Date:
June 18th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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
171/06:52:31
233 9
6 11
3 11
4
N/A -3
1 0
1 186
8
000/00:19:02
466 -5
1 0
2 186
2
Coasting Arc #1 (Orbit 2841)
---------------------------------------
Vector Time (GMT): 2008/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1494715
34 A = 6713854
08 meter
Y = -4507150
27 meter E =
0012509
Z = -4757185
98 I = 51
73507
XDOT = 7229
688977 Wp = 40
97885
YDOT = 366
682718 meter/sec RA = 19
44898 deg
ZDOT = -2613
588693 TA = 203
36568
MA = 203
42257
Ha = 185
900 n
mi
Hp = 179
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4903921
70 X = -1421094
83
Y = -14787238
42 feet Y = -4523452
45 meter
Z = -15607565
57 Z = -4764269
45
XDOT = 23719
452025 XDOT = 7237
747793
YDOT = 1203
027290 feet/sec YDOT = 447
574819 meter/sec
ZDOT = -8574
766052 ZDOT = -2578
446905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15187984
57 X = -4629297
70
Y = 3342626
26 feet Y = 1018832
48 meter
Z = -15635182
94 Z = -4765603
76
XDOT = 3770
079512 XDOT = 1149
120235
YDOT = -22428
130892 feet/sec YDOT = -6836
094296 meter/sec
ZDOT = -8439
441069 ZDOT = -2572
341638
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 08168
52029744
00020000 00000-0 20000-3 0 9005
2 25544 51
6396 19
8295 0006367 334
5059 25
5791 15
76967779 28426
Satellite: ISS
Catalog Number: 25544
Epoch time: 08168
52029744 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 19
8295 deg
Eccentricity:
0006367
Arg of perigee: 334
5059 deg
Mean anomaly: 25
5791 deg
Mean motion: 15
76967779 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2842
Checksum: 333
Coasting Arc #2 (Orbit 2857)
---------------------------------------
Vector Time (GMT): 2008/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6561945
65 A = 6722878
22 meter
Y = -588783
33 meter E =
0009724
Z = 1326628
59 I = 51
73821
XDOT = -746
011833 Wp = 96
28651
YDOT = -4952
152092 meter/sec RA = 14
26493 deg
ZDOT = -5852
433847 TA = 69
15294
MA = 69
04883
Ha = 186
004 n
mi
Hp = 179
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21528693
08 X = -6561318
64
Y = -1931703
84 feet Y = -662159
54 meter
Z = 4352456
00 Z = 1294751
87
XDOT = -2447
545385 XDOT = -662
150425
YDOT = -16247
218149 feet/sec YDOT = -4960
024292 meter/sec
ZDOT = -19200
898447 ZDOT = -5855
855340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3668185
23 X = -1118062
86
Y = 21326373
33 feet Y = 6500278
59 meter
Z = 4229680
39 Z = 1289206
58
XDOT = -14828
036145 XDOT = -4519
585417
YDOT = 1284
099747 feet/sec YDOT = 391
393603 meter/sec
ZDOT = -19214
447598 ZDOT = -5856
563628
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 08169
53420817
00020000 00000-0 20000-3 0 9014
2 25544 51
6401 14
5995 0006469 338
8758 21
2139 15
77018311 28584
Satellite: ISS
Catalog Number: 25544
Epoch time: 08169
53420817 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 14
5995 deg
Eccentricity:
0006469
Arg of perigee: 338
8758 deg
Mean anomaly: 21
2139 deg
Mean motion: 15
77018311 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2858
Checksum: 300
Coasting Arc #3 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2008/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -250131
36 A = 6711624
82 meter
Y = 4167277
15 meter E =
0005401
Z = 5254511
16 I = 51
67020
XDOT = -7641
958196 Wp = 5
00921
YDOT = -926
357275 meter/sec RA = 9
12569 deg
ZDOT = 376
155996 TA = 81
45430
MA = 81
39311
Ha = 186
159 n
mi
Hp = 179
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -820640
96 X = -322237
42
Y = 13672169
13 feet Y = 4164075
73 meter
Z = 17239209
85 Z = 5253121
78
XDOT = -25072
041326 XDOT = -7632
858855
YDOT = -3039
229904 feet/sec YDOT = -1011
763231 meter/sec
ZDOT = 1234
107597 ZDOT = 339
053198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13585956
19 X = 4140999
45
Y = 1788026
74 feet Y = 544990
55 meter
Z = 17234174
52 Z = 5252976
39
XDOT = -4500
302297 XDOT = -1371
692140
YDOT = 23843
411269 feet/sec YDOT = 7267
471755 meter/sec
ZDOT = 1091
179133 ZDOT = 332
591400
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 08170
54810481
00020000 00000-0 20000-3 0 9028
2 25544 51
6391 9
3682 0006351 342
5070 17
5875 15
76989413 28748
Satellite: ISS
Catalog Number: 25544
Epoch time: 08170
54810481 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 9
3682 deg
Eccentricity:
0006351
Arg of perigee: 342
5070 deg
Mean anomaly: 17
5875 deg
Mean motion: 15
76989413 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2874
Checksum: 298
Coasting Arc #4 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2008/171/07:02:02
466
Vector Time (MET): N/A
Weight (LBS) : 661038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 592665
98 A = 6718465
15 meter
Y = -4132509
24 meter E =
0005618
Z = -5268729
42 I = 51
64927
XDOT = 7649
903609 Wp = 88
16827
YDOT = 836
463568 meter/sec RA = 5
03357 deg
ZDOT = 204
804353 TA = 183
77368
MA = 183
77792
Ha = 186
838 n
mi
Hp = 186
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1944442
19 X = 664426
78
Y = -13558101
20 feet Y = -4125479
33 meter
Z = -17285857
68 Z = -5265676
85
XDOT = 25098
108954 XDOT = 7638
986683
YDOT = 2744
303045 feet/sec YDOT = 921
948085 meter/sec
ZDOT = 671
930291 ZDOT = 241
941191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -973289
49 X = -296658
64
Y = -13676663
91 feet Y = -4168647
16 meter
Z = -17274414
93 Z = -5265241
67
XDOT = 24088
932026 XDOT = 7342
306482
YDOT = -2742
140976 feet/sec YDOT = -835
804569 meter/sec
ZDOT = 814
988173 ZDOT = 248
408395
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 08171
30853553
00020000 00000-0 20000-3 0 9031
2 25544 51
6413 5
4475 0009429 273
9651 86
0434 15
74579497 28861
Satellite: ISS
Catalog Number: 25544
Epoch time: 08171
30853553 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 5
4475 deg
Eccentricity:
0009429
Arg of perigee: 273
9651 deg
Mean anomaly: 86
0434 deg
Mean motion: 15
74579497 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2886
Checksum: 314
Coasting Arc #5 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2008/172/07:02:02
466
Vector Time (MET): N/A
Weight (LBS) : 661038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6707618
13 A = 6730495
12 meter
Y = -297047
57 meter E =
0007493
Z = -390297
42 I = 51
66064
XDOT = 562
533306 Wp = 194
14006
YDOT = -4765
120317 meter/sec RA = 359
90069 deg
ZDOT = -6023
932497 TA = 350
10300
MA = 350
11775
Ha = 187
370 n
mi
Hp = 186
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22006621
17 X = -6701901
99
Y = -974565
51 feet Y = -372023
95 meter
Z = -1280503
35 Z = -422869
03
XDOT = 1845
581713 XDOT = 645
038827
YDOT = -15633
596841 feet/sec YDOT = -4758
367157 meter/sec
ZDOT = -19763
558062 ZDOT = -6021
000332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21609446
83 X = -6586559
39
Y = 4235086
86 feet Y = 1290854
48 meter
Z = -1405947
77 Z = -428532
88
XDOT = -1470
835989 XDOT = -448
310810
YDOT = -14079
254291 feet/sec YDOT = -4291
356708 meter/sec
ZDOT = -19752
626888 ZDOT = -6020
600675
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 08172
32399557
00020000 00000-0 20000-3 0 9044
2 25544 51
6415
2281 0009499 277
4183 82
5901 15
74563747 29027
Satellite: ISS
Catalog Number: 25544
Epoch time: 08172
32399557 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node:
2281 deg
Eccentricity:
0009499
Arg of perigee: 277
4183 deg
Mean anomaly: 82
5901 deg
Mean motion: 15
74563747 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2902
Checksum: 303
Coasting Arc #6 (Orbit 2917)
---------------------------------------
Vector Time (GMT): 2008/173/07:02:02
466
Vector Time (MET): N/A
Weight (LBS) : 661038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -396874
83 A = 6718445
40 meter
Y = 4202648
97 meter E =
0007565
Z = 5232757
14 I = 51
59152
XDOT = -7663
940183 Wp = 297
10671
YDOT = 148
594809 meter/sec RA = 354
74925 deg
ZDOT = -697
993730 TA = 159
55392
MA = 159
52363
Ha = 187
700 n
mi
Hp = 186
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1302082
78 X = -469259
58
Y = 13788218
42 feet Y = 4197805
13 meter
Z = 17167838
38 Z = 5230654
15
XDOT = -25144
160704 XDOT = -7661
641496
YDOT = 487
515777 feet/sec YDOT = 62
905232 meter/sec
ZDOT = -2290
005677 ZDOT = -735
219223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2123415
58 X = 647217
07
Y = 13695565
77 feet Y = 4174408
45 meter
Z = 17160059
61 Z = 5230386
17
XDOT = -23196
354482 XDOT = -7070
248846
YDOT = 6656
103215 feet/sec YDOT = 2028
780260 meter/sec
ZDOT = -2433
341986 ZDOT = -741
682637
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 08173
33944023
00020000 00000-0 20000-3 0 9051
2 25544 51
6416 355
0084 0009658 282
2435 77
7647 15
74645836 29181
Satellite: ISS
Catalog Number: 25544
Epoch time: 08173
33944023 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 355
0084 deg
Eccentricity:
0009658
Arg of perigee: 282
2435 deg
Mean anomaly: 77
7647 deg
Mean motion: 15
74645836 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2918
Checksum: 314
Coasting Arc #7 (Orbit 2933)
---------------------------------------
Vector Time (GMT): 2008/174/07:02:02
466
Vector Time (MET): N/A
Weight (LBS) : 661038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6648500
55 A = 6730077
33 meter
Y = -546290
62 meter E =
0010855
Z = 833468
68 I = 51
60198
XDOT = -347
463230 Wp = 9
09428
YDOT = 4867
276632 meter/sec RA = 349
61997 deg
ZDOT = 5961
909157 TA =
00765
MA =
00763
Ha = 188
006 n
mi
Hp = 186
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21812665
85 X = 6650066
33
Y = -1792292
06 feet Y = -471934
67 meter
Z = 2734477
29 Z = 865770
48
XDOT = -1139
971226 XDOT = -430
825639
YDOT = 15968
755353 feet/sec YDOT = 4862
923934 meter/sec
ZDOT = 19560
069414 ZDOT = 5960
019579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20512296
42 X = 6252147
95
Y = -7586493
18 feet Y = -2312363
12 meter
Z = 2858825
78 Z = 871370
10
XDOT = 2534
717984 XDOT = 772
582042
YDOT = 14221
577724 feet/sec YDOT = 4334
736890 meter/sec
ZDOT = 19553
166490 ZDOT = 5959
805146
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 08174
35487483
00020000 00000-0 20000-3 0 9067
2 25544 51
6420 349
7883 0009652 286
8640 73
1464 15
74625273 29343
Satellite: ISS
Catalog Number: 25544
Epoch time: 08174
35487483 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 349
7883 deg
Eccentricity:
0009652
Arg of perigee: 286
8640 deg
Mean anomaly: 73
1464 deg
Mean motion: 15
74625273 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2934
Checksum: 322
Coasting Arc #8 (Orbit 2948)
---------------------------------------
Vector Time (GMT): 2008/175/07:02:02
466
Vector Time (MET): N/A
Weight (LBS) : 661038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 204237
66 A = 6718717
01 meter
Y = -4308096
34 meter E =
0005029
Z = -5155706
28 I = 51
53569
XDOT = 7523
779836 Wp = 77
83232
YDOT = -1092
547718 meter/sec RA = 344
45586 deg
ZDOT = 1213
011626 TA = 203
76460
MA = 203
78783
Ha = 188
204 n
mi
Hp = 185
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 670071
05 X = 277441
53
Y = -14134174
33 feet Y = -4305402
32 meter
Z = -16915046
85 Z = -5154536
97
XDOT = 24684
317048 XDOT = 7529
545162
YDOT = -3584
474140 feet/sec YDOT = -1008
380455 meter/sec
ZDOT = 3979
696936 ZDOT = 1249
575629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3299070
03 X = -1005556
55
Y = -13765210
26 feet Y = -4195636
09 meter
Z = -16910878
53 Z = -5154435
78
XDOT = 21608
903470 XDOT = 6586
393778
YDOT = -10232
769743 feet/sec YDOT = -3118
948218 meter/sec
ZDOT = 4120
417081 ZDOT = 1255
903126
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 08175
30683099
00020000 00000-0 20000-3 0 9075
2 25544 51
6422 344
8951 0009732 290
4976 69
5143 15
74666326 29492
Satellite: ISS
Catalog Number: 25544
Epoch time: 08175
30683099 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 344
8951 deg
Eccentricity:
0009732
Arg of perigee: 290
4976 deg
Mean anomaly: 69
5143 deg
Mean motion: 15
74666326 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2949
Checksum: 329
Coasting Arc #9 (Orbit 2964)
---------------------------------------
Vector Time (GMT): 2008/176/07:02:02
466
Vector Time (MET): N/A
Weight (LBS) : 661038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6463848
66 A = 6729596
01 meter
Y = 1340070
81 meter E =
0004800
Z = -1293982
26 I = 51
54444
XDOT = 133
261911 Wp = 228
44953
YDOT = -5010
709555 meter/sec RA = 339
33167 deg
ZDOT = -5844
061902 TA = 325
77015
MA = 325
80108
Ha = 188
456 n
mi
Hp = 185
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21206852
56 X = -6472067
25
Y = 4396557
78 feet Y = 1267742
58 meter
Z = -4245348
63 Z = -1325403
19
XDOT = 437
210993 XDOT = 217
671733
YDOT = -16439
335811 feet/sec YDOT = -5008
746583 meter/sec
ZDOT = -19173
431436 ZDOT = -5843
210178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18867393
10 X = -5750781
42
Y = 10584928
28 feet Y = 3226286
14 meter
Z = -4366242
30 Z = -1330830
65
XDOT = -3668
978166 XDOT = -1118
304545
YDOT = -14461
860462 feet/sec YDOT = -4407
975069 meter/sec
ZDOT = -19170
544997 ZDOT = -5843
182115
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 08176
32223943
00020000 00000-0 20000-3 0 9087
2 25544 51
6423 339
6758 0009786 293
5684 66
4451 15
74636414 29650
Satellite: ISS
Catalog Number: 25544
Epoch time: 08176
32223943 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 339
6758 deg
Eccentricity:
0009786
Arg of perigee: 293
5684 deg
Mean anomaly: 66
4451 deg
Mean motion: 15
74636414 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2965
Checksum: 329
Coasting Arc #10 (Orbit 2980)
---------------------------------------
Vector Time (GMT): 2008/177/07:02:02
466
Vector Time (MET): N/A
Weight (LBS) : 661038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -21974
36 A = 6719106
65 meter
Y = 4460083
20 meter E =
0008959
Z = 5031088
31 I = 51
48284
XDOT = -7235
563166 Wp = 330
87544
YDOT = 1952
128944 meter/sec RA = 334
15435 deg
ZDOT = -1755
781395 TA = 136
11029
MA = 136
03908
Ha = 188
632 n
mi
Hp = 185
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -72094
35 X = -96286
11
Y = 14632818
90 feet Y = 4459421
34 meter
Z = 16506195
23 Z = 5030801
61
XDOT = -23738
724299 XDOT = -7248
325181
YDOT = 6404
622520 feet/sec YDOT = 1871
145594 meter/sec
ZDOT = -5760
437649 ZDOT = -1790
962392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4498359
84 X = 1371100
08
Y = 13925305
19 feet Y = 4244433
02 meter
Z = 16505444
61 Z = 5030859
52
XDOT = -19420
202678 XDOT = -5919
277776
YDOT = 13286
415685 feet/sec YDOT = 4049
699501 meter/sec
ZDOT = -5895
759549 ZDOT = -1797
027510
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 08177
33763212
00020000 00000-0 20000-3 0 9098
2 25544 51
6423 334
4557 0009948 298
5896 61
4266 15
74726511 29815
Satellite: ISS
Catalog Number: 25544
Epoch time: 08177
33763212 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 334
4557 deg
Eccentricity:
0009948
Arg of perigee: 298
5896 deg
Mean anomaly: 61
4266 deg
Mean motion: 15
74726511 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2981
Checksum: 325
Coasting Arc #11 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2008/178/07:02:02
466
Vector Time (MET): N/A
Weight (LBS) : 661038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6151265
80 A = 6728705
49 meter
Y = -2045846
38 meter E =
0012006
Z = 1772939
73 I = 51
48874
XDOT = 96
443338 Wp = 21
32386
YDOT = 5210
283034 meter/sec RA = 329
03328 deg
ZDOT = 5676
692142 TA = 358
37873
MA = 358
38261
Ha = 188
783 n
mi
Hp = 184
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20181318
25 X = 6165072
98
Y = -6712094
42 feet Y = -1976982
42 meter
Z = 5816731
41 Z = 1802855
90
XDOT = 316
415152 XDOT = 10
597591
YDOT = 17094
104441 feet/sec YDOT = 5210
880827 meter/sec
ZDOT = 18624
318051 ZDOT = 5676
952790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16742805
91 X = 5103207
24
Y = -13063871
96 feet Y = -3981868
17 meter
Z = 5931768
88 Z = 1808003
15
XDOT = 4962
505601 XDOT = 1512
571707
YDOT = 14818
634642 feet/sec YDOT = 4516
719839 meter/sec
ZDOT = 18625
736669 ZDOT = 5677
124537
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 08178
35301375
00020000 00000-0 20000-3 0 9101
2 25544 51
6416 329
2351 0010014 302
6593 57
3604 15
74723159 29970
Satellite: ISS
Catalog Number: 25544
Epoch time: 08178
35301375 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 329
2351 deg
Eccentricity:
0010014
Arg of perigee: 302
6593 deg
Mean anomaly: 57
3604 deg
Mean motion: 15
74723159 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2997
Checksum: 283
Coasting Arc #12 (Orbit 3011)
---------------------------------------
Vector Time (GMT): 2008/179/07:02:02
466
Vector Time (MET): N/A
Weight (LBS) : 661038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -209667
96 A = 6719784
85 meter
Y = -4642304
19 meter E =
0004295
Z = -4856118
05 I = 51
43347
XDOT = 6827
593769 Wp = 55
84339
YDOT = -2714
137221 meter/sec RA = 323
84367 deg
ZDOT = 2303
669385 TA = 236
63326
MA = 236
67437
Ha = 189
005 n
mi
Hp = 184
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -687886
99 X = -134151
12
Y = -15230656
79 feet Y = -4644225
93 meter
Z = -15932145
83 Z = -4856953
81
XDOT = 22400
242023 XDOT = 6846
245369
YDOT = -8904
649674 feet/sec YDOT = -2637
683176 meter/sec
ZDOT = 7557
970423 ZDOT = 2336
882961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5899089
12 X = -1798042
36
Y = -14054625
14 feet Y = -4283849
74 meter
Z = -15935734
21 Z = -4857211
79
XDOT = 16790
753399 XDOT = 5117
821636
YDOT = -15747
611178 feet/sec YDOT = -4799
871887 meter/sec
ZDOT = 7685
650297 ZDOT = 2342
586211
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 08179
30492159
00020000 00000-0 20000-3 0 9119
2 25544 51
6407 324
3408 0010051 306
3481 53
6755 15
74744542 30121
Satellite: ISS
Catalog Number: 25544
Epoch time: 08179
30492159 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 324
3408 deg
Eccentricity:
0010051
Arg of perigee: 306
3481 deg
Mean anomaly: 53
6755 deg
Mean motion: 15
74744542 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3012
Checksum: 272
Coasting Arc #13 (Orbit 3027)
---------------------------------------
Vector Time (GMT): 2008/180/07:02:02
466
Vector Time (MET): N/A
Weight (LBS) : 661038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5754708
58 A = 6727803
26 meter
Y = 2655427
88 meter E =
0004324
Z = -2258176
07 I = 51
43711
XDOT = -372
671879 Wp = 301
29582
YDOT = -5437
616601 meter/sec RA = 318
72739 deg
ZDOT = -5434
610601 TA = 264
12354
MA = 264
17283
Ha = 189
244 n
mi
Hp = 184
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18880277
50 X = -5773004
39
Y = 8712033
73 feet Y = 2590973
49 meter
Z = -7408714
15 Z = -2286176
71
XDOT = -1222
676768 XDOT = -285
439318
YDOT = -17839
949478 feet/sec YDOT = -5441
295446 meter/sec
ZDOT = -17830
087274 ZDOT = -5436
210011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14331374
01 X = -4368202
80
Y = 15012328
88 feet Y = 4575757
84 meter
Z = -7516325
97 Z = -2290976
16
XDOT = -6489
454798 XDOT = -1977
985822
YDOT = -15141
477363 feet/sec YDOT = -4615
122300 meter/sec
ZDOT = -17836
678372 ZDOT = -5436
619568
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 08180
32027722
00020000 00000-0 20000-3 0 9124
2 25544 51
6401 319
1212 0010110 309
9147 50
1127 15
74735011 30287
Satellite: ISS
Catalog Number: 25544
Epoch time: 08180
32027722 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 319
1212 deg
Eccentricity:
0010110
Arg of perigee: 309
9147 deg
Mean anomaly: 50
1127 deg
Mean motion: 15
74735011 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3028
Checksum: 233
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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