Date:
May 31st 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 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 797)
---------------------------------------
Vector Time (GMT): 2007/150/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 407712
56 A = 6708508
45 meter
Y = -4187386
64 meter E =
0006326
Z = 5230295
95 I = 51
53253
XDOT = 7538
645294 Wp = 241
19566
YDOT = 1473
026620 meter/sec RA = 194
55006 deg
ZDOT = 589
191621 TA = 203
18438
MA = 203
21293
Ha = 182
305 n
mi
Hp = 180
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1337639
64 X = 429097
95
Y = -13738145
14 feet Y = -4182708
63 meter
Z = 17159763
61 Z = 5232327
93
XDOT = 24733
088234 XDOT = 7518
751167
YDOT = 4832
764500 feet/sec YDOT = 1557
216649 meter/sec
ZDOT = 1933
043375 ZDOT = 625
766931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10035909
89 X = -3058945
34
Y = -9463670
36 feet Y = -2884526
73 meter
Z = 17166911
62 Z = 5232474
66
XDOT = 18382
867041 XDOT = 5603
097874
YDOT = -15722
649842 feet/sec YDOT = -4792
263672 meter/sec
ZDOT = 2071
201224 ZDOT = 631
302133
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 07150
50688397
00020000 00000-0 20000-3 0 9008
2 25544 51
6334 195
2750 0008354 257
6563 102
3667 15
78123593 7980
Satellite: ISS
Catalog Number: 25544
Epoch time: 07150
50688397 = yrday
fracday
Element set: 900
Inclination: 51
6334 deg
RA of node: 195
2750 deg
Eccentricity:
0008354
Arg of perigee: 257
6563 deg
Mean anomaly: 102
3667 deg
Mean motion: 15
78123593 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 798
Checksum: 310
Coasting Arc #2 (Orbit 813)
---------------------------------------
Vector Time (GMT): 2007/151/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6422821
03 A = 6720249
46 meter
Y = -1757813
50 meter E =
0007631
Z = 867319
65 I = 51
59925
XDOT = 2024
170065 Wp = 23
07731
YDOT = -4451
409207 meter/sec RA = 189
38053 deg
ZDOT = 5957
274199 TA = 346
40869
MA = 346
42922
Ha = 181
820 n
mi
Hp = 180
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21072247
49 X = -6406900
90
Y = -5767104
67 feet Y = -1829548
23 meter
Z = 2845536
91 Z = 836155
44
XDOT = 6640
977904 XDOT = 2044
856112
YDOT = -14604
360914 feet/sec YDOT = -4428
659215 meter/sec
ZDOT = 19544
862857 ZDOT = 5967
157221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17336077
80 X = -5284036
51
Y = 13319760
03 feet Y = 4059862
86 meter
Z = 2727744
46 Z = 831416
51
XDOT = -6720
197485 XDOT = -2048
316193
YDOT = -12764
141240 feet/sec YDOT = -3890
510250 meter/sec
ZDOT = 19581
602844 ZDOT = 5968
472547
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 07151
52006218
00020000 00000-0 20000-3 0 9018
2 25544 51
6325 190
0389 0008083 263
2310 96
7935 15
78097124 8146
Satellite: ISS
Catalog Number: 25544
Epoch time: 07151
52006218 = yrday
fracday
Element set: 901
Inclination: 51
6325 deg
RA of node: 190
0389 deg
Eccentricity:
0008083
Arg of perigee: 263
2310 deg
Mean anomaly: 96
7935 deg
Mean motion: 15
78097124 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 814
Checksum: 276
Coasting Arc #3 (Orbit 828)
---------------------------------------
Vector Time (GMT): 2007/152/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3075066
76 A = 6710319
86 meter
Y = 3573905
02 meter E =
0005197
Z = -4779217
95 I = 51
59510
XDOT = -6834
698778 Wp = 142
61910
YDOT = -2504
445457 meter/sec RA = 184
18178 deg
ZDOT = 2522
152702 TA = 152
08990
MA = 152
06201
Ha = 181
186 n
mi
Hp = 180
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10088801
70 X = -3091585
28
Y = 11725410
18 feet Y = 3539426
49 meter
Z = -15679848
91 Z = -4794196
23
XDOT = -22423
552421 XDOT = -6818
438045
YDOT = -8216
684571 feet/sec YDOT = -2580
784467 meter/sec
ZDOT = 8274
779206 ZDOT = 2488
988318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3559747
60 X = 1085011
07
Y = 14994517
02 feet Y = 4570328
79 meter
Z = -15735929
65 Z = -4796311
36
XDOT = -18803
797435 XDOT = -5731
397458
YDOT = 13025
402015 feet/sec YDOT = 3970
142534 meter/sec
ZDOT = 8149
334237 ZDOT = 2483
917075
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 07152
46989545
00020000 00000-0 20000-3 0 9026
2 25544 51
6325 185
1301 0008115 266
6091 93
4146 15
78156840 8299
Satellite: ISS
Catalog Number: 25544
Epoch time: 07152
46989545 = yrday
fracday
Element set: 902
Inclination: 51
6325 deg
RA of node: 185
1301 deg
Eccentricity:
0008115
Arg of perigee: 266
6091 deg
Mean anomaly: 93
4146 deg
Mean motion: 15
78156840 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 829
Checksum: 297
Coasting Arc #4 (Orbit 844)
---------------------------------------
Vector Time (GMT): 2007/153/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5186881
62 A = 6715315
15 meter
Y = 2593025
66 meter E =
0003158
Z = -3383725
33 I = 51
64148
XDOT = -4893
302528 Wp = 269
92590
YDOT = 3743
784495 meter/sec RA = 179
05831 deg
ZDOT = -4628
257156 TA = 310
06904
MA = 310
09673
Ha = 180
776 n
mi
Hp = 180
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17017328
14 X = 5173938
18
Y = 8507302
03 feet Y = 2650956
60 meter
Z = -11101461
04 Z = -3358558
15
XDOT = -16054
142151 XDOT = -4912
318978
YDOT = 12282
757531 feet/sec YDOT = 3688
959475 meter/sec
ZDOT = -15184
570723 ZDOT = -4652
074434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16796271
49 X = 5119503
55
Y = -9052932
73 feet Y = -2759333
90 meter
Z = -11006168
96 Z = -3354680
30
XDOT = 172
505228 XDOT = 52
579594
YDOT = 18904
392033 feet/sec YDOT = 5762
058692 meter/sec
ZDOT = -15273
996678 ZDOT = -4655
514188
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 07153
48303400
00020000 00000-0 20000-3 0 9030
2 25544 51
6329 179
8939 0007985 270
5190 89
5060 15
78206187 8457
Satellite: ISS
Catalog Number: 25544
Epoch time: 07153
48303400 = yrday
fracday
Element set: 903
Inclination: 51
6329 deg
RA of node: 179
8939 deg
Eccentricity:
0007985
Arg of perigee: 270
5190 deg
Mean anomaly: 89
5060 deg
Mean motion: 15
78206187 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 845
Checksum: 309
Coasting Arc #5 (Orbit 860)
---------------------------------------
Vector Time (GMT): 2007/154/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5243105
14 A = 6716138
34 meter
Y = -2941790
08 meter E =
0005242
Z = 2988307
79 I = 51
67290
XDOT = 4771
902015 Wp = 98
41427
YDOT = 3442
389290 meter/sec RA = 173
84132 deg
ZDOT = -4977
051405 TA = 47
01770
MA = 46
97376
Ha = 181
345 n
mi
Hp = 180
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17201788
53 X = 5261094
29
Y = -9651542
25 feet Y = -2883058
78 meter
Z = 9804159
41 Z = 3013821
97
XDOT = 15655
846506 XDOT = 4757
231746
YDOT = 11293
928117 feet/sec YDOT = 3495
670376 meter/sec
ZDOT = -16328
908810 ZDOT = -4953
904348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1659315
89 X = 505759
48
Y = -19606376
83 feet Y = -5976023
66 meter
Z = 9900100
84 Z = 3017550
74
XDOT = 16763
740645 XDOT = 5109
588149
YDOT = -6792
991108 feet/sec YDOT = -2070
503690 meter/sec
ZDOT = -16241
124795 ZDOT = -4950
294837
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 07154
49615243
00020000 00000-0 20000-3 0 9044
2 25544 51
6320 174
6576 0008010 275
1589 84
8662 15
78248038 8616
Satellite: ISS
Catalog Number: 25544
Epoch time: 07154
49615243 = yrday
fracday
Element set: 904
Inclination: 51
6320 deg
RA of node: 174
6576 deg
Eccentricity:
0008010
Arg of perigee: 275
1589 deg
Mean anomaly: 84
8662 deg
Mean motion: 15
78248038 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 861
Checksum: 302
Coasting Arc #6 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2007/155/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2920730
21 A = 6709331
24 meter
Y = -3427944
31 meter E =
0003555
Z = 4976364
11 I = 51
67818
XDOT = 6836
091286 Wp = 233
49789
YDOT = -2955
767338 meter/sec RA = 168
71632 deg
ZDOT = 1975
069516 TA = 197
42576
MA = 197
43797
Ha = 181
636 n
mi
Hp = 180
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9582448
21 X = -2906355
61
Y = -11246536
46 feet Y = -3460526
16 meter
Z = 16326653
90 Z = 4962209
46
XDOT = 22428
121018 XDOT = 6859
040517
YDOT = -9697
399403 feet/sec YDOT = -2879
194407 meter/sec
ZDOT = 6479
886865 ZDOT = 2008
334380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14708511
72 X = -4483154
37
Y = 1929520
09 feet Y = 588117
72 meter
Z = 16272804
27 Z = 4959950
74
XDOT = 4298
049067 XDOT = 1310
045355
YDOT = -22971
944344 feet/sec YDOT = -7001
848636 meter/sec
ZDOT = 6605
097046 ZDOT = 2013
233580
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 07155
50925274
00020000 00000-0 20000-3 0 9056
2 25544 51
6319 169
4207 0007872 279
0478 80
9796 15
78259895 8777
Satellite: ISS
Catalog Number: 25544
Epoch time: 07155
50925274 = yrday
fracday
Element set: 905
Inclination: 51
6319 deg
RA of node: 169
4207 deg
Eccentricity:
0007872
Arg of perigee: 279
0478 deg
Mean anomaly: 80
9796 deg
Mean motion: 15
78259895 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 877
Checksum: 345
Coasting Arc #7 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2007/156/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6354452
36 A = 6719926
17 meter
Y = 2140868
50 meter E =
0010323
Z = -319450
02 I = 51
74349
XDOT = -1798
159299 Wp =
37381
YDOT = -4437
220532 meter/sec RA = 163
53376 deg
ZDOT = 6042
866705 TA = 356
15188
MA = 356
15982
Ha = 181
914 n
mi
Hp = 180
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20847940
82 X = -6376367
77
Y = 7023846
78 feet Y = 2069686
97 meter
Z = -1048064
38 Z = -350372
69
XDOT = -5899
472765 XDOT = -1777
763040
YDOT = -14557
810145 feet/sec YDOT = -4457
215592 meter/sec
ZDOT = 19825
678167 ZDOT = 6034
180033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5177700
60 X = -1578163
14
Y = 21375330
35 feet Y = 6515200
69 meter
Z = -1164546
14 Z = -354953
66
XDOT = -13960
858182 XDOT = -4255
269574
YDOT = -2305
209088 feet/sec YDOT = -702
627730 meter/sec
ZDOT = 19792
340629 ZDOT = 6032
705424
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 07156
45901618
00020000 00000-0 20000-3 0 9068
2 25544 51
6329 164
5119 0007957 282
9469 77
0807 15
78294834 8922
Satellite: ISS
Catalog Number: 25544
Epoch time: 07156
45901618 = yrday
fracday
Element set: 906
Inclination: 51
6329 deg
RA of node: 164
5119 deg
Eccentricity:
0007957
Arg of perigee: 282
9469 deg
Mean anomaly: 77
0807 deg
Mean motion: 15
78294834 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 892
Checksum: 332
Coasting Arc #8 (Orbit 907)
---------------------------------------
Vector Time (GMT): 2007/157/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 175550
02 A = 6708378
81 meter
Y = 4301222
51 meter E =
0006409
Z = -5150487
98 I = 51
73210
XDOT = -7370
953269 Wp = 90
57220
YDOT = 1835
139101 meter/sec RA = 158
36484 deg
ZDOT = 1282
611557 TA = 191
66378
MA = 191
67864
Ha = 182
191 n
mi
Hp = 180
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 575951
50 X = 152460
09
Y = 14111622
40 feet Y = 4303057
30 meter
Z = -16897926
44 Z = -5149690
58
XDOT = -24182
917550 XDOT = -7397
156903
YDOT = 6020
797574 feet/sec YDOT = 1752
566258 meter/sec
ZDOT = 4208
043166 ZDOT = 1246
740264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12411442
70 X = 3783007
73
Y = 6748723
45 feet Y = 2057010
91 meter
Z = -16894388
04 Z = -5149409
47
XDOT = -6920
178670 XDOT = -2109
270459
YDOT = 22911
764383 feet/sec YDOT = 6983
505784 meter/sec
ZDOT = 4072
827611 ZDOT = 1241
397856
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 07157
47207798
00020000 00000-0 20000-3 0 9070
2 25544 51
6331 159
2752 0008026 286
9619 73
0666 15
78299733 9088
Satellite: ISS
Catalog Number: 25544
Epoch time: 07157
47207798 = yrday
fracday
Element set: 907
Inclination: 51
6331 deg
RA of node: 159
2752 deg
Eccentricity:
0008026
Arg of perigee: 286
9619 deg
Mean anomaly: 73
0666 deg
Mean motion: 15
78299733 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 908
Checksum: 330
Coasting Arc #9 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2007/158/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6171031
07 A = 6717246
97 meter
Y = -922402
08 meter E =
0003509
Z = -2483567
84 I = 51
78758
XDOT = -1346
265205 Wp = 256
91319
YDOT = 5388
059069 meter/sec RA = 153
23683 deg
ZDOT = -5340
758142 TA = 311
16455
MA = 311
19481
Ha = 182
299 n
mi
Hp = 180
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20246164
94 X = 6192951
55
Y = -3026253
53 feet Y = -853271
25 meter
Z = -8148188
46 Z = -2453535
93
XDOT = -4416
880595 XDOT = -1380
470852
YDOT = 17677
359150 feet/sec YDOT = 5372
813831 meter/sec
ZDOT = -17522
172381 ZDOT = -5347
380651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7614571
38 X = 2320921
36
Y = -19050382
53 feet Y = -5806556
60 meter
Z = -8034899
40 Z = -2449037
34
XDOT = 11701
205305 XDOT = 3566
527377
YDOT = 12085
387771 feet/sec YDOT = 3683
626193 meter/sec
ZDOT = -17546
516679 ZDOT = -5348
178284
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 07158
48512023
00020000 00000-0 20000-3 0 9083
2 25544 51
6322 154
0382 0007952 290
8452 69
1861 15
78335430 9242
Satellite: ISS
Catalog Number: 25544
Epoch time: 07158
48512023 = yrday
fracday
Element set: 908
Inclination: 51
6322 deg
RA of node: 154
0382 deg
Eccentricity:
0007952
Arg of perigee: 290
8452 deg
Mean anomaly: 69
1861 deg
Mean motion: 15
78335430 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 924
Checksum: 287
Coasting Arc #10 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2007/159/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2382899
28 A = 6713355
77 meter
Y = -5003031
94 meter E =
0006540
Z = 3790164
38 I = 51
79991
XDOT = 6452
444047 Wp = 39
43235
YDOT = -122
425799 meter/sec RA = 148
03076 deg
ZDOT = -4209
395773 TA = 94
64698
MA = 94
57228
Ha = 182
453 n
mi
Hp = 179
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7817911
02 X = 2420254
86
Y = -16414146
79 feet Y = -4976176
60 meter
Z = 12434922
49 Z = 3801830
66
XDOT = 21169
435850 XDOT = 6473
781973
YDOT = -401
659445 feet/sec YDOT = -50
151149 meter/sec
ZDOT = -13810
353585 ZDOT = -4177
997949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10526632
13 X = -3208517
47
Y = -14786876
69 feet Y = -4507040
02 meter
Z = 12478362
82 Z = 3803404
99
XDOT = 8963
769812 XDOT = 2732
157039
YDOT = -17960
016102 feet/sec YDOT = -5474
212908 meter/sec
ZDOT = -13691
800127 ZDOT = -4173
260679
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 07159
49814139
00020000 00000-0 20000-3 0 9099
2 25544 51
6316 148
8010 0008052 295
6902 64
3432 15
78403813 9409
Satellite: ISS
Catalog Number: 25544
Epoch time: 07159
49814139 = yrday
fracday
Element set: 909
Inclination: 51
6316 deg
RA of node: 148
8010 deg
Eccentricity:
0008052
Arg of perigee: 295
6902 deg
Mean anomaly: 64
3432 deg
Mean motion: 15
78403813 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 940
Checksum: 290
Coasting Arc #11 (Orbit 955)
---------------------------------------
Vector Time (GMT): 2007/160/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4836994
55 A = 6710637
20 meter
Y = -852004
81 meter E =
0000900
Z = 4571884
93 I = 51
81354
XDOT = 3898
315071 Wp = 62
94422
YDOT = -5923
622044 meter/sec RA = 142
92210 deg
ZDOT = 3020
404775 TA = 357
15095
MA = 357
15146
Ha = 182
752 n
mi
Hp = 179
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15869404
69 X = -4849317
33
Y = -2795291
36 feet Y = -906164
22 meter
Z = 14999622
47 Z = 4548356
63
XDOT = 12789
747607 XDOT = 3949
591478
YDOT = -19434
455524 feet/sec YDOT = -5879
742543 meter/sec
ZDOT = 9909
464486 ZDOT = 3039
466778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10023973
56 X = -3055307
14
Y = 12721337
81 feet Y = 3877463
77 meter
Z = 14910662
35 Z = 4544769
88
XDOT = -10147
519034 XDOT = -3092
963802
YDOT = -19694
485428 feet/sec YDOT = -6002
879159 meter/sec
ZDOT = 9980
727041 ZDOT = 3042
125602
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 07160
51114378
00020000 00000-0 20000-3 0 9104
2 25544 51
6308 143
5636 0008075 299
5711 60
4649 15
78405356 9560
Satellite: ISS
Catalog Number: 25544
Epoch time: 07160
51114378 = yrday
fracday
Element set: 910
Inclination: 51
6308 deg
RA of node: 143
5636 deg
Eccentricity:
0008075
Arg of perigee: 299
5711 deg
Mean anomaly: 60
4649 deg
Mean motion: 15
78405356 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 956
Checksum: 296
Coasting Arc #12 (Orbit 970)
---------------------------------------
Vector Time (GMT): 2007/161/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4158636
38 A = 6718765
65 meter
Y = 5114798
67 meter E =
0011541
Z = -1258311
77 I = 51
86386
XDOT = -4469
981713 Wp = 354
53059
YDOT = -2186
885325 meter/sec RA = 137
73231 deg
ZDOT = 5890
578622 TA = 351
67842
MA = 351
69755
Ha = 182
672 n
mi
Hp = 179
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13643820
15 X = -4209409
01
Y = 16780835
54 feet Y = 5068010
74 meter
Z = -4128319
44 Z = -1278637
32
XDOT = -14665
294334 XDOT = -4473
811100
YDOT = -7174
820619 feet/sec YDOT = -2236
893328 meter/sec
ZDOT = 19326
045347 ZDOT = 5868
853629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8660363
59 X = 2639678
82
Y = 19801865
80 feet Y = 6035608
70 meter
Z = -4204462
43 Z = -1281520
15
XDOT = -11709
598233 XDOT = -3569
085542
YDOT = 9202
465147 feet/sec YDOT = 2804
911377 meter/sec
ZDOT = 19243
729270 ZDOT = 5865
488682
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 07161
46081362
00020000 00000-0 20000-3 0 9116
2 25544 51
6307 138
6542 0007898 302
9516 57
0889 15
78470503 9715
Satellite: ISS
Catalog Number: 25544
Epoch time: 07161
46081362 = yrday
fracday
Element set: 911
Inclination: 51
6307 deg
RA of node: 138
6542 deg
Eccentricity:
0007898
Arg of perigee: 302
9516 deg
Mean anomaly: 57
0889 deg
Mean motion: 15
78470503 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 971
Checksum: 303
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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