Date:
June 22nd 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) : 82 1 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 1127)
---------------------------------------
Vector Time (GMT): 2007/171/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1188768
62 A = 6718578
39 meter
Y = -6312048
24 meter E =
0002698
Z = -1976878
95 I = 51
96697
XDOT = 4557
799695 Wp = 33
33906
YDOT = 2620
135451 meter/sec RA = 86
73494 deg
ZDOT = -5626
553321 TA = 168
59049
MA = 168
58437
Ha = 184
645 n
mi
Hp = 177
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3900159
52 X = 1268865
73
Y = -20708819
70 feet Y = -6298306
62 meter
Z = -6485823
32 Z = -1970910
36
XDOT = 14953
411072 XDOT = 4555
494696
YDOT = 8596
244917 feet/sec YDOT = 2671
091278 meter/sec
ZDOT = -18459
820608 ZDOT = -5604
416970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11076379
86 X = -3376080
58
Y = -17934971
98 feet Y = -5466579
46 meter
Z = -6463973
33 Z = -1970219
07
XDOT = 15603
106007 XDOT = 4755
826711
YDOT = -3015
044196 feet/sec YDOT = -918
985471 meter/sec
ZDOT = -18375
839038 ZDOT = -5600
955739
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 07171
40281764
00020000 00000-0 20000-3 0 9007
2 25544 51
6322 87
2947 0008074 339
3520 20
7318 15
78191165 11289
Satellite: ISS
Catalog Number: 25544
Epoch time: 07171
40281764 = yrday
fracday
Element set: 900
Inclination: 51
6322 deg
RA of node: 87
2947 deg
Eccentricity:
0008074
Arg of perigee: 339
3520 deg
Mean anomaly: 20
7318 deg
Mean motion: 15
78191165 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1128
Checksum: 278
Coasting Arc #2 (Orbit 1143)
---------------------------------------
Vector Time (GMT): 2007/172/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3852327
28 A = 6712571
64 meter
Y = -3545324
80 meter E =
0012873
Z = 4201608
22 I = 51
94396
XDOT = 1944
636903 Wp = 34
98619
YDOT = -6487
375743 meter/sec RA = 81
54638 deg
ZDOT = -3675
245797 TA = 92
36942
MA = 92
22203
Ha = 184
771 n
mi
Hp = 177
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12638869
02 X = -3832807
12
Y = -11631643
05 feet Y = -3588295
11 meter
Z = 13784803
88 Z = 4182940
69
XDOT = 6380
042332 XDOT = 2034
888705
YDOT = -21284
041151 feet/sec YDOT = -6465
124599 meter/sec
ZDOT = -12057
893034 ZDOT = -3665
580480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17230727
36 X = -5251925
70
Y = 299718
67 feet Y = 91354
25 meter
Z = 13713830
66 Z = 4179975
58
XDOT = -9933
919195 XDOT = -3027
858571
YDOT = -18629
695851 feet/sec YDOT = -5678
331295 meter/sec
ZDOT = -12022
084171 ZDOT = -3664
331255
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 07172
41594651
00020000 00000-0 20000-3 0 9012
2 25544 51
6322 82
0587 0008119 342
6263 17
4623 15
78217481 11443
Satellite: ISS
Catalog Number: 25544
Epoch time: 07172
41594651 = yrday
fracday
Element set: 901
Inclination: 51
6322 deg
RA of node: 82
0587 deg
Eccentricity:
0008119
Arg of perigee: 342
6263 deg
Mean anomaly: 17
4623 deg
Mean motion: 15
78217481 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1144
Checksum: 277
Coasting Arc #3 (Orbit 1159)
---------------------------------------
Vector Time (GMT): 2007/173/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2242289
51 A = 6712396
71 meter
Y = 4724879
05 meter E =
0009210
Z = 4197769
87 I = 51
93906
XDOT = -4240
620794 Wp = 57
52566
YDOT = -5285
902440 meter/sec RA = 76
45048 deg
ZDOT = 3683
505782 TA = 355
12989
MA = 355
13884
Ha = 184
817 n
mi
Hp = 177
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7356592
88 X = -2315349
08
Y = 15501571
70 feet Y = 4699395
47 meter
Z = 13772210
88 Z = 4186700
03
XDOT = -13912
797882 XDOT = -4199
091629
YDOT = -17342
199605 feet/sec YDOT = -5333
091724 meter/sec
ZDOT = 12084
992723 ZDOT = 3663
005095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5544061
60 X = 1689829
98
Y = 16273230
39 feet Y = 4960080
62 meter
Z = 13730889
63 Z = 4185175
16
XDOT = -20937
022292 XDOT = -6381
604395
YDOT = -3000
799456 feet/sec YDOT = -914
643674 meter/sec
ZDOT = 12006
894977 ZDOT = 3659
701589
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 07173
42905849
00020000 00000-0 20000-3 0 9020
2 25544 51
6329 76
8227 0008017 345
6486 14
4450 15
78265618 11607
Satellite: ISS
Catalog Number: 25544
Epoch time: 07173
42905849 = yrday
fracday
Element set: 902
Inclination: 51
6329 deg
RA of node: 76
8227 deg
Eccentricity:
0008017
Arg of perigee: 345
6486 deg
Mean anomaly: 14
4450 deg
Mean motion: 15
78265618 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1160
Checksum: 299
Coasting Arc #4 (Orbit 1174)
---------------------------------------
Vector Time (GMT): 2007/174/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3464319
87 A = 6718451
52 meter
Y = 5397007
29 meter E =
0013716
Z = -1976305
26 I = 51
95094
XDOT = -3250
808987 Wp = 12
07065
YDOT = 4142
291175 meter/sec RA = 71
26039 deg
ZDOT = 5633
649539 TA = 325
96864
MA = 326
05652
Ha = 185
019 n
mi
Hp = 177
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11365878
84 X = 3413312
81
Y = 17706716
84 feet Y = 5435462
34 meter
Z = -6483941
16 Z = -1959598
75
XDOT = -10665
383816 XDOT = -3324
254348
YDOT = 13590
194143 feet/sec YDOT = 4105
527388 meter/sec
ZDOT = 18483
102161 ZDOT = 5617
679260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20614969
90 X = 6283442
83
Y = 4307763
59 feet Y = 1313006
34 meter
Z = -6420179
51 Z = -1956870
71
XDOT = 2434
905723 XDOT = 742
159264
YDOT = 15705
957977 feet/sec YDOT = 4787
175991 meter/sec
ZDOT = 18423
184202 ZDOT = 5615
386545
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 07174
37883877
00020000 00000-0 20000-3 0 9032
2 25544 51
6326 71
9134 0008203 349
7130 10
3866 15
78242813 11759
Satellite: ISS
Catalog Number: 25544
Epoch time: 07174
37883877 = yrday
fracday
Element set: 903
Inclination: 51
6326 deg
RA of node: 71
9134 deg
Eccentricity:
0008203
Arg of perigee: 349
7130 deg
Mean anomaly: 10
3866 deg
Mean motion: 15
78242813 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1175
Checksum: 293
Coasting Arc #5 (Orbit 1190)
---------------------------------------
Vector Time (GMT): 2007/175/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3466175
21 A = 6708072
46 meter
Y = -2346489
28 meter E =
0016762
Z = -5254613
87 I = 51
90667
XDOT = 3572
391095 Wp = 55
54693
YDOT = 6785
311527 meter/sec RA = 66
13615 deg
ZDOT = -665
747299 TA = 208
09815
MA = 208
18872
Ha = 185
035 n
mi
Hp = 176
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11371965
92 X = 3517682
44
Y = -7698455
63 feet Y = -2307439
79 meter
Z = -17239546
81 Z = -5237650
35
XDOT = 11720
443225 XDOT = 3499
485331
YDOT = 22261
520759 feet/sec YDOT = 6824
852471 meter/sec
ZDOT = -2184
210297 ZDOT = -648
568644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2332849
38 X = 711052
49
Y = -13614108
92 feet Y = -4149580
40 meter
Z = -17175670
42 Z = -5235144
34
XDOT = 23219
827851 XDOT = 7077
403529
YDOT = 6683
900695 feet/sec YDOT = 2037
252932 meter/sec
ZDOT = -2118
516307 ZDOT = -645
723770
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 07175
39192137
00020000 00000-0 20000-3 0 9048
2 25544 51
6336 66
6767 0008192 353
3405 6
7650 15
78280328 11917
Satellite: ISS
Catalog Number: 25544
Epoch time: 07175
39192137 = yrday
fracday
Element set: 904
Inclination: 51
6336 deg
RA of node: 66
6767 deg
Eccentricity:
0008192
Arg of perigee: 353
3405 deg
Mean anomaly: 6
7650 deg
Mean motion: 15
78280328 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1191
Checksum: 297
Coasting Arc #6 (Orbit 1206)
---------------------------------------
Vector Time (GMT): 2007/176/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2617661
44 A = 6719612
70 meter
Y = -6128021
18 meter E =
0005942
Z = -871549
97 I = 51
93381
XDOT = 4709
172796 Wp = 87
40271
YDOT = -1165
894573 meter/sec RA = 60
99060 deg
ZDOT = -5980
690702 TA = 102
07844
MA = 102
01185
Ha = 185
095 n
mi
Hp = 176
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8588128
08 X = -2544708
60
Y = -20105056
37 feet Y = -6156885
30 meter
Z = -2859415
92 Z = -884090
45
XDOT = 15450
041981 XDOT = 4750
913285
YDOT = -3825
113427 feet/sec YDOT = -1112
999594 meter/sec
ZDOT = -19621
688654 ZDOT = -5957
712204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20600102
62 X = -6278911
28
Y = -7302584
55 feet Y = -2225827
77 meter
Z = -2907494
78 Z = -886204
41
XDOT = 7186
375471 XDOT = 2190
407243
YDOT = -12538
861086 feet/sec YDOT = -3821
844859 meter/sec
ZDOT = -19534
937767 ZDOT = -5954
249031
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 07176
40498843
00020000 00000-0 20000-3 0 9055
2 25544 51
6344 61
4404 0008203 357
1265 2
9852 15
78302626 12072
Satellite: ISS
Catalog Number: 25544
Epoch time: 07176
40498843 = yrday
fracday
Element set: 905
Inclination: 51
6344 deg
RA of node: 61
4404 deg
Eccentricity:
0008203
Arg of perigee: 357
1265 deg
Mean anomaly: 2
9852 deg
Mean motion: 15
78302626 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1207
Checksum: 279
Coasting Arc #7 (Orbit 1222)
---------------------------------------
Vector Time (GMT): 2007/177/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4708508
87 A = 6710031
23 meter
Y = -269006
76 meter E =
0013609
Z = 4772249
93 I = 51
88639
XDOT = -2240
389976 Wp = 28
84694
YDOT = -6907
369830 meter/sec RA = 55
81281 deg
ZDOT = -2585
108806 TA = 86
46146
MA = 86
30583
Ha = 185
263 n
mi
Hp = 176
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15447863
76 X = -4728333
73
Y = -882568
10 feet Y = -321771
67 meter
Z = 15656987
95 Z = 4749327
64
XDOT = -7350
360814 XDOT = -2150
426173
YDOT = -22661
974508 feet/sec YDOT = -6931
919640 meter/sec
ZDOT = -8481
328103 ZDOT = -2595
775439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10979065
48 X = -3346419
16
Y = 11026461
16 feet Y = 3360865
36 meter
Z = 15570291
21 Z = 4745824
76
XDOT = -20986
840592 XDOT = -6396
789013
YDOT = -8793
720100 feet/sec YDOT = -2680
325887 meter/sec
ZDOT = -8522
398574 ZDOT = -2597
627085
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 07177
41803987
00020000 00000-0 20000-3 0 9067
2 25544 51
6343 56
2044 0008252
8759 359
2420 15
78331117 12231
Satellite: ISS
Catalog Number: 25544
Epoch time: 07177
41803987 = yrday
fracday
Element set: 906
Inclination: 51
6343 deg
RA of node: 56
2044 deg
Eccentricity:
0008252
Arg of perigee:
8759 deg
Mean anomaly: 359
2420 deg
Mean motion: 15
78331117 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1223
Checksum: 280
Coasting Arc #8 (Orbit 1238)
---------------------------------------
Vector Time (GMT): 2007/178/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1103939
37 A = 6714577
58 meter
Y = 5635807
77 meter E =
0015225
Z = 3460305
27 I = 51
88503
XDOT = -5987
939465 Wp = 58
52902
YDOT = -1643
548266 meter/sec RA = 50
70741 deg
ZDOT = 4580
331604 TA = 342
46340
MA = 342
51592
Ha = 185
285 n
mi
Hp = 176
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3621848
32 X = 1024027
27
Y = 18490182
97 feet Y = 5647705
12 meter
Z = 11352707
58 Z = 3465475
28
XDOT = -19645
470685 XDOT = -5991
366564
YDOT = -5392
218720 feet/sec YDOT = -1710
528858 meter/sec
ZDOT = 15027
334660 ZDOT = 4551
233379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16348259
00 X = 4982949
34
Y = 9342444
58 feet Y = 2847577
11 meter
Z = 11372852
67 Z = 3466445
49
XDOT = -16260
086067 XDOT = -4956
074233
YDOT = 10266
971299 feet/sec YDOT = 3129
372852 meter/sec
ZDOT = 14917
136748 ZDOT = 4546
743281
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 07178
43107609
00020000 00000-0 20000-3 0 9079
2 25544 51
6346 50
9674 0008284 4
7277 355
3965 15
78346791 12399
Satellite: ISS
Catalog Number: 25544
Epoch time: 07178
43107609 = yrday
fracday
Element set: 907
Inclination: 51
6346 deg
RA of node: 50
9674 deg
Eccentricity:
0008284
Arg of perigee: 4
7277 deg
Mean anomaly: 355
3965 deg
Mean motion: 15
78346791 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1239
Checksum: 320
Coasting Arc #9 (Orbit 1253)
---------------------------------------
Vector Time (GMT): 2007/179/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5555096
06 A = 6716149
54 meter
Y = 2418266
10 meter E =
0011535
Z = -2889209
52 I = 51
87172
XDOT = 108
158610 Wp = 26
87236
YDOT = 5797
787794 meter/sec RA = 45
50555 deg
ZDOT = 5078
587835 TA = 299
95315
MA = 300
06762
Ha = 185
381 n
mi
Hp = 176
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18225380
77 X = 5541677
07
Y = 7933943
91 feet Y = 2480311
91 meter
Z = -9479033
85 Z = -2862254
86
XDOT = 354
851083 XDOT = 18
647949
YDOT = 19021
613497 feet/sec YDOT = 5798
495692 meter/sec
ZDOT = 16662
033580 ZDOT = 5078
897120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17772607
95 X = 5417090
90
Y = -9009607
83 feet Y = -2746128
47 meter
Z = -9376855
89 Z = -2858065
67
XDOT = 14154
944840 XDOT = 4314
427187
YDOT = 10641
129923 feet/sec YDOT = 3243
416401 meter/sec
ZDOT = 16663
810246 ZDOT = 5079
129363
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 07179
38078296
00020000 00000-0 20000-3 0 9084
2 25544 51
6351 46
0581 0008279 7
8119 352
3174 15
78384185 12546
Satellite: ISS
Catalog Number: 25544
Epoch time: 07179
38078296 = yrday
fracday
Element set: 908
Inclination: 51
6351 deg
RA of node: 46
0581 deg
Eccentricity:
0008279
Arg of perigee: 7
8119 deg
Mean anomaly: 352
3174 deg
Mean motion: 15
78384185 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1254
Checksum: 312
Coasting Arc #10 (Orbit 1269)
---------------------------------------
Vector Time (GMT): 2007/180/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1069886
91 A = 6708541
64 meter
Y = -4302655
01 meter E =
0018610
Z = -5050158
71 I = 51
82577
XDOT = 6506
495193 Wp = 52
49571
YDOT = 3705
983269 meter/sec RA = 40
38971 deg
ZDOT = -1772
360794 TA = 200
42977
MA = 200
50431
Ha = 185
368 n
mi
Hp = 175
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3510127
64 X = 1142453
01
Y = -14116322
22 feet Y = -4290284
04 meter
Z = -16568762
18 Z = -5044785
93
XDOT = 21346
769006 XDOT = 6473
180555
YDOT = 12158
737760 feet/sec YDOT = 3778
556683 meter/sec
ZDOT = -5814
832002 ZDOT = -1740
832377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8770623
46 X = -2673286
03
Y = -11632960
98 feet Y = -3545726
51 meter
Z = -16548891
56 Z = -5044102
15
XDOT = 22002
757837 XDOT = 6706
440589
YDOT = -8455
811864 feet/sec YDOT = -2577
331456 meter/sec
ZDOT = -5695
219336 ZDOT = -1735
902854
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 07180
39378888
00020000 00000-0 20000-3 0 9098
2 25544 51
6356 40
8213 0008356 11
6640 348
4718 15
78420022 12702
Satellite: ISS
Catalog Number: 25544
Epoch time: 07180
39378888 = yrday
fracday
Element set: 909
Inclination: 51
6356 deg
RA of node: 40
8213 deg
Eccentricity:
0008356
Arg of perigee: 11
6640 deg
Mean anomaly: 348
4718 deg
Mean motion: 15
78420022 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1270
Checksum: 292
Coasting Arc #11 (Orbit 1285)
---------------------------------------
Vector Time (GMT): 2007/181/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5521054
63 A = 6719675
06 meter
Y = -3828820
77 meter E =
0010996
Z = 71258
06 I = 51
84018
XDOT = 2652
444976 Wp = 93
23125
YDOT = -3952
281615 meter/sec RA = 35
21860 deg
ZDOT = -6055
716153 TA = 85
99594
MA = 85
87025
Ha = 185
441 n
mi
Hp = 175
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18113696
30 X = -5478176
02
Y = -12561747
93 feet Y = -3890320
57 meter
Z = 233786
28 Z = 44540
24
XDOT = 8702
247297 XDOT = 2725
860187
YDOT = -12966
803199 feet/sec YDOT = -3922
208614 meter/sec
ZDOT = -19867
835146 ZDOT = -6042
653247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21014754
80 X = -6405297
26
Y = 6657381
26 feet Y = 2029169
81 meter
Z = 132347
19 Z = 40339
42
XDOT = -4389
106978 XDOT = -1337
799807
YDOT = -13368
923034 feet/sec YDOT = -4074
847741 meter/sec
ZDOT = -19818
841983 ZDOT = -6040
783036
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 07181
40678019
00020000 00000-0 20000-3 0 9102
2 25544 51
6355 35
5840 0008248 15
0780 345
0630 15
78402195 12865
Satellite: ISS
Catalog Number: 25544
Epoch time: 07181
40678019 = yrday
fracday
Element set: 910
Inclination: 51
6355 deg
RA of node: 35
5840 deg
Eccentricity:
0008248
Arg of perigee: 15
0780 deg
Mean anomaly: 345
0630 deg
Mean motion: 15
78402195 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1286
Checksum: 279
Coasting Arc #12 (Orbit 1301)
---------------------------------------
Vector Time (GMT): 2007/182/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3547336
29 A = 6708216
62 meter
Y = 2568381
71 meter E =
0012792
Z = 5078346
12 I = 51
77786
XDOT = -5803
346753 Wp = 30
67116
YDOT = -4817
196956 meter/sec RA = 30
04784 deg
ZDOT = -1604
896609 TA = 74
76205
MA = 74
62065
Ha = 185
506 n
mi
Hp = 175
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11638242
41 X = -3600462
05
Y = 8426449
19 feet Y = 2528415
25 meter
Z = 16661240
54 Z = 5060984
88
XDOT = -19039
851551 XDOT = -5741
252632
YDOT = -15804
451956 feet/sec YDOT = -4881
745698 meter/sec
ZDOT = -5265
408823 ZDOT = -1632
939167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -254062
42 X = -77438
23
Y = 14441747
62 feet Y = 4401844
67 meter
Z = 16595844
27 Z = 5058413
33
XDOT = -22979
082517 XDOT = -7004
024351
YDOT = 5816
537073 feet/sec YDOT = 1772
880500 meter/sec
ZDOT = -5371
967034 ZDOT = -1637
375552
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 07182
41975357
00020000 00000-0 20000-3 0 9110
2 25544 51
6354 30
3467 0008405 17
4197 342
7255 15
78492893 13025
Satellite: ISS
Catalog Number: 25544
Epoch time: 07182
41975357 = yrday
fracday
Element set: 911
Inclination: 51
6354 deg
RA of node: 30
3467 deg
Eccentricity:
0008405
Arg of perigee: 17
4197 deg
Mean anomaly: 342
7255 deg
Mean motion: 15
78492893 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1302
Checksum: 297
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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