Date:
May 26th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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
146/06:29:55
633 0
8 -2
4 2
4
N/A -1
6 0
0 190
5
000/00:09:51
266 -1
7 0
0 182
3
Coasting Arc #1 (Orbit 1974)
---------------------------------------
Vector Time (GMT): 2010/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816784
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3069812
54 A = 6721090
84 meter
Y = 3455377
43 meter E =
0007914
Z = 4874199
58 I = 51
58384
XDOT = -6795
213082 Wp = 24
31235
YDOT = 2828
060663 meter/sec RA = 351
62883 deg
ZDOT = 2280
622283 TA = 43
52441
MA = 43
46198
Ha = 191
875 n
mi
Hp = 182
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10071563
44 X = 3007267
34
Y = 11336540
12 feet Y = 3489355
78 meter
Z = 15991468
43 Z = 4888961
35
XDOT = -22294
006176 XDOT = -6837
410968
YDOT = 9278
414250 feet/sec YDOT = 2751
836410 meter/sec
ZDOT = 7482
356570 ZDOT = 2247
508303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14740962
76 X = 4493045
45
Y = -3282396
51 feet Y = -1000474
46 meter
Z = 16050248
75 Z = 4892115
82
XDOT = -2867
971926 XDOT = -874
157843
YDOT = 22969
996371 feet/sec YDOT = 7001
254894 meter/sec
ZDOT = 7350
464901 ZDOT = 2240
421702
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 10144
55147307
00016717 00000-0 10270-3 0 9009
2 25544 51
6468 351
8551 0010914 348
6984 11
3932 15
74228635 19751
Satellite: ISS
Catalog Number: 25544
Epoch time: 10144
55147307 = yrday
fracday
Element set: 900
Inclination: 51
6468 deg
RA of node: 351
8551 deg
Eccentricity:
0010914
Arg of perigee: 348
6984 deg
Mean anomaly: 11
3932 deg
Mean motion: 15
74228635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1975
Checksum: 314
Coasting Arc #2 (Orbit 1989)
---------------------------------------
Vector Time (GMT): 2010/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816784
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5741729
62 A = 6729864
97 meter
Y = -2931494
86 meter E =
0016629
Z = -1897420
27 I = 51
58282
XDOT = 3741
024635 Wp = 9
37783
YDOT = 3695
144217 meter/sec RA = 346
45143 deg
ZDOT = 5634
653618 TA = 329
49983
MA = 329
59644
Ha = 191
987 n
mi
Hp = 182
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18837695
62 X = 5783300
89
Y = -9617765
29 feet Y = -2867054
77 meter
Z = -6225132
12 Z = -1869425
76
XDOT = 12273
702870 XDOT = 3672
054172
YDOT = 12123
176564 feet/sec YDOT = 3736
592328 meter/sec
ZDOT = 18486
396384 ZDOT = 5652
660739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 298544
72 X = 90996
43
Y = -21181285
78 feet Y = -6456055
90 meter
Z = -6113628
96 Z = -1863434
11
XDOT = 14854
117766 XDOT = 4527
535095
YDOT = -5124
941361 feet/sec YDOT = -1562
082127 meter/sec
ZDOT = 18558
096140 ZDOT = 5656
507704
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 10145
50364799
00016717 00000-0 10270-3 0 9012
2 25544 51
6457 346
9631 0010897 351
2789 8
8183 15
74280537 19901
Satellite: ISS
Catalog Number: 25544
Epoch time: 10145
50364799 = yrday
fracday
Element set: 901
Inclination: 51
6457 deg
RA of node: 346
9631 deg
Eccentricity:
0010897
Arg of perigee: 351
2789 deg
Mean anomaly: 8
8183 deg
Mean motion: 15
74280537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1990
Checksum: 337
Coasting Arc #3 (Orbit 2002)
---------------------------------------
Vector Time (GMT): 2010/146/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5095346
50 A = 6722823
65 meter
Y = 1737582
57 meter E =
0010957
Z = 4014432
17 I = 51
54304
XDOT = -4682
338851 Wp = 51
45176
YDOT = 4721
700344 meter/sec RA = 342
51399 deg
ZDOT = 3898
963789 TA = 358
31193
MA = 358
31562
Ha = 190
492 n
mi
Hp = 182
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16717016
08 X = 5056036
08
Y = 5700730
22 feet Y = 1794341
45 meter
Z = 13170709
22 Z = 4039090
57
XDOT = -15362
004105 XDOT = -4753
730568
YDOT = 15491
142862 feet/sec YDOT = 4668
939966 meter/sec
ZDOT = 12791
875948 ZDOT = 3876
043752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14001185
25 X = 4267561
26
Y = 10645539
06 feet Y = 3244760
31 meter
Z = 13268905
10 Z = 4044362
27
XDOT = -18750
167464 XDOT = -5715
051043
YDOT = 8828
479207 feet/sec YDOT = 2690
920462 meter/sec
ZDOT = 12700
571883 ZDOT = 3871
134310
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 10146
32883819
00016717 00000-0 10270-3 0 9023
2 25544 51
6473 342
7254 0009345 348
9458 11
1499 15
74779267 20032
Satellite: ISS
Catalog Number: 25544
Epoch time: 10146
32883819 = yrday
fracday
Element set: 902
Inclination: 51
6473 deg
RA of node: 342
7254 deg
Eccentricity:
0009345
Arg of perigee: 348
9458 deg
Mean anomaly: 11
1499 deg
Mean motion: 15
74779267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2003
Checksum: 329
Coasting Arc #4 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2010/147/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3958374
28 A = 6725485
17 meter
Y = -4399364
61 meter E =
0010671
Z = -3186335
88 I = 51
52399
XDOT = 5770
965795 Wp = 17
10569
YDOT = 1724
424541 meter/sec RA = 337
31422 deg
ZDOT = 4802
428404 TA = 305
62595
MA = 305
72530
Ha = 190
713 n
mi
Hp = 182
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12986792
26 X = 4022753
47
Y = -14433610
93 feet Y = -4354739
27 meter
Z = -10453857
89 Z = -3166950
06
XDOT = 18933
614812 XDOT = 5727
924338
YDOT = 5657
560831 feet/sec YDOT = 1788
717531 meter/sec
ZDOT = 15755
998702 ZDOT = 4830
359940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16758504
42 X = 5107992
15
Y = -9886718
01 feet Y = -3013471
65 meter
Z = -10376626
58 Z = -3162795
78
XDOT = 15575
298862 XDOT = 4747
351093
YDOT = 9796
321846 feet/sec YDOT = 2985
918899 meter/sec
ZDOT = 15867
230341 ZDOT = 4836
331808
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 10147
28070004
00016717 00000-0 10270-3 0 9034
2 25544 51
6477 337
8319 0009404 352
2259 7
8757 15
74818387 20188
Satellite: ISS
Catalog Number: 25544
Epoch time: 10147
28070004 = yrday
fracday
Element set: 903
Inclination: 51
6477 deg
RA of node: 337
8319 deg
Eccentricity:
0009404
Arg of perigee: 352
2259 deg
Mean anomaly: 7
8757 deg
Mean motion: 15
74818387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2018
Checksum: 316
Coasting Arc #5 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2010/148/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4948912
01 A = 6721358
67 meter
Y = -1320322
20 meter E =
0015067
Z = -4366435
95 I = 51
48374
XDOT = 4396
405826 Wp = 31
66267
YDOT = -5340
241571 meter/sec RA = 332
21210 deg
ZDOT = -3360
724591 TA = 204
34788
MA = 204
41914
Ha = 190
765 n
mi
Hp = 181
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16236587
97 X = -4912568
49
Y = -4331765
74 feet Y = -1375459
94 meter
Z = -14325577
26 Z = -4390390
02
XDOT = 14423
903627 XDOT = 4472
120618
YDOT = -17520
477596 feet/sec YDOT = -5290
654439 meter/sec
ZDOT = -11025
999314 ZDOT = -3339
183550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14277210
16 X = -4351693
66
Y = -8706891
88 feet Y = -2653860
65 meter
Z = -14420972
60 Z = -4395512
45
XDOT = 18202
779022 XDOT = 5548
207046
YDOT = -11688
484595 feet/sec YDOT = -3562
650105 meter/sec
ZDOT = -10940
174692 ZDOT = -3334
565246
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 10148
29600223
00016717 00000-0 10270-3 0 9049
2 25544 51
6483 332
6120 0009517 356
0739 4
0348 15
74855069 20349
Satellite: ISS
Catalog Number: 25544
Epoch time: 10148
29600223 = yrday
fracday
Element set: 904
Inclination: 51
6483 deg
RA of node: 332
6120 deg
Eccentricity:
0009517
Arg of perigee: 356
0739 deg
Mean anomaly: 4
0348 deg
Mean motion: 15
74855069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2034
Checksum: 292
Coasting Arc #6 (Orbit 2049)
---------------------------------------
Vector Time (GMT): 2010/149/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3705033
38 A = 6726719
43 meter
Y = 4938425
66 meter E =
0014905
Z = 2669082
65 I = 51
47484
XDOT = -5531
768315 Wp = 63
44472
YDOT = -1331
695977 meter/sec RA = 327
01178 deg
ZDOT = -5186
019559 TA = 86
07529
MA = 85
90490
Ha = 190
907 n
mi
Hp = 181
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12155621
31 X = -3772946
40
Y = 16202183
91 feet Y = 4896613
58 meter
Z = 8756832
84 Z = 2650919
35
XDOT = -18148
846178 XDOT = -5491
272962
YDOT = -4369
081288 feet/sec YDOT = -1393
328173 meter/sec
ZDOT = -17014
499864 ZDOT = -5212
794988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16066410
20 X = -4897041
83
Y = 12385581
10 feet Y = 3775125
12 meter
Z = 8684460
73 Z = 2647023
63
XDOT = -15340
250432 XDOT = -4675
708332
YDOT = -7827
344629 feet/sec YDOT = -2385
774643 meter/sec
ZDOT = -17121
135919 ZDOT = -5218
522228
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 10149
31128784
00016717 00000-0 10270-3 0 9051
2 25544 51
6478 327
3919 0009472 359
9277
1884 15
74848031 20500
Satellite: ISS
Catalog Number: 25544
Epoch time: 10149
31128784 = yrday
fracday
Element set: 905
Inclination: 51
6478 deg
RA of node: 327
3919 deg
Eccentricity:
0009472
Arg of perigee: 359
9277 deg
Mean anomaly:
1884 deg
Mean motion: 15
74848031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2050
Checksum: 325
Coasting Arc #7 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2010/150/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4711043
20 A = 6720014
88 meter
Y = 1037980
44 meter E =
0009478
Z = 4669425
17 I = 51
42879
XDOT = -4040
672675 Wp = 50
96294
YDOT = 5959
304041 meter/sec RA = 321
89987 deg
ZDOT = 2754
131625 TA = 11
85674
MA = 11
83444
Ha = 190
848 n
mi
Hp = 181
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15456178
48 X = 4676402
87
Y = 3405447
63 feet Y = 1090467
63 meter
Z = 15319636
38 Z = 4692227
55
XDOT = -13256
800114 XDOT = -4120
389498
YDOT = 19551
522444 feet/sec YDOT = 5913
672634 meter/sec
ZDOT = 9035
864910 ZDOT = 2734
309361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14036872
16 X = 4278438
64
Y = 7117999
02 feet Y = 2169566
10 meter
Z = 15410454
10 Z = 4697106
41
XDOT = -17232
583118 XDOT = -5252
491334
YDOT = 14606
686525 feet/sec YDOT = 4452
118053 meter/sec
ZDOT = 8956
878693 ZDOT = 2730
056626
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 10150
32655431
00016717 00000-0 10270-3 0 9069
2 25544 51
6485 322
1715 0009585 3
4008 356
7219 15
74888984 20663
Satellite: ISS
Catalog Number: 25544
Epoch time: 10150
32655431 = yrday
fracday
Element set: 906
Inclination: 51
6485 deg
RA of node: 322
1715 deg
Eccentricity:
0009585
Arg of perigee: 3
4008 deg
Mean anomaly: 356
7219 deg
Mean motion: 15
74888984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2066
Checksum: 316
Coasting Arc #8 (Orbit 2080)
---------------------------------------
Vector Time (GMT): 2010/151/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3311643
67 A = 6727605
91 meter
Y = -5447917
03 meter E =
0015386
Z = -2124349
64 I = 51
43188
XDOT = 5276
885629 Wp = 19
67372
YDOT = 1067
946804 meter/sec RA = 316
70235 deg
ZDOT = 5513
162701 TA = 316
47820
MA = 316
59951
Ha = 191
031 n
mi
Hp = 181
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10864972
67 X = 3382636
84
Y = -17873743
55 feet Y = -5410486
97 meter
Z = -6969651
06 Z = -2108090
13
XDOT = 17312
616893 XDOT = 5237
769512
YDOT = 3503
762479 feet/sec YDOT = 1126
736462 meter/sec
ZDOT = 18087
804137 ZDOT = 5538
702986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14752680
96 X = 4496617
16
Y = -14858522
22 feet Y = -4528877
57 meter
Z = -6904860
42 Z = -2104601
46
XDOT = 14840
850781 XDOT = 4523
491318
YDOT = 6322
034257 feet/sec YDOT = 1926
956042 meter/sec
ZDOT = 18189
531492 ZDOT = 5544
169199
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 10151
27835057
00016717 00000-0 10270-3 0 9079
2 25544 51
6490 317
2778 0009671 6
1558 353
9723 15
74927014 20813
Satellite: ISS
Catalog Number: 25544
Epoch time: 10151
27835057 = yrday
fracday
Element set: 907
Inclination: 51
6490 deg
RA of node: 317
2778 deg
Eccentricity:
0009671
Arg of perigee: 6
1558 deg
Mean anomaly: 353
9723 deg
Mean motion: 15
74927014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2081
Checksum: 316
Coasting Arc #9 (Orbit 2096)
---------------------------------------
Vector Time (GMT): 2010/152/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4489846
29 A = 6718746
47 meter
Y = -880856
22 meter E =
0019105
Z = -4936169
93 I = 51
38110
XDOT = 3555
836900 Wp = 46
81655
YDOT = -6496
230514 meter/sec RA = 311
57932 deg
ZDOT = -2067
229608 TA = 203
01291
MA = 203
09861
Ha = 191
064 n
mi
Hp = 180
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14730466
83 X = -4455683
73
Y = -2889948
22 feet Y = -930872
60 meter
Z = -16194783
24 Z = -4957898
72
XDOT = 11666
131562 XDOT = 3638
256852
YDOT = -21313
092238 feet/sec YDOT = -6456
005886 meter/sec
ZDOT = -6782
249371 ZDOT = -2049
756153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13670500
21 X = -4166768
46
Y = -5970349
79 feet Y = -1819762
62 meter
Z = -16281333
03 Z = -4962550
31
XDOT = 15580
579905 XDOT = 4748
960755
YDOT = -17300
006376 feet/sec YDOT = -5273
041943 meter/sec
ZDOT = -6712
623497 ZDOT = -2046
007642
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 10152
29358264
00016717 00000-0 10270-3 0 9083
2 25544 51
6488 312
0576 0009761 9
4181 350
7164 15
74965616 20978
Satellite: ISS
Catalog Number: 25544
Epoch time: 10152
29358264 = yrday
fracday
Element set: 908
Inclination: 51
6488 deg
RA of node: 312
0576 deg
Eccentricity:
0009761
Arg of perigee: 9
4181 deg
Mean anomaly: 350
7164 deg
Mean motion: 15
74965616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2097
Checksum: 325
Coasting Arc #10 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2010/153/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2887463
41 A = 6728559
74 meter
Y = 5895995
33 meter E =
0014847
Z = 1469557
31 I = 51
39468
XDOT = -4993
891902 Wp = 79
53812
YDOT = -993
711090 meter/sec RA = 306
38813 deg
ZDOT = -5773
356103 TA = 84
22997
MA = 84
06073
Ha = 191
199 n
mi
Hp = 180
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9473305
14 X = -2960317
72
Y = 19343816
71 feet Y = 5863298
45 meter
Z = 4821382
23 Z = 1455353
85
XDOT = -16384
159785 XDOT = -4954
363035
YDOT = -3260
206989 feet/sec YDOT = -1049
333988 meter/sec
ZDOT = -18941
457032 ZDOT = -5797
520493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13147828
96 X = -4007458
27
Y = 17076412
07 feet Y = 5204890
40 meter
Z = 4764790
28 Z = 1452308
08
XDOT = -14057
477008 XDOT = -4284
718992
YDOT = -5463
167952 feet/sec YDOT = -1665
173592 meter/sec
ZDOT = -19037
711314 ZDOT = -5802
694409
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 10153
30879859
00016717 00000-0 10270-3 0 9095
2 25544 51
6488 306
8375 0009673 13
8761 346
2667 15
74948859 21138
Satellite: ISS
Catalog Number: 25544
Epoch time: 10153
30879859 = yrday
fracday
Element set: 909
Inclination: 51
6488 deg
RA of node: 306
8375 deg
Eccentricity:
0009673
Arg of perigee: 13
8761 deg
Mean anomaly: 346
2667 deg
Mean motion: 15
74948859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2113
Checksum: 357
Coasting Arc #11 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2010/154/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4253714
52 A = 6717794
25 meter
Y = 881429
34 meter E =
0009370
Z = 5117530
95 I = 51
34171
XDOT = -3010
425397 Wp = 41
74320
YDOT = 6975
390602 meter/sec RA = 301
25043 deg
ZDOT = 1306
388805 TA = 35
75410
MA = 35
69139
Ha = 191
126 n
mi
Hp = 180
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13955756
30 X = 4218682
06
Y = 2891828
55 feet Y = 928800
44 meter
Z = 16789799
72 Z = 5138110
49
XDOT = -9876
723745 XDOT = -3094
547926
YDOT = 22885
139771 feet/sec YDOT = 6941
255727 meter/sec
ZDOT = 4286
052509 ZDOT = 1291
560645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13102118
43 X = 3993525
70
Y = 5357315
96 feet Y = 1632909
90 meter
Z = 16871776
41 Z = 5142517
45
XDOT = -13497
332681 XDOT = -4113
987001
YDOT = 19754
619768 feet/sec YDOT = 6021
208105 meter/sec
ZDOT = 4226
977875 ZDOT = 1288
382856
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 10154
32399434
00016717 00000-0 10270-3 0 9106
2 25544 51
6485 301
6168 0009810 16
9560 343
1929 15
74995455 21290
Satellite: ISS
Catalog Number: 25544
Epoch time: 10154
32399434 = yrday
fracday
Element set: 910
Inclination: 51
6485 deg
RA of node: 301
6168 deg
Eccentricity:
0009810
Arg of perigee: 16
9560 deg
Mean anomaly: 343
1929 deg
Mean motion: 15
74995455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2129
Checksum: 320
Coasting Arc #12 (Orbit 2143)
---------------------------------------
Vector Time (GMT): 2010/155/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2340421
48 A = 6728982
27 meter
Y = -6246085
53 meter E =
0020000
Z = -803676
14 I = 51
36419
XDOT = 4787
840594 Wp = 29
49749
YDOT = 1038
499030 meter/sec RA = 296
06768 deg
ZDOT = 5951
546163 TA = 321
69353
MA = 321
83542
Ha = 191
261 n
mi
Hp = 180
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7678548
16 X = 2413996
51
Y = -20492406
59 feet Y = -6219502
08 meter
Z = -2636732
76 Z = -792128
30
XDOT = 15708
138433 XDOT = 4746
960495
YDOT = 3407
149047 feet/sec YDOT = 1091
810322 meter/sec
ZDOT = 19526
070089 ZDOT = 5974
706336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10958473
14 X = 3340142
61
Y = -18948645
26 feet Y = -5775547
08 meter
Z = -2590733
23 Z = -789655
49
XDOT = 13438
410565 XDOT = 4096
027540
YDOT = 5125
887384 feet/sec YDOT = 1562
370475 meter/sec
ZDOT = 19618
328028 ZDOT = 5979
666383
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 10155
27572422
00016717 00000-0 10270-3 0 9112
2 25544 51
6478 296
7222 0009874 19
5147 340
6393 15
75028194 21449
Satellite: ISS
Catalog Number: 25544
Epoch time: 10155
27572422 = yrday
fracday
Element set: 911
Inclination: 51
6478 deg
RA of node: 296
7222 deg
Eccentricity:
0009874
Arg of perigee: 19
5147 deg
Mean anomaly: 340
6393 deg
Mean motion: 15
75028194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2144
Checksum: 315
Coasting Arc #13 (Orbit 2159)
---------------------------------------
Vector Time (GMT): 2010/156/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4114922
83 A = 6717134
35 meter
Y = -977134
00 meter E =
0021310
Z = -5235346
56 I = 51
31120
XDOT = 2368
137542 Wp = 61
67235
YDOT = -7297
992799 meter/sec RA = 290
91406 deg
ZDOT = -490
774846 TA = 203
58776
MA = 203
68562
Ha = 191
278 n
mi
Hp = 179
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13500403
00 X = -4078258
03
Y = -3205820
22 feet Y = -1022944
00 meter
Z = -17176333
85 Z = -5255247
98
XDOT = 7769
480124 XDOT = 2451
953117
YDOT = -23943
545927 feet/sec YDOT = -7271
042187 meter/sec
ZDOT = -1610
153695 ZDOT = -479
067514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12779720
63 X = -3895258
85
Y = -5146572
60 feet Y = -1568675
33 meter
Z = -17255611
84 Z = -5259510
49
XDOT = 10848
322284 XDOT = 3306
568632
YDOT = -21603
318921 feet/sec YDOT = -6584
691607 meter/sec
ZDOT = -1563
526541 ZDOT = -476
562890
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 10156
29088564
00016717 00000-0 10270-3 0 9125
2 25544 51
6466 291
5006 0009878 23
1387 337
0220 15
75069641 21609
Satellite: ISS
Catalog Number: 25544
Epoch time: 10156
29088564 = yrday
fracday
Element set: 912
Inclination: 51
6466 deg
RA of node: 291
5006 deg
Eccentricity:
0009878
Arg of perigee: 23
1387 deg
Mean anomaly: 337
0220 deg
Mean motion: 15
75069641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2160
Checksum: 308
Coasting Arc #14 (Orbit 2175)
---------------------------------------
Vector Time (GMT): 2010/157/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1799005
51 A = 6729125
68 meter
Y = 6484140
02 meter E =
0013255
Z = 34868
41 I = 51
34208
XDOT = -4643
808110 Wp = 89
26887
YDOT = -1245
506364 meter/sec RA = 285
74402 deg
ZDOT = -6009
836714 TA = 90
35094
MA = 90
19905
Ha = 191
371 n
mi
Hp = 179
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5902249
05 X = -1871548
02
Y = 21273425
28 feet Y = 6463616
86 meter
Z = 114397
67 Z = 25953
21
XDOT = -15235
590912 XDOT = -4600
340552
YDOT = -4086
306970 feet/sec YDOT = -1297
192550 meter/sec
ZDOT = -19717
312055 ZDOT = -6032
291065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8626159
57 X = -2629253
44
Y = 20322189
84 feet Y = 6194203
46 meter
Z = 78897
11 Z = 24047
84
XDOT = -12975
102011 XDOT = -3954
811093
YDOT = -5394
286411 feet/sec YDOT = -1644
178498 meter/sec
ZDOT = -19806
761034 ZDOT = -6037
100763
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 10157
30602996
00016717 00000-0 10270-3 0 9130
2 25544 51
6467 286
2801 0009838 27
0816 333
0859 15
75070412 21769
Satellite: ISS
Catalog Number: 25544
Epoch time: 10157
30602996 = yrday
fracday
Element set: 913
Inclination: 51
6467 deg
RA of node: 286
2801 deg
Eccentricity:
0009838
Arg of perigee: 27
0816 deg
Mean anomaly: 333
0859 deg
Mean motion: 15
75070412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2176
Checksum: 313
Coasting Arc #15 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2010/158/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4035674
42 A = 6717016
01 meter
Y = 1205050
92 meter E =
0011938
Z = 5226650
98 I = 51
29378
XDOT = -1720
311893 Wp = 38
63284
YDOT = 7503
986600 meter/sec RA = 280
57304 deg
ZDOT = -392
105964 TA = 55
16058
MA = 55
04836
Ha = 191
294 n
mi
Hp = 179
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13240401
63 X = 3996508
95
Y = 3953579
14 feet Y = 1249960
68 meter
Z = 17147805
04 Z = 5246161
51
XDOT = -5644
067889 XDOT = -1802
190167
YDOT = 24619
378609 feet/sec YDOT = 7484
291284 meter/sec
ZDOT = -1286
436891 ZDOT = -400
661405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12606297
72 X = 3842399
55
Y = 5417439
86 feet Y = 1651235
67 meter
Z = 17225528
84 Z = 5250341
19
XDOT = -7994
667864 XDOT = -2436
774765
YDOT = 22902
850266 feet/sec YDOT = 6980
788761 meter/sec
ZDOT = -1320
498426 ZDOT = -402
487920
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 10158
32115546
00016717 00000-0 10270-3 0 9144
2 25544 51
6460 281
0580 0009851 30
6197 329
5540 15
75097144 21922
Satellite: ISS
Catalog Number: 25544
Epoch time: 10158
32115546 = yrday
fracday
Element set: 914
Inclination: 51
6460 deg
RA of node: 281
0580 deg
Eccentricity:
0009851
Arg of perigee: 30
6197 deg
Mean anomaly: 329
5540 deg
Mean motion: 15
75097144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 300
Coasting Arc #16 (Orbit 2207)
---------------------------------------
Vector Time (GMT): 2010/159/06:34:51
266
Vector Time (MET): N/A
Weight (LBS) : 816529
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1198224
80 A = 6728734
53 meter
Y = -6569708
46 meter E =
0023002
Z = 715787
99 I = 51
32820
XDOT = 4650
558044 Wp = 44
68999
YDOT = 1508
700445 meter/sec RA = 275
41521 deg
ZDOT = 5962
669321 TA = 323
15563
MA = 323
31347
Ha = 191
384 n
mi
Hp = 179
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3931183
73 X = 1268122
20
Y = -21554161
61 feet Y = -6555918
47 meter
Z = 2348385
78 Z = 721778
01
XDOT = 15257
736366 XDOT = 4604
375859
YDOT = 4949
804611 feet/sec YDOT = 1560
446792 meter/sec
ZDOT = 19562
563388 ZDOT = 5985
150069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5972663
82 X = 1820467
93
Y = -21077258
41 feet Y = -6424348
36 meter
Z = 2372228
71 Z = 723055
31
XDOT = 13058
546339 XDOT = 3980
244924
YDOT = 5948
644342 feet/sec YDOT = 1813
146796 meter/sec
ZDOT = 19652
122395 ZDOT = 5989
966906
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 10159
33626303
00016717 00000-0 10270-3 0 9155
2 25544 51
6450 275
8359 0009862 34
1791 326
0005 15
75134475 22082
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
33626303 = yrday
fracday
Element set: 915
Inclination: 51
6450 deg
RA of node: 275
8359 deg
Eccentricity:
0009862
Arg of perigee: 34
1791 deg
Mean anomaly: 326
0005 deg
Mean motion: 15
75134475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2208
Checksum: 301
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list