[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 22nd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
145/00:25:05
707 -2
5 3
0 3
1
N/A -0
3 -0
5 220
1
000/00:06:11
415 -1
8 -0
0 211
8
Coasting Arc #1 (Orbit 1385)
---------------------------------------
Vector Time (GMT): 2012/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4145364
69 A = 6777036
75 meter
Y = 3827373
92 meter E =
0014370
Z = 3757455
07 I = 51
30123
XDOT = -1839
272887 Wp = 34
59527
YDOT = 6140
854671 meter/sec RA = 254
95964 deg
ZDOT = -4206
399109 TA = 100
15054
MA = 99
98842
Ha = 219
599 n
mi
Hp = 210
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13600277
84 X = 4084004
96
Y = 12557001
03 feet Y = 3873386
47 meter
Z = 12327608
48 Z = 3777444
75
XDOT = -6034
359864 XDOT = -1887
370410
YDOT = 20147
160995 feet/sec YDOT = 6120
018302 meter/sec
ZDOT = -13800
522011 ZDOT = -4215
450537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17753949
60 X = 5411403
84
Y = -5041783
69 feet Y = -1536735
67 meter
Z = 12409409
90 Z = 3782388
14
XDOT = 13763
392677 XDOT = 4195
082088
YDOT = 14248
585964 feet/sec YDOT = 4342
969002 meter/sec
ZDOT = -13838
270669 ZDOT = -4217
904900
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 12142
54023742
00016717 00000-0 10270-3 0 9004
2 25544 51
6395 255
6524 0010982 342
5602 17
5173 15
56270542 13861
Satellite: ISS
Catalog Number: 25544
Epoch time: 12142
54023742 = yrday
fracday
Element set: 900
Inclination: 51
6395 deg
RA of node: 255
6524 deg
Eccentricity:
0010982
Arg of perigee: 342
5602 deg
Mean anomaly: 17
5173 deg
Mean motion: 15
56270542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1386
Checksum: 289
Coasting Arc #2 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2012/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3490547
27 A = 6781736
62 meter
Y = -5540717
35 meter E =
0017005
Z = -1722662
28 I = 51
32656
XDOT = 3405
948236 Wp = 6
66012
YDOT = -3901
274100 meter/sec RA = 249
94448 deg
ZDOT = 5668
833898 TA = 334
32223
MA = 334
40657
Ha = 219
743 n
mi
Hp = 210
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11451926
75 X = -3419962
00
Y = -18178206
54 feet Y = -5579355
95 meter
Z = -5651779
14 Z = -1739448
62
XDOT = 11174
370852 XDOT = 3421
781662
YDOT = -12799
455709 feet/sec YDOT = -3863
098809 meter/sec
ZDOT = 18598
536412 ZDOT = 5685
418068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21455447
60 X = -6539620
43
Y = 691866
17 feet Y = 210880
81 meter
Z = -5720272
37 Z = -1743539
02
XDOT = -5423
333505 XDOT = -1653
032052
YDOT = -14440
987018 feet/sec YDOT = -4401
612843 meter/sec
ZDOT = 18667
042007 ZDOT = 5689
714404
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 12143
50341608
00016717 00000-0 10270-3 0 9016
2 25544 51
6400 250
8349 0011310 346
0241 14
0598 15
56298193 14017
Satellite: ISS
Catalog Number: 25544
Epoch time: 12143
50341608 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 250
8349 deg
Eccentricity:
0011310
Arg of perigee: 346
0241 deg
Mean anomaly: 14
0598 deg
Mean motion: 15
56298193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1401
Checksum: 267
Coasting Arc #3 (Orbit 1416)
---------------------------------------
Vector Time (GMT): 2012/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2331734
65 A = 6782645
64 meter
Y = 6331938
07 meter E =
0005659
Z = -711784
12 I = 51
34098
XDOT = -4732
143942 Wp = 58
68396
YDOT = 1079
598751 meter/sec RA = 244
94301 deg
ZDOT = -5930
189696 TA = 129
03661
MA = 128
98623
Ha = 219
839 n
mi
Hp = 210
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7650048
06 X = 2264214
05
Y = 20774075
04 feet Y = 6357635
53 meter
Z = -2335249
74 Z = -700619
80
XDOT = -15525
406633 XDOT = -4715
056725
YDOT = 3541
990654 feet/sec YDOT = 1026
777242 meter/sec
ZDOT = -19456
002941 ZDOT = -5953
136833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21867065
52 X = 6665081
57
Y = 3482315
55 feet Y = 1061409
78 meter
Z = -2289922
33 Z = -697968
33
XDOT = -4197
710892 XDOT = -1279
462280
YDOT = 13573
952384 feet/sec YDOT = 4137
340687 meter/sec
ZDOT = -19550
415168 ZDOT = -5958
966543
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 12144
53078738
00016717 00000-0 10270-3 0 9022
2 25544 51
6395 245
6963 0011201 349
8943 10
1984 15
56356075 14170
Satellite: ISS
Catalog Number: 25544
Epoch time: 12144
53078738 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 245
6963 deg
Eccentricity:
0011201
Arg of perigee: 349
8943 deg
Mean anomaly: 10
1984 deg
Mean motion: 15
56356075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1417
Checksum: 316
Coasting Arc #4 (Orbit 1424)
---------------------------------------
Vector Time (GMT): 2012/145/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -63727
52 A = 6779375
49 meter
Y = 5838930
50 meter E =
0009997
Z = -3456096
85 I = 51
33068
XDOT = -5532
757977 Wp = 13
64846
YDOT = -2746
731284 meter/sec RA = 242
35333 deg
ZDOT = -4531
618302 TA = 207
07156
MA = 207
12373
Ha = 220
094 n
mi
Hp = 211
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -209079
80 X = -112225
82
Y = 19156596
13 feet Y = 5837947
10 meter
Z = -11338900
44 Z = -3456523
55
XDOT = -18152
093099 XDOT = -5479
618503
YDOT = -9011
585579 feet/sec YDOT = -2808
304348 meter/sec
ZDOT = -14867
514114 ZDOT = -4558
367664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17741643
79 X = -5407653
03
Y = -7225063
82 feet Y = -2202199
45 meter
Z = -11341167
55 Z = -3456787
87
XDOT = 14534
245223 XDOT = 4430
037944
YDOT = -12144
861226 feet/sec YDOT = -3701
753702 meter/sec
ZDOT = -14977
223121 ZDOT = -4565
057607
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 12145
04447333
00016717 00000-0 10270-3 0 9031
2 25544 51
6386 243
1290 0009911 344
6626 15
4226 15
55811082 14251
Satellite: ISS
Catalog Number: 25544
Epoch time: 12145
04447333 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 243
1290 deg
Eccentricity:
0009911
Arg of perigee: 344
6626 deg
Mean anomaly: 15
4226 deg
Mean motion: 15
55811082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1425
Checksum: 286
Coasting Arc #5 (Orbit 1440)
---------------------------------------
Vector Time (GMT): 2012/146/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1725222
79 A = 6774475
82 meter
Y = -4440903
14 meter E =
0007452
Z = 4810058
60 I = 51
32895
XDOT = 5445
181244 Wp = 34
86375
YDOT = 4804
251409 meter/sec RA = 237
32763 deg
ZDOT = 2486
620187 TA = 30
64219
MA = 30
59868
Ha = 220
109 n
mi
Hp = 211
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5660179
75 X = 1751387
35
Y = -14569892
21 feet Y = -4421464
88 meter
Z = 15781032
16 Z = 4818502
76
XDOT = 17864
767861 XDOT = 5378
974926
YDOT = 15761
979688 feet/sec YDOT = 4864
772335 meter/sec
ZDOT = 8158
202712 ZDOT = 2512
912494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11651978
95 X = 3551523
19
Y = 10365413
53 feet Y = 3159378
04 meter
Z = 15816129
70 Z = 4820756
33
XDOT = -20296
510285 XDOT = -6186
376335
YDOT = 10223
689138 feet/sec YDOT = 3116
180449 meter/sec
ZDOT = 8265
869029 ZDOT = 2519
436880
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 12146
07218992
00016717 00000-0 10270-3 0 9043
2 25544 51
6380 237
9917 0009909 348
4440 11
6484 15
55834666 14410
Satellite: ISS
Catalog Number: 25544
Epoch time: 12146
07218992 = yrday
fracday
Element set: 904
Inclination: 51
6380 deg
RA of node: 237
9917 deg
Eccentricity:
0009909
Arg of perigee: 348
4440 deg
Mean anomaly: 11
6484 deg
Mean motion: 15
55834666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 327
Coasting Arc #6 (Orbit 1455)
---------------------------------------
Vector Time (GMT): 2012/147/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3360958
19 A = 6772274
83 meter
Y = 2578941
07 meter E =
0016760
Z = -5295338
31 I = 51
33961
XDOT = -4673
849070 Wp = 53
82188
YDOT = -6070
734016 meter/sec RA = 232
28967 deg
ZDOT = 19
673797 TA = 216
30959
MA = 216
42343
Ha = 220
251 n
mi
Hp = 211
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11026765
71 X = -3363823
01
Y = 8461092
74 feet Y = 2541341
26 meter
Z = -17373157
17 Z = -5311672
44
XDOT = -15334
150492 XDOT = -4605
713084
YDOT = -19917
106353 feet/sec YDOT = -6122
618921 meter/sec
ZDOT = 64
546577 ZDOT = -2
866727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4267922
34 X = -1300862
73
Y = -13138453
56 feet Y = -4004600
64 meter
Z = -17440530
95 Z = -5315873
83
XDOT = 22971
551830 XDOT = 7001
728998
YDOT = -7383
181645 feet/sec YDOT = -2250
393765 meter/sec
ZDOT = -27
604268 ZDOT = -8
413781
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 12147
03565592
00016717 00000-0 10270-3 0 9052
2 25544 51
6383 233
1758 0010031 351
9848 8
1144 15
55875543 14562
Satellite: ISS
Catalog Number: 25544
Epoch time: 12147
03565592 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 233
1758 deg
Eccentricity:
0010031
Arg of perigee: 351
9848 deg
Mean anomaly: 8
1144 deg
Mean motion: 15
55875543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1456
Checksum: 308
Coasting Arc #7 (Orbit 1471)
---------------------------------------
Vector Time (GMT): 2012/148/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4773412
41 A = 6774268
89 meter
Y = -469677
30 meter E =
0014744
Z = 4784583
57 I = 51
36587
XDOT = 3212
087052 Wp = 22
00206
YDOT = 6480
606118 meter/sec RA = 227
25217 deg
ZDOT = -2552
432352 TA = 93
29682
MA = 93
12813
Ha = 220
282 n
mi
Hp = 210
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15660801
88 X = 4755067
19
Y = -1540936
02 feet Y = -416401
03 meter
Z = 15697452
66 Z = 4807728
05
XDOT = 10538
343347 XDOT = 3151
780031
YDOT = 21261
831097 feet/sec YDOT = 6516
188686 meter/sec
ZDOT = -8374
121889 ZDOT = -2536
974073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3553556
44 X = -1083124
00
Y = 15231859
70 feet Y = 4642670
84 meter
Z = 15792653
55 Z = 4813600
80
XDOT = -22427
823095 XDOT = -6836
000479
YDOT = 3438
800126 feet/sec YDOT = 1048
146278 meter/sec
ZDOT = -8311
108181 ZDOT = -2533
225773
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 12148
06333307
00016717 00000-0 10270-3 0 9064
2 25544 51
6379 228
0383 0010169 355
2259 4
8796 15
55923800 14723
Satellite: ISS
Catalog Number: 25544
Epoch time: 12148
06333307 = yrday
fracday
Element set: 906
Inclination: 51
6379 deg
RA of node: 228
0383 deg
Eccentricity:
0010169
Arg of perigee: 355
2259 deg
Mean anomaly: 4
8796 deg
Mean motion: 15
55923800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1472
Checksum: 311
Coasting Arc #8 (Orbit 1486)
---------------------------------------
Vector Time (GMT): 2012/149/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5669902
19 A = 6779102
04 meter
Y = -1478249
32 meter E =
0011131
Z = -3402999
40 I = 51
40377
XDOT = -1179
100389 Wp = 25
33122
YDOT = -6026
731837 meter/sec RA = 222
22997 deg
ZDOT = 4597
986099 TA = 294
68412
MA = 294
79997
Ha = 220
396 n
mi
Hp = 210
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18602041
32 X = -5636419
65
Y = -4849899
35 feet Y = -1541466
23 meter
Z = -11164696
19 Z = -3430462
40
XDOT = -3868
439598 XDOT = -1133
956666
YDOT = -19772
742249 feet/sec YDOT = -6039
665182 meter/sec
ZDOT = 15085
256230 ZDOT = 4592
367288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10283150
75 X = 3134304
35
Y = -16164241
03 feet Y = -4926860
67 meter
Z = -11277500
99 Z = -3437382
30
XDOT = 18857
356661 XDOT = 5747
722310
YDOT = 1522
471608 feet/sec YDOT = 464
049346 meter/sec
ZDOT = 15062
651124 ZDOT = 4591
096063
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 12149
02676407
00016717 00000-0 10270-3 0 9073
2 25544 51
6382 223
2217 0010203 358
7286 1
3840 15
55918303 14877
Satellite: ISS
Catalog Number: 25544
Epoch time: 12149
02676407 = yrday
fracday
Element set: 907
Inclination: 51
6382 deg
RA of node: 223
2217 deg
Eccentricity:
0010203
Arg of perigee: 358
7286 deg
Mean anomaly: 1
3840 deg
Mean motion: 15
55918303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1487
Checksum: 294
Coasting Arc #9 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2012/150/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5871570
08 A = 6783330
05 meter
Y = 3122097
44 meter E =
0012940
Z = 1337627
46 I = 51
44095
XDOT = -1249
465820 Wp = 76
03704
YDOT = 4855
727249 meter/sec RA = 217
22747 deg
ZDOT = -5798
659042 TA = 89
35639
MA = 89
20811
Ha = 220
593 n
mi
Hp = 210
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19263681
35 X = 5829723
82
Y = 10243101
85 feet Y = 3187522
92 meter
Z = 4388541
54 Z = 1366050
01
XDOT = -4099
297309 XDOT = -1275
501938
YDOT = 15930
863679 feet/sec YDOT = 4841
609726 meter/sec
ZDOT = -19024
471923 ZDOT = -5804
791875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15369183
53 X = -4684527
14
Y = 15451909
59 feet Y = 4709742
04 meter
Z = 4505168
03 Z = 1373175
22
XDOT = -12970
066080 XDOT = -3953
276141
YDOT = -7299
502658 feet/sec YDOT = -2224
888410 meter/sec
ZDOT = -19050
089475 ZDOT = -5806
467272
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 12150
05440547
00016717 00000-0 10270-3 0 9083
2 25544 51
6381 218
0840 0010086 3
1084 357
0130 15
55917852 15036
Satellite: ISS
Catalog Number: 25544
Epoch time: 12150
05440547 = yrday
fracday
Element set: 908
Inclination: 51
6381 deg
RA of node: 218
0840 deg
Eccentricity:
0010086
Arg of perigee: 3
1084 deg
Mean anomaly: 357
0130 deg
Mean motion: 15
55917852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 273
Coasting Arc #10 (Orbit 1518)
---------------------------------------
Vector Time (GMT): 2012/151/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5228278
32 A = 6783592
82 meter
Y = -4194230
72 meter E =
0021664
Z = 953126
24 I = 51
46724
XDOT = 3684
928729 Wp = 34
23825
YDOT = -3239
722956 meter/sec RA = 212
23496 deg
ZDOT = 5909
177527 TA = 336
12989
MA = 336
23020
Ha = 220
626 n
mi
Hp = 210
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17153144
11 X = -5185619
12
Y = -13760599
48 feet Y = -4252458
10 meter
Z = 3127054
59 Z = 927830
62
XDOT = 12089
661185 XDOT = 3692
176360
YDOT = -10629
012324 feet/sec YDOT = -3198
475620 meter/sec
ZDOT = 19387
065378 ZDOT = 5927
096343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17921768
18 X = 5462554
94
Y = -12768414
71 feet Y = -3891812
80 meter
Z = 3023364
36 Z = 921521
46
XDOT = 6029
183803 XDOT = 1837
695223
YDOT = 13108
996298 feet/sec YDOT = 3995
622072 meter/sec
ZDOT = 19461
021673 ZDOT = 5931
719406
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 12151
08202515
00016717 00000-0 10270-3 0 9099
2 25544 51
6382 212
9457 0010288 5
9649 354
1626 15
55983229 15191
Satellite: ISS
Catalog Number: 25544
Epoch time: 12151
08202515 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 212
9457 deg
Eccentricity:
0010288
Arg of perigee: 5
9649 deg
Mean anomaly: 354
1626 deg
Mean motion: 15
55983229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1519
Checksum: 314
Coasting Arc #11 (Orbit 1533)
---------------------------------------
Vector Time (GMT): 2012/152/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3764468
25 A = 6779911
32 meter
Y = 4717423
80 meter E =
0010612
Z = -3104747
56 I = 51
48081
XDOT = -5753
003314 Wp = 34
13356
YDOT = 1390
873089 meter/sec RA = 207
23848 deg
ZDOT = -4861
610679 TA = 181
64635
MA = 181
64985
Ha = 220
710 n
mi
Hp = 210
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12350617
61 X = 3726519
64
Y = 15477112
19 feet Y = 4759308
43 meter
Z = -10186179
67 Z = -3086551
56
XDOT = -18874
682788 XDOT = -5744
511820
YDOT = 4563
231920 feet/sec YDOT = 1326
587241 meter/sec
ZDOT = -15950
166270 ZDOT = -4889
538191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18139327
63 X = -5528867
06
Y = 8034603
75 feet Y = 2448947
22 meter
Z = -10111723
35 Z = -3082053
28
XDOT = 985
037398 XDOT = 300
239399
YDOT = -17996
586630 feet/sec YDOT = -5485
359605 meter/sec
ZDOT = -16065
142903 ZDOT = -4896
655557
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 12152
04540311
00016717 00000-0 10270-3 0 9107
2 25544 51
6378 208
1292 0010223 8
9190 351
2144 15
55983576 15348
Satellite: ISS
Catalog Number: 25544
Epoch time: 12152
04540311 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 208
1292 deg
Eccentricity:
0010223
Arg of perigee: 8
9190 deg
Mean anomaly: 351
2144 deg
Mean motion: 15
55983576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 279
Coasting Arc #12 (Orbit 1549)
---------------------------------------
Vector Time (GMT): 2012/153/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1622211
42 A = 6774735
45 meter
Y = -4650853
00 meter E =
0011894
Z = 4639639
49 I = 51
49103
XDOT = 7100
527510 Wp = 56
69530
YDOT = 411
706513 meter/sec RA = 202
22510 deg
ZDOT = 2896
384942 TA = 4
49529
MA = 4
48462
Ha = 220
877 n
mi
Hp = 209
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5322215
94 X = -1592622
78
Y = -15258704
07 feet Y = -4668828
52 meter
Z = 15221914
33 Z = 4631830
20
XDOT = 23295
693930 XDOT = 7081
325762
YDOT = 1350
743152 feet/sec YDOT = 491
001400 meter/sec
ZDOT = 9502
575268 ZDOT = 2930
832983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16110470
15 X = 4910471
30
Y = -1603796
83 feet Y = -488837
27 meter
Z = 15190171
02 Z = 4629964
13
XDOT = -6993
266387 XDOT = -2131
547595
YDOT = 21062
961745 feet/sec YDOT = 6419
990740 meter/sec
ZDOT = 9644
236627 ZDOT = 2939
563324
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 12153
07298856
00016717 00000-0 10270-3 0 9116
2 25544 51
6376 202
9906 0010412 13
5779 346
5653 15
56005989 15509
Satellite: ISS
Catalog Number: 25544
Epoch time: 12153
07298856 = yrday
fracday
Element set: 911
Inclination: 51
6376 deg
RA of node: 202
9906 deg
Eccentricity:
0010412
Arg of perigee: 13
5779 deg
Mean anomaly: 346
5653 deg
Mean motion: 15
56005989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1550
Checksum: 319
Coasting Arc #13 (Orbit 1564)
---------------------------------------
Vector Time (GMT): 2012/154/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -856183
51 A = 6771763
49 meter
Y = 4147048
29 meter E =
0020718
Z = -5300416
93 I = 51
50900
XDOT = -7386
313905 Wp = 59
10654
YDOT = -1990
623107 meter/sec RA = 197
19752 deg
ZDOT = -354
966651 TA = 207
44360
MA = 207
55317
Ha = 220
820 n
mi
Hp = 209
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2809001
03 X = -876744
31
Y = 13605801
47 feet Y = 4137359
55 meter
Z = -17389819
31 Z = -5304625
78
XDOT = -24233
313337 XDOT = -7361
780998
YDOT = -6530
915707 feet/sec YDOT = -2073
084231 meter/sec
ZDOT = -1164
588749 ZDOT = -390
790340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12660982
44 X = -3859067
45
Y = -5665114
18 feet Y = -1726726
80 meter
Z = -17407473
71 Z = -5305797
99
XDOT = 11349
356140 XDOT = 3459
283751
YDOT = -21239
469032 feet/sec YDOT = -6473
790161 meter/sec
ZDOT = -1311
794552 ZDOT = -399
834979
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 12154
03633059
00016717 00000-0 10270-3 0 9122
2 25544 51
6363 198
1732 0010377 16
3922 343
7565 15
56071983 15653
Satellite: ISS
Catalog Number: 25544
Epoch time: 12154
03633059 = yrday
fracday
Element set: 912
Inclination: 51
6363 deg
RA of node: 198
1732 deg
Eccentricity:
0010377
Arg of perigee: 16
3922 deg
Mean anomaly: 343
7565 deg
Mean motion: 15
56071983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1565
Checksum: 309
Coasting Arc #14 (Orbit 1580)
---------------------------------------
Vector Time (GMT): 2012/155/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3344159
36 A = 6773283
31 meter
Y = -3261207
76 meter E =
0015966
Z = 4901736
26 I = 51
54387
XDOT = 6557
190813 Wp = 34
73012
YDOT = 3268
465715 meter/sec RA = 192
16963 deg
ZDOT = -2282
482036 TA = 77
68189
MA = 77
50319
Ha = 220
761 n
mi
Hp = 209
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10971651
45 X = 3356566
37
Y = -10699500
54 feet Y = -3223742
63 meter
Z = 16081811
88 Z = 4918011
99
XDOT = 21513
093217 XDOT = 6531
242784
YDOT = 10723
312713 feet/sec YDOT = 3341
647519 meter/sec
ZDOT = -7488
458122 ZDOT = -2250
689511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8230188
51 X = 2508561
46
Y = 12843421
23 feet Y = 3914674
79 meter
Z = 16149044
82 Z = 4922228
86
XDOT = -13995
681395 XDOT = -4265
883689
YDOT = 18288
169657 feet/sec YDOT = 5574
234111 meter/sec
ZDOT = -7357
925881 ZDOT = -2242
695809
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 12155
06387809
00016717 00000-0 10270-3 0 9136
2 25544 51
6362 193
0349 0010331 19
7339 340
4213 15
56103417 15819
Satellite: ISS
Catalog Number: 25544
Epoch time: 12155
06387809 = yrday
fracday
Element set: 913
Inclination: 51
6362 deg
RA of node: 193
0349 deg
Eccentricity:
0010331
Arg of perigee: 19
7339 deg
Mean anomaly: 340
4213 deg
Mean motion: 15
56103417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1581
Checksum: 289
Coasting Arc #15 (Orbit 1595)
---------------------------------------
Vector Time (GMT): 2012/156/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5332122
80 A = 6778033
33 meter
Y = 2183321
12 meter E =
0012860
Z = -3569752
27 I = 51
58821
XDOT = -4667
018219 Wp = 47
75399
YDOT = -4145
603585 meter/sec RA = 187
15603 deg
ZDOT = 4454
307502 TA = 270
01355
MA = 270
16092
Ha = 220
832 n
mi
Hp = 209
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17493841
20 X = -5338799
57
Y = 7163127
04 feet Y = 2123657
28 meter
Z = -11711785
66 Z = -3595671
68
XDOT = -15311
739564 XDOT = -4641
952661
YDOT = -13601
061632 feet/sec YDOT = -4197
653656 meter/sec
ZDOT = 14613
869758 ZDOT = 4431
695245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3739517
10 X = -1139804
81
Y = -18462040
50 feet Y = -5627229
94 meter
Z = -11818623
64 Z = -3602316
49
XDOT = 14920
105559 XDOT = 4547
648174
YDOT = -12278
963463 feet/sec YDOT = -3742
628064 meter/sec
ZDOT = 14521
169158 ZDOT = 4426
052359
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 12156
02718780
00016717 00000-0 10270-3 0 9140
2 25544 51
6345 188
2167 0010309 23
6076 336
5549 15
56117114 15964
Satellite: ISS
Catalog Number: 25544
Epoch time: 12156
02718780 = yrday
fracday
Element set: 914
Inclination: 51
6345 deg
RA of node: 188
2167 deg
Eccentricity:
0010309
Arg of perigee: 23
6076 deg
Mean anomaly: 336
5549 deg
Mean motion: 15
56117114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1596
Checksum: 308
Coasting Arc #16 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2012/157/00:28:11
415
Vector Time (MET): N/A
Weight (LBS) : 924612
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6554616
14 A = 6782401
64 meter
Y = -919795
98 meter E =
0017214
Z = 1473781
07 I = 51
63366
XDOT = 1963
958151 Wp = 81
03701
YDOT = 4648
035059 meter/sec RA = 182
16447 deg
ZDOT = -5773
555087 TA = 82
86975
MA = 82
67405
Ha = 220
923 n
mi
Hp = 208
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21504646
14 X = 6557254
99
Y = -3017703
33 feet Y = -846483
71 meter
Z = 4835239
72 Z = 1505629
56
XDOT = 6443
432253 XDOT = 1939
883716
YDOT = 15249
458856 feet/sec YDOT = 4669
863664 meter/sec
ZDOT = -18942
109864 ZDOT = -5764
071859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -724172
19 X = -220727
68
Y = 21673634
02 feet Y = 6606123
65 meter
Z = 4966391
56 Z = 1513756
15
XDOT = -14569
155455 XDOT = -4440
678583
YDOT = 3888
928335 feet/sec YDOT = 1185
345357 meter/sec
ZDOT = -18903
471454 ZDOT = -5761
778099
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 12157
05469821
00016717 00000-0 10270-3 0 9154
2 25544 51
6345 183
0779 0010468 26
8372 333
3321 15
56179219 16122
Satellite: ISS
Catalog Number: 25544
Epoch time: 12157
05469821 = yrday
fracday
Element set: 915
Inclination: 51
6345 deg
RA of node: 183
0779 deg
Eccentricity:
0010468
Arg of perigee: 26
8372 deg
Mean anomaly: 333
3321 deg
Mean motion: 15
56179219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1612
Checksum: 310
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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