Date:
November 8th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 1561)
---------------------------------------
Vector Time (GMT): 2006/310/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4665186
32 A = 6716066
41 meter
Y = -3337208
94 meter E =
0016184
Z = 3472622
97 I = 51
67448
XDOT = 5494
007596 Wp = 134
60688
YDOT = 2947
526983 meter/sec RA = 173
01404 deg
ZDOT = -4546
449895 TA = 4
08081
MA = 4
06763
Ha = 186
968 n
mi
Hp = 176
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15305729
39 X = 4685286
80
Y = -10948848
23 feet Y = -3284928
09 meter
Z = 11393120
00 Z = 3495335
79
XDOT = 18024
959304 XDOT = 5482
726161
YDOT = 9670
364119 feet/sec YDOT = 3008
901259 meter/sec
ZDOT = -14916
174197 ZDOT = -4519
786332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1459351
97 X = -444810
48
Y = 18710560
57 feet Y = 5702978
86 meter
Z = 11477413
82 Z = 3498315
73
XDOT = -17702
629153 XDOT = -5395
761366
YDOT = 7711
272369 feet/sec YDOT = 2350
395818 meter/sec
ZDOT = -14816
278323 ZDOT = -4516
001633
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 06310
55291377
00020000 00000-0 20000-3 0 9008
2 25544 51
6339 173
8153 0011791 183
4591 176
6494 15
77785978 15622
Satellite: ISS
Catalog Number: 25544
Epoch time: 06310
55291377 = yrday
fracday
Element set: 900
Inclination: 51
6339 deg
RA of node: 173
8153 deg
Eccentricity:
0011791
Arg of perigee: 183
4591 deg
Mean anomaly: 176
6494 deg
Mean motion: 15
77785978 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1562
Checksum: 322
Coasting Arc #2 (Orbit 1577)
---------------------------------------
Vector Time (GMT): 2006/311/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3823829
28 A = 6712138
15 meter
Y = -2949029
40 meter E =
0016414
Z = 4664003
80 I = 51
68730
XDOT = 6211
761233 Wp = 159
60907
YDOT = -3595
422117 meter/sec RA = 167
89944 deg
ZDOT = 2801
344190 TA = 262
69149
MA = 262
87809
Ha = 187
045 n
mi
Hp = 177
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12545371
65 X = -3813226
15
Y = -9675293
32 feet Y = -2991730
73 meter
Z = 15301849
72 Z = 4645452
59
XDOT = 20379
794073 XDOT = 6237
895264
YDOT = -11796
004320 feet/sec YDOT = -3525
812896 meter/sec
ZDOT = 9190
761779 ZDOT = 2831
584925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15477989
52 X = 4717691
20
Y = -3681793
71 feet Y = -1122210
72 meter
Z = 15232218
85 Z = 4642780
31
XDOT = -3961
105805 XDOT = -1207
345049
YDOT = 22082
706788 feet/sec YDOT = 6730
809029 meter/sec
ZDOT = 9303
128647 ZDOT = 2835
593612
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 06311
56632402
00020000 00000-0 20000-3 0 9019
2 25544 51
6325 168
5802 0011803 187
0363 173
0638 15
77743316 15788
Satellite: ISS
Catalog Number: 25544
Epoch time: 06311
56632402 = yrday
fracday
Element set: 901
Inclination: 51
6325 deg
RA of node: 168
5802 deg
Eccentricity:
0011803
Arg of perigee: 187
0363 deg
Mean anomaly: 173
0638 deg
Mean motion: 15
77743316 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1578
Checksum: 279
Coasting Arc #3 (Orbit 1592)
---------------------------------------
Vector Time (GMT): 2006/312/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5944806
16 A = 6720670
37 meter
Y = 2882888
27 meter E =
0005395
Z = -1249479
28 I = 51
74342
XDOT = -3114
517117 Wp = 145
47043
YDOT = -3880
489747 meter/sec RA = 162
70535 deg
ZDOT = 5872
943558 TA = 200
84114
MA = 200
86314
Ha = 186
744 n
mi
Hp = 177
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19503957
23 X = -5970531
31
Y = 9458294
86 feet Y = 2816266
45 meter
Z = -4099341
48 Z = -1278421
99
XDOT = -10218
232010 XDOT = -3099
423792
YDOT = -12731
265574 feet/sec YDOT = -3915
234219 meter/sec
ZDOT = 19268
187527 ZDOT = 5857
849158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4606510
01 X = 1404064
25
Y = -21160096
62 feet Y = -6449597
45 meter
Z = -4206978
32 Z = -1282286
99
XDOT = 14846
754056 XDOT = 4525
290636
YDOT = -582
366311 feet/sec YDOT = -177
505251 meter/sec
ZDOT = 19211
326121 ZDOT = 5855
612202
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 06312
51637492
00020000 00000-0 20000-3 0 9020
2 25544 51
6315 163
6720 0011850 191
6051 168
4842 15
77794864 15935
Satellite: ISS
Catalog Number: 25544
Epoch time: 06312
51637492 = yrday
fracday
Element set: 902
Inclination: 51
6315 deg
RA of node: 163
6720 deg
Eccentricity:
0011850
Arg of perigee: 191
6051 deg
Mean anomaly: 168
4842 deg
Mean motion: 15
77794864 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1593
Checksum: 297
Coasting Arc #4 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2006/313/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1538638
63 A = 6709174
59 meter
Y = 3865612
87 meter E =
0016584
Z = -5273583
72 I = 51
73077
XDOT = -7127
865682 Wp = 134
07418
YDOT = 2908
740756 meter/sec RA = 157
55832 deg
ZDOT = 41
266775 TA = 136
38263
MA = 136
25142
Ha = 186
546 n
mi
Hp = 177
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5048027
01 X = 1520917
00
Y = 12682456
92 feet Y = 3882720
22 meter
Z = -17301783
86 Z = -5266151
55
XDOT = -23385
386096 XDOT = -7160
062336
YDOT = 9543
112717 feet/sec YDOT = 2828
852986 meter/sec
ZDOT = 135
389681 ZDOT = 6
561105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13212284
05 X = -4027104
18
Y = -3569319
25 feet Y = -1087928
51 meter
Z = -17273520
93 Z = -5264969
18
XDOT = 6274
481578 XDOT = 1912
461985
YDOT = -23434
546605 feet/sec YDOT = -7142
849805 meter/sec
ZDOT = 6
227624 ZDOT = 1
898180
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 06313
52974520
00020000 00000-0 20000-3 0 9039
2 25544 51
6305 158
4362 0011858 195
1852 164
8959 15
77841967 16098
Satellite: ISS
Catalog Number: 25544
Epoch time: 06313
52974520 = yrday
fracday
Element set: 903
Inclination: 51
6305 deg
RA of node: 158
4362 deg
Eccentricity:
0011858
Arg of perigee: 195
1852 deg
Mean anomaly: 164
8959 deg
Mean motion: 15
77841967 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1609
Checksum: 319
Coasting Arc #5 (Orbit 1624)
---------------------------------------
Vector Time (GMT): 2006/314/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6237801
11 A = 6720503
64 meter
Y = -2087531
00 meter E =
0018410
Z = -1319098
95 I = 51
79535
XDOT = 432
460591 Wp = 175
55701
YDOT = 4986
932610 meter/sec RA = 152
41561 deg
ZDOT = -5870
398782 TA = 18
93335
MA = 18
86499
Ha = 186
393 n
mi
Hp = 177
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20465226
75 X = 6267088
59
Y = -6848854
98 feet Y = -2017612
58 meter
Z = -4327752
45 Z = -1288724
37
XDOT = 1418
833960 XDOT = 405
181567
YDOT = 16361
327460 feet/sec YDOT = 4991
616617 meter/sec
ZDOT = -19259
838522 ZDOT = -5868
363683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6576828
13 X = -2004617
21
Y = 20577754
05 feet Y = 6272099
43 meter
Z = -4214633
05 Z = -1284620
15
XDOT = -12602
218879 XDOT = -3841
156314
YDOT = -7954
644776 feet/sec YDOT = -2424
575728 meter/sec
ZDOT = -19251
571427 ZDOT = -5867
878971
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 06314
54309609
00020000 00000-0 20000-3 0 9043
2 25544 51
6308 153
2022 0011836 199
4313 160
6403 15
77858835 16250
Satellite: ISS
Catalog Number: 25544
Epoch time: 06314
54309609 = yrday
fracday
Element set: 904
Inclination: 51
6308 deg
RA of node: 153
2022 deg
Eccentricity:
0011836
Arg of perigee: 199
4313 deg
Mean anomaly: 160
6403 deg
Mean motion: 15
77858835 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1625
Checksum: 285
Coasting Arc #6 (Orbit 1640)
---------------------------------------
Vector Time (GMT): 2006/315/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 720153
08 A = 6711730
55 meter
Y = -4799192
38 meter E =
0007712
Z = 4630911
72 I = 51
79071
XDOT = 6928
767671 Wp = 161
17747
YDOT = -1749
331093 meter/sec RA = 147
22603 deg
ZDOT = -2896
224977 TA = 317
34877
MA = 317
40862
Ha = 186
158 n
mi
Hp = 177
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2362706
96 X = 751268
43
Y = -15745381
81 feet Y = -4790965
58 meter
Z = 15193279
92 Z = 4634485
50
XDOT = 22732
177398 XDOT = 6961
883454
YDOT = -5739
275241 feet/sec YDOT = -1671
664406 meter/sec
ZDOT = -9502
050448 ZDOT = -2862
484360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11548645
61 X = 3520027
18
Y = 10942676
20 feet Y = 3335327
70 meter
Z = 15205979
40 Z = 4634782
52
XDOT = -7654
344584 XDOT = -2333
044229
YDOT = 21080
991168 feet/sec YDOT = 6425
486108 meter/sec
ZDOT = -9376
305336 ZDOT = -2857
897867
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 06315
55642696
00020000 00000-0 20000-3 0 9052
2 25544 51
6307 147
9665 0011885 203
5559 156
5063 15
77888383 16410
Satellite: ISS
Catalog Number: 25544
Epoch time: 06315
55642696 = yrday
fracday
Element set: 905
Inclination: 51
6307 deg
RA of node: 147
9665 deg
Eccentricity:
0011885
Arg of perigee: 203
5559 deg
Mean anomaly: 156
5063 deg
Mean motion: 15
77888383 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1641
Checksum: 324
Coasting Arc #7 (Orbit 1656)
---------------------------------------
Vector Time (GMT): 2006/316/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5623354
61 A = 6715460
35 meter
Y = 801681
42 meter E =
0013129
Z = 3587044
97 I = 51
82619
XDOT = 1991
621982 Wp = 149
68442
YDOT = -5970
287522 meter/sec RA = 142
11949 deg
ZDOT = 4438
430641 TA = 253
09658
MA = 253
24057
Ha = 185
927 n
mi
Hp = 177
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18449326
14 X = -5649326
57
Y = 2630188
39 feet Y = 738652
55 meter
Z = 11768520
24 Z = 3559663
40
XDOT = 6534
192854 XDOT = 2036
673240
YDOT = -19587
557487 feet/sec YDOT = -5947
764437 meter/sec
ZDOT = 14561
780319 ZDOT = 4448
215157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8241829
17 X = 2512109
53
Y = -16785749
17 feet Y = -5116296
35 meter
Z = 11666382
12 Z = 3555913
27
XDOT = 11338
704475 XDOT = 3456
037124
YDOT = 15754
534699 feet/sec YDOT = 4801
982176 meter/sec
ZDOT = 14597
514959 ZDOT = 4449
322560
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 06316
56973762
00020000 00000-0 20000-3 0 9066
2 25544 51
6300 142
7304 0011936 207
4930 152
5605 15
77946541 16575
Satellite: ISS
Catalog Number: 25544
Epoch time: 06316
56973762 = yrday
fracday
Element set: 906
Inclination: 51
6300 deg
RA of node: 142
7304 deg
Eccentricity:
0011936
Arg of perigee: 207
4930 deg
Mean anomaly: 152
5605 deg
Mean motion: 15
77946541 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1657
Checksum: 293
Coasting Arc #8 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2006/317/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2604069
44 A = 6717357
40 meter
Y = 5501388
50 meter E =
0008398
Z = -2851233
82 I = 51
85461
XDOT = -5769
736638 Wp = 192
86527
YDOT = -84
170754 meter/sec RA = 136
91710 deg
ZDOT = 5096
292463 TA = 134
49199
MA = 134
42331
Ha = 185
720 n
mi
Hp = 178
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8543534
91 X = -2651542
26
Y = 18049174
88 feet Y = 5472003
02 meter
Z = -9354441
67 Z = -2863999
65
XDOT = -18929
582146 XDOT = -5793
123761
YDOT = -276
150769 feet/sec YDOT = -148
822098 meter/sec
ZDOT = 16720
119628 ZDOT = 5068
205948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10438171
64 X = -3181554
72
Y = -16997911
44 feet Y = -5180963
41 meter
Z = -9401375
48 Z = -2865539
25
XDOT = 9421
242276 XDOT = 2871
594646
YDOT = -14994
804604 feet/sec YDOT = -4570
416443 meter/sec
ZDOT = 16615
222783 ZDOT = 5064
319904
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 06317
51970005
00020000 00000-0 20000-3 0 9070
2 25544 51
6300 137
8215 0011853 210
2466 149
8016 15
77955644 16721
Satellite: ISS
Catalog Number: 25544
Epoch time: 06317
51970005 = yrday
fracday
Element set: 907
Inclination: 51
6300 deg
RA of node: 137
8215 deg
Eccentricity:
0011853
Arg of perigee: 210
2466 deg
Mean anomaly: 149
8016 deg
Mean motion: 15
77955644 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1672
Checksum: 283
Coasting Arc #9 (Orbit 1687)
---------------------------------------
Vector Time (GMT): 2006/318/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4326208
56 A = 6709915
91 meter
Y = 1075997
25 meter E =
0009060
Z = -5018416
23 I = 51
84976
XDOT = -3778
304771 Wp = 136
18976
YDOT = 6444
681311 meter/sec RA = 131
80605 deg
ZDOT = -1883
761083 TA = 115
74245
MA = 115
64891
Ha = 185
534 n
mi
Hp = 178
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14193597
65 X = 4338233
99
Y = 3530174
70 feet Y = 1124442
67 meter
Z = -16464620
17 Z = -4997369
96
XDOT = -12396
013029 XDOT = -3840
938180
YDOT = 21143
967555 feet/sec YDOT = 6402
080056 meter/sec
ZDOT = -6180
318514 ZDOT = -1902
268335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10610742
87 X = -3234154
43
Y = 10194078
28 feet Y = 3107155
06 meter
Z = -16385877
12 Z = -4994415
35
XDOT = -10536
608123 XDOT = -3211
558156
YDOT = -20966
593295 feet/sec YDOT = -6390
617636 meter/sec
ZDOT = -6248
571740 ZDOT = -1904
564666
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 06318
53297288
00020000 00000-0 20000-3 0 9089
2 25544 51
6301 132
5867 0011710 213
7200 146
3221 15
77999206 16882
Satellite: ISS
Catalog Number: 25544
Epoch time: 06318
53297288 = yrday
fracday
Element set: 908
Inclination: 51
6301 deg
RA of node: 132
5867 deg
Eccentricity:
0011710
Arg of perigee: 213
7200 deg
Mean anomaly: 146
3221 deg
Mean motion: 15
77999206 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1688
Checksum: 293
Coasting Arc #10 (Orbit 1703)
---------------------------------------
Vector Time (GMT): 2006/319/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3790993
93 A = 6720613
10 meter
Y = -5525326
93 meter E =
0017748
Z = 325496
62 I = 51
90420
XDOT = 4096
637836 Wp = 172
58678
YDOT = 2452
640594 meter/sec RA = 126
63698 deg
ZDOT = -6059
925507 TA = 3
87861
MA = 3
86487
Ha = 185
103 n
mi
Hp = 178
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12437644
12 X = 3850915
92
Y = -18127713
04 feet Y = -5482598
90 meter
Z = 1067902
29 Z = 344059
05
XDOT = 13440
412849 XDOT = 4098
346164
YDOT = 8046
721108 feet/sec YDOT = 2498
461146 meter/sec
ZDOT = -19881
645364 ZDOT = -6040
019472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9038116
18 X = 2754817
81
Y = 20036722
07 feet Y = 6107192
89 meter
Z = 1136490
86 Z = 346402
41
XDOT = -12451
535531 XDOT = -3795
228030
YDOT = 6743
400215 feet/sec YDOT = 2055
388386 meter/sec
ZDOT = -19806
974194 ZDOT = -6037
165734
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 06319
54622363
00020000 00000-0 20000-3 0 9098
2 25544 51
6298 127
3504 0011636 219
1215 140
9110 15
78057635 17048
Satellite: ISS
Catalog Number: 25544
Epoch time: 06319
54622363 = yrday
fracday
Element set: 909
Inclination: 51
6298 deg
RA of node: 127
3504 deg
Eccentricity:
0011636
Arg of perigee: 219
1215 deg
Mean anomaly: 140
9110 deg
Mean motion: 15
78057635 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1704
Checksum: 278
Coasting Arc #11 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2006/320/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2792198
48 A = 6709150
16 meter
Y = -3224938
74 meter E =
0007926
Z = 5181138
37 I = 51
88071
XDOT = 4732
017703 Wp = 214
33070
YDOT = -5967
420355 meter/sec RA = 121
48150 deg
ZDOT = -1171
462608 TA = 246
76968
MA = 246
85317
Ha = 185
139 n
mi
Hp = 178
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9160756
17 X = -2781098
85
Y = -10580507
68 feet Y = -3256100
72 meter
Z = 16998485
48 Z = 5167600
45
XDOT = 15524
992465 XDOT = 4804
085418
YDOT = -19578
150771 feet/sec YDOT = -5914
101328 meter/sec
ZDOT = -3843
381259 ZDOT = -1148
299025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13804198
78 X = 4207519
79
Y = -2653600
86 feet Y = -808817
54 meter
Z = 16947495
49 Z = 5165596
62
XDOT = 8869
234997 XDOT = 2703
342827
YDOT = 22292
474733 feet/sec YDOT = 6794
746299 meter/sec
ZDOT = -3757
659013 ZDOT = -1145
334467
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 06320
55945838
00020000 00000-0 20000-3 0 9108
2 25544 51
6295 122
1142 0011636 221
3847 138
6438 15
78001694 17201
Satellite: ISS
Catalog Number: 25544
Epoch time: 06320
55945838 = yrday
fracday
Element set: 910
Inclination: 51
6295 deg
RA of node: 122
1142 deg
Eccentricity:
0011636
Arg of perigee: 221
3847 deg
Mean anomaly: 138
6438 deg
Mean motion: 15
78001694 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1720
Checksum: 281
Coasting Arc #12 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2006/321/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4308876
36 A = 6718238
41 meter
Y = 4605317
63 meter E =
0006437
Z = 2317878
14 I = 51
92689
XDOT = -2323
303527 Wp = 129
15335
YDOT = -4922
844810 meter/sec RA = 116
36331 deg
ZDOT = 5448
085823 TA = 256
83579
MA = 256
90761
Ha = 184
727 n
mi
Hp = 178
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14136733
47 X = -4371313
55
Y = 15109309
82 feet Y = 4556784
20 meter
Z = 7604587
08 Z = 2296793
56
XDOT = -7622
386898 XDOT = -2294
549437
YDOT = -16151
065651 feet/sec YDOT = -4948
664695 meter/sec
ZDOT = 17874
297321 ZDOT = 5436
868590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6234702
52 X = -1900337
33
Y = -19759792
49 feet Y = -6022784
75 meter
Z = 7526440
51 Z = 2294059
07
XDOT = 16422
460780 XDOT = 5005
566046
YDOT = 1628
034872 feet/sec YDOT = 496
225029 meter/sec
ZDOT = 17831
754114 ZDOT = 5435
118654
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 06321
57266728
00020000 00000-0 20000-3 0 9116
2 25544 51
6304 116
8779 0011755 225
6788 134
3414 15
78101669 17368
Satellite: ISS
Catalog Number: 25544
Epoch time: 06321
57266728 = yrday
fracday
Element set: 911
Inclination: 51
6304 deg
RA of node: 116
8779 deg
Eccentricity:
0011755
Arg of perigee: 225
6788 deg
Mean anomaly: 134
3414 deg
Mean motion: 15
78101669 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1736
Checksum: 306
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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