomaly: 236
7462 deg
Mean motion: 15
75862982 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3103
Checksum: 296
Coasting Arc #10 (Orbit 3118)
---------------------------------------
Vector Time (GMT): 2007/297/12:57:44
867
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1398458
14 A = 6714720
82 meter
Y = -3921737
33 meter E =
0004178
Z = 5264453
36 I = 51
74645
XDOT = 7120
734376 Wp = 100
87651
YDOT = -2935
789002 meter/sec RA = 155
85781 deg
ZDOT = -296
019381 TA = 351
92335
MA = 351
93008
Ha = 187
905 n
mi
Hp = 180
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4588117
27 X = -1380075
21
Y = -12866592
28 feet Y = -3937272
57 meter
Z = 17271828
61 Z = 5257704
36
XDOT = 23361
989422 XDOT = 7154
471625
YDOT = -9631
853682 feet/sec YDOT = -2855
972301 meter/sec
ZDOT = -971
192194 ZDOT = -261
343780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12534181
30 X = 3820418
46
Y = 5513395
15 feet Y = 1680482
84 meter
Z = 17245661
88 Z = 5256477
74
XDOT = -8799
621940 XDOT = -2682
124767
YDOT = 22625
801733 feet/sec YDOT = 6896
344368 meter/sec
ZDOT = -839
724612 ZDOT = -255
948062
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 07297
58725784
00020000 00000-0 20000-3 0 9099
2 25544 51
6352 156
5901 0002125 127
2199 232
9160 15
75895031 31193
Satellite: ISS
Catalog Number: 25544
Epoch time: 07297
58725784 = yrday
fracday
Element set: 909
Inclination: 51
6352 deg
RA of node: 156
5901 deg
Eccentricity:
0002125
Arg of perigee: 127
2199 deg
Mean anomaly: 232
9160 deg
Mean motion: 15
75895031 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3119
Checksum: 304
Coasting Arc #11 (Orbit 3134)
---------------------------------------
Vector Time (GMT): 2007/298/12:57:44
867
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6122943
91 A = 6726339
96 meter
Y = 2620055
53 meter E =
0014190
Z = 900598
05 I = 51
81038
XDOT = -1141
274024 Wp = 62
77094
YDOT = -4740
090660 meter/sec RA = 150
72730 deg
ZDOT = 5965
757017 TA = 307
04583
MA = 307
17553
Ha = 187
738 n
mi
Hp = 180
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20088398
67 X = -6156161
78
Y = 8595982
71 feet Y = 2551399
61 meter
Z = 2954718
01 Z = 870771
01
XDOT = -3744
337348 XDOT = -1117
166325
YDOT = -15551
478543 feet/sec YDOT = -4752
718006 meter/sec
ZDOT = 19572
693624 ZDOT = 5960
271269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7340683
49 X = 2237440
33
Y = -20596225
55 feet Y = -6277729
55 meter
Z = 2841636
37 Z = 866130
77
XDOT = 12532
199301 XDOT = 3819
814347
YDOT = 7194
672757 feet/sec YDOT = 2192
936256 meter/sec
ZDOT = 19551
229753 ZDOT = 5959
214829
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 07298
60184998
00020000 00000-0 20000-3 0 9101
2 25544 51
6337 151
3631 0002070 132
3916 227
7424 15
75941707 31357
Satellite: ISS
Catalog Number: 25544
Epoch time: 07298
60184998 = yrday
fracday
Element set: 910
Inclination: 51
6337 deg
RA of node: 151
3631 deg
Eccentricity:
0002070
Arg of perigee: 132
3916 deg
Mean anomaly: 227
7424 deg
Mean motion: 15
75941707 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3135
Checksum: 290
Coasting Arc #12 (Orbit 3149)
---------------------------------------
Vector Time (GMT): 2007/299/12:57:44
867
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 611155
15 A = 6715514
39 meter
Y = 4399865
11 meter E =
0015312
Z = -5050150
37 I = 51
79756
XDOT = -6855
651108 Wp = 107
70155
YDOT = 2999
060888 meter/sec RA = 145
56398 deg
ZDOT = 1783
083983 TA = 179
45505
MA = 179
45338
Ha = 187
683 n
mi
Hp = 180
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2005102
20 X = 586443
38
Y = 14435252
98 feet Y = 4406561
20 meter
Z = -16568734
81 Z = -5047241
32
XDOT = -22492
293661 XDOT = -6897
339738
YDOT = 9839
438609 feet/sec YDOT = 2922
164031 meter/sec
ZDOT = 5850
013067 ZDOT = 1749
676751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12162539
44 X = -3707142
02
Y = -8053221
63 feet Y = -2454621
95 meter
Z = -16557119
08 Z = -5046609
90
XDOT = 7083
324747 XDOT = 2158
997383
YDOT = -22465
737933 feet/sec YDOT = -6847
556922 meter/sec
ZDOT = 5723
352407 ZDOT = 1744
477814
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 07299
55301459
00020000 00000-0 20000-3 0 9110
2 25544 51
6324 146
4623 0002127 135
2586 224
8750 15
75966730 31507
Satellite: ISS
Catalog Number: 25544
Epoch time: 07299
55301459 = yrday
fracday
Element set: 911
Inclination: 51
6324 deg
RA of node: 146
4623 deg
Eccentricity:
0002127
Arg of perigee: 135
2586 deg
Mean anomaly: 224
8750 deg
Mean motion: 15
75966730 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3150
Checksum: 289
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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