Date:
February 10th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23680 6 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 320)
---------------------------------------
Vector Time (GMT): 2010/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4922221
80 A = 6720268
20 meter
Y = -2322063
96 meter E =
0003611
Z = 3938698
29 I = 51
69615
XDOT = 5144
124780 Wp = 18
92155
YDOT = -4090
661888 meter/sec RA = 170
39220 deg
ZDOT = 4019
328552 TA = 29
41841
MA = 29
39809
Ha = 187
233 n
mi
Hp = 183
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16149021
64 X = -4915023
31
Y = -7618320
09 feet Y = -2377067
09 meter
Z = 12922238
50 Z = 3914804
03
XDOT = 16877
049804 XDOT = 5169
960213
YDOT = -13420
806718 feet/sec YDOT = -4032
992967 meter/sec
ZDOT = 13186
773463 ZDOT = 4044
380740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6877532
16 X = -2096271
80
Y = -16552117
00 feet Y = -5045085
26 meter
Z = 12827350
57 Z = 3909776
45
XDOT = 20250
799409 XDOT = 6172
443660
YDOT = 1875
886024 feet/sec YDOT = 571
770060 meter/sec
ZDOT = 13286
001569 ZDOT = 4049
573278
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 10039
55498280
00016717 00000-0 10270-3 0 9001
2 25544 51
6441 171
1159 0011231 298
8801 61
1236 15
75843839 3210
Satellite: ISS
Catalog Number: 25544
Epoch time: 10039
55498280 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 171
1159 deg
Eccentricity:
0011231
Arg of perigee: 298
8801 deg
Mean anomaly: 61
1236 deg
Mean motion: 15
75843839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 321
Checksum: 295
Coasting Arc #2 (Orbit 335)
---------------------------------------
Vector Time (GMT): 2010/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4718391
10 A = 6722909
95 meter
Y = 3708083
70 meter E =
0009130
Z = -3016943
92 I = 51
73522
XDOT = -5262
658732 Wp = 326
41875
YDOT = -2658
604806 meter/sec RA = 165
19855 deg
ZDOT = 4963
312465 TA = 358
68648
MA = 358
68887
Ha = 187
408 n
mi
Hp = 182
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15480285
75 X = -4744849
47
Y = 12165628
93 feet Y = 3655172
04 meter
Z = -9898109
97 Z = -3039929
39
XDOT = -17265
940723 XDOT = -5256
648873
YDOT = -8722
456714 feet/sec YDOT = -2717
421576 meter/sec
ZDOT = 16283
833547 ZDOT = 4937
761606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19615087
08 X = -5978678
54
Y = -1038882
34 feet Y = -316651
34 meter
Z = -9989166
00 Z = -3044697
80
XDOT = -7362
249485 XDOT = -2244
013643
YDOT = -16580
638274 feet/sec YDOT = -5053
778546 meter/sec
ZDOT = 16182
346736 ZDOT = 4932
379285
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 10040
50621736
00016717 00000-0 10270-3 0 9013
2 25544 51
6445 166
2187 0011310 303
5452 56
4632 15
75835825 3363
Satellite: ISS
Catalog Number: 25544
Epoch time: 10040
50621736 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 166
2187 deg
Eccentricity:
0011310
Arg of perigee: 303
5452 deg
Mean anomaly: 56
4632 deg
Mean motion: 15
75835825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 336
Checksum: 280
Coasting Arc #3 (Orbit 351)
---------------------------------------
Vector Time (GMT): 2010/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4216254
39 A = 6717462
24 meter
Y = 2382277
31 meter E =
0010520
Z = -4661119
36 I = 51
74646
XDOT = -5635
652584 Wp = 6
55699
YDOT = 4414
359495 meter/sec RA = 160
10284 deg
ZDOT = -2831
990806 TA = 235
45980
MA = 235
55914
Ha = 187
654 n
mi
Hp = 182
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13832855
61 X = 4211944
21
Y = 7815870
43 feet Y = 2429402
00 meter
Z = -15292386
35 Z = -4640647
78
XDOT = -18489
673833 XDOT = -5670
838978
YDOT = 14482
806743 feet/sec YDOT = 4351
141634 meter/sec
ZDOT = -9291
308418 ZDOT = -2859
453356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5559592
71 X = 1694563
86
Y = 14966882
80 feet Y = 4561905
88 meter
Z = -15211053
66 Z = -4636329
16
XDOT = -22335
186569 XDOT = -6807
764866
YDOT = -1289
117103 feet/sec YDOT = -392
922893 meter/sec
ZDOT = -9400
113803 ZDOT = -2865
154687
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 10041
52084199
00016717 00000-0 10270-3 0 9023
2 25544 51
6450 160
9944 0011319 307
2783 52
7348 15
75883317 3528
Satellite: ISS
Catalog Number: 25544
Epoch time: 10041
52084199 = yrday
fracday
Element set: 902
Inclination: 51
6450 deg
RA of node: 160
9944 deg
Eccentricity:
0011319
Arg of perigee: 307
2783 deg
Mean anomaly: 52
7348 deg
Mean motion: 15
75883317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 352
Checksum: 305
Coasting Arc #4 (Orbit 367)
---------------------------------------
Vector Time (GMT): 2010/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5071386
66 A = 6725132
90 meter
Y = -4000216
64 meter E =
0004979
Z = 1872958
41 I = 51
80129
XDOT = 4360
748099 Wp = 67
61735
YDOT = 2873
610210 meter/sec RA = 154
92380 deg
ZDOT = -5656
402846 TA = 91
62716
MA = 91
57013
Ha = 187
764 n
mi
Hp = 182
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16638407
66 X = 5106642
66
Y = -13124070
33 feet Y = -3943308
28 meter
Z = 6144876
69 Z = 1897680
03
XDOT = 14306
916334 XDOT = 4355
767715
YDOT = 9427
855021 feet/sec YDOT = 2922
346905 meter/sec
ZDOT = -18557
752118 ZDOT = -5635
231047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21159571
52 X = 6449437
40
Y = 370034
45 feet Y = 112786
50 meter
Z = 6242831
80 Z = 1902815
13
XDOT = 5203
170959 XDOT = 1585
926508
YDOT = 14885
509060 feet/sec YDOT = 4537
103161 meter/sec
ZDOT = -18473
610567 ZDOT = -5630
756501
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 10042
53544153
00016717 00000-0 10270-3 0 9037
2 25544 51
6454 155
7700 0011236 311
5406 48
4793 15
75922245 3689
Satellite: ISS
Catalog Number: 25544
Epoch time: 10042
53544153 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 155
7700 deg
Eccentricity:
0011236
Arg of perigee: 311
5406 deg
Mean anomaly: 48
4793 deg
Mean motion: 15
75922245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 368
Checksum: 290
Coasting Arc #5 (Orbit 383)
---------------------------------------
Vector Time (GMT): 2010/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3383825
10 A = 6715074
39 meter
Y = -2705355
29 meter E =
0006895
Z = 5133053
20 I = 51
79584
XDOT = 5914
317943 Wp = 322
55727
YDOT = -4727
402042 meter/sec RA = 149
81408 deg
ZDOT = 1413
645639 TA = 113
97204
MA = 113
89983
Ha = 187
949 n
mi
Hp = 182
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11101788
39 X = -3378256
50
Y = -8875837
55 feet Y = -2743164
06 meter
Z = 16840725
73 Z = 5116628
64
XDOT = 19403
930259 XDOT = 5959
874011
YDOT = -15509
849219 feet/sec YDOT = -4661
009906 meter/sec
ZDOT = 4637
945009 ZDOT = 1442
487166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3278744
99 X = -999361
47
Y = -13909536
72 feet Y = -4239626
79 meter
Z = 16775424
29 Z = 5113149
32
XDOT = 23804
523695 XDOT = 7255
618822
YDOT = 94
957423 feet/sec YDOT = 28
943022 meter/sec
ZDOT = 4752
232161 ZDOT = 1448
480363
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 10043
55001386
00016717 00000-0 10270-3 0 9047
2 25544 51
6464 150
5449 0011359 315
8069 44
2187 15
76005019 3842
Satellite: ISS
Catalog Number: 25544
Epoch time: 10043
55001386 = yrday
fracday
Element set: 904
Inclination: 51
6464 deg
RA of node: 150
5449 deg
Eccentricity:
0011359
Arg of perigee: 315
8069 deg
Mean anomaly: 44
2187 deg
Mean motion: 15
76005019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 293
Coasting Arc #6 (Orbit 398)
---------------------------------------
Vector Time (GMT): 2010/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5186588
31 A = 6726373
95 meter
Y = 4226579
23 meter E =
0017163
Z = -570150
42 I = 51
85965
XDOT = -3416
599353 Wp = 359
67568
YDOT = -3381
422398 meter/sec RA = 144
66003 deg
ZDOT = 6029
502148 TA = 354
12675
MA = 354
14685
Ha = 188
186 n
mi
Hp = 181
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17016365
85 X = -5230695
59
Y = 13866729
76 feet Y = 4168333
09 meter
Z = -1870572
23 Z = -595453
32
XDOT = -11209
315461 XDOT = -3407
823086
YDOT = -11093
905505 feet/sec YDOT = -3419
579613 meter/sec
ZDOT = 19781
831195 ZDOT = 6012
926227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21930853
07 X = -6684524
02
Y = 703852
88 feet Y = 214534
36 meter
Z = -1970841
54 Z = -600712
50
XDOT = -2219
562592 XDOT = -676
522678
YDOT = -14090
610770 feet/sec YDOT = -4294
818163 meter/sec
ZDOT = 19715
895070 ZDOT = 6009
404817
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 10044
50115481
00016717 00000-0 10270-3 0 9056
2 25544 51
6467 145
6473 0011469 320
5238 39
5089 15
75987312 3998
Satellite: ISS
Catalog Number: 25544
Epoch time: 10044
50115481 = yrday
fracday
Element set: 905
Inclination: 51
6467 deg
RA of node: 145
6473 deg
Eccentricity:
0011469
Arg of perigee: 320
5238 deg
Mean anomaly: 39
5089 deg
Mean motion: 15
75987312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 399
Checksum: 318
Coasting Arc #7 (Orbit 414)
---------------------------------------
Vector Time (GMT): 2010/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2583354
89 A = 6714263
13 meter
Y = 3251924
36 meter E =
0012356
Z = -5282660
44 I = 51
84309
XDOT = -5924
866483 Wp = 42
83237
YDOT = 4913
893983 meter/sec RA = 139
53007 deg
ZDOT = 136
564357 TA = 228
40729
MA = 228
51325
Ha = 188
335 n
mi
Hp = 181
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8475573
78 X = 2572460
77
Y = 10669043
19 feet Y = 3280751
83 meter
Z = -17331563
12 Z = -5270137
47
XDOT = -19438
538329 XDOT = -5980
037556
YDOT = 16121
699419 feet/sec YDOT = 4847
330140 meter/sec
ZDOT = 448
045792 ZDOT = 107
647964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 579622
14 X = 176668
83
Y = 13676739
89 feet Y = 4168670
32 meter
Z = -17281716
86 Z = -5267467
30
XDOT = -24216
689251 XDOT = -7381
246884
YDOT = 1409
998226 feet/sec YDOT = 429
767459 meter/sec
ZDOT = 333
453090 ZDOT = 101
636502
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 10045
51567929
00016717 00000-0 10270-3 0 9067
2 25544 51
6465 140
4232 0011484 324
2054 35
8339 15
76049045 4155
Satellite: ISS
Catalog Number: 25544
Epoch time: 10045
51567929 = yrday
fracday
Element set: 906
Inclination: 51
6465 deg
RA of node: 140
4232 deg
Eccentricity:
0011484
Arg of perigee: 324
2054 deg
Mean anomaly: 35
8339 deg
Mean motion: 15
76049045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 415
Checksum: 296
Coasting Arc #8 (Orbit 430)
---------------------------------------
Vector Time (GMT): 2010/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5113494
81 A = 6725971
24 meter
Y = -4291698
47 meter E =
0001747
Z = -829282
83 I = 51
90427
XDOT = 2507
300556 Wp = 19
80996
YDOT = 4143
028609 meter/sec RA = 134
40489 deg
ZDOT = -5982
586054 TA = 169
20209
MA = 169
19834
Ha = 188
399 n
mi
Hp = 181
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16776557
79 X = 5165133
71
Y = -14080375
56 feet Y = -4234227
66 meter
Z = -2720744
19 Z = -804316
42
XDOT = 8226
051693 XDOT = 2489
847716
YDOT = 13592
613545 feet/sec YDOT = 4170
968795 meter/sec
ZDOT = -19627
907001 ZDOT = -5970
448532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21843931
48 X = 6658030
31
Y = -1755315
94 feet Y = -535020
30 meter
Z = -2621800
82 Z = -799124
89
XDOT = -1198
579953 XDOT = -365
327170
YDOT = 14318
645312 feet/sec YDOT = 4364
323091 meter/sec
ZDOT = -19579
552477 ZDOT = -5967
847595
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 10046
53017895
00016717 00000-0 10270-3 0 9073
2 25544 51
6456 135
1982 0011409 328
4034 31
6444 15
76082618 4311
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
53017895 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 135
1982 deg
Eccentricity:
0011409
Arg of perigee: 328
4034 deg
Mean anomaly: 31
6444 deg
Mean motion: 15
76082618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 431
Checksum: 298
Coasting Arc #9 (Orbit 446)
---------------------------------------
Vector Time (GMT): 2010/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1834332
67 A = 6714929
96 meter
Y = -4024510
21 meter E =
0013338
Z = 5056964
46 I = 51
88865
XDOT = 5730
163773 Wp = 355
37224
YDOT = -4835
369229 meter/sec RA = 129
24890 deg
ZDOT = -1756
934251 TA = 111
55484
MA = 111
41263
Ha = 188
522 n
mi
Hp = 180
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6018151
80 X = -1813758
85
Y = -13203773
65 feet Y = -4044907
43 meter
Z = 16591090
74 Z = 5048103
70
XDOT = 18799
749911 XDOT = 5792
342542
YDOT = -15864
072272 feet/sec YDOT = -4770
943597 meter/sec
ZDOT = -5764
219982 ZDOT = -1728
946348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2413532
86 X = 735644
81
Y = -14349357
94 feet Y = -4373684
30 meter
Z = 16555750
29 Z = 5046192
69
XDOT = 23455
993667 XDOT = 7149
386870
YDOT = -2625
477742 feet/sec YDOT = -800
245616 meter/sec
ZDOT = -5653
296030 ZDOT = -1723
124630
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 10047
54465121
00016717 00000-0 10270-3 0 9085
2 25544 51
6462 129
9721 0011596 332
2780 27
7765 15
76163206 4470
Satellite: ISS
Catalog Number: 25544
Epoch time: 10047
54465121 = yrday
fracday
Element set: 908
Inclination: 51
6462 deg
RA of node: 129
9721 deg
Eccentricity:
0011596
Arg of perigee: 332
2780 deg
Mean anomaly: 27
7765 deg
Mean motion: 15
76163206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 447
Checksum: 309
Coasting Arc #10 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2010/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4855212
15 A = 6723946
44 meter
Y = 4073448
21 meter E =
0017520
Z = 2210837
82 I = 51
93646
XDOT = -1762
065387 Wp = 30
12358
YDOT = -5095
658572 meter/sec RA = 124
15101 deg
ZDOT = 5515
189432 TA = 354
60662
MA = 354
62546
Ha = 188
765 n
mi
Hp = 180
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15929173
72 X = -4911140
99
Y = 13364331
38 feet Y = 4018841
78 meter
Z = 7253404
93 Z = 2187115
47
XDOT = -5781
054418 XDOT = -1731
745213
YDOT = -16718
039934 feet/sec YDOT = -5115
193118 meter/sec
ZDOT = 18094
453518 ZDOT = 5506
703466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20691287
23 X = -6306704
35
Y = 2360030
28 feet Y = 719337
23 meter
Z = 7159378
59 Z = 2182178
59
XDOT = 4464
239119 XDOT = 1360
700083
YDOT = -15687
572565 feet/sec YDOT = -4781
572118 meter/sec
ZDOT = 18060
560879 ZDOT = 5504
858956
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 10048
55910059
00016717 00000-0 10270-3 0 9093
2 25544 51
6455 124
7468 0011555 336
9383 23
1261 15
76166175 4635
Satellite: ISS
Catalog Number: 25544
Epoch time: 10048
55910059 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 124
7468 deg
Eccentricity:
0011555
Arg of perigee: 336
9383 deg
Mean anomaly: 23
1261 deg
Mean motion: 15
76166175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 312
Coasting Arc #11 (Orbit 477)
---------------------------------------
Vector Time (GMT): 2010/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1293084
88 A = 6717225
21 meter
Y = 4861880
80 meter E =
0009225
Z = -4451315
09 I = 51
92943
XDOT = -5385
961054 Wp = 34
82623
YDOT = 4424
582970 meter/sec RA = 118
97697 deg
ZDOT = 3278
804461 TA = 267
85108
MA = 267
95672
Ha = 188
835 n
mi
Hp = 180
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4242404
48 X = 1260245
77
Y = 15951052
48 feet Y = 4876156
94 meter
Z = -14604052
13 Z = -4445113
44
XDOT = -17670
475900 XDOT = -5450
964866
YDOT = 14516
348326 feet/sec YDOT = 4363
990709 meter/sec
ZDOT = 10757
232484 ZDOT = 3252
481629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4900443
51 X = -1493655
18
Y = 15784287
61 feet Y = 4811050
86 meter
Z = -14579243
04 Z = -4443753
28
XDOT = -21601
548519 XDOT = -6584
151989
YDOT = 3100
576308 feet/sec YDOT = 945
055659 meter/sec
ZDOT = 10652
885888 ZDOT = 3246
999619
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 10049
51012277
00016717 00000-0 10270-3 0 9107
2 25544 51
6444 119
8480 0011602 341
1812 18
8922 15
76227399 4787
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
51012277 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 119
8480 deg
Eccentricity:
0011602
Arg of perigee: 341
1812 deg
Mean anomaly: 18
8922 deg
Mean motion: 15
76227399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 478
Checksum: 298
Coasting Arc #12 (Orbit 493)
---------------------------------------
Vector Time (GMT): 2010/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4542873
31 A = 6720649
22 meter
Y = -3543324
83 meter E =
0011674
Z = -3473453
61 I = 51
95417
XDOT = 1227
097845 Wp = 10
17296
YDOT = 6064
395179 meter/sec RA = 113
89499 deg
ZDOT = -4572
569294 TA = 210
79399
MA = 210
86253
Ha = 188
945 n
mi
Hp = 179
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14904439
98 X = 4599031
00
Y = -11625081
45 feet Y = -3492209
90 meter
Z = -11395845
17 Z = -3451247
97
XDOT = 4025
911564 XDOT = 1181
405994
YDOT = 19896
309642 feet/sec YDOT = 6077
861608 meter/sec
ZDOT = -15001
867764 ZDOT = -4566
719404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18837148
63 X = 5741562
90
Y = -2108447
40 feet Y = -642654
77 meter
Z = -11307803
42 Z = -3446618
48
XDOT = -7022
722494 XDOT = -2140
525816
YDOT = 17746
817380 feet/sec YDOT = 5409
229937 meter/sec
ZDOT = -14978
417255 ZDOT = -4565
421579
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 10050
52452229
00016717 00000-0 10270-3 0 9116
2 25544 51
6441 114
6214 0011639 345
2095 14
8727 15
76237020 4949
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
52452229 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 114
6214 deg
Eccentricity:
0011639
Arg of perigee: 345
2095 deg
Mean anomaly: 14
8727 deg
Mean motion: 15
76237020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 494
Checksum: 279
Coasting Arc #13 (Orbit 509)
---------------------------------------
Vector Time (GMT): 2010/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -906112
44 A = 6720459
73 meter
Y = -5705337
50 meter E =
0015579
Z = 3437146
93 I = 51
96606
XDOT = 5019
693592 Wp = 40
72081
YDOT = -3586
547293 meter/sec RA = 108
71333 deg
ZDOT = -4606
830356 TA = 98
79933
MA = 98
62288
Ha = 189
028 n
mi
Hp = 179
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2972809
86 X = -858943
89
Y = -18718298
89 feet Y = -5715206
34 meter
Z = 11276728
76 Z = 3432859
84
XDOT = 16468
810996 XDOT = 5081
804876
YDOT = -11766
887443 feet/sec YDOT = -3530
066973 meter/sec
ZDOT = -15114
272821 ZDOT = -4582
293916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6868590
67 X = 2093546
44
Y = -17675489
41 feet Y = -5387489
17 meter
Z = 11259505
29 Z = 3431897
21
XDOT = 18948
408405 XDOT = 5775
474882
YDOT = -2251
291097 feet/sec YDOT = -686
193526 meter/sec
ZDOT = -15016
966664 ZDOT = -4577
171439
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 10051
53889414
00016717 00000-0 10270-3 0 9129
2 25544 51
6446 109
3948 0011864 348
8356 11
2544 15
76318459 5101
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051
53889414 = yrday
fracday
Element set: 912
Inclination: 51
6446 deg
RA of node: 109
3948 deg
Eccentricity:
0011864
Arg of perigee: 348
8356 deg
Mean anomaly: 11
2544 deg
Mean motion: 15
76318459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 510
Checksum: 314
Coasting Arc #14 (Orbit 525)
---------------------------------------
Vector Time (GMT): 2010/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4244395
33 A = 6716873
64 meter
Y = 2637956
00 meter E =
0010844
Z = 4477656
54 I = 51
96226
XDOT = -914
401814 Wp = 40
41722
YDOT = -6943
491933 meter/sec RA = 103
63234 deg
ZDOT = 3227
670012 TA = 17
49932
MA = 17
46199
Ha = 189
264 n
mi
Hp = 179
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13925181
53 X = -4295329
40
Y = 8654711
29 feet Y = 2590207
94 meter
Z = 14690474
22 Z = 4456913
71
XDOT = -3000
005951 XDOT = -852
369778
YDOT = -22780
485344 feet/sec YDOT = -6953
370425 meter/sec
ZDOT = 10589
468543 ZDOT = 3223
378678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16456428
42 X = -5015919
38
Y = 641494
08 feet Y = 195527
39 meter
Z = 14608189
14 Z = 4452576
05
XDOT = 8588
753548 XDOT = 2617
852082
YDOT = -20138
927195 feet/sec YDOT = -6138
345009 meter/sec
ZDOT = 10572
195323 ZDOT = 3222
405134
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 10052
55324261
00016717 00000-0 10270-3 0 9137
2 25544 51
6443 104
1681 0011759 353
5378 6
5633 15
76333097 5263
Satellite: ISS
Catalog Number: 25544
Epoch time: 10052
55324261 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 104
1681 deg
Eccentricity:
0011759
Arg of perigee: 353
5378 deg
Mean anomaly: 6
5633 deg
Mean motion: 15
76333097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 526
Checksum: 294
Coasting Arc #15 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2010/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 735096
03 A = 6723487
44 meter
Y = 6327688
25 meter E =
0017033
Z = -2121564
21 I = 51
99121
XDOT = -4757
767451 Wp = 12
57742
YDOT = 2411
202930 meter/sec RA = 98
46048 deg
ZDOT = 5567
569605 TA = 323
77987
MA = 323
89508
Ha = 189
285 n
mi
Hp = 178
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2411732
37 X = 674590
10
Y = 20760132
04 feet Y = 6335570
22 meter
Z = -6960512
51 Z = -2118140
14
XDOT = -15609
473266 XDOT = -4811
422250
YDOT = 7910
770767 feet/sec YDOT = 2357
698757 meter/sec
ZDOT = 18266
304479 ZDOT = 5544
326335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7745862
88 X = -2360939
01
Y = 19416309
16 feet Y = 5918091
03 meter
Z = -6946712
65 Z = -2117358
02
XDOT = -16171
137898 XDOT = -4928
962831
YDOT = 22
175518 feet/sec YDOT = 6
759098 meter/sec
ZDOT = 18174
071245 ZDOT = 5539
456915
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 10053
50417101
00016717 00000-0 10270-3 0 9140
2 25544 51
6447 99
2683 0011839 357
4912 2
6191 15
76367404 5411
Satellite: ISS
Catalog Number: 25544
Epoch time: 10053
50417101 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 99
2683 deg
Eccentricity:
0011839
Arg of perigee: 357
4912 deg
Mean anomaly: 2
6191 deg
Mean motion: 15
76367404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 295
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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