[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 23rd 2012
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) : 129 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
060/10:21:41
429 2
6 4
2 4
2
N/A -3
3 -0
0 220
0
000/00:01:22
857 0
2 0
0 201
4
Coasting Arc #1 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2012/053/11:23:58
707
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2866708
87 A = 6763278
29 meter
Y = 3339712
33 meter E =
0023120
Z = 5114652
07 I = 51
51891
XDOT = -6709
758972 Wp = 80
20328
YDOT = 3453
354471 meter/sec RA = 341
88114 deg
ZDOT = 1503
906684 TA = 355
32780
MA = 355
34934
Ha = 220
256 n
mi
Hp = 199
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9405212
83 X = 2804305
25
Y = 10957061
46 feet Y = 3371421
22 meter
Z = 16780354
55 Z = 5128426
17
XDOT = -22013
644922 XDOT = -6755
181857
YDOT = 11329
903121 feet/sec YDOT = 3378
067980 meter/sec
ZDOT = 4934
077047 ZDOT = 1471
201103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 579656
16 X = 176679
20
Y = 14362812
80 feet Y = 4377785
34 meter
Z = 16836541
52 Z = 5131777
86
XDOT = -23296
878339 XDOT = -7100
888518
YDOT = -4693
461904 feet/sec YDOT = -1430
567188 meter/sec
ZDOT = 4799
708124 ZDOT = 1462
951036
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 12053
52561241
00016717 00000-0 10270-3 0 9004
2 25544 51
6426 342
1479 0020108 71
5570 288
7769 15
59210703 39981
Satellite: ISS
Catalog Number: 25544
Epoch time: 12053
52561241 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 342
1479 deg
Eccentricity:
0020108
Arg of perigee: 71
5570 deg
Mean anomaly: 288
7769 deg
Mean motion: 15
59210703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 309
Coasting Arc #2 (Orbit 4012)
---------------------------------------
Vector Time (GMT): 2012/054/11:23:58
707
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 817088
36 A = 6764402
96 meter
Y = -4603504
36 meter E =
0031194
Z = -4914707
57 I = 51
49377
XDOT = 7222
743137 Wp = 86
35008
YDOT = -1127
243323 meter/sec RA = 336
81898 deg
ZDOT = 2271
084418 TA = 205
85170
MA = 206
00789
Ha = 220
399 n
mi
Hp = 199
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2680736
09 X = 892379
00
Y = -15103360
75 feet Y = -4593946
73 meter
Z = -16124368
65 Z = -4910554
90
XDOT = 23696
663836 XDOT = 7223
779196
YDOT = -3698
304866 feet/sec YDOT = -1046
468114 meter/sec
ZDOT = 7451
064364 ZDOT = 2306
174100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11315206
97 X = 3448875
08
Y = -10383880
61 feet Y = -3165006
81 meter
Z = -16106962
19 Z = -4909402
08
XDOT = 20350
057198 XDOT = 6202
697434
YDOT = 10467
673791 feet/sec YDOT = 3190
546971 meter/sec
ZDOT = 7595
001887 ZDOT = 2314
956575
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 12054
48701238
00016717 00000-0 10270-3 0 9013
2 25544 51
6427 337
3183 0020226 74
9327 285
4065 15
59199594 40134
Satellite: ISS
Catalog Number: 25544
Epoch time: 12054
48701238 = yrday
fracday
Element set: 901
Inclination: 51
6427 deg
RA of node: 337
3183 deg
Eccentricity:
0020226
Arg of perigee: 74
9327 deg
Mean anomaly: 285
4065 deg
Mean motion: 15
59199594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4013
Checksum: 311
Coasting Arc #3 (Orbit 4028)
---------------------------------------
Vector Time (GMT): 2012/055/11:23:58
707
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4135319
57 A = 6771520
06 meter
Y = 4632908
87 meter E =
0033137
Z = 2672974
41 I = 51
49052
XDOT = -5387
129209 Wp = 87
78956
YDOT = -1787
063540 meter/sec RA = 331
78087 deg
ZDOT = -5180
230705 TA = 61
86264
MA = 61
52819
Ha = 220
381 n
mi
Hp = 199
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13567321
41 X = -4199802
83
Y = 15199832
26 feet Y = 4586304
93 meter
Z = 8769601
08 Z = 2652728
41
XDOT = -17674
308428 XDOT = -5341
581537
YDOT = -5863
069356 feet/sec YDOT = -1847
051643 meter/sec
ZDOT = -16995
507563 ZDOT = -5206
289876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19957203
72 X = -6082955
69
Y = 4274630
93 feet Y = 1302907
51 meter
Z = 8686228
42 Z = 2647562
42
XDOT = -10443
844335 XDOT = -3183
283753
YDOT = -13625
731070 feet/sec YDOT = -4153
122830 meter/sec
ZDOT = -17102
178238 ZDOT = -5212
743927
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 12055
51248060
00016717 00000-0 10270-3 0 9028
2 25544 51
6428 332
1667 0020216 78
8490 281
4937 15
59242499 40292
Satellite: ISS
Catalog Number: 25544
Epoch time: 12055
51248060 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 332
1667 deg
Eccentricity:
0020216
Arg of perigee: 78
8490 deg
Mean anomaly: 281
4937 deg
Mean motion: 15
59242499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 314
Coasting Arc #4 (Orbit 4044)
---------------------------------------
Vector Time (GMT): 2012/056/11:23:58
707
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5872121
70 A = 6774293
90 meter
Y = -3310719
42 meter E =
0032169
Z = 562906
61 I = 51
47355
XDOT = 1904
229323 Wp = 69
79922
YDOT = 4438
339445 meter/sec RA = 326
77347 deg
ZDOT = 5973
627065 TA = 296
30676
MA = 296
63686
Ha = 220
301 n
mi
Hp = 199
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19265491
14 X = 5905971
96
Y = -10861940
35 feet Y = -3244864
41 meter
Z = 1846806
45 Z = 591515
31
XDOT = 6247
471532 XDOT = 1825
439228
YDOT = 14561
481120 feet/sec YDOT = 4459
193798 meter/sec
ZDOT = 19598
513992 ZDOT = 5982
685764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21999616
21 X = 6705483
02
Y = 2170216
83 feet Y = 661482
09 meter
Z = 1964341
28 Z = 598731
22
XDOT = -3191
350627 XDOT = -972
723671
YDOT = 13836
142226 feet/sec YDOT = 4217
256151 meter/sec
ZDOT = 19635
279636 ZDOT = 5984
833233
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 12056
53792509
00016717 00000-0 10270-3 0 9034
2 25544 51
6425 327
0156 0020170 82
5083 277
8363 15
59265489 40458
Satellite: ISS
Catalog Number: 25544
Epoch time: 12056
53792509 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 327
0156 deg
Eccentricity:
0020170
Arg of perigee: 82
5083 deg
Mean anomaly: 277
8363 deg
Mean motion: 15
59265489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4045
Checksum: 316
Coasting Arc #5 (Orbit 4059)
---------------------------------------
Vector Time (GMT): 2012/057/11:23:58
707
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5653581
79 A = 6768415
71 meter
Y = 725051
51 meter E =
0025839
Z = -3674708
89 I = 51
43041
XDOT = 2027
100228 Wp = 84
08116
YDOT = -5987
918848 meter/sec RA = 321
75484 deg
ZDOT = -4323
810195 TA = 139
78987
MA = 139
59843
Ha = 220
190 n
mi
Hp = 199
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18548496
69 X = -5643418
55
Y = 2378777
91 feet Y = 661886
15 meter
Z = -12056131
52 Z = -3702148
83
XDOT = 6650
591299 XDOT = 2114
911563
YDOT = -19645
403046 feet/sec YDOT = -5964
759986 meter/sec
ZDOT = -14185
728985 ZDOT = -4313
748886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16634975
86 X = -5070340
64
Y = -8381942
14 feet Y = -2554815
96 meter
Z = -12168658
32 Z = -3709007
06
XDOT = 15976
529935 XDOT = 4869
646324
YDOT = -11284
993370 feet/sec YDOT = -3439
665979 meter/sec
ZDOT = -14144
001467 ZDOT = -4311
091647
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 12057
49925602
00016717 00000-0 10270-3 0 9043
2 25544 51
6432 322
1851 0020142 86
1382 274
2076 15
59323169 40604
Satellite: ISS
Catalog Number: 25544
Epoch time: 12057
49925602 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 322
1851 deg
Eccentricity:
0020142
Arg of perigee: 86
1382 deg
Mean anomaly: 274
2076 deg
Mean motion: 15
59323169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4060
Checksum: 291
Coasting Arc #6 (Orbit 4075)
---------------------------------------
Vector Time (GMT): 2012/058/11:23:58
707
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3623462
21 A = 6762353
36 meter
Y = 2299215
33 meter E =
0022958
Z = 5206655
47 I = 51
38672
XDOT = -5014
930014 Wp = 94
06931
YDOT = 5759
545284 meter/sec RA = 316
69720 deg
ZDOT = 941
488022 TA = 346
89191
MA = 346
95148
Ha = 219
960 n
mi
Hp = 199
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11887999
37 X = 3572190
08
Y = 7543357
39 feet Y = 2339448
86 meter
Z = 17082203
00 Z = 5224133
21
XDOT = -16453
182460 XDOT = -5083
535183
YDOT = 18896
145946 feet/sec YDOT = 5703
081725 meter/sec
ZDOT = 3088
871464 ZDOT = 916
958835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5753645
30 X = 1753711
09
Y = 12754461
95 feet Y = 3887560
00 meter
Z = 17153649
62 Z = 5228432
40
XDOT = -23186
832723 XDOT = -7067
346614
YDOT = 6418
588825 feet/sec YDOT = 1956
385874 meter/sec
ZDOT = 2987
868709 ZDOT = 910
702383
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 12058
52465194
00016717 00000-0 10270-3 0 9054
2 25544 51
6426 317
0333 0019961 90
1525 270
1918 15
59380998 40766
Satellite: ISS
Catalog Number: 25544
Epoch time: 12058
52465194 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 317
0333 deg
Eccentricity:
0019961
Arg of perigee: 90
1525 deg
Mean anomaly: 270
1918 deg
Mean motion: 15
59380998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4076
Checksum: 324
Coasting Arc #7 (Orbit 4090)
---------------------------------------
Vector Time (GMT): 2012/059/11:23:58
707
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -644470
08 A = 6764858
95 meter
Y = -4884621
87 meter E =
0030285
Z = -4663658
67 I = 51
37405
XDOT = 6171
535785 Wp = 98
68423
YDOT = -3521
012338 meter/sec RA = 311
62572 deg
ZDOT = 2846
383219 TA = 199
68175
MA = 199
79888
Ha = 220
056 n
mi
Hp = 199
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2114403
14 X = -567146
55
Y = -16025662
30 feet Y = -4891396
71 meter
Z = -15300717
42 Z = -4666601
30
XDOT = 20247
820817 XDOT = 6196
622801
YDOT = -11551
877750 feet/sec YDOT = -3451
857955 meter/sec
ZDOT = 9338
527623 ZDOT = 2876
425174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6805566
08 X = 2074336
54
Y = -14649904
55 feet Y = -4465290
91 meter
Z = -15312383
01 Z = -4667214
34
XDOT = 22174
008867 XDOT = 6758
637903
YDOT = 450
076729 feet/sec YDOT = 137
183387 meter/sec
ZDOT = 9461
939258 ZDOT = 2883
999086
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 12059
48594083
00016717 00000-0 10270-3 0 9061
2 25544 51
6432 312
2030 0019967 93
3905 266
9535 15
59381843 40912
Satellite: ISS
Catalog Number: 25544
Epoch time: 12059
48594083 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 312
2030 deg
Eccentricity:
0019967
Arg of perigee: 93
3905 deg
Mean anomaly: 266
9535 deg
Mean motion: 15
59381843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4091
Checksum: 327
Coasting Arc #8 (Orbit 4105)
---------------------------------------
Vector Time (GMT): 2012/060/10:22:22
857
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2964029
57 A = 6764416
93 meter
Y = -3076699
20 meter E =
0031280
Z = -5271857
83 I = 51
34627
XDOT = 4949
245366 Wp = 96
10011
YDOT = -5804
957303 meter/sec RA = 306
81354 deg
ZDOT = 605
019624 TA = 179
71147
MA = 179
70966
Ha = 219
987 n
mi
Hp = 201
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9724506
45 X = -2903795
75
Y = -10094157
49 feet Y = -3109508
33 meter
Z = -17296121
48 Z = -5286110
33
XDOT = 16237
681648 XDOT = 5010
850706
YDOT = -19045
135509 feet/sec YDOT = -5749
267298 meter/sec
ZDOT = 1984
972519 ZDOT = 629
212574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 716292
98 X = 218326
10
Y = -13925855
36 feet Y = -4244600
71 meter
Z = -17354288
69 Z = -5289587
19
XDOT = 23969
492275 XDOT = 7305
901245
YDOT = -1365
537824 feet/sec YDOT = -416
215929 meter/sec
ZDOT = 2084
593068 ZDOT = 635
383967
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 12060
44720864
00016717 00000-0 10270-3 0 9078
2 25544 51
6428 307
3722 0016587 97
7003 262
6036 15
58633571 41065
Satellite: ISS
Catalog Number: 25544
Epoch time: 12060
44720864 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 307
3722 deg
Eccentricity:
0016587
Arg of perigee: 97
7003 deg
Mean anomaly: 262
6036 deg
Mean motion: 15
58633571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4106
Checksum: 307
Coasting Arc #9 (Orbit 4121)
---------------------------------------
Vector Time (GMT): 2012/061/10:22:22
857
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 384808
91 A = 6769364
89 meter
Y = 5438902
80 meter E =
0026969
Z = 3987699
38 I = 51
34527
XDOT = -5732
181190 Wp = 92
13986
YDOT = 3298
349054 meter/sec RA = 301
75428 deg
ZDOT = -3923
589625 TA = 38
75350
MA = 38
56035
Ha = 219
908 n
mi
Hp = 201
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1262496
42 X = 304590
28
Y = 17844169
29 feet Y = 5442757
65 meter
Z = 13083003
21 Z = 3989373
62
XDOT = -18806
368734 XDOT = -5749
578272
YDOT = 10821
355164 feet/sec YDOT = 3234
150796 meter/sec
ZDOT = -12872
669373 ZDOT = -3951
478400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11916448
78 X = -3632133
59
Y = 13335599
74 feet Y = 4064690
80 meter
Z = 13089433
75 Z = 3989659
41
XDOT = -19864
195728 XDOT = -6054
606858
YDOT = -4932
149746 feet/sec YDOT = -1503
319242 meter/sec
ZDOT = -12987
234860 ZDOT = -3958
509185
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 12061
47305420
00016717 00000-0 10270-3 0 9080
2 25544 51
6424 302
2232 0016588 101
4033 258
8986 15
58664039 41220
Satellite: ISS
Catalog Number: 25544
Epoch time: 12061
47305420 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 302
2232 deg
Eccentricity:
0016588
Arg of perigee: 101
4033 deg
Mean anomaly: 258
8986 deg
Mean motion: 15
58664039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4122
Checksum: 294
Coasting Arc #10 (Orbit 4136)
---------------------------------------
Vector Time (GMT): 2012/062/10:22:22
857
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2004240
56 A = 6775296
75 meter
Y = -6336787
11 meter E =
0021485
Z = -1325233
16 I = 51
35122
XDOT = 4999
867653 Wp = 82
44815
YDOT = 385
659850 meter/sec RA = 296
72673 deg
ZDOT = 5801
208191 TA = 263
05156
MA = 263
29600
Ha = 219
794 n
mi
Hp = 201
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6575592
38 X = 2081388
42
Y = -20789983
95 feet Y = -6313943
16 meter
Z = -4347877
81 Z = -1315309
09
XDOT = 16403
765265 XDOT = 4967
002974
YDOT = 1265
288222 feet/sec YDOT = 441
387979 meter/sec
ZDOT = 19032
835272 ZDOT = 5825
417122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19296967
41 X = 5881715
67
Y = -10170801
92 feet Y = -3100060
43 meter
Z = -4306707
14 Z = -1312684
34
XDOT = 9968
566813 XDOT = 3038
419165
YDOT = 10929
359625 feet/sec YDOT = 3331
268814 meter/sec
ZDOT = 19132
029262 ZDOT = 5831
442519
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 12062
43476277
00016717 00000-0 10270-3 0 9097
2 25544 51
6431 297
3959 0016453 105
0673 255
2304 15
58710481 41373
Satellite: ISS
Catalog Number: 25544
Epoch time: 12062
43476277 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 297
3959 deg
Eccentricity:
0016453
Arg of perigee: 105
0673 deg
Mean anomaly: 255
2304 deg
Mean motion: 15
58710481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4137
Checksum: 314
Coasting Arc #11 (Orbit 4152)
---------------------------------------
Vector Time (GMT): 2012/063/10:22:22
857
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3756786
00 A = 6774454
55 meter
Y = 5301202
10 meter E =
0022556
Z = -1910802
99 I = 51
33586
XDOT = -3136
333756 Wp = 118
23647
YDOT = -4215
988461 meter/sec RA = 291
71425 deg
ZDOT = -5591
138346 TA = 82
94585
MA = 82
68938
Ha = 219
685 n
mi
Hp = 201
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12325413
38 X = -3806503
81
Y = 17392395
35 feet Y = 5258913
32 meter
Z = -6269038
70 Z = -1929174
01
XDOT = -10289
808910 XDOT = -3061
796616
YDOT = -13831
983139 feet/sec YDOT = -4250
644415 meter/sec
ZDOT = -18343
629743 ZDOT = -5606
192974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20892237
04 X = -6367953
85
Y = 4119554
75 feet Y = 1255640
29 meter
Z = -6344744
09 Z = -1933878
00
XDOT = 2470
636085 XDOT = 753
049879
YDOT = -15512
895576 feet/sec YDOT = -4728
330572 meter/sec
ZDOT = -18405
012021 ZDOT = -5609
847664
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 12063
46056366
00016717 00000-0 10270-3 0 9106
2 25544 51
6433 292
2461 0016328 109
2680 251
0243 15
58705459 41535
Satellite: ISS
Catalog Number: 25544
Epoch time: 12063
46056366 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 292
2461 deg
Eccentricity:
0016328
Arg of perigee: 109
2680 deg
Mean anomaly: 251
0243 deg
Mean motion: 15
58705459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4153
Checksum: 295
Coasting Arc #12 (Orbit 4168)
---------------------------------------
Vector Time (GMT): 2012/064/10:22:22
857
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4439420
21 A = 6767622
29 meter
Y = -2617942
13 meter E =
0025701
Z = 4370829
09 I = 51
30299
XDOT = 737
404185 Wp = 111
22117
YDOT = 6879
566937 meter/sec RA = 286
67823 deg
ZDOT = 3346
536733 TA = 304
74751
MA = 304
98924
Ha = 219
529 n
mi
Hp = 201
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14565026
95 X = 4447132
55
Y = -8589048
98 feet Y = -2568254
38 meter
Z = 14339990
45 Z = 4392414
06
XDOT = 2419
305069 XDOT = 644
164287
YDOT = 22570
757666 feet/sec YDOT = 6887
291933 meter/sec
ZDOT = 10979
451225 ZDOT = 3349
892010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16468966
28 X = 5019740
92
Y = 3483385
72 feet Y = 1061735
97 meter
Z = 14428661
49 Z = 4397856
02
XDOT = -13298
452000 XDOT = -4053
368170
YDOT = 17001
591008 feet/sec YDOT = 5182
084939 meter/sec
ZDOT = 10992
688705 ZDOT = 3350
571517
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 12064
48634126
00016717 00000-0 10270-3 0 9116
2 25544 51
6430 287
0971 0016345 112
3465 247
9424 15
58761876 41692
Satellite: ISS
Catalog Number: 25544
Epoch time: 12064
48634126 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 287
0971 deg
Eccentricity:
0016345
Arg of perigee: 112
3465 deg
Mean anomaly: 247
9424 deg
Mean motion: 15
58761876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4169
Checksum: 322
Coasting Arc #13 (Orbit 4183)
---------------------------------------
Vector Time (GMT): 2012/065/10:22:22
857
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4114841
72 A = 6763758
70 meter
Y = -1046908
36 meter E =
0030319
Z = -5290727
29 I = 51
28243
XDOT = 1672
994303 Wp = 104
06326
YDOT = -7466
999834 meter/sec RA = 281
60837 deg
ZDOT = 169
970291 TA = 167
60508
MA = 167
53034
Ha = 219
417 n
mi
Hp = 201
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13500136
88 X = -4077128
56
Y = -3434738
70 feet Y = -1092712
65 meter
Z = -17358029
16 Z = -5310624
87
XDOT = 5488
826455 XDOT = 1755
541799
YDOT = -24498
030952 feet/sec YDOT = -7447
829816 meter/sec
ZDOT = 557
645312 ZDOT = 178
298591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7728532
41 X = -2355656
68
Y = -11466710
99 feet Y = -3495053
51 meter
Z = -17439513
41 Z = -5315563
69
XDOT = 19539
282827 XDOT = 5955
573406
YDOT = -14102
098917 feet/sec YDOT = -4298
319750 meter/sec
ZDOT = 592
327822 ZDOT = 180
541520
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 12065
44798565
00016717 00000-0 10270-3 0 9122
2 25544 51
6427 282
2688 0016126 115
9635 244
3183 15
58818023 41842
Satellite: ISS
Catalog Number: 25544
Epoch time: 12065
44798565 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 282
2688 deg
Eccentricity:
0016126
Arg of perigee: 115
9635 deg
Mean anomaly: 244
3183 deg
Mean motion: 15
58818023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4184
Checksum: 328
Coasting Arc #14 (Orbit 4199)
---------------------------------------
Vector Time (GMT): 2012/066/10:22:22
857
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2875791
92 A = 6767943
73 meter
Y = 4441250
17 meter E =
0024164
Z = 4196434
85 I = 51
29175
XDOT = -3584
574799 Wp = 101
98197
YDOT = 5758
589789 meter/sec RA = 276
54067 deg
ZDOT = -3625
327667 TA = 25
23743
MA = 25
11957
Ha = 219
150 n
mi
Hp = 201
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9435012
84 X = 2805530
32
Y = 14571030
76 feet Y = 4473016
66 meter
Z = 13767830
87 Z = 4210233
87
XDOT = -11760
416006 XDOT = -3631
091442
YDOT = 18893
011118 feet/sec YDOT = 5718
244372 meter/sec
ZDOT = -11894
119643 ZDOT = -3642
854620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2397265
31 X = -730686
47
Y = 17147463
79 feet Y = 5226546
96 meter
Z = 13824079
57 Z = 4213579
45
XDOT = -19924
234274 XDOT = -6072
906607
YDOT = 6895
197522 feet/sec YDOT = 2101
656205 meter/sec
ZDOT = -11966
372323 ZDOT = -3647
350284
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 12066
47371715
00016717 00000-0 10270-3 0 9131
2 25544 51
6424 277
1191 0015969 119
4546 240
8205 15
58880105 42000
Satellite: ISS
Catalog Number: 25544
Epoch time: 12066
47371715 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 277
1191 deg
Eccentricity:
0015969
Arg of perigee: 119
4546 deg
Mean anomaly: 240
8205 deg
Mean motion: 15
58880105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4200
Checksum: 305
Coasting Arc #15 (Orbit 4214)
---------------------------------------
Vector Time (GMT): 2012/067/10:22:22
857
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1098637
97 A = 6774473
50 meter
Y = -6499711
47 meter E =
0018377
Z = -1584536
79 I = 51
31038
XDOT = 4632
183023 Wp = 97
37545
YDOT = -2161
922125 meter/sec RA = 271
50512 deg
ZDOT = 5711
154061 TA = 245
20114
MA = 245
39242
Ha = 219
176 n
mi
Hp = 201
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3604455
28 X = -1018178
05
Y = -21324512
69 feet Y = -6511547
45 meter
Z = -5198611
53 Z = -1589677
55
XDOT = 15197
450864 XDOT = 4628
270799
YDOT = -7092
920357 feet/sec YDOT = -2110
143320 meter/sec
ZDOT = 18737
382090 ZDOT = 5733
647366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10860471
11 X = 3310271
60
Y = -18696583
70 feet Y = -5698718
71 meter
Z = -5219236
21 Z = -1590823
20
XDOT = 14774
547923 XDOT = 4503
282207
YDOT = 3375
780072 feet/sec YDOT = 1028
937766 meter/sec
ZDOT = 18829
733842 ZDOT = 5739
302875
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 12067
43532026
00016717 00000-0 10270-3 0 9143
2 25544 51
6416 272
2905 0015916 123
2170 237
0513 15
58875677 42152
Satellite: ISS
Catalog Number: 25544
Epoch time: 12067
43532026 = yrday
fracday
Element set: 914
Inclination: 51
6416 deg
RA of node: 272
2905 deg
Eccentricity:
0015916
Arg of perigee: 123
2170 deg
Mean anomaly: 237
0513 deg
Mean motion: 15
58875677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4215
Checksum: 299
Coasting Arc #16 (Orbit 4230)
---------------------------------------
Vector Time (GMT): 2012/068/10:22:22
857
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -970173
82 A = 6774310
04 meter
Y = 6477617
70 meter E =
0023355
Z = -1704365
64 I = 51
30948
XDOT = -4688
392391 Wp = 132
26105
YDOT = -2178
601253 meter/sec RA = 266
48946 deg
ZDOT = -5676
501953 TA = 66
56131
MA = 66
31593
Ha = 219
072 n
mi
Hp = 202
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3182984
98 X = -1034256
43
Y = 21252026
56 feet Y = 6466410
06 meter
Z = -5591750
78 Z = -1709235
21
XDOT = -15381
864801 XDOT = -4636
107577
YDOT = -7147
641907 feet/sec YDOT = -2230
738221 meter/sec
ZDOT = -18623
694071 ZDOT = -5699
150338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15739153
63 X = -4797294
03
Y = 14622945
94 feet Y = 4457073
92 meter
Z = -5612147
38 Z = -1710582
52
XDOT = -6386
073333 XDOT = -1946
475152
YDOT = -13974
823041 feet/sec YDOT = -4259
526063 meter/sec
ZDOT = -18716
386134 ZDOT = -5704
754494
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 12068
46100674
00016717 00000-0 10270-3 0 9158
2 25544 51
6410 267
1397 0015868 127
6821 232
5776 15
58876352 42311
Satellite: ISS
Catalog Number: 25544
Epoch time: 12068
46100674 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 267
1397 deg
Eccentricity:
0015868
Arg of perigee: 127
6821 deg
Mean anomaly: 232
5776 deg
Mean motion: 15
58876352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4231
Checksum: 323
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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