Date:
June 10th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 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 2226)
---------------------------------------
Vector Time (GMT): 2010/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4157238
84 A = 6726688
10 meter
Y = -962227
67 meter E =
0005943
Z = 5204083
30 I = 51
29097
XDOT = 756
234267 Wp = 299
79056
YDOT = 7614
265828 meter/sec RA = 269
17877 deg
ZDOT = 807
356795 TA = 142
50226
MA = 142
46079
Ha = 193
020 n
mi
Hp = 189
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13639235
06 X = 4142408
79
Y = -3156914
91 feet Y = -915822
66 meter
Z = 17073764
10 Z = 5224243
31
XDOT = 2481
083554 XDOT = 667
111911
YDOT = 24981
187099 feet/sec YDOT = 7622
224057 meter/sec
ZDOT = 2648
808381 ZDOT = 810
815320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -23715
21 X = -7228
40
Y = -13901273
40 feet Y = -4237108
13 meter
Z = 17154075
34 Z = 5228562
17
XDOT = 23880
437415 XDOT = 7278
757324
YDOT = 3230
391224 feet/sec YDOT = 984
623245 meter/sec
ZDOT = 2662
609872 ZDOT = 811
563489
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 10160
54905963
00016717 00000-0 10270-3 0 9006
2 25544 51
6489 269
6974 0009174 299
9626 60
0625 15
71765802 22276
Satellite: ISS
Catalog Number: 25544
Epoch time: 10160
54905963 = yrday
fracday
Element set: 900
Inclination: 51
6489 deg
RA of node: 269
6974 deg
Eccentricity:
0009174
Arg of perigee: 299
9626 deg
Mean anomaly: 60
0625 deg
Mean motion: 15
71765802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2227
Checksum: 336
Coasting Arc #2 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2010/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1804007
71 A = 6737769
76 meter
Y = -6326209
99 meter E =
0012321
Z = -1417992
73 I = 51
32973
XDOT = 4391
629436 Wp = 348
78188
YDOT = -2549
268644 meter/sec RA = 264
01735 deg
ZDOT = 5789
600483 TA = 355
56076
MA = 355
57168
Ha = 193
376 n
mi
Hp = 189
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5918660
47 X = -1726244
36
Y = -20755282
13 feet Y = -6345948
43 meter
Z = -4652207
13 Z = -1426568
96
XDOT = 14408
233058 XDOT = 4391
684198
YDOT = -8363
742270 feet/sec YDOT = -2500
159549 meter/sec
ZDOT = 18994
752241 ZDOT = 5810
935003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21527720
34 X = -6561649
16
Y = 1431872
80 feet Y = 436434
83 meter
Z = -4686395
90 Z = -1428413
47
XDOT = -5092
588669 XDOT = -1552
221026
YDOT = -14156
093200 feet/sec YDOT = -4314
777207 meter/sec
ZDOT = 19079
743261 ZDOT = 5815
505746
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 10161
50277403
00016717 00000-0 10270-3 0 9015
2 25544 51
6491 264
8175 0009240 304
8188 55
2105 15
71726377 22422
Satellite: ISS
Catalog Number: 25544
Epoch time: 10161
50277403 = yrday
fracday
Element set: 901
Inclination: 51
6491 deg
RA of node: 264
8175 deg
Eccentricity:
0009240
Arg of perigee: 304
8188 deg
Mean anomaly: 55
2105 deg
Mean motion: 15
71726377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 291
Coasting Arc #3 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2010/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3271878
48 A = 6728422
37 meter
Y = 3377827
60 meter E =
0010134
Z = -4819205
86 I = 51
30270
XDOT = -3236
028417 Wp = 24
32545
YDOT = -6554
990911 meter/sec RA = 258
90934 deg
ZDOT = -2390
119815 TA = 222
17090
MA = 222
24891
Ha = 193
496 n
mi
Hp = 189
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10734509
44 X = -3285995
71
Y = 11082111
55 feet Y = 3341161
53 meter
Z = -15811042
84 Z = -4835134
44
XDOT = -10616
891131 XDOT = -3150
877923
YDOT = -21505
875692 feet/sec YDOT = -6590
701532 meter/sec
ZDOT = -7841
600444 ZDOT = -2405
635075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8835580
59 X = 2693084
96
Y = 12568404
01 feet Y = 3830849
54 meter
Z = -15874498
46 Z = -4838547
13
XDOT = -22217
422083 XDOT = -6771
870251
YDOT = 5606
209802 feet/sec YDOT = 1708
772748 meter/sec
ZDOT = -7903
443309 ZDOT = -2408
969521
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 10162
52005525
00016717 00000-0 10270-3 0 9023
2 25544 51
6490 259
6123 0009224 307
8854 52
1473 15
71758722 22581
Satellite: ISS
Catalog Number: 25544
Epoch time: 10162
52005525 = yrday
fracday
Element set: 902
Inclination: 51
6490 deg
RA of node: 259
6123 deg
Eccentricity:
0009224
Arg of perigee: 307
8854 deg
Mean anomaly: 52
1473 deg
Mean motion: 15
71758722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2258
Checksum: 298
Coasting Arc #4 (Orbit 2273)
---------------------------------------
Vector Time (GMT): 2010/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3702915
25 A = 6735239
20 meter
Y = 4926156
53 meter E =
0007588
Z = 2716941
15 I = 51
33240
XDOT = -2833
538915 Wp = 61
41038
YDOT = 4973
072546 meter/sec RA = 253
72672 deg
ZDOT = -5140
523952 TA = 87
48064
MA = 87
39377
Ha = 193
692 n
mi
Hp = 188
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12148672
09 X = 3634356
40
Y = 16161930
86 feet Y = 4967180
83 meter
Z = 8913848
92 Z = 2734764
51
XDOT = -9296
387516 XDOT = -2863
966257
YDOT = 16315
854809 feet/sec YDOT = 4941
217175 meter/sec
ZDOT = -16865
236063 ZDOT = -5154
362224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18028087
63 X = 5494961
11
Y = -9083759
62 feet Y = -2768729
93 meter
Z = 8984893
60 Z = 2738595
57
XDOT = 13793
684932 XDOT = 4204
315167
YDOT = 10592
897273 feet/sec YDOT = 3228
715089 meter/sec
ZDOT = -16920
360718 ZDOT = -5157
325947
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 10163
53732349
00016717 00000-0 10270-3 0 9037
2 25544 51
6484 254
4068 0009123 312
8907 47
1489 15
71784634 22748
Satellite: ISS
Catalog Number: 25544
Epoch time: 10163
53732349 = yrday
fracday
Element set: 903
Inclination: 51
6484 deg
RA of node: 254
4068 deg
Eccentricity:
0009123
Arg of perigee: 312
8907 deg
Mean anomaly: 47
1489 deg
Mean motion: 15
71784634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2274
Checksum: 319
Coasting Arc #5 (Orbit 2289)
---------------------------------------
Vector Time (GMT): 2010/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1514868
34 A = 6731041
48 meter
Y = -5119388
64 meter E =
0005644
Z = 4093087
24 I = 51
32821
XDOT = 4993
925800 Wp = 42
88553
YDOT = 4489
067570 meter/sec RA = 248
63398 deg
ZDOT = 3767
416593 TA = 8
31121
MA = 8
30186
Ha = 193
747 n
mi
Hp = 188
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4970040
49 X = 1552118
23
Y = -16795894
49 feet Y = -5102241
06 meter
Z = 13428763
91 Z = 4100535
88
XDOT = 16384
270998 XDOT = 4925
055664
YDOT = 14727
911975 feet/sec YDOT = 4544
526762 meter/sec
ZDOT = 12360
290660 ZDOT = 3791
510721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15812709
61 X = -4819713
89
Y = -7480915
69 feet Y = -2280183
10 meter
Z = 13458424
49 Z = 4102127
78
XDOT = 16573
199141 XDOT = 5051
511098
YDOT = -12628
127519 feet/sec YDOT = -3849
053268 meter/sec
ZDOT = 12456
338251 ZDOT = 3796
691899
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 10164
55457625
00016717 00000-0 10270-3 0 9042
2 25544 51
6484 249
2001 0009244 316
5711 43
4722 15
71833854 22901
Satellite: ISS
Catalog Number: 25544
Epoch time: 10164
55457625 = yrday
fracday
Element set: 904
Inclination: 51
6484 deg
RA of node: 249
2001 deg
Eccentricity:
0009244
Arg of perigee: 316
5711 deg
Mean anomaly: 43
4722 deg
Mean motion: 15
71833854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2290
Checksum: 297
Coasting Arc #6 (Orbit 2304)
---------------------------------------
Vector Time (GMT): 2010/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4798476
26 A = 6731889
39 meter
Y = -2780955
16 meter E =
0005490
Z = -3811451
53 I = 51
34255
XDOT = 467
280386 Wp = 3
37428
YDOT = -6472
601474 meter/sec RA = 243
44357 deg
ZDOT = 4140
028481 TA = 310
13230
MA = 310
18039
Ha = 193
869 n
mi
Hp = 188
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15743032
36 X = -4748507
26
Y = -9123868
64 feet Y = -2834334
44 meter
Z = -12504762
25 Z = -3834641
57
XDOT = 1533
072131 XDOT = 519
512072
YDOT = -21235
569139 feet/sec YDOT = -6467
084834 meter/sec
ZDOT = 13582
770607 ZDOT = 4142
424118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11240520
05 X = -3426110
51
Y = 14227369
86 feet Y = 4336502
33 meter
Z = -12597213
25 Z = -3839630
60
XDOT = -19781
251087 XDOT = -6029
325331
YDOT = -3609
992365 feet/sec YDOT = -1100
325673 meter/sec
ZDOT = 13592
278514 ZDOT = 4142
926491
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 10165
50824071
00016717 00000-0 10270-3 0 9052
2 25544 51
6474 244
3204 0009265 320
8104 39
2386 15
71853698 23052
Satellite: ISS
Catalog Number: 25544
Epoch time: 10165
50824071 = yrday
fracday
Element set: 905
Inclination: 51
6474 deg
RA of node: 244
3204 deg
Eccentricity:
0009265
Arg of perigee: 320
8104 deg
Mean anomaly: 39
2386 deg
Mean motion: 15
71853698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2305
Checksum: 298
Coasting Arc #7 (Orbit 2320)
---------------------------------------
Vector Time (GMT): 2010/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 752312
94 A = 6734178
23 meter
Y = 5936668
16 meter E =
0006535
Z = -3095401
79 I = 51
36347
XDOT = -5679
165892 Wp = 351
66018
YDOT = -1816
381468 meter/sec RA = 238
35485 deg
ZDOT = -4856
261015 TA = 224
36781
MA = 224
42019
Ha = 194
197 n
mi
Hp = 188
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2468218
31 X = 700908
89
Y = 19477257
74 feet Y = 5944794
09 meter
Z = -10155517
68 Z = -3091870
91
XDOT = -18632
434030 XDOT = -5634
842078
YDOT = -5959
256785 feet/sec YDOT = -1879
640613 meter/sec
ZDOT = -15932
614879 ZDOT = -4883
742811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19640083
28 X = 5986297
38
Y = -97147
64 feet Y = -29610
60 meter
Z = -10141395
42 Z = -3091097
32
XDOT = -8216
299228 XDOT = -2504
328005
YDOT = 16225
278670 feet/sec YDOT = 4945
464939 meter/sec
ZDOT = -16042
181444 ZDOT = -4889
656904
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 10166
52546963
00016717 00000-0 10270-3 0 9067
2 25544 51
6463 239
1138 0009313 325
1145 34
9406 15
71844593 23212
Satellite: ISS
Catalog Number: 25544
Epoch time: 10166
52546963 = yrday
fracday
Element set: 906
Inclination: 51
6463 deg
RA of node: 239
1138 deg
Eccentricity:
0009313
Arg of perigee: 325
1145 deg
Mean anomaly: 34
9406 deg
Mean motion: 15
71844593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2321
Checksum: 303
Coasting Arc #8 (Orbit 2336)
---------------------------------------
Vector Time (GMT): 2010/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4889309
88 A = 6728805
94 meter
Y = 380292
59 meter E =
0011982
Z = 4610706
64 I = 51
36351
XDOT = 2202
730698 Wp = 11
64504
YDOT = 6784
917336 meter/sec RA = 233
16934 deg
ZDOT = -2882
583642 TA = 107
08246
MA = 106
95117
Ha = 194
255 n
mi
Hp = 187
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16041042
92 X = 4862296
23
Y = 1247679
09 feet Y = 434816
04 meter
Z = 15126990
30 Z = 4634393
13
XDOT = 7226
806752 XDOT = 2140
699746
YDOT = 22260
227480 feet/sec YDOT = 6809
203177 meter/sec
ZDOT = -9457
295415 ZDOT = -2872
032544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2943510
51 X = 897182
00
Y = -15727095
76 feet Y = -4793618
79 meter
Z = 15221425
74 Z = 4639490
56
XDOT = 21763
195472 XDOT = 6633
421980
YDOT = -5079
817770 feet/sec YDOT = -1548
328456 meter/sec
ZDOT = -9415
166231 ZDOT = -2869
742667
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 10167
54268326
00016717 00000-0 10270-3 0 9075
2 25544 51
6468 233
9067 0009533 328
8738 31
1858 15
71908684 23371
Satellite: ISS
Catalog Number: 25544
Epoch time: 10167
54268326 = yrday
fracday
Element set: 907
Inclination: 51
6468 deg
RA of node: 233
9067 deg
Eccentricity:
0009533
Arg of perigee: 328
8738 deg
Mean anomaly: 31
1858 deg
Mean motion: 15
71908684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2337
Checksum: 340
Coasting Arc #9 (Orbit 2352)
---------------------------------------
Vector Time (GMT): 2010/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3059891
43 A = 6736698
94 meter
Y = -5679134
04 meter E =
0016624
Z = 1902548
76 I = 51
40793
XDOT = 5197
514613 Wp = 32
38168
YDOT = -917
042643 meter/sec RA = 228
07116 deg
ZDOT = 5613
086613 TA = 348
83630
MA = 348
87314
Ha = 194
565 n
mi
Hp = 187
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10039013
89 X = -3005401
08
Y = -18632329
52 feet Y = -5713047
13 meter
Z = 6241957
89 Z = 1887815
56
XDOT = 17052
213298 XDOT = 5180
115703
YDOT = -3008
670090 feet/sec YDOT = -859
018925 meter/sec
ZDOT = 18415
638493 ZDOT = 5638
293578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19460052
75 X = -5931424
08
Y = 8365554
38 feet Y = 2549820
98 meter
Z = 6183153
60 Z = 1884625
22
XDOT = -867
680529 XDOT = -264
469025
YDOT = -15725
487105 feet/sec YDOT = -4793
128470 meter/sec
ZDOT = 18516
129865 ZDOT = 5643
716383
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 10168
55988746
00016717 00000-0 10270-3 0 9083
2 25544 51
6461 228
6998 0009487 334
3924 25
6767 15
71873845 23530
Satellite: ISS
Catalog Number: 25544
Epoch time: 10168
55988746 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 228
6998 deg
Eccentricity:
0009487
Arg of perigee: 334
3924 deg
Mean anomaly: 25
6767 deg
Mean motion: 15
71873845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2353
Checksum: 367
Coasting Arc #10 (Orbit 2367)
---------------------------------------
Vector Time (GMT): 2010/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3955194
57 A = 6726761
91 meter
Y = 1892562
99 meter E =
0011896
Z = -5108791
77 I = 51
39571
XDOT = -4686
091104 Wp = 58
59450
YDOT = -5926
260851 meter/sec RA = 222
90551 deg
ZDOT = 1441
113306 TA = 225
22960
MA = 225
32643
Ha = 194
641 n
mi
Hp = 187
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12976360
13 X = -3951246
09
Y = 6209196
15 feet Y = 1848356
30 meter
Z = -16761127
84 Z = -5127996
23
XDOT = -15374
314646 XDOT = -4626
474943
YDOT = -19443
113027 feet/sec YDOT = -5978
330346 meter/sec
ZDOT = 4728
062029 ZDOT = 1418
492490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5259203
26 X = 1603005
15
Y = 13293185
19 feet Y = 4051762
85 meter
Z = -16837679
59 Z = -5132124
74
XDOT = -19538
585600 XDOT = -5955
360891
YDOT = 13569
056295 feet/sec YDOT = 4135
848359 meter/sec
ZDOT = 4637
794395 ZDOT = 1413
599732
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 10169
51350221
00016717 00000-0 10270-3 0 9092
2 25544 51
6460 223
8182 0009584 337
7276 22
3469 15
71894091 23681
Satellite: ISS
Catalog Number: 25544
Epoch time: 10169
51350221 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 223
8182 deg
Eccentricity:
0009584
Arg of perigee: 337
7276 deg
Mean anomaly: 22
3469 deg
Mean motion: 15
71894091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2368
Checksum: 317
Coasting Arc #11 (Orbit 2383)
---------------------------------------
Vector Time (GMT): 2010/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4986515
56 A = 6737858
05 meter
Y = 4490266
16 meter E =
0004316
Z = -618940
31 I = 51
45716
XDOT = -3627
268122 Wp = 78
61012
YDOT = 3209
463153 meter/sec RA = 217
78846 deg
ZDOT = -5973
672260 TA = 108
13374
MA = 108
08673
Ha = 194
814 n
mi
Hp = 186
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16359959
20 X = 4938940
69
Y = 14731844
36 feet Y = 4545762
42 meter
Z = -2030644
07 Z = -594830
84
XDOT = -11900
485965 XDOT = -3633
868282
YDOT = 10529
734755 feet/sec YDOT = 3168
864653 meter/sec
ZDOT = -19598
662270 ZDOT = -5991
309218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15614550
95 X = 4759315
13
Y = -15531990
35 feet Y = -4734150
66 meter
Z = -1934449
05 Z = -589620
07
XDOT = 8728
729916 XDOT = 2660
516878
YDOT = 11210
084569 feet/sec YDOT = 3416
833777 meter/sec
ZDOT = -19668
950880 ZDOT = -5995
096228
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 10170
53067918
00016717 00000-0 10270-3 0 9106
2 25544 51
6466 218
6110 0009613 342
6408 17
4424 15
71950214 23849
Satellite: ISS
Catalog Number: 25544
Epoch time: 10170
53067918 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 218
6110 deg
Eccentricity:
0009613
Arg of perigee: 342
6408 deg
Mean anomaly: 17
4424 deg
Mean motion: 15
71950214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2384
Checksum: 289
Coasting Arc #12 (Orbit 2399)
---------------------------------------
Vector Time (GMT): 2010/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2225105
53 A = 6725902
41 meter
Y = -3553222
53 meter E =
0009159
Z = 5259205
49 I = 51
44103
XDOT = 6500
888479 Wp =
98482
YDOT = 4123
428149 meter/sec RA = 212
65005 deg
ZDOT = 44
437235 TA = 88
64470
MA = 88
53978
Ha = 194
846 n
mi
Hp = 186
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7300215
00 X = 2239124
54
Y = -11657554
23 feet Y = -3528262
35 meter
Z = 17254611
18 Z = 5270048
71
XDOT = 21328
374276 XDOT = 6454
080526
YDOT = 13528
307576 feet/sec YDOT = 4195
863237 meter/sec
ZDOT = 145
791455 ZDOT = 75
905543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11374173
81 X = -3466848
18
Y = -7637233
24 feet Y = -2327828
69 meter
Z = 17297807
81 Z = 5272371
82
XDOT = 13774
436044 XDOT = 4198
448106
YDOT = -19966
606779 feet/sec YDOT = -6085
821746 meter/sec
ZDOT = 271
335555 ZDOT = 82
703077
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 10171
54784289
00016717 00000-0 10270-3 0 9116
2 25544 51
6460 213
4040 0009595 346
4470 13
6433 15
71964569 24003
Satellite: ISS
Catalog Number: 25544
Epoch time: 10171
54784289 = yrday
fracday
Element set: 911
Inclination: 51
6460 deg
RA of node: 213
4040 deg
Eccentricity:
0009595
Arg of perigee: 346
4470 deg
Mean anomaly: 13
6433 deg
Mean motion: 15
71964569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2400
Checksum: 303
Coasting Arc #13 (Orbit 2414)
---------------------------------------
Vector Time (GMT): 2010/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6170564
52 A = 6737768
04 meter
Y = -2583561
86 meter E =
0018463
Z = -702810
68 I = 51
50728
XDOT = 1288
374106 Wp = 16
45507
YDOT = -4687
918262 meter/sec RA = 207
51111 deg
ZDOT = 5976
825444 TA = 335
87330
MA = 335
95967
Ha = 195
069 n
mi
Hp = 186
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20244634
26 X = -6137801
90
Y = -8476252
83 feet Y = -2652381
50 meter
Z = -2305809
32 Z = -732708
31
XDOT = 4226
949166 XDOT = 1311
664955
YDOT = -15380
309257 feet/sec YDOT = -4673
381554 meter/sec
ZDOT = 19609
007361 ZDOT = 5983
140291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8897695
14 X = -2712017
48
Y = 20048911
24 feet Y = 6110908
15 meter
Z = -2425080
26 Z = -739164
46
XDOT = -13828
313749 XDOT = -4214
870031
YDOT = -3783
050837 feet/sec YDOT = -1153
073895 meter/sec
ZDOT = 19634
134387 ZDOT = 5984
484161
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 10172
50142299
00016717 00000-0 10270-3 0 9123
2 25544 51
6463 208
5224 0009760 350
4655 9
6320 15
71955326 24156
Satellite: ISS
Catalog Number: 25544
Epoch time: 10172
50142299 = yrday
fracday
Element set: 912
Inclination: 51
6463 deg
RA of node: 208
5224 deg
Eccentricity:
0009760
Arg of perigee: 350
4655 deg
Mean anomaly: 9
6320 deg
Mean motion: 15
71955326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2415
Checksum: 293
Coasting Arc #14 (Orbit 2430)
---------------------------------------
Vector Time (GMT): 2010/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 34543
01 A = 6726679
93 meter
Y = 4402142
82 meter E =
0017616
Z = -5099660
58 I = 51
49777
XDOT = -7336
228448 Wp = 45
49679
YDOT = -1715
050286 meter/sec RA = 202
40142 deg
ZDOT = -1521
259167 TA = 209
80314
MA = 209
90359
Ha = 195
184 n
mi
Hp = 186
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 113330
07 X = 10088
28
Y = 14442725
80 feet Y = 4402393
25 meter
Z = -16731169
88 Z = -5099551
41
XDOT = -24068
990971 XDOT = -7309
115142
YDOT = -5626
805401 feet/sec YDOT = -1796
936505 meter/sec
ZDOT = -4991
007765 ZDOT = -1556
833264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14442866
50 X = 4402185
71
Y = -158454
20 feet Y = -48296
84 meter
Z = -16730681
90 Z = -5099511
84
XDOT = -5727
890574 XDOT = -1745
861047
YDOT = 22964
803695 feet/sec YDOT = 6999
672166 meter/sec
ZDOT = -5132
921644 ZDOT = -1564
514517
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 10173
51856176
00016717 00000-0 10270-3 0 9132
2 25544 51
6467 203
3152 0009650 354
2653 5
8397 15
71981661 24312
Satellite: ISS
Catalog Number: 25544
Epoch time: 10173
51856176 = yrday
fracday
Element set: 913
Inclination: 51
6467 deg
RA of node: 203
3152 deg
Eccentricity:
0009650
Arg of perigee: 354
2653 deg
Mean anomaly: 5
8397 deg
Mean motion: 15
71981661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2431
Checksum: 308
Coasting Arc #15 (Orbit 2446)
---------------------------------------
Vector Time (GMT): 2010/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6441712
55 A = 6736125
82 meter
Y = 397037
06 meter E =
0013607
Z = 1927726
08 I = 51
55702
XDOT = 1374
988674 Wp = 71
25795
YDOT = 5085
991223 meter/sec RA = 197
24265 deg
ZDOT = -5605
662497 TA = 87
30947
MA = 87
15372
Ha = 195
286 n
mi
Hp = 185
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21134227
54 X = 6427429
46
Y = 1302615
04 feet Y = 468991
90 meter
Z = 6324560
63 Z = 1958985
46
XDOT = 4511
117698 XDOT = 1345
245429
YDOT = 16686
322909 feet/sec YDOT = 5101
201934 meter/sec
ZDOT = -18391
281158 ZDOT = -5599
054042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1018270
38 X = 310368
81
Y = -21112142
49 feet Y = -6434981
03 meter
Z = 6449264
44 Z = 1965735
80
XDOT = 15082
391805 XDOT = 4597
113022
YDOT = -4918
494576 feet/sec YDOT = -1499
157147 meter/sec
ZDOT = -18364
860352 ZDOT = -5597
609435
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 10174
53568684
00016717 00000-0 10270-3 0 9140
2 25544 51
6451 198
1076 0009765 358
9058 1
2081 15
72026045 24472
Satellite: ISS
Catalog Number: 25544
Epoch time: 10174
53568684 = yrday
fracday
Element set: 914
Inclination: 51
6451 deg
RA of node: 198
1076 deg
Eccentricity:
0009765
Arg of perigee: 358
9058 deg
Mean anomaly: 1
2081 deg
Mean motion: 15
72026045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2447
Checksum: 316
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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