[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 15th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 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
There are no maneuvers
Coasting Arc #1 (Orbit 3190)
---------------------------------------
Vector Time (GMT): 2012/258/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5709010
27 A = 6796589
51 meter
Y = -699563
99 meter E =
0029124
Z = 3605692
71 I = 51
86029
XDOT = -2104
786167 Wp = 71
61279
YDOT = -5888
399681 meter/sec RA = 36
47438 deg
ZDOT = -4436
690344 TA = 65
90759
MA = 65
60321
Ha = 234
298 n
mi
Hp = 215
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18730348
67 X = -5718278
84
Y = -2295157
45 feet Y = -763457
09 meter
Z = 11829700
50 Z = 3577936
34
XDOT = -6905
466426 XDOT = -2017
232109
YDOT = -19318
896591 feet/sec YDOT = -5911
447712 meter/sec
ZDOT = -14556
070684 ZDOT = -4446
701855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18941611
69 X = 5773403
24
Y = -101735
42 feet Y = -31008
96 meter
Z = 11714969
89 Z = 3570722
82
XDOT = 9197
262822 XDOT = 2803
325708
YDOT = 16921
490152 feet/sec YDOT = 5157
670198 meter/sec
ZDOT = -14596
855216 ZDOT = -4449
121470
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
57923750
00016717 00000-0 10270-3 0 9003
2 25544 51
6474 36
8845 0017785 61
8548 298
4397 15
49791334 31915
Satellite: ISS
Catalog Number: 25544
Epoch time: 12258
57923750 = yrday
fracday
Element set: 900
Inclination: 51
6474 deg
RA of node: 36
8845 deg
Eccentricity:
0017785
Arg of perigee: 61
8548 deg
Mean anomaly: 298
4397 deg
Mean motion: 15
49791334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3191
Checksum: 352
Coasting Arc #2 (Orbit 3205)
---------------------------------------
Vector Time (GMT): 2012/259/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5853777
52 A = 6797033
25 meter
Y = 422028
79 meter E =
0022272
Z = -3438420
90 I = 51
83804
XDOT = 2285
038062 Wp = 69
36806
YDOT = 5658
885595 meter/sec RA = 31
53656 deg
ZDOT = 4616
584429 TA = 250
62274
MA = 250
86364
Ha = 234
266 n
mi
Hp = 215
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19205306
82 X = 5865326
28
Y = 1384608
88 feet Y = 487553
49 meter
Z = -11280908
46 Z = -3409955
57
XDOT = 7496
844035 XDOT = 2199
163110
YDOT = 18565
897620 feet/sec YDOT = 5683
958780 meter/sec
ZDOT = 15146
274372 ZDOT = 4627
475673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19273106
46 X = -5874442
85
Y = 1396305
24 feet Y = 425593
84 meter
Z = -11163222
94 Z = -3402550
35
XDOT = -9889
947763 XDOT = -3014
456078
YDOT = -15906
762004 feet/sec YDOT = -4848
381059 meter/sec
ZDOT = 15190
716891 ZDOT = 4630
130508
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
54645303
00016717 00000-0 10270-3 0 9017
2 25544 51
6484 32
0952 0017787 64
5751 295
7238 15
49808026 32069
Satellite: ISS
Catalog Number: 25544
Epoch time: 12259
54645303 = yrday
fracday
Element set: 901
Inclination: 51
6484 deg
RA of node: 32
0952 deg
Eccentricity:
0017787
Arg of perigee: 64
5751 deg
Mean anomaly: 295
7238 deg
Mean motion: 15
49808026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3206
Checksum: 320
Coasting Arc #3 (Orbit 3221)
---------------------------------------
Vector Time (GMT): 2012/260/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6002297
47 A = 6797725
54 meter
Y = -222096
22 meter E =
0029989
Z = 3164133
18 I = 51
81457
XDOT = -2374
933136 Wp = 79
25120
YDOT = -5449
130702 meter/sec RA = 26
59612 deg
ZDOT = -4843
257567 TA = 64
38126
MA = 64
07170
Ha = 234
305 n
mi
Hp = 215
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19692577
02 X = -6014738
54
Y = -728662
13 feet Y = -289286
79 meter
Z = 10381014
37 Z = 3134944
01
XDOT = -7791
775381 XDOT = -2290
295784
YDOT = -17877
725399 feet/sec YDOT = -5475
216104 meter/sec
ZDOT = -15889
952649 ZDOT = -4854
588603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19616469
06 X = 5979099
77
Y = -2452332
32 feet Y = -747470
89 meter
Z = 10260321
89 Z = 3127346
11
XDOT = 10285
416010 XDOT = 3134
994800
YDOT = 14981
480086 feet/sec YDOT = 4566
355130 meter/sec
ZDOT = -15936
229622 ZDOT = -4857
362789
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
57813743
00016717 00000-0 10270-3 0 9028
2 25544 51
6488 26
9851 0017846 68
8136 291
4920 15
49832374 32225
Satellite: ISS
Catalog Number: 25544
Epoch time: 12260
57813743 = yrday
fracday
Element set: 902
Inclination: 51
6488 deg
RA of node: 26
9851 deg
Eccentricity:
0017846
Arg of perigee: 68
8136 deg
Mean anomaly: 291
4920 deg
Mean motion: 15
49832374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3222
Checksum: 327
Coasting Arc #4 (Orbit 3236)
---------------------------------------
Vector Time (GMT): 2012/261/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6118441
98 A = 6798179
34 meter
Y = -86272
18 meter E =
0022376
Z = -2969956
93 I = 51
78957
XDOT = 2485
518789 Wp = 69
83159
YDOT = 5227
539509 meter/sec RA = 21
65510 deg
ZDOT = 5006
734705 TA = 256
40862
MA = 256
65794
Ha = 234
270 n
mi
Hp = 215
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20073628
55 X = 6133379
45
Y = -283045
21 feet Y = -17768
80 meter
Z = -9743953
18 Z = -2940197
29
XDOT = 8154
589202 XDOT = 2402
556846
YDOT = 17150
720174 feet/sec YDOT = 5254
870889 meter/sec
ZDOT = 16426
294965 ZDOT = 5018
607170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19763011
18 X = -6023765
81
Y = 3851938
18 feet Y = 1174070
76 meter
Z = -9620876
40 Z = -2932443
13
XDOT = -10688
923115 XDOT = -3257
983765
YDOT = -14009
134575 feet/sec YDOT = -4269
984219 meter/sec
ZDOT = 16474
826592 ZDOT = 5021
527145
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
54532766
00016717 00000-0 10270-3 0 9030
2 25544 51
6496 22
1958 0017814 71
3770 288
9313 15
49844064 32370
Satellite: ISS
Catalog Number: 25544
Epoch time: 12261
54532766 = yrday
fracday
Element set: 903
Inclination: 51
6496 deg
RA of node: 22
1958 deg
Eccentricity:
0017814
Arg of perigee: 71
3770 deg
Mean anomaly: 288
9313 deg
Mean motion: 15
49844064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3237
Checksum: 324
Coasting Arc #5 (Orbit 3252)
---------------------------------------
Vector Time (GMT): 2012/262/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6237374
58 A = 6798825
12 meter
Y = 317899
74 meter E =
0030622
Z = 2662690
71 I = 51
76334
XDOT = -2503
598863 Wp = 86
83619
YDOT = -5037
875040 meter/sec RA = 16
71192 deg
ZDOT = -5209
857771 TA = 63
20983
MA = 62
89692
Ha = 234
294 n
mi
Hp = 214
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20463827
37 X = -6253400
72
Y = 1042978
15 feet Y = 248060
20 meter
Z = 8735861
91 Z = 2632350
54
XDOT = -8213
907030 XDOT = -2421
769629
YDOT = -16528
461417 feet/sec YDOT = -5065
414866 meter/sec
ZDOT = -17092
709223 ZDOT = -5221
820973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19922836
27 X = 6072480
49
Y = -5011337
91 feet Y = -1527455
80 meter
Z = 8610366
12 Z = 2624439
59
XDOT = 10801
768561 XDOT = 3292
379057
YDOT = 13185
415020 feet/sec YDOT = 4018
914498 meter/sec
ZDOT = -17141
627907 ZDOT = -5224
768186
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
57698491
00016717 00000-0 10270-3 0 9043
2 25544 51
6495 17
0861 0017924 75
6934 284
6205 15
49874542 32531
Satellite: ISS
Catalog Number: 25544
Epoch time: 12262
57698491 = yrday
fracday
Element set: 904
Inclination: 51
6495 deg
RA of node: 17
0861 deg
Eccentricity:
0017924
Arg of perigee: 75
6934 deg
Mean anomaly: 284
6205 deg
Mean motion: 15
49874542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3253
Checksum: 338
Coasting Arc #6 (Orbit 3267)
---------------------------------------
Vector Time (GMT): 2012/263/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6314472
79 A = 6799257
92 meter
Y = -651541
50 meter E =
0022790
Z = -2441399
25 I = 51
73618
XDOT = 2550
036566 Wp = 70
44798
YDOT = 4842
530114 meter/sec RA = 11
76724 deg
ZDOT = 5351
296738 TA = 262
34686
MA = 262
60575
Ha = 234
253 n
mi
Hp = 214
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20716774
26 X = 6333149
07
Y = -2137603
36 feet Y = -580824
91 meter
Z = -8009840
04 Z = -2410678
04
XDOT = 8366
261701 XDOT = 2469
701158
YDOT = 15887
565992 feet/sec YDOT = 4870
597485 meter/sec
ZDOT = 17556
747829 ZDOT = 5363
489304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19845397
15 X = -6048877
05
Y = 6475669
51 feet Y = 1973784
07 meter
Z = -7882736
69 Z = -2402658
14
XDOT = -10955
913565 XDOT = -3339
362455
YDOT = -12338
823270 feet/sec YDOT = -3760
873333 meter/sec
ZDOT = 17606
628353 ZDOT = 5366
500322
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
54414937
00016717 00000-0 10270-3 0 9053
2 25544 51
6500 12
2965 0017843 78
2289 282
0862 15
49881846 32684
Satellite: ISS
Catalog Number: 25544
Epoch time: 12263
54414937 = yrday
fracday
Element set: 905
Inclination: 51
6500 deg
RA of node: 12
2965 deg
Eccentricity:
0017843
Arg of perigee: 78
2289 deg
Mean anomaly: 282
0862 deg
Mean motion: 15
49881846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3268
Checksum: 331
Coasting Arc #7 (Orbit 3283)
---------------------------------------
Vector Time (GMT): 2012/264/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6392337
02 A = 6799803
39 meter
Y = 907137
96 meter E =
0030916
Z = 2102335
52 I = 51
70773
XDOT = -2504
554772 Wp = 94
27211
YDOT = -4691
401063 meter/sec RA = 6
82047 deg
ZDOT = -5523
216455 TA = 62
49364
MA = 62
17975
Ha = 234
252 n
mi
Hp = 214
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20972234
32 X = -6412218
51
Y = 2976174
42 feet Y = 835543
83 meter
Z = 6897426
24 Z = 2071233
15
XDOT = -8217
043216 XDOT = -2425
077577
YDOT = -15391
735771 feet/sec YDOT = -4718
964526 meter/sec
ZDOT = -18120
788893 ZDOT = -5535
190249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19782000
47 X = 6029553
74
Y = -7689186
63 feet Y = -2343664
09 meter
Z = 6768720
83 Z = 2063106
11
XDOT = 10841
181683 XDOT = 3304
392177
YDOT = 11696
902140 feet/sec YDOT = 3565
215772 meter/sec
ZDOT = -18169
775341 ZDOT = -5538
147524
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
57577902
00016717 00000-0 10270-3 0 9060
2 25544 51
6493 7
1866 0017985 82
4526 277
8667 15
49920116 32843
Satellite: ISS
Catalog Number: 25544
Epoch time: 12264
57577902 = yrday
fracday
Element set: 906
Inclination: 51
6493 deg
RA of node: 7
1866 deg
Eccentricity:
0017985
Arg of perigee: 82
4526 deg
Mean anomaly: 277
8667 deg
Mean motion: 15
49920116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3284
Checksum: 347
Coasting Arc #8 (Orbit 3298)
---------------------------------------
Vector Time (GMT): 2012/265/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6421097
52 A = 6800192
40 meter
Y = -1256742
22 meter E =
0023518
Z = -1854628
69 I = 51
67920
XDOT = 2497
290160 Wp = 71
61845
YDOT = 4538
769160 meter/sec RA = 1
87167 deg
ZDOT = 5636
525681 TA = 268
04085
MA = 268
31021
Ha = 234
215 n
mi
Hp = 214
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21066592
90 X = 6443682
87
Y = -4123170
02 feet Y = -1184811
32 meter
Z = -6084739
81 Z = -1823380
13
XDOT = 8193
209187 XDOT = 2418
969914
YDOT = 14890
974933 feet/sec YDOT = 4566
257780 meter/sec
ZDOT = 18492
538325 ZDOT = 5648
467034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19452814
15 X = -5929217
75
Y = 9162273
74 feet Y = 2792661
04 meter
Z = -5955391
48 Z = -1815203
32
XDOT = -10810
238203 XDOT = -3294
960604
YDOT = -11043
714902 feet/sec YDOT = -3366
124302 meter/sec
ZDOT = 18541
403873 ZDOT = 5651
419900
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
54291750
00016717 00000-0 10270-3 0 9073
2 25544 51
6496 2
3965 0017864 85
0719 275
2471 15
49919270 32992
Satellite: ISS
Catalog Number: 25544
Epoch time: 12265
54291750 = yrday
fracday
Element set: 907
Inclination: 51
6496 deg
RA of node: 2
3965 deg
Eccentricity:
0017864
Arg of perigee: 85
0719 deg
Mean anomaly: 275
2471 deg
Mean motion: 15
49919270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3299
Checksum: 339
Coasting Arc #9 (Orbit 3314)
---------------------------------------
Vector Time (GMT): 2012/266/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6448396
56 A = 6800570
48 meter
Y = 1524510
80 meter E =
0030785
Z = 1486300
93 I = 51
64983
XDOT = -2401
841135 Wp = 101
44045
YDOT = -4441
795506 meter/sec RA = 356
92079 deg
ZDOT = -5769
142015 TA = 62
35381
MA = 62
04165
Ha = 234
172 n
mi
Hp = 214
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21156156
70 X = -6472184
84
Y = 5001675
86 feet Y = 1452267
87 meter
Z = 4876315
38 Z = 1454916
94
XDOT = -7880
056217 XDOT = -2323
968249
YDOT = -14572
819903 feet/sec YDOT = -4468
219240 meter/sec
ZDOT = -18927
631284 ZDOT = -5780
620741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19142069
10 X = 5834502
66
Y = -10364905
81 feet Y = -3159223
29 meter
Z = 4746377
27 Z = 1446695
79
XDOT = 10547
227193 XDOT = 3214
794848
YDOT = 10642
555885 feet/sec YDOT = 3243
851034 meter/sec
ZDOT = -18974
593489 ZDOT = -5783
456095
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
57451930
00016717 00000-0 10270-3 0 9086
2 25544 51
6489 357
2860 0018012 89
0797 271
2417 15
49969909 33155
Satellite: ISS
Catalog Number: 25544
Epoch time: 12266
57451930 = yrday
fracday
Element set: 908
Inclination: 51
6489 deg
RA of node: 357
2860 deg
Eccentricity:
0018012
Arg of perigee: 89
0797 deg
Mean anomaly: 271
2417 deg
Mean motion: 15
49969909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3315
Checksum: 345
Coasting Arc #10 (Orbit 3329)
---------------------------------------
Vector Time (GMT): 2012/267/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6421901
34 A = 6800896
69 meter
Y = -1877329
67 meter E =
0024525
Z = -1214129
47 I = 51
62076
XDOT = 2355
917667 Wp = 73
71430
YDOT = 4344
944258 meter/sec RA = 351
96787 deg
ZDOT = 5847
860826 TA = 273
12013
MA = 273
40072
Ha = 234
165 n
mi
Hp = 214
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21069230
13 X = 6448314
71
Y = -6159218
09 feet Y = -1805368
35 meter
Z = -3983364
41 Z = -1182867
92
XDOT = 7729
388672 XDOT = 2278
748916
YDOT = 14255
066464 feet/sec YDOT = 4370
858430 meter/sec
ZDOT = 19185
895097 ZDOT = 5859
118096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18550518
31 X = -5654197
98
Y = 11778853
47 feet Y = 3590194
54 meter
Z = -3853894
04 Z = -1174666
90
XDOT = -10414
967299 XDOT = -3174
482033
YDOT = -10226
575820 feet/sec YDOT = -3117
060310 meter/sec
ZDOT = 19231
953190 ZDOT = 5861
899332
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
54163197
00016717 00000-0 10270-3 0 9090
2 25544 51
6490 352
4957 0017895 91
8365 268
4835 15
49954954 33304
Satellite: ISS
Catalog Number: 25544
Epoch time: 12267
54163197 = yrday
fracday
Element set: 909
Inclination: 51
6490 deg
RA of node: 352
4957 deg
Eccentricity:
0017895
Arg of perigee: 91
8365 deg
Mean anomaly: 268
4835 deg
Mean motion: 15
49954954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3330
Checksum: 358
Coasting Arc #11 (Orbit 3345)
---------------------------------------
Vector Time (GMT): 2012/268/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6392602
54 A = 6801045
35 meter
Y = 2141923
60 meter E =
0030204
Z = 820502
94 I = 51
59179
XDOT = -2228
599256 Wp = 108
21338
YDOT = -4313
279856 meter/sec RA = 347
01290 deg
ZDOT = -5932
954674 TA = 62
91778
MA = 62
60993
Ha = 234
070 n
mi
Hp = 214
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20973105
44 X = -6420064
67
Y = 7027308
40 feet Y = 2070284
04 meter
Z = 2691938
76 Z = 789381
21
XDOT = -7311
677349 XDOT = -2151
380760
YDOT = -14151
180630 feet/sec YDOT = -4337
770096 meter/sec
ZDOT = -19465
074389 ZDOT = -5943
593218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17990206
99 X = 5483415
09
Y = -12895120
40 feet Y = -3930432
70 meter
Z = 2563020
05 Z = 781208
51
XDOT = 10099
668543 XDOT = 3078
378972
YDOT = 10096
002295 feet/sec YDOT = 3077
261500 meter/sec
ZDOT = -19508
579772 ZDOT = -5946
215114
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
57320597
00016717 00000-0 10270-3 0 9105
2 25544 51
6488 347
3847 0018027 95
6627 264
6580 15
50020841 33466
Satellite: ISS
Catalog Number: 25544
Epoch time: 12268
57320597 = yrday
fracday
Element set: 910
Inclination: 51
6488 deg
RA of node: 347
3847 deg
Eccentricity:
0018027
Arg of perigee: 95
6627 deg
Mean anomaly: 264
6580 deg
Mean motion: 15
50020841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3346
Checksum: 325
Coasting Arc #12 (Orbit 3360)
---------------------------------------
Vector Time (GMT): 2012/269/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6307622
14 A = 6801276
05 meter
Y = -2482454
24 meter E =
0025718
Z = -527207
95 I = 51
56284
XDOT = 2162
596831 Wp = 77
04231
YDOT = 4280
412424 meter/sec RA = 342
05610 deg
ZDOT = 5970
506110 TA = 277
27640
MA = 277
56865
Ha = 234
108 n
mi
Hp = 214
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20694298
36 X = 6337473
71
Y = -8144534
91 feet Y = -2411751
61 meter
Z = -1729684
89 Z = -496493
21
XDOT = 7095
133959 XDOT = 2085
568380
YDOT = 14043
347848 feet/sec YDOT = 4304
165771 meter/sec
ZDOT = 19588
274640 ZDOT = 5980
824385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17147934
56 X = -5226690
45
Y = 14176030
63 feet Y = 4320854
14 meter
Z = -1602416
63 Z = -488416
59
XDOT = -9960
811210 XDOT = -3036
055257
YDOT = -9930
877262 feet/sec YDOT = -3026
931390 meter/sec
ZDOT = 19630
462091 ZDOT = 5983
364845
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 12269
54029313
00016717 00000-0 10270-3 0 9116
2 25544 51
6486 342
5944 0017957 98
5188 261
7998 15
49990772 33619
Satellite: ISS
Catalog Number: 25544
Epoch time: 12269
54029313 = yrday
fracday
Element set: 911
Inclination: 51
6486 deg
RA of node: 342
5944 deg
Eccentricity:
0017957
Arg of perigee: 98
5188 deg
Mean anomaly: 261
7998 deg
Mean motion: 15
49990772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3361
Checksum: 359
Coasting Arc #13 (Orbit 3376)
---------------------------------------
Vector Time (GMT): 2012/270/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6220454
97 A = 6801162
41 meter
Y = 2726042
85 meter E =
0029194
Z = 113691
96 I = 51
53504
XDOT = -2024
561550 Wp = 114
43406
YDOT = -4319
332615 meter/sec RA = 337
09712 deg
ZDOT = -6000
118197 TA = 64
34104
MA = 64
03977
Ha = 233
967 n
mi
Hp = 214
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20408316
83 X = -6251028
12
Y = 8943710
14 feet Y = 2656310
91 meter
Z = 373005
12 Z = 83398
80
XDOT = -6642
262303 XDOT = -1946
964260
YDOT = -14171
038763 feet/sec YDOT = -4341
539306 meter/sec
ZDOT = -19685
427157 ZDOT = -6009
764448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16362079
27 X = 4987161
76
Y = -15127775
93 feet Y = -4610946
10 meter
Z = 247460
92 Z = 75426
09
XDOT = 9695
366464 XDOT = 2955
147698
YDOT = 10066
401322 feet/sec YDOT = 3068
239123 meter/sec
ZDOT = -19724
834395 ZDOT = -6012
129524
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 12270
57183942
00016717 00000-0 10270-3 0 9121
2 25544 51
6490 337
4832 0018057 102
3485 257
9688 15
50066944 33776
Satellite: ISS
Catalog Number: 25544
Epoch time: 12270
57183942 = yrday
fracday
Element set: 912
Inclination: 51
6490 deg
RA of node: 337
4832 deg
Eccentricity:
0018057
Arg of perigee: 102
3485 deg
Mean anomaly: 257
9688 deg
Mean motion: 15
50066944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3377
Checksum: 331
Coasting Arc #14 (Orbit 3392)
---------------------------------------
Vector Time (GMT): 2012/271/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6078564
59 A = 6801238
55 meter
Y = -3037127
88 meter E =
0026930
Z = 196045
86 I = 51
50684
XDOT = 1958
920698 Wp = 81
78018
YDOT = 4352
676608 meter/sec RA = 332
13651 deg
ZDOT = 5990
105424 TA = 280
33145
MA = 280
63493
Ha = 234
035 n
mi
Hp = 214
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19942797
22 X = 6111122
27
Y = -9964330
33 feet Y = -2968971
52 meter
Z = 643195
07 Z = 225654
71
XDOT = 6426
905176 XDOT = 1881
003980
YDOT = 14280
435064 feet/sec YDOT = 4374
147565 meter/sec
ZDOT = 19652
576850 ZDOT = 5999
431977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15306020
17 X = -4665274
95
Y = 16203574
62 feet Y = 4938849
54 meter
Z = 765934
75 Z = 233456
91
XDOT = -9644
476024 XDOT = -2939
636292
YDOT = -10132
601891 feet/sec YDOT = -3088
417056 meter/sec
ZDOT = 19690
660825 ZDOT = 6001
713419
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 12271
60337326
00016717 00000-0 10270-3 0 9134
2 25544 51
6484 332
3734 0018043 105
4453 254
8692 15
50032279 33931
Satellite: ISS
Catalog Number: 25544
Epoch time: 12271
60337326 = yrday
fracday
Element set: 913
Inclination: 51
6484 deg
RA of node: 332
3734 deg
Eccentricity:
0018043
Arg of perigee: 105
4453 deg
Mean anomaly: 254
8692 deg
Mean motion: 15
50032279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3393
Checksum: 299
Coasting Arc #15 (Orbit 3407)
---------------------------------------
Vector Time (GMT): 2012/272/12:56:39
676
Vector Time (MET): N/A
Weight (LBS) : 922647
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5937904
86 A = 6800867
75 meter
Y = 3240995
22 meter E =
0027794
Z = -622461
16 I = 51
48060
XDOT = -1832
538171 Wp = 119
86473
YDOT = -4460
502706 meter/sec RA = 327
17340 deg
ZDOT = -5956
921693 TA = 66
86067
MA = 66
56804
Ha = 233
868 n
mi
Hp = 214
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19481315
16 X = -5970681
23
Y = 10633186
42 feet Y = 3174410
52 meter
Z = -2042195
41 Z = -651387
39
XDOT = -6012
264342 XDOT = -1753
586195
YDOT = -14634
195231 feet/sec YDOT = -4480
554635 meter/sec
ZDOT = -19543
706341 ZDOT = -5965
631754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14346041
44 X = 4372673
43
Y = -16919608
89 feet Y = -5157096
79 meter
Z = -2162125
31 Z = -659015
80
XDOT = 9524
987167 XDOT = 2903
216088
YDOT = 10493
614586 feet/sec YDOT = 3198
453726 meter/sec
ZDOT = -19579
231437 ZDOT = -5967
749742
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 12272
57041965
00016717 00000-0 10270-3 0 9143
2 25544 51
6490 327
5814 0018099 109
2320 251
0791 15
50104461 34088
Satellite: ISS
Catalog Number: 25544
Epoch time: 12272
57041965 = yrday
fracday
Element set: 914
Inclination: 51
6490 deg
RA of node: 327
5814 deg
Eccentricity:
0018099
Arg of perigee: 109
2320 deg
Mean anomaly: 251
0791 deg
Mean motion: 15
50104461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3408
Checksum: 295
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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