Date:
March 1st 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7071 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3360)
---------------------------------------
Vector Time (GMT): 2007/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5110094
58 A = 6711631
31 meter
Y = 1755864
87 meter E =
0014034
Z = -3968565
57 I = 51
37113
XDOT = 794
967644 Wp = 266
74125
YDOT = -6591
866162 meter/sec RA = 305
09806 deg
ZDOT = -3929
044271 TA = 322
52472
MA = 322
62249
Ha = 184
091 n
mi
Hp = 175
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16765402
16 X = -5110071
12
Y = 5760711
53 feet Y = 1698721
02 meter
Z = -13020228
26 Z = -3993389
64
XDOT = 2608
161563 XDOT = 887
705773
YDOT = -21626
857488 feet/sec YDOT = -6582
457921 meter/sec
ZDOT = -12890
565193 ZDOT = -3924
957084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17620716
77 X = -5370794
47
Y = -1159197
27 feet Y = -353323
33 meter
Z = -13113254
87 Z = -3996920
09
XDOT = 10767
919951 XDOT = 3282
062001
YDOT = -17612
741922 feet/sec YDOT = -5368
363738 meter/sec
ZDOT = -12876
052763 ZDOT = -3924
620882
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 07059
52291071
00020000 00000-0 20000-3 0 9007
2 25544 51
6358 305
5409 0021062 261
8477 98
0299 15
78771046 33618
Satellite: ISS
Catalog Number: 25544
Epoch time: 07059
52291071 = yrday
fracday
Element set: 900
Inclination: 51
6358 deg
RA of node: 305
5409 deg
Eccentricity:
0021062
Arg of perigee: 261
8477 deg
Mean anomaly: 98
0299 deg
Mean motion: 15
78771046 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3361
Checksum: 297
Coasting Arc #2 (Orbit 3376)
---------------------------------------
Vector Time (GMT): 2007/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1635759
69 A = 6716721
37 meter
Y = 6173968
22 meter E =
0010123
Z = 2071744
07 I = 51
37260
XDOT = -5346
204997 Wp = 228
52224
YDOT = 432
139356 meter/sec RA = 299
86156 deg
ZDOT = -5532
951320 TA = 288
21491
MA = 288
32507
Ha = 184
034 n
mi
Hp = 175
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5366665
65 X = -1714740
17
Y = 20255801
23 feet Y = 6155234
71 meter
Z = 6797060
59 Z = 2063605
71
XDOT = -17540
042641 XDOT = -5323
762634
YDOT = 1417
780041 feet/sec YDOT = 372
480374 meter/sec
ZDOT = -18152
727429 ZDOT = -5558
867906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12545616
85 X = -3823904
02
Y = 16796129
28 feet Y = 5119460
20 meter
Z = 6767285
68 Z = 2062668
67
XDOT = -15491
783881 XDOT = -4721
895727
YDOT = -4250
157766 feet/sec YDOT = -1295
448087 meter/sec
ZDOT = -18250
028855 ZDOT = -5562
608795
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 07060
53565944
00020000 00000-0 20000-3 0 9014
2 25544 51
6354 300
3025 0020882 265
5152 94
3628 15
78789013 33776
Satellite: ISS
Catalog Number: 25544
Epoch time: 07060
53565944 = yrday
fracday
Element set: 901
Inclination: 51
6354 deg
RA of node: 300
3025 deg
Eccentricity:
0020882
Arg of perigee: 265
5152 deg
Mean anomaly: 94
3628 deg
Mean motion: 15
78789013 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3377
Checksum: 292
Coasting Arc #3 (Orbit 3392)
---------------------------------------
Vector Time (GMT): 2007/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4064774
10 A = 6706440
77 meter
Y = 1164298
14 meter E =
0018457
Z = 5221542
81 I = 51
32504
XDOT = -2783
446615 Wp = 265
82320
YDOT = 7151
298941 meter/sec RA = 294
69133 deg
ZDOT = 572
625873 TA = 178
70971
MA = 178
70494
Ha = 183
947 n
mi
Hp = 174
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13335873
03 X = 4026088
06
Y = 3819875
79 feet Y = 1209536
73 meter
Z = 17131045
95 Z = 5241194
88
XDOT = -9132
042700 XDOT = -2865
988227
YDOT = 23462
266866 feet/sec YDOT = 7119
711407 meter/sec
ZDOT = 1878
693810 ZDOT = 558
903352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11016280
98 X = 3357762
44
Y = 8278793
46 feet Y = 2523376
25 meter
Z = 17205023
34 Z = 5244091
11
XDOT = -16285
087535 XDOT = -4963
694681
YDOT = 17873
635796 feet/sec YDOT = 5447
884191 meter/sec
ZDOT = 1828
078550 ZDOT = 557
198342
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 07061
54838219
00020000 00000-0 20000-3 0 9025
2 25544 51
6352 295
0630 0020990 269
7464 90
1297 15
78845198 33939
Satellite: ISS
Catalog Number: 25544
Epoch time: 07061
54838219 = yrday
fracday
Element set: 902
Inclination: 51
6352 deg
RA of node: 295
0630 deg
Eccentricity:
0020990
Arg of perigee: 269
7464 deg
Mean anomaly: 90
1297 deg
Mean motion: 15
78845198 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3393
Checksum: 316
Coasting Arc #4 (Orbit 3408)
---------------------------------------
Vector Time (GMT): 2007/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3040708
89 A = 6717685
83 meter
Y = -5877430
72 meter E =
0012866
Z = 1130657
67 I = 51
35189
XDOT = 3879
941354 Wp = 312
82994
YDOT = 3128
632872 meter/sec RA = 289
50196 deg
ZDOT = 5879
721400 TA = 59
62362
MA = 59
49648
Ha = 183
915 n
mi
Hp = 174
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9976079
05 X = 3100712
78
Y = -19282909
19 feet Y = -5843092
23 meter
Z = 3709506
79 Z = 1145575
27
XDOT = 12729
466385 XDOT = 3816
106268
YDOT = 10264
543543 feet/sec YDOT = 3171
664090 meter/sec
ZDOT = 19290
424541 ZDOT = 5898
414376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15910740
05 X = 4849593
57
Y = -14757643
55 feet Y = -4498129
75 meter
Z = 3764769
41 Z = 1147501
72
XDOT = 7311
200765 XDOT = 2228
453993
YDOT = 12779
728625 feet/sec YDOT = 3895
261285 meter/sec
ZDOT = 19361
060333 ZDOT = 5901
251189
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 07062
56108101
00020000 00000-0 20000-3 0 9039
2 25544 51
6342 289
8230 0021163 273
7420 86
1326 15
78904730 34099
Satellite: ISS
Catalog Number: 25544
Epoch time: 07062
56108101 = yrday
fracday
Element set: 903
Inclination: 51
6342 deg
RA of node: 289
8230 deg
Eccentricity:
0021163
Arg of perigee: 273
7420 deg
Mean anomaly: 86
1326 deg
Mean motion: 15
78904730 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3409
Checksum: 270
Coasting Arc #5 (Orbit 3423)
---------------------------------------
Vector Time (GMT): 2007/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2672083
51 A = 6709163
00 meter
Y = -4168965
14 meter E =
0011460
Z = -4517450
10 I = 51
31400
XDOT = 3997
990032 Wp = 265
98454
YDOT = -5859
121336 meter/sec RA = 284
27163 deg
ZDOT = 3034
927239 TA = 34
31378
MA = 34
23980
Ha = 183
900 n
mi
Hp = 174
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8766678
17 X = -2603322
45
Y = -13677707
16 feet Y = -4198461
82 meter
Z = -14821030
51 Z = -4530263
42
XDOT = 13116
765198 XDOT = 4048
467607
YDOT = -19222
839029 feet/sec YDOT = -5814
131069 meter/sec
ZDOT = 9957
110364 ZDOT = 3054
472199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3796057
38 X = -1157038
29
Y = -15750511
37 feet Y = -4800755
87 meter
Z = -14869721
07 Z = -4532290
98
XDOT = 17425
686360 XDOT = 5311
349203
YDOT = -13691
477287 feet/sec YDOT = -4173
162277 meter/sec
ZDOT = 10029
750741 ZDOT = 3057
068026
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 07063
51046627
00020000 00000-0 20000-3 0 9040
2 25544 51
6331 284
9105 0021198 277
4949 82
3808 15
78932494 34247
Satellite: ISS
Catalog Number: 25544
Epoch time: 07063
51046627 = yrday
fracday
Element set: 904
Inclination: 51
6331 deg
RA of node: 284
9105 deg
Eccentricity:
0021198
Arg of perigee: 277
4949 deg
Mean anomaly: 82
3808 deg
Mean motion: 15
78932494 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3424
Checksum: 309
Coasting Arc #6 (Orbit 3439)
---------------------------------------
Vector Time (GMT): 2007/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3793271
75 A = 6711396
27 meter
Y = 3921644
20 meter E =
0015636
Z = -3900701
82 I = 51
31490
XDOT = -2256
990537 Wp = 293
40258
YDOT = -6189
158157 meter/sec RA = 279
12437 deg
ZDOT = -4008
741846 TA = 294
76158
MA = 294
92421
Ha = 184
054 n
mi
Hp = 174
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12445117
30 X = -3817893
61
Y = 12866286
76 feet Y = 3879087
69 meter
Z = -12797578
13 Z = -3919189
40
XDOT = -7404
824595 XDOT = -2168
141305
YDOT = -20305
636999 feet/sec YDOT = -6213
900680 meter/sec
ZDOT = -13152
040176 ZDOT = -4019
489742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15725780
53 X = -4793217
90
Y = 8447086
83 feet Y = 2574672
07 meter
Z = -12866500
56 Z = -3921709
37
XDOT = -128
715872 XDOT = -39
232598
YDOT = -20428
942477 feet/sec YDOT = -6226
741667 meter/sec
ZDOT = -13193
246809 ZDOT = -4021
301627
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 07064
52312023
00020000 00000-0 20000-3 0 9059
2 25544 51
6321 279
6714 0021280 281
4694 78
4082 15
78949201 34409
Satellite: ISS
Catalog Number: 25544
Epoch time: 07064
52312023 = yrday
fracday
Element set: 905
Inclination: 51
6321 deg
RA of node: 279
6714 deg
Eccentricity:
0021280
Arg of perigee: 281
4694 deg
Mean anomaly: 78
4082 deg
Mean motion: 15
78949201 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3440
Checksum: 280
Coasting Arc #7 (Orbit 3455)
---------------------------------------
Vector Time (GMT): 2007/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1259360
42 A = 6715958
38 meter
Y = 6256644
67 meter E =
0007332
Z = 2099104
54 I = 51
32836
XDOT = -4609
370774 Wp = 277
10595
YDOT = 2771
729118 meter/sec RA = 273
88142 deg
ZDOT = -5511
635063 TA = 239
30450
MA = 239
37676
Ha = 184
187 n
mi
Hp = 174
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4131759
89 X = 1179107
16
Y = 20527049
44 feet Y = 6270279
01 meter
Z = 6886825
91 Z = 2105026
95
XDOT = -15122
607525 XDOT = -4613
247835
YDOT = 9093
599468 feet/sec YDOT = 2720
162387 meter/sec
ZDOT = -18082
792202 ZDOT = -5534
036799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2047107
03 X = -623958
22
Y = 20830793
31 feet Y = 6349225
80 meter
Z = 6909918
42 Z = 2106143
14
XDOT = -15496
856983 XDOT = -4723
442008
YDOT = 4486
364709 feet/sec YDOT = 1367
443963 meter/sec
ZDOT = -18166
570490 ZDOT = -5537
170685
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 07065
53574942
00020000 00000-0 20000-3 0 9062
2 25544 51
6326 274
4311 0021318 285
8250 74
0565 15
79030295 34568
Satellite: ISS
Catalog Number: 25544
Epoch time: 07065
53574942 = yrday
fracday
Element set: 906
Inclination: 51
6326 deg
RA of node: 274
4311 deg
Eccentricity:
0021318
Arg of perigee: 285
8250 deg
Mean anomaly: 74
0565 deg
Mean motion: 15
79030295 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3456
Checksum: 292
Coasting Arc #8 (Orbit 3471)
---------------------------------------
Vector Time (GMT): 2007/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4169613
33 A = 6706002
32 meter
Y = -689085
10 meter E =
0018411
Z = 5221262
33 I = 51
29271
XDOT = 602
711865 Wp = 288
68517
YDOT = 7654
323366 meter/sec RA = 268
70611 deg
ZDOT = 536
235871 TA = 156
23515
MA = 156
15002
Ha = 184
351 n
mi
Hp = 174
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13679833
77 X = 4151645
12
Y = -2260777
88 feet Y = -642558
20 meter
Z = 17130125
76 Z = 5241474
58
XDOT = 1977
401131 XDOT = 514
470411
YDOT = 25112
609468 feet/sec YDOT = 7660
569886 meter/sec
ZDOT = 1759
304038 ZDOT = 538
948885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13683864
57 X = 4170841
92
Y = 1548208
70 feet Y = 471894
01 meter
Z = 17205960
53 Z = 5244376
77
XDOT = -4876
635101 XDOT = -1486
398379
YDOT = 23692
604474 feet/sec YDOT = 7221
505844 meter/sec
ZDOT = 1770
532021 ZDOT = 539
658160
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 07066
54835706
00020000 00000-0 20000-3 0 9073
2 25544 51
6316 269
1897 0021188 289
4306 70
4570 15
78996829 34721
Satellite: ISS
Catalog Number: 25544
Epoch time: 07066
54835706 = yrday
fracday
Element set: 907
Inclination: 51
6316 deg
RA of node: 269
1897 deg
Eccentricity:
0021188
Arg of perigee: 289
4306 deg
Mean anomaly: 70
4570 deg
Mean motion: 15
78996829 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3472
Checksum: 336
Coasting Arc #9 (Orbit 3487)
---------------------------------------
Vector Time (GMT): 2007/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 230578
95 A = 6717141
39 meter
Y = -6592786
63 meter E =
0017436
Z = 1216934
41 I = 51
33214
XDOT = 4860
368239 Wp = 333
71620
YDOT = 1242
817127 meter/sec RA = 263
51399 deg
ZDOT = 5859
400390 TA = 39
71908
MA = 39
59153
Ha = 184
479 n
mi
Hp = 174
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 756492
62 X = 298371
68
Y = -21629877
40 feet Y = -6589829
04 meter
Z = 3992566
97 Z = 1218219
64
XDOT = 15946
090023 XDOT = 4817
645860
YDOT = 4077
484011 feet/sec YDOT = 1296
929978 meter/sec
ZDOT = 19223
754560 ZDOT = 5882
908104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6278222
95 X = 1913602
36
Y = -20711744
57 feet Y = -6312939
74 meter
Z = 3996501
21 Z = 1218133
57
XDOT = 12744
908623 XDOT = 3884
648148
YDOT = 7559
816588 feet/sec YDOT = 2304
232096 meter/sec
ZDOT = 19312
232325 ZDOT = 5886
368413
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 07067
56093716
00020000 00000-0 20000-3 0 9084
2 25544 51
6306 263
9481 0021283 293
1820 66
7104 15
79072615 34887
Satellite: ISS
Catalog Number: 25544
Epoch time: 07067
56093716 = yrday
fracday
Element set: 908
Inclination: 51
6306 deg
RA of node: 263
9481 deg
Eccentricity:
0021283
Arg of perigee: 293
1820 deg
Mean anomaly: 66
7104 deg
Mean motion: 15
79072615 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3488
Checksum: 303
Coasting Arc #10 (Orbit 3502)
---------------------------------------
Vector Time (GMT): 2007/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4201947
79 A = 6708918
98 meter
Y = -2742802
06 meter E =
0011488
Z = -4441498
76 I = 51
30883
XDOT = 1163
552081 Wp = 302
19348
YDOT = -6933
738346 meter/sec RA = 258
27976 deg
ZDOT = 3181
135992 TA = 359
68633
MA = 359
68705
Ha = 184
544 n
mi
Hp = 174
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13785917
95 X = -4149389
16
Y = -8998694
42 feet Y = -2789496
92 meter
Z = -14571846
33 Z = -4461783
97
XDOT = 3817
428086 XDOT = 1225
546323
YDOT = -22748
485386 feet/sec YDOT = -6920
380086 meter/sec
ZDOT = 10436
797875 ZDOT = 3186
939405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11134568
69 X = -3393816
54
Y = -12033776
21 feet Y = -3667894
99 meter
Z = -14648424
86 Z = -4464839
90
XDOT = 8248
895279 XDOT = 2514
263281
YDOT = -20362
072966 feet/sec YDOT = -6206
359840 meter/sec
ZDOT = 10457
659190 ZDOT = 3187
494521
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 07068
51021026
00020000 00000-0 20000-3 0 9096
2 25544 51
6300 259
0345 0021191 296
8181 63
0817 15
79110025 35031
Satellite: ISS
Catalog Number: 25544
Epoch time: 07068
51021026 = yrday
fracday
Element set: 909
Inclination: 51
6300 deg
RA of node: 259
0345 deg
Eccentricity:
0021191
Arg of perigee: 296
8181 deg
Mean anomaly: 63
0817 deg
Mean motion: 15
79110025 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3503
Checksum: 259
Coasting Arc #11 (Orbit 3518)
---------------------------------------
Vector Time (GMT): 2007/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1855735
73 A = 6710355
26 meter
Y = 5026127
95 meter E =
0017361
Z = -4040143
14 I = 51
32108
XDOT = -4655
201591 Wp = 320
42074
YDOT = -4808
745109 meter/sec RA = 253
13186 deg
ZDOT = -3821
833775 TA = 270
04486
MA = 270
24380
Ha = 184
852 n
mi
Hp = 174
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6088371
83 X = -1892174
48
Y = 16489921
11 feet Y = 5005172
23 meter
Z = -13255062
78 Z = -4049246
91
XDOT = -15272
971099 XDOT = -4582
517821
YDOT = -15776
722798 feet/sec YDOT = -4860
395885 meter/sec
ZDOT = -12538
824722 ZDOT = -3844
271977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9556410
75 X = -2912794
00
Y = 14723146
20 feet Y = 4487614
96 meter
Z = -13288583
01 Z = -4050360
10
XDOT = -10207
818761 XDOT = -3111
343158
YDOT = -18085
040442 feet/sec YDOT = -5512
320327 meter/sec
ZDOT = -12623
776892 ZDOT = -3847
727197
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 07069
52274376
00020000 00000-0 20000-3 0 9108
2 25544 51
6299 253
7947 0021165 301
1668 58
7422 15
79161238 35190
Satellite: ISS
Catalog Number: 25544
Epoch time: 07069
52274376 = yrday
fracday
Element set: 910
Inclination: 51
6299 deg
RA of node: 253
7947 deg
Eccentricity:
0021165
Arg of perigee: 301
1668 deg
Mean anomaly: 58
7422 deg
Mean motion: 15
79161238 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3519
Checksum: 310
Coasting Arc #12 (Orbit 3534)
---------------------------------------
Vector Time (GMT): 2007/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3731906
25 A = 6715825
35 meter
Y = 5278584
27 meter E =
0008068
Z = 1839086
39 I = 51
35013
XDOT = -3157
702974 Wp = 325
05446
YDOT = 4192
474979 meter/sec RA = 247
89053 deg
ZDOT = -5631
326322 TA = 194
43568
MA = 194
45874
Ha = 185
118 n
mi
Hp = 174
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12243786
90 X = 3663669
10
Y = 17318189
85 feet Y = 5319935
02 meter
Z = 6033748
01 Z = 1857050
06
XDOT = -10359
917895 XDOT = -3176
993342
YDOT = 13754
839171 feet/sec YDOT = 4157
055842 meter/sec
ZDOT = -18475
480059 ZDOT = -5646
713266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8355399
96 X = 2546725
91
Y = 19472789
06 feet Y = 5935306
10 meter
Z = 6101959
53 Z = 1859877
27
XDOT = -11465
174985 XDOT = -3494
585335
YDOT = 10721
111484 feet/sec YDOT = 3267
794780 meter/sec
ZDOT = -18532
722330 ZDOT = -5648
773766
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 07070
53525015
00020000 00000-0 20000-3 0 9111
2 25544 51
6300 248
5532 0021462 304
9413 54
9737 15
79227731 35350
Satellite: ISS
Catalog Number: 25544
Epoch time: 07070
53525015 = yrday
fracday
Element set: 911
Inclination: 51
6300 deg
RA of node: 248
5532 deg
Eccentricity:
0021462
Arg of perigee: 304
9413 deg
Mean anomaly: 54
9737 deg
Mean motion: 15
79227731 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3535
Checksum: 273
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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