[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 11th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 ET - UTC (sec) : 67 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
256/15:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 232
1
000/00:00:00
000 0
0 0
0 215
0
258/03:19:29
550 -3
4 4
2 4
2
N/A -1
6 -0
5 234
6
000/00:08:59
101 2
0 -0
0 214
8
Coasting Arc #1 (Orbit 3128)
---------------------------------------
Vector Time (GMT): 2012/254/12:55:11
385
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4567859
96 A = 6789457
47 meter
Y = 224184
39 meter E =
0021542
Z = 5006548
53 I = 51
92244
XDOT = -2642
826285 Wp = 55
81327
YDOT = -6893
996618 meter/sec RA = 56
24715 deg
ZDOT = -2084
358100 TA = 54
47781
MA = 54
27709
Ha = 232
312 n
mi
Hp = 215
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14986417
20 X = -4594347
88
Y = 735513
09 feet Y = 172955
87 meter
Z = 16425684
14 Z = 4984293
85
XDOT = -8670
689912 XDOT = -2555
414483
YDOT = -22618
099139 feet/sec YDOT = -6923
061702 meter/sec
ZDOT = -6838
445210 ZDOT = -2096
984101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15028673
77 X = 4580739
76
Y = -1512968
24 feet Y = -461152
72 meter
Z = 16333605
59 Z = 4978482
98
XDOT = 9672
389588 XDOT = 2948
144346
YDOT = 21047
953277 feet/sec YDOT = 6415
416159 meter/sec
ZDOT = -6889
953030 ZDOT = -2100
057683
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 12254
58306973
00016717 00000-0 10270-3 0 9002
2 25544 51
6441 56
6937 0015387 55
8183 304
4424 15
50480159 31297
Satellite: ISS
Catalog Number: 25544
Epoch time: 12254
58306973 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 56
6937 deg
Eccentricity:
0015387
Arg of perigee: 55
8183 deg
Mean anomaly: 304
4424 deg
Mean motion: 15
50480159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3129
Checksum: 313
Coasting Arc #2 (Orbit 3143)
---------------------------------------
Vector Time (GMT): 2012/255/12:55:11
385
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4787523
30 A = 6790082
94 meter
Y = -82869
04 meter E =
0024266
Z = -4833091
27 I = 51
90858
XDOT = 2722
514974 Wp = 79
39883
YDOT = 6656
686912 meter/sec RA = 51
30620 deg
ZDOT = 2598
127727 TA = 216
09509
MA = 216
25915
Ha = 232
135 n
mi
Hp = 215
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15707097
44 X = 4811572
02
Y = -271880
06 feet Y = -29197
80 meter
Z = -15856598
65 Z = -4809775
46
XDOT = 8932
135741 XDOT = 2635
255158
YDOT = 21839
523990 feet/sec YDOT = 6686
644032 meter/sec
ZDOT = 8524
041098 ZDOT = 2611
141121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15747772
76 X = -4799921
14
Y = 1357952
54 feet Y = 413903
93 meter
Z = -15760144
91 Z = -4803692
17
XDOT = -10260
198001 XDOT = -3127
308351
YDOT = -20030
081727 feet/sec YDOT = -6105
168910 meter/sec
ZDOT = 8577
171741 ZDOT = 2614
321947
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 12255
54984044
00016717 00000-0 10270-3 0 9011
2 25544 51
6453 51
9014 0015341 58
9548 301
3107 15
50538172 31443
Satellite: ISS
Catalog Number: 25544
Epoch time: 12255
54984044 = yrday
fracday
Element set: 901
Inclination: 51
6453 deg
RA of node: 51
9014 deg
Eccentricity:
0015341
Arg of perigee: 58
9548 deg
Mean anomaly: 301
3107 deg
Mean motion: 15
50538172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3144
Checksum: 288
Coasting Arc #3 (Orbit 3159)
---------------------------------------
Vector Time (GMT): 2012/256/12:55:11
385
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5031177
00 A = 6791132
24 meter
Y = -108549
73 meter E =
0024229
Z = 4546875
11 I = 51
89212
XDOT = -2728
445033 Wp = 64
21926
YDOT = -6440
852215 meter/sec RA = 46
36184 deg
ZDOT = -3149
513306 TA = 57
34891
MA = 57
11538
Ha = 232
272 n
mi
Hp = 215
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16506486
23 X = -5051676
75
Y = -356134
30 feet Y = -164925
75 meter
Z = 14917569
27 Z = 4522384
32
XDOT = -8951
591317 XDOT = -2640
919813
YDOT = -21131
404906 feet/sec YDOT = -6470
874259 meter/sec
ZDOT = -10333
048905 ZDOT = -3162
554740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16566704
27 X = 5049531
46
Y = -1071010
07 feet Y = -326443
87 meter
Z = 14816276
16 Z = 4516000
97
XDOT = 10591
453535 XDOT = 3228
275037
YDOT = 19082
926676 feet/sec YDOT = 5816
476051 meter/sec
ZDOT = -10386
314769 ZDOT = -3165
748741
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 12256
58104494
00016717 00000-0 10270-3 0 9020
2 25544 51
6450 46
7870 0015386 62
8135 297
4582 15
50546022 31600
Satellite: ISS
Catalog Number: 25544
Epoch time: 12256
58104494 = yrday
fracday
Element set: 902
Inclination: 51
6450 deg
RA of node: 46
7870 deg
Eccentricity:
0015386
Arg of perigee: 62
8135 deg
Mean anomaly: 297
4582 deg
Mean motion: 15
50546022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3160
Checksum: 304
Coasting Arc #4 (Orbit 3161)
---------------------------------------
Vector Time (GMT): 2012/256/15:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2085031
92 A = 6787961
78 meter
Y = 3754610
99 meter E =
0017334
Z = 5241510
04 I = 51
88253
XDOT = -5882
872713 Wp = 72
83329
YDOT = -4805
873401 meter/sec RA = 45
79606 deg
ZDOT = 1104
379816 TA = 6
64136
MA = 6
61841
Ha = 232
068 n
mi
Hp = 214
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6840655
91 X = -2152323
64
Y = 12318277
53 feet Y = 3730919
05 meter
Z = 17196555
24 Z = 5231217
38
XDOT = -19300
763495 XDOT = -5834
059991
YDOT = -15767
301186 feet/sec YDOT = -4871
386333 meter/sec
ZDOT = 3623
293358 ZDOT = 1075
920304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4681840
08 X = -1427024
86
Y = -13345072
62 feet Y = -4067578
13 meter
Z = 17153584
37 Z = 5228412
52
XDOT = 23621
649658 XDOT = 7199
878816
YDOT = -3788
889701 feet/sec YDOT = -1154
853581 meter/sec
ZDOT = 3506
079614 ZDOT = 1068
653066
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 12256
70994096
00016717 00000-0 10270-3 0 9030
2 25544 51
6477 46
1503 0015192 62
5023 297
7670 15
50613590 31622
Satellite: ISS
Catalog Number: 25544
Epoch time: 12256
70994096 = yrday
fracday
Element set: 903
Inclination: 51
6477 deg
RA of node: 46
1503 deg
Eccentricity:
0015192
Arg of perigee: 62
5023 deg
Mean anomaly: 297
7670 deg
Mean motion: 15
50613590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3162
Checksum: 306
Coasting Arc #5 (Orbit 3176)
---------------------------------------
Vector Time (GMT): 2012/257/15:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2308727
06 A = 6787755
77 meter
Y = -3542126
75 meter E =
0029437
Z = -5335204
77 I = 51
85938
XDOT = 6016
811353 Wp = 75
39423
YDOT = 4683
075815 meter/sec RA = 40
84997 deg
ZDOT = -500
587725 TA = 189
79879
MA = 189
85633
Ha = 232
036 n
mi
Hp = 214
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7574563
84 X = 2374081
28
Y = -11621150
76 feet Y = -3515944
27 meter
Z = -17503952
67 Z = -5323830
06
XDOT = 19740
194729 XDOT = 5966
428767
YDOT = 15364
421964 feet/sec YDOT = 4750
077794 meter/sec
ZDOT = -1642
348180 ZDOT = -471
481436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3903205
46 X = 1189697
02
Y = 13373410
96 feet Y = 4076215
66 meter
Z = -17456528
51 Z = -5320749
89
XDOT = -23513
766893 XDOT = -7166
996149
YDOT = 4854
486543 feet/sec YDOT = 1479
647498 meter/sec
ZDOT = -1522
450809 ZDOT = -464
043007
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 12257
67667425
00016717 00000-0 10270-3 0 9041
2 25544 51
6474 41
3575 0015207 65
4828 294
7907 15
50592320 31770
Satellite: ISS
Catalog Number: 25544
Epoch time: 12257
67667425 = yrday
fracday
Element set: 904
Inclination: 51
6474 deg
RA of node: 41
3575 deg
Eccentricity:
0015207
Arg of perigee: 65
4828 deg
Mean anomaly: 294
7907 deg
Mean motion: 15
50592320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3177
Checksum: 325
Coasting Arc #6 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2012/258/03:23:59
101
Vector Time (MET): N/A
Weight (LBS) : 924491
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1372703
42 A = 6790356
21 meter
Y = 4124465
60 meter E =
0021288
Z = 5197839
48 I = 51
84996
XDOT = -6513
080665 Wp = 74
45538
YDOT = -3842
213707 meter/sec RA = 38
47720 deg
ZDOT = 1329
783681 TA = 2
82757
MA = 2
81555
Ha = 234
614 n
mi
Hp = 214
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4503620
13 X = -1443971
78
Y = 13531711
30 feet Y = 4108717
29 meter
Z = 17053279
13 Z = 5190997
41
XDOT = -21368
374886 XDOT = -6476
091910
YDOT = -12605
688016 feet/sec YDOT = -3914
840069 meter/sec
ZDOT = 4362
807354 ZDOT = 1298
233942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6019088
30 X = 1834618
11
Y = 12966868
84 feet Y = 3952301
62 meter
Z = 17024541
78 Z = 5189080
34
XDOT = -23230
560867 XDOT = -7080
674952
YDOT = 5230
669926 feet/sec YDOT = 1594
308194 meter/sec
ZDOT = 4232
717165 ZDOT = 1290
132192
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 12258
19229104
00016717 00000-0 10270-3 0 9058
2 25544 51
6475 38
8038 0018845 65
1756 295
1352 15
49852821 31855
Satellite: ISS
Catalog Number: 25544
Epoch time: 12258
19229104 = yrday
fracday
Element set: 905
Inclination: 51
6475 deg
RA of node: 38
8038 deg
Eccentricity:
0018845
Arg of perigee: 65
1756 deg
Mean anomaly: 295
1352 deg
Mean motion: 15
49852821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 327
Coasting Arc #7 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2012/259/03:23:59
101
Vector Time (MET): N/A
Weight (LBS) : 924491
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1337053
09 A = 6790124
98 meter
Y = -4093032
55 meter E =
0033073
Z = -5279093
01 I = 51
82590
XDOT = 6713
001106 Wp = 74
06407
YDOT = 3498
137545 meter/sec RA = 33
53584 deg
ZDOT = -1008
425649 TA = 186
24517
MA = 186
28650
Ha = 234
590 n
mi
Hp = 214
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4386657
11 X = 1408367
41
Y = -13428584
47 feet Y = -4077682
73 meter
Z = -17319858
94 Z = -5272423
93
XDOT = 22024
281844 XDOT = 6678
283966
YDOT = 11476
829215 feet/sec YDOT = 3573
012265 meter/sec
ZDOT = -3308
483101 ZDOT = -975
899097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6250719
91 X = -1905219
43
Y = -12707002
55 feet Y = -3873094
38 meter
Z = -17291840
33 Z = -5270552
93
XDOT = 22816
273657 XDOT = 6954
400211
YDOT = -6888
020082 feet/sec YDOT = -2099
468521 meter/sec
ZDOT = -3174
324356 ZDOT = -967
534064
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 12259
15949608
00016717 00000-0 10270-3 0 9064
2 25544 51
6486 34
0131 0018978 68
3991 291
9180 15
49865014 32001
Satellite: ISS
Catalog Number: 25544
Epoch time: 12259
15949608 = yrday
fracday
Element set: 906
Inclination: 51
6486 deg
RA of node: 34
0131 deg
Eccentricity:
0018978
Arg of perigee: 68
3991 deg
Mean anomaly: 291
9180 deg
Mean motion: 15
49865014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 329
Coasting Arc #8 (Orbit 3215)
---------------------------------------
Vector Time (GMT): 2012/260/03:23:59
101
Vector Time (MET): N/A
Weight (LBS) : 924491
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1326405
25 A = 6789759
18 meter
Y = 4019098
30 meter E =
0021079
Z = 5291076
27 I = 51
79952
XDOT = -6954
121623 Wp = 76
90608
YDOT = -3183
406985 meter/sec RA = 28
59258 deg
ZDOT = 677
204471 TA = 6
66374
MA = 6
63575
Ha = 234
564 n
mi
Hp = 214
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4351723
26 X = -1396951
95
Y = 13186018
05 feet Y = 4003871
88 meter
Z = 17359174
12 Z = 5284460
75
XDOT = -22815
359656 XDOT = -6921
296967
YDOT = -10444
248640 feet/sec YDOT = -3260
988687 meter/sec
ZDOT = 2221
799446 ZDOT = 643
501791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6319084
52 X = 1926056
96
Y = 12403297
34 feet Y = 3780525
03 meter
Z = 17331384
22 Z = 5282605
91
XDOT = -22518
021704 XDOT = -6863
493015
YDOT = 8572
959570 feet/sec YDOT = 2613
038077 meter/sec
ZDOT = 2082
753397 ZDOT = 634
823235
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 12260
19115901
00016717 00000-0 10270-3 0 9072
2 25544 51
6487 28
9032 0018843 71
9868 288
3334 15
49914254 32167
Satellite: ISS
Catalog Number: 25544
Epoch time: 12260
19115901 = yrday
fracday
Element set: 907
Inclination: 51
6487 deg
RA of node: 28
9032 deg
Eccentricity:
0018843
Arg of perigee: 71
9868 deg
Mean anomaly: 288
3334 deg
Mean motion: 15
49914254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3216
Checksum: 323
Coasting Arc #9 (Orbit 3230)
---------------------------------------
Vector Time (GMT): 2012/261/03:23:59
101
Vector Time (MET): N/A
Weight (LBS) : 924491
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1340010
11 A = 6789657
54 meter
Y = -4007751
49 meter E =
0033501
Z = -5343134
78 I = 51
77299
XDOT = 7089
627574 Wp = 80
22307
YDOT = 2818
563031 meter/sec RA = 23
64736 deg
ZDOT = -332
369218 TA = 186
57884
MA = 186
62293
Ha = 234
511 n
mi
Hp = 214
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4396358
63 X = 1410681
93
Y = -13148790
96 feet Y = -3992372
20 meter
Z = -17529969
74 Z = -5336452
85
XDOT = 23259
932985 XDOT = 7059
197481
YDOT = 9247
254040 feet/sec YDOT = 2897
673482 meter/sec
ZDOT = -1090
450191 ZDOT = -298
002205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6473085
12 X = -1972996
35
Y = -12300447
46 feet Y = -3749176
38 meter
Z = -17501904
85 Z = -5334580
60
XDOT = 21796
495539 XDOT = 6643
571840
YDOT = -10103
055431 feet/sec YDOT = -3079
411295 meter/sec
ZDOT = -948
629543 ZDOT = -289
142285
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 12261
15832571
00016717 00000-0 10270-3 0 9089
2 25544 51
6496 24
1127 0018910 75
1403 285
1840 15
49927675 32311
Satellite: ISS
Catalog Number: 25544
Epoch time: 12261
15832571 = yrday
fracday
Element set: 908
Inclination: 51
6496 deg
RA of node: 24
1127 deg
Eccentricity:
0018910
Arg of perigee: 75
1403 deg
Mean anomaly: 285
1840 deg
Mean motion: 15
49927675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3231
Checksum: 304
Coasting Arc #10 (Orbit 3246)
---------------------------------------
Vector Time (GMT): 2012/262/03:23:59
101
Vector Time (MET): N/A
Weight (LBS) : 924491
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1379750
15 A = 6789444
18 meter
Y = 3961759
01 meter E =
0021197
Z = 5320324
20 I = 51
74483
XDOT = -7265
071516 Wp = 79
02414
YDOT = -2484
211200 meter/sec RA = 18
69995 deg
ZDOT = -30
186286 TA = 11
28644
MA = 11
23898
Ha = 234
484 n
mi
Hp = 214
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4526739
34 X = -1449794
01
Y = 12997897
01 feet Y = 3945938
75 meter
Z = 17455131
89 Z = 5313450
78
XDOT = -23835
536469 XDOT = -7236
605950
YDOT = -8150
299212 feet/sec YDOT = -2565
294605 meter/sec
ZDOT = -99
036373 ZDOT = -65
410595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6484671
01 X = 1976527
72
Y = 12181634
58 feet Y = 3712962
22 meter
Z = 17426277
45 Z = 5311529
37
XDOT = -21192
173808 XDOT = -6459
374577
YDOT = 11649
958720 feet/sec YDOT = 3550
907418 meter/sec
ZDOT = -244
426673 ZDOT = -74
501250
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 12262
18994774
00016717 00000-0 10270-3 0 9098
2 25544 51
6497 19
0027 0018807 78
7382 281
5881 15
49977269 32470
Satellite: ISS
Catalog Number: 25544
Epoch time: 12262
18994774 = yrday
fracday
Element set: 909
Inclination: 51
6497 deg
RA of node: 19
0027 deg
Eccentricity:
0018807
Arg of perigee: 78
7382 deg
Mean anomaly: 281
5881 deg
Mean motion: 15
49977269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3247
Checksum: 362
Coasting Arc #11 (Orbit 3261)
---------------------------------------
Vector Time (GMT): 2012/263/03:23:59
101
Vector Time (MET): N/A
Weight (LBS) : 924491
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1433487
72 A = 6789510
89 meter
Y = -3984876
18 meter E =
0033382
Z = -5335645
46 I = 51
71614
XDOT = 7327
892427 Wp = 86
47868
YDOT = 2113
594268 meter/sec RA = 13
75025 deg
ZDOT = 394
343627 TA = 187
26891
MA = 187
31743
Ha = 234
405 n
mi
Hp = 214
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4703043
70 X = 1503860
56
Y = -13073740
75 feet Y = -3968453
05 meter
Z = -17505398
48 Z = -5328510
25
XDOT = 24041
641821 XDOT = 7301
797491
YDOT = 6934
364395 feet/sec YDOT = 2195
393463 meter/sec
ZDOT = 1293
778304 ZDOT = 429
879033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6633455
75 X = -2021877
31
Y = -12250959
59 feet Y = -3734092
48 meter
Z = -17475455
56 Z = -5326518
85
XDOT = 20194
221000 XDOT = 6155
198561
YDOT = -12969
867333 feet/sec YDOT = -3953
215563 meter/sec
ZDOT = 1440
485715 ZDOT = 439
060046
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 12263
15707551
00016717 00000-0 10270-3 0 9103
2 25544 51
6498 14
2120 0018811 81
8892 278
4392 15
49989572 32627
Satellite: ISS
Catalog Number: 25544
Epoch time: 12263
15707551 = yrday
fracday
Element set: 910
Inclination: 51
6498 deg
RA of node: 14
2120 deg
Eccentricity:
0018811
Arg of perigee: 81
8892 deg
Mean anomaly: 278
4392 deg
Mean motion: 15
49989572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3262
Checksum: 324
Coasting Arc #12 (Orbit 3277)
---------------------------------------
Vector Time (GMT): 2012/264/03:23:59
101
Vector Time (MET): N/A
Weight (LBS) : 924491
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1512418
77 A = 6789489
90 meter
Y = 3979840
17 meter E =
0021754
Z = 5270508
62 I = 51
68697
XDOT = -7428
518626 Wp = 81
26073
YDOT = -1776
673748 meter/sec RA = 8
79831 deg
ZDOT = -784
089035 TA = 16
25227
MA = 16
18261
Ha = 234
376 n
mi
Hp = 214
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4962003
84 X = -1582413
00
Y = 13057218
40 feet Y = 3962536
37 meter
Z = 17291694
95 Z = 5262990
97
XDOT = -24371
780268 XDOT = -7404
290410
YDOT = -5828
982113 feet/sec YDOT = -1859
608664 meter/sec
ZDOT = -2572
470588 ZDOT = -820
117877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6663686
04 X = 2031091
51
Y = 12320594
54 feet Y = 3755317
22 meter
Z = 17260167
64 Z = 5260899
10
XDOT = -19321
469856 XDOT = -5889
184012
YDOT = 14290
025976 feet/sec YDOT = 4355
599918 meter/sec
ZDOT = -2721
248708 ZDOT = -829
436606
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 12264
18865599
00016717 00000-0 10270-3 0 9115
2 25544 51
6498 9
1018 0018738 85
5054 274
8236 15
50039570 32785
Satellite: ISS
Catalog Number: 25544
Epoch time: 12264
18865599 = yrday
fracday
Element set: 911
Inclination: 51
6498 deg
RA of node: 9
1018 deg
Eccentricity:
0018738
Arg of perigee: 85
5054 deg
Mean anomaly: 274
8236 deg
Mean motion: 15
50039570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3278
Checksum: 334
Coasting Arc #13 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2012/265/03:23:59
101
Vector Time (MET): N/A
Weight (LBS) : 924491
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1592582
44 A = 6789751
05 meter
Y = -4048282
27 meter E =
0032656
Z = -5241578
94 I = 51
65706
XDOT = 7413
896893 Wp = 92
77571
YDOT = 1418
873655 meter/sec RA = 3
84357 deg
ZDOT = 1161
496030 TA = 188
37773
MA = 188
43238
Ha = 234
284 n
mi
Hp = 214
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5225008
02 X = 1663195
45
Y = -13281765
98 feet Y = -4030078
48 meter
Z = -17196781
30 Z = -5233670
44
XDOT = 24323
808703 XDOT = 7391
837394
YDOT = 4655
097292 feet/sec YDOT = 1501
657193 meter/sec
ZDOT = 3810
682514 ZDOT = 1197
459072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6881595
67 X = -2097510
36
Y = -12549455
88 feet Y = -3825074
15 meter
Z = -17163627
28 Z = -5231473
60
XDOT = 18105
283778 XDOT = 5518
490496
YDOT = -15321
828315 feet/sec YDOT = -4670
093271 meter/sec
ZDOT = 3959
224699 ZDOT = 1206
771688
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 12265
15574445
00016717 00000-0 10270-3 0 9121
2 25544 51
6491 4
3102 0018710 88
7382 271
5912 15
50049951 32934
Satellite: ISS
Catalog Number: 25544
Epoch time: 12265
15574445 = yrday
fracday
Element set: 912
Inclination: 51
6491 deg
RA of node: 4
3102 deg
Eccentricity:
0018710
Arg of perigee: 88
7382 deg
Mean anomaly: 271
5912 deg
Mean motion: 15
50049951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 299
Coasting Arc #14 (Orbit 3308)
---------------------------------------
Vector Time (GMT): 2012/266/03:23:59
101
Vector Time (MET): N/A
Weight (LBS) : 924491
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1695136
48 A = 6789955
55 meter
Y = 4092910
92 meter E =
0022794
Z = 5126599
28 I = 51
62802
XDOT = -7434
669644 Wp = 84
18178
YDOT = -1100
222525 meter/sec RA = 358
88699 deg
ZDOT = -1571
658293 TA = 20
99943
MA = 20
90598
Ha = 234
244 n
mi
Hp = 214
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5561471
39 X = -1765682
27
Y = 13428185
42 feet Y = 4073560
63 meter
Z = 16819551
45 Z = 5118192
80
XDOT = -24391
960774 XDOT = -7414
179360
YDOT = -3609
653955 feet/sec YDOT = -1183
247140 meter/sec
ZDOT = -5156
359229 ZDOT = -1607
725953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7003548
23 X = 2134681
50
Y = 12782016
96 feet Y = 3895958
77 meter
Z = 16784331
78 Z = 5115864
33
XDOT = -17031
432109 XDOT = -5191
180507
YDOT = 16334
194947 feet/sec YDOT = 4978
662620 meter/sec
ZDOT = -5305
368235 ZDOT = -1617
076238
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 12266
18728306
00016717 00000-0 10270-3 0 9133
2 25544 51
6491 359
1996 0018642 92
3718 267
9568 15
50099550 33098
Satellite: ISS
Catalog Number: 25544
Epoch time: 12266
18728306 = yrday
fracday
Element set: 913
Inclination: 51
6491 deg
RA of node: 359
1996 deg
Eccentricity:
0018642
Arg of perigee: 92
3718 deg
Mean anomaly: 267
9568 deg
Mean motion: 15
50099550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3309
Checksum: 345
Coasting Arc #15 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2012/267/03:23:59
101
Vector Time (MET): N/A
Weight (LBS) : 924491
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1784415
71 A = 6790417
85 meter
Y = -4212386
33 meter E =
0031299
Z = -5046390
19 I = 51
59820
XDOT = 7342
936568 Wp = 98
96584
YDOT = 776
409128 meter/sec RA = 353
92740 deg
ZDOT = 1954
037830 TA = 190
05612
MA = 190
11890
Ha = 234
158 n
mi
Hp = 214
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5854382
25 X = 1855901
12
Y = -13820165
11 feet Y = -4192032
42 meter
Z = -16556398
28 Z = -5037547
73
XDOT = 24090
999238 XDOT = 7324
216566
YDOT = 2547
274041 feet/sec YDOT = 858
417847 meter/sec
ZDOT = 6410
885269 ZDOT = 1989
664019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7356623
31 X = -2242298
79
Y = -13129197
43 feet Y = -4001779
38 meter
Z = -16519362
80 Z = -5035101
78
XDOT = 15682
514420 XDOT = 4780
030395
YDOT = -17015
439265 feet/sec YDOT = -5186
305888 meter/sec
ZDOT = 6558
104633 ZDOT = 1998
910292
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 12267
15433223
00016717 00000-0 10270-3 0 9143
2 25544 51
6481 354
4073 0018634 95
7408 264
5868 15
50108900 33248
Satellite: ISS
Catalog Number: 25544
Epoch time: 12267
15433223 = yrday
fracday
Element set: 914
Inclination: 51
6481 deg
RA of node: 354
4073 deg
Eccentricity:
0018634
Arg of perigee: 95
7408 deg
Mean anomaly: 264
5868 deg
Mean motion: 15
50108900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 305
Coasting Arc #16 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2012/268/03:23:59
101
Vector Time (MET): N/A
Weight (LBS) : 924491
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1891970
92 A = 6790864
48 meter
Y = 4309443
06 meter E =
0024286
Z = 4874645
53 I = 51
57041
XDOT = -7284
643022 Wp = 88
27609
YDOT = -499
404887 meter/sec RA = 348
96655 deg
ZDOT = -2374
904465 TA = 25
03833
MA = 24
92074
Ha = 234
097 n
mi
Hp = 214
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6207253
66 X = -1963699
27
Y = 14138592
72 feet Y = 4287885
10 meter
Z = 15992931
53 Z = 4865279
95
XDOT = -23899
747448 XDOT = -7266
980433
YDOT = -1638
467476 feet/sec YDOT = -580
767696 meter/sec
ZDOT = -7791
681316 ZDOT = -2410
249922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7629965
33 X = 2325613
43
Y = 13470930
22 feet Y = 4105939
53 meter
Z = 15953724
62 Z = 4862695
26
XDOT = -14503
549518 XDOT = -4420
681893
YDOT = 17658
239869 feet/sec YDOT = 5382
231512 meter/sec
ZDOT = -7937
769729 ZDOT = -2419
432213
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 12268
18582904
00016717 00000-0 10270-3 0 9159
2 25544 51
6483 349
2963 0018544 99
4047 260
9201 15
50156666 33401
Satellite: ISS
Catalog Number: 25544
Epoch time: 12268
18582904 = yrday
fracday
Element set: 915
Inclination: 51
6483 deg
RA of node: 349
2963 deg
Eccentricity:
0018544
Arg of perigee: 99
4047 deg
Mean anomaly: 260
9201 deg
Mean motion: 15
50156666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3340
Checksum: 324
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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