Date:
June 15th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 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 2304)
---------------------------------------
Vector Time (GMT): 2010/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4799390
75 A = 6731909
22 meter
Y = -2767140
95 meter E =
0005381
Z = -3820444
16 I = 51
34174
XDOT = 454
000932 Wp = 3
01149
YDOT = -6480
498404 meter/sec RA = 243
44714 deg
ZDOT = 4129
037854 TA = 310
35231
MA = 310
39929
Ha = 193
864 n
mi
Hp = 188
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15746032
64 X = -4749532
46
Y = -9078546
42 feet Y = -2820531
07 meter
Z = -12534265
63 Z = -3843638
91
XDOT = 1489
504370 XDOT = 506
375301
YDOT = -21261
477705 feet/sec YDOT = -6475
129464 meter/sec
ZDOT = 13546
712120 ZDOT = 4131
369325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11196048
80 X = -3412555
68
Y = 14236551
92 feet Y = 4339301
02 meter
Z = -12626735
31 Z = -3848628
92
XDOT = -19812
340043 XDOT = -6038
801245
YDOT = -3573
963304 feet/sec YDOT = -1089
344015 meter/sec
ZDOT = 13555
964222 ZDOT = 4131
857895
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
50826600
00016717 00000-0 10270-3 0 9007
2 25544 51
6468 244
3240 0009251 320
1648 39
8830 15
71836290 23055
Satellite: ISS
Catalog Number: 25544
Epoch time: 10165
50826600 = yrday
fracday
Element set: 900
Inclination: 51
6468 deg
RA of node: 244
3240 deg
Eccentricity:
0009251
Arg of perigee: 320
1648 deg
Mean anomaly: 39
8830 deg
Mean motion: 15
71836290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2305
Checksum: 286
Coasting Arc #2 (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 = 771276
18 A = 6734298
06 meter
Y = 5942885
13 meter E =
0006412
Z = -3078796
45 I = 51
36291
XDOT = -5675
753488 Wp = 350
59716
YDOT = -1790
326868 meter/sec RA = 238
35844 deg
ZDOT = -4869
984948 TA = 225
20782
MA = 225
25999
Ha = 194
206 n
mi
Hp = 188
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2530433
66 X = 719720
54
Y = 19497654
62 feet Y = 5951222
27 meter
Z = -10101038
22 Z = -3075173
82
XDOT = -18621
238479 XDOT = -5631
654607
YDOT = -5873
775813 feet/sec YDOT = -1853
549108 meter/sec
ZDOT = -15977
640907 ZDOT = -4897
450709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19667988
25 X = 5994802
82
Y = -156038
24 feet Y = -47560
45 meter
Z = -10086550
15 Z = -3074380
49
XDOT = -8134
352744 XDOT = -2479
350717
YDOT = 16222
454440 feet/sec YDOT = 4944
604113 meter/sec
ZDOT = -16087
143340 ZDOT = -4903
361290
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
52550931
00016717 00000-0 10270-3 0 9012
2 25544 51
6457 239
1175 0009298 324
4631 35
5911 15
71818236 23213
Satellite: ISS
Catalog Number: 25544
Epoch time: 10166
52550931 = yrday
fracday
Element set: 901
Inclination: 51
6457 deg
RA of node: 239
1175 deg
Eccentricity:
0009298
Arg of perigee: 324
4631 deg
Mean anomaly: 35
5911 deg
Mean motion: 15
71818236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2321
Checksum: 299
Coasting Arc #3 (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 = 4878081
11 A = 6728847
52 meter
Y = 345867
47 meter E =
0011888
Z = 4625409
55 I = 51
36261
XDOT = 2234
773904 Wp = 10
85777
YDOT = 6787
412911 meter/sec RA = 233
17332 deg
ZDOT = -2851
687783 TA = 107
53458
MA = 107
40464
Ha = 194
278 n
mi
Hp = 187
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16004203
12 X = 4851381
82
Y = 1134735
78 feet Y = 400267
11 meter
Z = 15175228
18 Z = 4649042
24
XDOT = 7331
935379 XDOT = 2172
562579
YDOT = 22268
415062 feet/sec YDOT = 6812
056065 meter/sec
ZDOT = -9355
931045 ZDOT = -2840
981457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2827251
66 X = 861746
31
Y = -15702237
85 feet Y = -4786042
10 meter
Z = 15269448
83 Z = 4654128
00
XDOT = 21784
308347 XDOT = 6639
857184
YDOT = -5174
396928 feet/sec YDOT = -1577
156184 meter/sec
ZDOT = -9313
182997 ZDOT = -2838
658177
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
54274301
00016717 00000-0 10270-3 0 9020
2 25544 51
6462 233
9104 0009518 328
2206 31
8380 15
71873549 23372
Satellite: ISS
Catalog Number: 25544
Epoch time: 10167
54274301 = yrday
fracday
Element set: 902
Inclination: 51
6462 deg
RA of node: 233
9104 deg
Eccentricity:
0009518
Arg of perigee: 328
2206 deg
Mean anomaly: 31
8380 deg
Mean motion: 15
71873549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2337
Checksum: 296
Coasting Arc #4 (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 = -3097199
51 A = 6736892
79 meter
Y = -5672653
04 meter E =
0016605
Z = 1861799
30 I = 51
40746
XDOT = 5168
224739 Wp = 31
84734
YDOT = -970
775453 meter/sec RA = 228
07489 deg
ZDOT = 5630
898996 TA = 348
89446
MA = 348
93107
Ha = 194
604 n
mi
Hp = 187
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10161415
73 X = -3042580
91
Y = -18611066
39 feet Y = -5706982
61 meter
Z = 6108265
43 Z = 1846885
17
XDOT = 16956
117910 XDOT = 5151
342327
YDOT = -3184
958836 feet/sec YDOT = -913
076386 meter/sec
ZDOT = 18474
078072 ZDOT = 5655
964921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19449776
88 X = -5928291
99
Y = 8488580
21 feet Y = 2587319
25 meter
Z = 6048739
85 Z = 1843655
91
XDOT = -1042
928867 XDOT = -317
884719
YDOT = -15645
982520 feet/sec YDOT = -4768
895472 meter/sec
ZDOT = 18574
006515 ZDOT = 5661
357186
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
55997308
00016717 00000-0 10270-3 0 9032
2 25544 51
6455 228
7036 0009473 333
7515 26
3165 15
71829207 23534
Satellite: ISS
Catalog Number: 25544
Epoch time: 10168
55997308 = yrday
fracday
Element set: 903
Inclination: 51
6455 deg
RA of node: 228
7036 deg
Eccentricity:
0009473
Arg of perigee: 333
7515 deg
Mean anomaly: 26
3165 deg
Mean motion: 15
71829207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2353
Checksum: 320
Coasting Arc #5 (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 = -3908783
23 A = 6726853
01 meter
Y = 1950919
21 meter E =
0011933
Z = -5122754
26 I = 51
39481
XDOT = -4736
412789 Wp = 58
47419
YDOT = -5901
766881 meter/sec RA = 222
91037 deg
ZDOT = 1374
893783 TA = 224
70129
MA = 224
79754
Ha = 194
693 n
mi
Hp = 187
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12824091
97 X = -3905422
93
Y = 6400653
59 feet Y = 1907228
24 meter
Z = -16806936
56 Z = -5141734
69
XDOT = -15539
412036 XDOT = -4676
745102
YDOT = -19362
752233 feet/sec YDOT = -5954
398808 meter/sec
ZDOT = 4510
806374 ZDOT = 1352
028632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5461209
32 X = 1664576
60
Y = 13154923
83 feet Y = 4009620
78 meter
Z = -16882594
29 Z = -5145814
74
XDOT = -19480
395675 XDOT = -5937
624602
YDOT = 13723
529179 feet/sec YDOT = 4182
931694 meter/sec
ZDOT = 4419
564803 ZDOT = 1347
083352
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
51361720
00016717 00000-0 10270-3 0 9043
2 25544 51
6453 223
8222 0009566 337
0600 23
0134 15
71841130 23685
Satellite: ISS
Catalog Number: 25544
Epoch time: 10169
51361720 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 223
8222 deg
Eccentricity:
0009566
Arg of perigee: 337
0600 deg
Mean anomaly: 23
0134 deg
Mean motion: 15
71841130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2368
Checksum: 272
Coasting Arc #6 (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 = 5033096
23 A = 6738068
94 meter
Y = 4448318
39 meter E =
0004398
Z = -540910
89 I = 51
45660
XDOT = -3542
268663 Wp = 80
46597
YDOT = 3285
293313 meter/sec RA = 217
79241 deg
ZDOT = -5983
466707 TA = 105
42443
MA = 105
37585
Ha = 194
880 n
mi
Hp = 187
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16512782
90 X = 4985607
90
Y = 14594220
44 feet Y = 4504336
01 meter
Z = -1774642
02 Z = -516574
92
XDOT = -11621
616347 XDOT = -3549
675507
YDOT = 10778
521368 feet/sec YDOT = 3245
640818 meter/sec
ZDOT = -19630
796283 ZDOT = -6000
692689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15485512
82 X = 4719984
31
Y = -15690677
52 feet Y = -4782518
51 meter
Z = -1677544
36 Z = -511315
52
XDOT = 8980
994208 XDOT = 2737
407035
YDOT = 10954
623771 feet/sec YDOT = 3338
969325 meter/sec
ZDOT = -19699
445135 ZDOT = -6004
390877
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
53083105
00016717 00000-0 10270-3 0 9056
2 25544 51
6460 218
6151 0009600 341
9925 18
0896 15
71889406 23844
Satellite: ISS
Catalog Number: 25544
Epoch time: 10170
53083105 = yrday
fracday
Element set: 905
Inclination: 51
6460 deg
RA of node: 218
6151 deg
Eccentricity:
0009600
Arg of perigee: 341
9925 deg
Mean anomaly: 18
0896 deg
Mean motion: 15
71889406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2384
Checksum: 304
Coasting Arc #7 (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 = 2116891
39 A = 6726113
68 meter
Y = -3621246
95 meter E =
0008886
Z = 5257672
53 I = 51
44038
XDOT = 6547
622182 Wp =
50022
YDOT = 4045
825146 meter/sec RA = 212
65616 deg
ZDOT = 159
064804 TA = 88
03653
MA = 87
93477
Ha = 194
929 n
mi
Hp = 186
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6945181
72 X = 2131686
54
Y = -11880731
47 feet Y = -3597492
55 meter
Z = 17249581
78 Z = 5267991
92
XDOT = 21481
700073 XDOT = 6501
121683
YDOT = 13273
704548 feet/sec YDOT = 4118
784543 meter/sec
ZDOT = 521
866155 ZDOT = 190
760882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11610719
54 X = -3538947
32
Y = -7291000
02 feet Y = -2222296
81 meter
Z = 17290688
58 Z = 5270201
88
XDOT = 13551
037010 XDOT = 4130
356081
YDOT = -20110
053014 feet/sec YDOT = -6129
544159 meter/sec
ZDOT = 648
317587 ZDOT = 197
607201
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
54803741
00016717 00000-0 10270-3 0 9065
2 25544 51
6454 213
4083 0009582 345
8182 14
2709 15
71894220 24001
Satellite: ISS
Catalog Number: 25544
Epoch time: 10171
54803741 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 213
4083 deg
Eccentricity:
0009582
Arg of perigee: 345
8182 deg
Mean anomaly: 14
2709 deg
Mean motion: 15
71894220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2400
Checksum: 290
Coasting Arc #8 (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 = -6195522
54 A = 6737896
24 meter
Y = -2486365
35 meter E =
0018140
Z = -826332
44 I = 51
50635
XDOT = 1120
818196 Wp = 15
38550
YDOT = -4756
644981 meter/sec RA = 207
51556 deg
ZDOT = 5955
832923 TA = 335
58449
MA = 335
67031
Ha = 195
152 n
mi
Hp = 186
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20326517
51 X = -6163244
88
Y = -8157366
63 feet Y = -2555466
78 meter
Z = -2711064
43 Z = -856352
48
XDOT = 3677
225054 XDOT = 1144
991993
YDOT = -15605
790620 feet/sec YDOT = -4743
977043 meter/sec
ZDOT = 19540
134263 ZDOT = 5961
335913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8580554
78 X = -2615353
10
Y = 20135052
50 feet Y = 6137164
00 meter
Z = -2830822
35 Z = -862834
65
XDOT = -14058
957918 XDOT = -4285
170374
YDOT = -3261
706647 feet/sec YDOT = -994
168186 meter/sec
ZDOT = 19562
022555 ZDOT = 5962
504475
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
50166265
00016717 00000-0 10270-3 0 9076
2 25544 51
6458 208
5270 0009736 349
7995 10
2968 15
71880052 24151
Satellite: ISS
Catalog Number: 25544
Epoch time: 10172
50166265 = yrday
fracday
Element set: 907
Inclination: 51
6458 deg
RA of node: 208
5270 deg
Eccentricity:
0009736
Arg of perigee: 349
7995 deg
Mean anomaly: 10
2968 deg
Mean motion: 15
71880052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2415
Checksum: 321
Coasting Arc #9 (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 = 219583
78 A = 6727110
25 meter
Y = 4443853
16 meter E =
0017441
Z = -5059171
66 I = 51
49772
XDOT = -7331
869092 Wp = 44
01815
YDOT = -1570
253708 meter/sec RA = 202
40889 deg
ZDOT = -1688
660033 TA = 209
62758
MA = 209
72650
Ha = 195
296 n
mi
Hp = 186
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 720419
23 X = 194452
21
Y = 14579570
75 feet Y = 4446169
03 meter
Z = -16598332
22 Z = -5058165
20
XDOT = -24054
688623 XDOT = -7305
562043
YDOT = -5151
751009 feet/sec YDOT = -1652
095657 meter/sec
ZDOT = -5540
223204 ZDOT = -1724
214885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14581969
78 X = 4444584
39
Y = -764234
91 feet Y = -232938
80 meter
Z = -16594264
73 Z = -5057931
89
XDOT = -5296
966440 XDOT = -1614
515371
YDOT = 22938
880361 feet/sec YDOT = 6991
770734 meter/sec
ZDOT = -5682
058583 ZDOT = -1731
891456
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
51885517
00016717 00000-0 10270-3 0 9087
2 25544 51
6461 203
3201 0009641 353
6583 6
4456 15
71895298 24319
Satellite: ISS
Catalog Number: 25544
Epoch time: 10173
51885517 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 203
3201 deg
Eccentricity:
0009641
Arg of perigee: 353
6583 deg
Mean anomaly: 6
4456 deg
Mean motion: 15
71895298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2431
Checksum: 310
Coasting Arc #10 (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 = 6396406
85 A = 6736098
10 meter
Y = 243073
58 meter E =
0013850
Z = 2096676
27 I = 51
55535
XDOT = 1628
669420 Wp = 69
17513
YDOT = 5098
733698 meter/sec RA = 197
24821 deg
ZDOT = -5525
559891 TA = 87
40654
MA = 87
24800
Ha = 195
412 n
mi
Hp = 186
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20985586
77 X = 6383028
03
Y = 797485
48 feet Y = 314526
80 meter
Z = 6878859
16 Z = 2127717
73
XDOT = 5343
403609 XDOT = 1598
375706
YDOT = 16728
128932 feet/sec YDOT = 5116
778126 meter/sec
ZDOT = -18128
477333 ZDOT = -5517
720383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 515253
22 X = 157049
18
Y = -20953433
12 feet Y = -6386606
42 meter
Z = 7002691
84 Z = 2134420
47
XDOT = 15124
575746 XDOT = 4609
970687
YDOT = -5713
021045 feet/sec YDOT = -1741
328815 meter/sec
ZDOT = -18097
145499 ZDOT = -5516
009948
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
53603976
00016717 00000-0 10270-3 0 9098
2 25544 51
6445 198
1128 0009769 358
2790 1
8337 15
71930942 24472
Satellite: ISS
Catalog Number: 25544
Epoch time: 10174
53603976 = yrday
fracday
Element set: 909
Inclination: 51
6445 deg
RA of node: 198
1128 deg
Eccentricity:
0009769
Arg of perigee: 358
2790 deg
Mean anomaly: 1
8337 deg
Mean motion: 15
71930942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2447
Checksum: 334
Coasting Arc #11 (Orbit 2462)
---------------------------------------
Vector Time (GMT): 2010/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2606552
68 A = 6729262
79 meter
Y = -4234639
90 meter E =
0010579
Z = 4523425
16 I = 51
56044
XDOT = 6986
611240 Wp = 53
64955
YDOT = -1002
076940 meter/sec RA = 192
16444 deg
ZDOT = 3088
996657 TA = 5
56732
MA = 5
55557
Ha = 195
623 n
mi
Hp = 185
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8551682
03 X = -2580980
45
Y = -13893175
53 feet Y = -4263645
87 meter
Z = 14840633
73 Z = 4510823
76
XDOT = 22921
952888 XDOT = 6982
291583
YDOT = -3287
654002 feet/sec YDOT = -923
973271 meter/sec
ZDOT = 10134
503468 ZDOT = 3122
926962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13621088
53 X = -4151707
78
Y = 9061383
73 feet Y = 2761909
76 meter
Z = 14790310
12 Z = 4508086
52
XDOT = -3326
407587 XDOT = -1013
889032
YDOT = -21756
790829 feet/sec YDOT = -6631
469845 meter/sec
ZDOT = 10269
865383 ZDOT = 3130
254969
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 10175
55321776
00016717 00000-0 10270-3 0 9108
2 25544 51
6438 192
9053 0009811 2
4560 357
6649 15
71919800 24630
Satellite: ISS
Catalog Number: 25544
Epoch time: 10175
55321776 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 192
9053 deg
Eccentricity:
0009811
Arg of perigee: 2
4560 deg
Mean anomaly: 357
6649 deg
Mean motion: 15
71919800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2463
Checksum: 312
Coasting Arc #12 (Orbit 2477)
---------------------------------------
Vector Time (GMT): 2010/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5565957
81 A = 6733325
98 meter
Y = 1920255
00 meter E =
0011662
Z = -3260397
41 I = 51
60509
XDOT = -4257
907556 Wp = 29
52335
YDOT = -4311
847244 meter/sec RA = 186
99378 deg
ZDOT = 4746
464946 TA = 292
29933
MA = 292
42294
Ha = 195
587 n
mi
Hp = 185
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18261016
42 X = -5571178
41
Y = 6300049
23 feet Y = 1857984
63 meter
Z = -10696841
88 Z = -3287449
03
XDOT = -13969
512980 XDOT = -4232
432626
YDOT = -14146
480460 feet/sec YDOT = -4359
320250 meter/sec
ZDOT = 15572
391555 ZDOT = 4725
841081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7163567
65 X = 2183455
42
Y = 17875069
33 feet Y = 5448321
13 meter
Z = -10804765
72 Z = -3293292
59
XDOT = -12153
174353 XDOT = -3704
287543
YDOT = 14199
944610 feet/sec YDOT = 4328
143117 meter/sec
ZDOT = 15490
047586 ZDOT = 4721
366504
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 10176
50681416
00016717 00000-0 10270-3 0 9115
2 25544 51
6444 188
0244 0009880 5
6740 354
4532 15
71942232 24783
Satellite: ISS
Catalog Number: 25544
Epoch time: 10176
50681416 = yrday
fracday
Element set: 911
Inclination: 51
6444 deg
RA of node: 188
0244 deg
Eccentricity:
0009880
Arg of perigee: 5
6740 deg
Mean anomaly: 354
4532 deg
Mean motion: 15
71942232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2478
Checksum: 302
Coasting Arc #13 (Orbit 2493)
---------------------------------------
Vector Time (GMT): 2010/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4682909
77 A = 6732128
58 meter
Y = 3106368
55 meter E =
0013080
Z = -3722753
78 I = 51
62954
XDOT = -5525
218866 Wp = 33
94000
YDOT = 3201
485795 meter/sec RA = 181
92280 deg
ZDOT = -4275
422386 TA = 190
84259
MA = 190
87081
Ha = 195
763 n
mi
Hp = 185
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15363877
19 X = 4665910
07
Y = 10191497
85 feet Y = 3158641
34 meter
Z = -12213759
12 Z = -3700045
04
XDOT = -18127
358483 XDOT = -5539
838749
YDOT = 10503
562319 feet/sec YDOT = 3139
618629 meter/sec
ZDOT = -14026
976331 ZDOT = -4302
298557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9165512
08 X = 2793648
08
Y = -16065964
46 feet Y = -4896905
97 meter
Z = -12123095
18 Z = -3695119
41
XDOT = 10482
961449 XDOT = 3195
206650
YDOT = 16654
421672 feet/sec YDOT = 5076
267726 meter/sec
ZDOT = -14134
201518 ZDOT = -4308
104623
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 10177
52397701
00016717 00000-0 10270-3 0 9120
2 25544 51
6431 182
8163 0009871 9
1865 350
9476 15
71943580 24941
Satellite: ISS
Catalog Number: 25544
Epoch time: 10177
52397701 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 182
8163 deg
Eccentricity:
0009871
Arg of perigee: 9
1865 deg
Mean anomaly: 350
9476 deg
Mean motion: 15
71943580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2494
Checksum: 325
Coasting Arc #14 (Orbit 2509)
---------------------------------------
Vector Time (GMT): 2010/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3932885
62 A = 6730311
42 meter
Y = -3526202
29 meter E =
0017310
Z = 4168721
10 I = 51
65386
XDOT = 6244
027032 Wp = 44
00809
YDOT = 2572
241643 meter/sec RA = 176
75204 deg
ZDOT = -3693
621872 TA = 83
81433
MA = 83
61715
Ha = 195
776 n
mi
Hp = 185
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12903168
04 X = 3951773
29
Y = -11568905
14 feet Y = -3482117
61 meter
Z = 13676906
48 Z = 4187872
04
XDOT = 20485
652991 XDOT = 6232
742429
YDOT = 8439
113002 feet/sec YDOT = 2642
003688 meter/sec
ZDOT = -12118
181995 ZDOT = -3663
315644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12583265
49 X = -3835379
32
Y = -11827808
58 feet Y = -3605116
05 meter
Z = 13753307
10 Z = 4192008
00
XDOT = 5857
901259 XDOT = 1785
488304
YDOT = -20263
413389 feet/sec YDOT = -6176
288401 meter/sec
ZDOT = -11997
184638 ZDOT = -3656
741878
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 10178
54113150
00016717 00000-0 10270-3 0 9138
2 25544 51
6427 177
6084 0009982 12
4746 347
6661 15
71979943 25108
Satellite: ISS
Catalog Number: 25544
Epoch time: 10178
54113150 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 177
6084 deg
Eccentricity:
0009982
Arg of perigee: 12
4746 deg
Mean anomaly: 347
6661 deg
Mean motion: 15
71979943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2510
Checksum: 320
Coasting Arc #15 (Orbit 2525)
---------------------------------------
Vector Time (GMT): 2010/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6038267
38 A = 6734852
02 meter
Y = -1252705
11 meter E =
0020330
Z = 2675397
31 I = 51
69915
XDOT = 3277
607316 Wp = 52
76276
YDOT = -4638
226317 meter/sec RA = 171
68298 deg
ZDOT = 5210
764356 TA = 337
71149
MA = 337
79973
Ha = 195
934 n
mi
Hp = 185
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19810588
51 X = -6036807
04
Y = -4109924
91 feet Y = -1320220
92 meter
Z = 8777550
24 Z = 2646067
14
XDOT = 10753
304844 XDOT = 3303
916606
YDOT = -15217
277942 feet/sec YDOT = -4601
427969 meter/sec
ZDOT = 17095
683582 ZDOT = 5226
749847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2116409
81 X = -645081
71
Y = 20172103
00 feet Y = 6148456
99 meter
Z = 8660447
94 Z = 2639704
53
XDOT = -14728
554670 XDOT = -4489
263463
YDOT = -8933
591382 feet/sec YDOT = -2722
958653 meter/sec
ZDOT = 17159
442887 ZDOT = 5230
198192
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 10179
55827854
00016717 00000-0 10270-3 0 9144
2 25544 51
6427 172
4015 0009890 16
1026 344
0449 15
72000150 25263
Satellite: ISS
Catalog Number: 25544
Epoch time: 10179
55827854 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 172
4015 deg
Eccentricity:
0009890
Arg of perigee: 16
1026 deg
Mean anomaly: 344
0449 deg
Mean motion: 15
72000150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2526
Checksum: 291
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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