[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 8th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20989 63 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 3838)
---------------------------------------
Vector Time (GMT): 2014/342/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4528505
84 A = 6795709
70 meter
Y = 5044492
63 meter E =
0019571
Z = 345750
91 I = 51
40923
XDOT = -3775
404468 Wp = 122
82985
YDOT = -2963
173932 meter/sec RA = 314
24744 deg
ZDOT = -5979
790617 TA = 53
43360
MA = 53
25363
Ha = 227
060 n
mi
Hp = 215
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14857302
62 X = -4586257
51
Y = 16550172
66 feet Y = 4993529
00 meter
Z = 1134353
37 Z = 323612
18
XDOT = -12386
497600 XDOT = -3712
940961
YDOT = -9721
699252 feet/sec YDOT = -3005
043136 meter/sec
ZDOT = -19618
735619 ZDOT = -5997
979630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19764600
17 X = -6024250
13
Y = -10208601
71 feet Y = -3111581
80 meter
Z = 1038963
49 Z = 316676
07
XDOT = 5571
412474 XDOT = 1698
166522
YDOT = -12877
317503 feet/sec YDOT = -3925
006375 meter/sec
ZDOT = -19695
689414 ZDOT = -6003
246133
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 14342
61120316
00016717 00000-0 10270-3 0 9001
2 25544 51
6455 314
7158 0007276 108
7979 251
3962 15
51922655 38392
Satellite: ISS
Catalog Number: 25544
Epoch time: 14342
61120316 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 314
7158 deg
Eccentricity:
0007276
Arg of perigee: 108
7979 deg
Mean anomaly: 251
3962 deg
Mean motion: 15
51922655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3839
Checksum: 317
Coasting Arc #2 (Orbit 3854)
---------------------------------------
Vector Time (GMT): 2014/343/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4649310
90 A = 6795438
99 meter
Y = -4910787
85 meter E =
0017856
Z = 614714
00 I = 51
38742
XDOT = 3107
335904 Wp = 72
31244
YDOT = 3703
588219 meter/sec RA = 309
27013 deg
ZDOT = 5947
410733 TA = 294
34047
MA = 294
52679
Ha = 226
971 n
mi
Hp = 215
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15253644
67 X = 4700892
84
Y = -16111508
69 feet Y = -4858507
88 meter
Z = 2016778
21 Z = 637424
58
XDOT = 10194
671601 XDOT = 3036
799945
YDOT = 12150
879985 feet/sec YDOT = 3737
941568 meter/sec
ZDOT = 19512
502405 ZDOT = 5962
334734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19615694
03 X = 5978863
54
Y = 10347700
52 feet Y = 3153979
12 meter
Z = 2114574
20 Z = 644522
22
XDOT = -8242
869010 XDOT = -2512
426474
YDOT = 11537
370135 feet/sec YDOT = 3516
590417 meter/sec
ZDOT = 19575
394922 ZDOT = 5966
580372
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 14343
64148044
00016717 00000-0 10270-3 0 9014
2 25544 51
6454 309
5971 0007244 112
6551 247
5368 15
51969362 38552
Satellite: ISS
Catalog Number: 25544
Epoch time: 14343
64148044 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 309
5971 deg
Eccentricity:
0007244
Arg of perigee: 112
6551 deg
Mean anomaly: 247
5368 deg
Mean motion: 15
51969362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3855
Checksum: 320
Coasting Arc #3 (Orbit 3869)
---------------------------------------
Vector Time (GMT): 2014/344/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4716602
27 A = 6794345
96 meter
Y = 4605885
26 meter E =
0014644
Z = -1628925
64 I = 51
36594
XDOT = -2443
498791 Wp = 129
16053
YDOT = -4502
556161 meter/sec RA = 304
29025 deg
ZDOT = -5699
598840 TA = 68
72280
MA = 68
56649
Ha = 226
846 n
mi
Hp = 215
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15474416
91 X = -4759843
02
Y = 15111172
12 feet Y = 4552899
50 meter
Z = -5344244
21 Z = -1651942
90
XDOT = -8016
728317 XDOT = -2365
281768
YDOT = -14772
165884 feet/sec YDOT = -4529
443204 meter/sec
ZDOT = -18699
471261 ZDOT = -5711
279339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18888764
97 X = -5757295
56
Y = -10485766
40 feet Y = -3196061
60 meter
Z = -5443281
06 Z = -1659112
07
XDOT = 11140
690794 XDOT = 3395
682554
YDOT = -10408
886843 feet/sec YDOT = -3172
628710 meter/sec
ZDOT = -18748
385200 ZDOT = -5714
507809
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 14344
60734324
00016717 00000-0 10270-3 0 9024
2 25544 51
6463 304
7977 0007239 115
9710 244
2188 15
52003003 38705
Satellite: ISS
Catalog Number: 25544
Epoch time: 14344
60734324 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 304
7977 deg
Eccentricity:
0007239
Arg of perigee: 115
9710 deg
Mean anomaly: 244
2188 deg
Mean motion: 15
52003003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3870
Checksum: 293
Coasting Arc #4 (Orbit 3885)
---------------------------------------
Vector Time (GMT): 2014/345/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4684561
87 A = 6792651
04 meter
Y = -4206754
82 meter E =
0019555
Z = 2532548
18 I = 51
34331
XDOT = 1866
003198 Wp = 90
74548
YDOT = 5262
690266 meter/sec RA = 299
30709 deg
ZDOT = 5254
595421 TA = 297
80156
MA = 297
99964
Ha = 226
774 n
mi
Hp = 215
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15369297
46 X = 4718952
33
Y = -13801689
03 feet Y = -4154176
86 meter
Z = 8308885
10 Z = 2555388
37
XDOT = 6122
057737 XDOT = 1781
490795
YDOT = 17266
044180 feet/sec YDOT = 5283
084286 meter/sec
ZDOT = 17239
486289 ZDOT = 5263
455214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17780289
55 X = 5419432
26
Y = 10436559
36 feet Y = 3181063
29 meter
Z = 8407082
04 Z = 2562478
60
XDOT = -13886
295004 XDOT = -4232
542717
YDOT = 9647
977418 feet/sec YDOT = 2940
703517 meter/sec
ZDOT = 17276
234608 ZDOT = 5265
796309
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 14345
63757303
00016717 00000-0 10270-3 0 9031
2 25544 51
6460 299
6788 0007244 119
7451 240
4422 15
52034579 38862
Satellite: ISS
Catalog Number: 25544
Epoch time: 14345
63757303 = yrday
fracday
Element set: 903
Inclination: 51
6460 deg
RA of node: 299
6788 deg
Eccentricity:
0007244
Arg of perigee: 119
7451 deg
Mean anomaly: 240
4422 deg
Mean motion: 15
52034579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3886
Checksum: 327
Coasting Arc #5 (Orbit 3900)
---------------------------------------
Vector Time (GMT): 2014/346/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4630050
32 A = 6790269
88 meter
Y = 3616642
23 meter E =
0011656
Z = -3410064
68 I = 51
32199
XDOT = -1317
855516 Wp = 109
11817
YDOT = -5992
691850 meter/sec RA = 294
31887 deg
ZDOT = -4583
009945 TA = 110
89959
MA = 110
77477
Ha = 226
652 n
mi
Hp = 215
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15190453
79 X = -4653583
36
Y = 11865624
13 feet Y = 3564734
58 meter
Z = -11187876
25 Z = -3432613
78
XDOT = -4323
672954 XDOT = -1228
483132
YDOT = -19661
062500 feet/sec YDOT = -6006
929046 meter/sec
ZDOT = -15036
121868 ZDOT = -4589
195088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16058796
35 X = -4894721
13
Y = -10558496
63 feet Y = -3218229
77 meter
Z = -11284711
18 Z = -3439579
97
XDOT = 16525
110726 XDOT = 5036
853749
YDOT = -9094
155648 feet/sec YDOT = -2771
898642 meter/sec
ZDOT = -15061
335713 ZDOT = -4590
695125
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 14346
60339034
00016717 00000-0 10270-3 0 9047
2 25544 51
6466 294
8790 0007249 123
0725 237
1124 15
52085897 39014
Satellite: ISS
Catalog Number: 25544
Epoch time: 14346
60339034 = yrday
fracday
Element set: 904
Inclination: 51
6466 deg
RA of node: 294
8790 deg
Eccentricity:
0007249
Arg of perigee: 123
0725 deg
Mean anomaly: 237
1124 deg
Mean motion: 15
52085897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3901
Checksum: 315
Coasting Arc #6 (Orbit 3916)
---------------------------------------
Vector Time (GMT): 2014/347/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4522304
79 A = 6787937
70 meter
Y = -2937824
67 meter E =
0017322
Z = 4113361
72 I = 51
30181
XDOT = 867
752925 Wp = 113
33046
YDOT = 6627
606216 meter/sec RA = 289
32620 deg
ZDOT = 3760
126649 TA = 297
66331
MA = 297
83901
Ha = 226
542 n
mi
Hp = 215
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14836957
96 X = 4534838
73
Y = -9638532
37 feet Y = -2887183
39 meter
Z = 13495281
24 Z = 4135360
78
XDOT = 2846
958415 XDOT = 775
311502
YDOT = 21744
114883 feet/sec YDOT = 6636
792984 meter/sec
ZDOT = 12336
373520 ZDOT = 3764
117782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14015899
42 X = 4272046
14
Y = 10678746
19 feet Y = 3254881
84 meter
Z = 13589635
26 Z = 4142120
83
XDOT = -18788
243012 XDOT = -5726
656470
YDOT = 8860
119055 feet/sec YDOT = 2700
564288 meter/sec
ZDOT = 12352
122468 ZDOT = 3764
926928
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 14347
63357203
00016717 00000-0 10270-3 0 9050
2 25544 51
6461 289
7595 0007275 127
3015 232
8800 15
52110765 39176
Satellite: ISS
Catalog Number: 25544
Epoch time: 14347
63357203 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 289
7595 deg
Eccentricity:
0007275
Arg of perigee: 127
3015 deg
Mean anomaly: 232
8800 deg
Mean motion: 15
52110765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3917
Checksum: 310
Coasting Arc #7 (Orbit 3931)
---------------------------------------
Vector Time (GMT): 2014/348/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4429919
23 A = 6785574
45 meter
Y = 2088540
37 meter E =
0015904
Z = -4709889
98 I = 51
28556
XDOT = -451
105538 Wp = 93
91857
YDOT = -7129
942576 meter/sec RA = 284
32776 deg
ZDOT = -2746
514273 TA = 148
74903
MA = 148
65439
Ha = 226
456 n
mi
Hp = 215
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14533855
74 X = -4430065
35
Y = 6852166
58 feet Y = 2039001
47 meter
Z = -15452394
96 Z = -4731410
24
XDOT = -1480
005047 XDOT = -358
001615
YDOT = -23392
200054 feet/sec YDOT = -7134
466470 meter/sec
ZDOT = -9010
873599 ZDOT = -2748
479768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11477250
23 X = -3498265
87
Y = -11117625
37 feet Y = -3388652
21 meter
Z = -15544542
22 Z = -4737976
47
XDOT = 20598
430971 XDOT = 6278
401760
YDOT = -8697
603222 feet/sec YDOT = -2651
029462 meter/sec
ZDOT = -9017
902003 ZDOT = -2748
656531
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 14348
59934455
00016717 00000-0 10270-3 0 9067
2 25544 51
6467 284
9593 0007239 130
4896 229
6888 15
52164105 39323
Satellite: ISS
Catalog Number: 25544
Epoch time: 14348
59934455 = yrday
fracday
Element set: 906
Inclination: 51
6467 deg
RA of node: 284
9593 deg
Eccentricity:
0007239
Arg of perigee: 130
4896 deg
Mean anomaly: 229
6888 deg
Mean motion: 15
52164105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3932
Checksum: 354
Coasting Arc #8 (Orbit 3947)
---------------------------------------
Vector Time (GMT): 2014/349/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4325826
39 A = 6783863
85 meter
Y = -1184838
75 meter E =
0012221
Z = 5083568
23 I = 51
27293
XDOT = 106
539102 Wp = 130
87369
YDOT = 7491
249693 meter/sec RA = 279
32579 deg
ZDOT = 1644
879787 TA = 303
11282
MA = 303
23006
Ha = 226
243 n
mi
Hp = 215
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14192343
79 X = 4314059
57
Y = -3887266
25 feet Y = -1136530
51 meter
Z = 16678373
45 Z = 5104553
96
XDOT = 349
537736 XDOT = 14
771946
YDOT = 24577
590857 feet/sec YDOT = 7491
927932 meter/sec
ZDOT = 5396
587228 ZDOT = 1645
174677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8780223
88 X = 2676212
24
Y = 11680801
13 feet Y = 3560308
18 meter
Z = 16768069
53 Z = 5110907
59
XDOT = -21898
836123 XDOT = -6674
765250
YDOT = 8665
184153 feet/sec YDOT = 2641
148130 meter/sec
ZDOT = 5396
435667 ZDOT = 1644
833591
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 14349
62947797
00016717 00000-0 10270-3 0 9076
2 25544 51
6463 279
8393 0007222 135
3041 224
8694 15
52200465 39487
Satellite: ISS
Catalog Number: 25544
Epoch time: 14349
62947797 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 279
8393 deg
Eccentricity:
0007222
Arg of perigee: 135
3041 deg
Mean anomaly: 224
8694 deg
Mean motion: 15
52200465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3948
Checksum: 337
Coasting Arc #9 (Orbit 3962)
---------------------------------------
Vector Time (GMT): 2014/350/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4266116
56 A = 6782942
06 meter
Y = 173518
02 meter E =
0020020
Z = -5287217
93 I = 51
26659
XDOT = 224
719456 Wp = 102
90362
YDOT = -7635
354132 meter/sec RA = 274
32008 deg
ZDOT = -437
692389 TA = 162
92459
MA = 162
85713
Ha = 226
235 n
mi
Hp = 215
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13996445
42 X = -4242056
03
Y = 569284
83 feet Y = 125946
25 meter
Z = -17346515
53 Z = -5307883
82
XDOT = 737
268555 XDOT = 312
209251
YDOT = -25050
374450 feet/sec YDOT = -7632
351974 meter/sec
ZDOT = -1435
998652 ZDOT = -436
388497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5837716
07 X = -1779335
86
Y = -12612688
19 feet Y = -3844347
36 meter
Z = -17434659
10 Z = -5314084
10
XDOT = 22510
169139 XDOT = 6861
099554
YDOT = -8469
506987 feet/sec YDOT = -2581
505730 meter/sec
ZDOT = -1429
013378 ZDOT = -435
563278
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 14350
59520683
00016717 00000-0 10270-3 0 9086
2 25544 51
6470 275
0386 0007170 138
3451 221
8248 15
52234192 39638
Satellite: ISS
Catalog Number: 25544
Epoch time: 14350
59520683 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 275
0386 deg
Eccentricity:
0007170
Arg of perigee: 138
3451 deg
Mean anomaly: 221
8248 deg
Mean motion: 15
52234192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3963
Checksum: 308
Coasting Arc #10 (Orbit 3978)
---------------------------------------
Vector Time (GMT): 2014/351/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4214891
75 A = 6782895
89 meter
Y = 835092
99 meter E =
0008168
Z = 5241723
03 I = 51
26553
XDOT = -537
532034 Wp = 120
19950
YDOT = 7612
560560 meter/sec RA = 269
31401 deg
ZDOT = -783
698247 TA = 337
30747
MA = 337
34356
Ha = 225
910 n
mi
Hp = 215
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13828385
00 X = 4179777
46
Y = 2739806
41 feet Y = 882030
05 meter
Z = 17197254
03 Z = 5262113
30
XDOT = -1763
556543 XDOT = -618
810528
YDOT = 24975
592390 feet/sec YDOT = 7606
095113 meter/sec
ZDOT = -2571
188473 ZDOT = -786
506568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2952167
04 X = 899820
51
Y = 13675637
62 feet Y = 4168334
35 meter
Z = 17284037
80 Z = 5268174
72
XDOT = -22606
084220 XDOT = -6890
334470
YDOT = 8133
632225 feet/sec YDOT = 2479
131102 meter/sec
ZDOT = -2584
575587 ZDOT = -787
778639
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 14351
62529286
00016717 00000-0 10270-3 0 9090
2 25544 51
6469 269
9183 0007069 143
1717 216
9921 15
52291972 39798
Satellite: ISS
Catalog Number: 25544
Epoch time: 14351
62529286 = yrday
fracday
Element set: 909
Inclination: 51
6469 deg
RA of node: 269
9183 deg
Eccentricity:
0007069
Arg of perigee: 143
1717 deg
Mean anomaly: 216
9921 deg
Mean motion: 15
52291972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3979
Checksum: 352
Coasting Arc #11 (Orbit 3993)
---------------------------------------
Vector Time (GMT): 2014/352/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4213634
02 A = 6784019
42 meter
Y = -1858792
57 meter E =
0018651
Z = -4998234
67 I = 51
27094
XDOT = 872
298222 Wp = 119
40492
YDOT = -7336
282148 meter/sec RA = 264
30808 deg
ZDOT = 1989
572504 TA = 170
08454
MA = 170
04769
Ha = 225
977 n
mi
Hp = 215
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13824258
61 X = -4168255
38
Y = -6098400
82 feet Y = -1905658
09 meter
Z = -16398407
71 Z = -5018594
00
XDOT = 2861
870808 XDOT = 944
604624
YDOT = -24069
167152 feet/sec YDOT = -7326
123391 meter/sec
ZDOT = 6527
468846 ZDOT = 1993
985171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -130422
60 X = -39752
81
Y = -15014668
21 feet Y = -4576470
87 meter
Z = -16484875
57 Z = -5024590
07
XDOT = 21980
501227 XDOT = 6699
656774
YDOT = -7391
695492 feet/sec YDOT = -2252
988786 meter/sec
ZDOT = 6547
638764 ZDOT = 1995
720295
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 14352
59097895
00016717 00000-0 10270-3 0 9105
2 25544 51
6473 265
1175 0007049 146
5063 213
6536 15
52297219 39944
Satellite: ISS
Catalog Number: 25544
Epoch time: 14352
59097895 = yrday
fracday
Element set: 910
Inclination: 51
6473 deg
RA of node: 265
1175 deg
Eccentricity:
0007049
Arg of perigee: 146
5063 deg
Mean anomaly: 213
6536 deg
Mean motion: 15
52297219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3994
Checksum: 333
Coasting Arc #12 (Orbit 4009)
---------------------------------------
Vector Time (GMT): 2014/353/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4208814
76 A = 6785744
03 meter
Y = 2812232
07 meter E =
0011822
Z = 4507818
05 I = 51
28147
XDOT = -1250
596326 Wp = 102
90297
YDOT = 6893
525419 meter/sec RA = 259
30549 deg
ZDOT = -3128
575695 TA = 18
62536
MA = 18
58213
Ha = 225
636 n
mi
Hp = 215
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13808447
37 X = 4155157
22
Y = 9226483
16 feet Y = 2858997
35 meter
Z = 14789429
31 Z = 4528133
96
XDOT = -4103
006319 XDOT = -1312
390663
YDOT = 22616
553211 feet/sec YDOT = 6879
195204 meter/sec
ZDOT = -10264
355955 ZDOT = -3134
800446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2438093
00 X = -743130
75
Y = 16349382
38 feet Y = 4983291
75 meter
Z = 14875544
63 Z = 4534066
00
XDOT = -20963
747526 XDOT = -6389
750246
YDOT = 6251
070461 feet/sec YDOT = 1905
326276 meter/sec
ZDOT = -10292
165934 ZDOT = -3137
052177
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 14353
62101958
00016717 00000-0 10270-3 0 9117
2 25544 51
6473 259
9971 0006930 150
4523 209
7021 15
52362890 40105
Satellite: ISS
Catalog Number: 25544
Epoch time: 14353
62101958 = yrday
fracday
Element set: 911
Inclination: 51
6473 deg
RA of node: 259
9971 deg
Eccentricity:
0006930
Arg of perigee: 150
4523 deg
Mean anomaly: 209
7021 deg
Mean motion: 15
52362890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4010
Checksum: 296
Coasting Arc #13 (Orbit 4024)
---------------------------------------
Vector Time (GMT): 2014/354/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4229538
36 A = 6788176
22 meter
Y = -3683533
54 meter E =
0012000
Z = -3838291
79 I = 51
29592
XDOT = 1681
688269 Wp = 131
22334
YDOT = -6225
638350 meter/sec RA = 254
30640 deg
ZDOT = 4122
202890 TA = 182
41633
MA = 182
42214
Ha = 225
691 n
mi
Hp = 215
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13876438
18 X = -4169388
61
Y = -12085083
78 feet Y = -3730494
26 meter
Z = -12592820
84 Z = -3858692
67
XDOT = 5517
349964 XDOT = 1731
155402
YDOT = -20425
322672 feet/sec YDOT = -6206
556465 meter/sec
ZDOT = 13524
287696 ZDOT = 4130
491833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4679504
27 X = 1426312
90
Y = -17734861
61 feet Y = -5405585
82 meter
Z = -12679150
09 Z = -3864604
95
XDOT = 19413
165258 XDOT = 5917
132771
YDOT = -4571
038481 feet/sec YDOT = -1393
252529 meter/sec
ZDOT = 13560
773821 ZDOT = 4133
323861
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 14354
58666306
00016717 00000-0 10270-3 0 9127
2 25544 51
6470 255
1962 0006929 154
7562 205
3930 15
52358331 40250
Satellite: ISS
Catalog Number: 25544
Epoch time: 14354
58666306 = yrday
fracday
Element set: 912
Inclination: 51
6470 deg
RA of node: 255
1962 deg
Eccentricity:
0006929
Arg of perigee: 154
7562 deg
Mean anomaly: 205
3930 deg
Mean motion: 15
52358331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4025
Checksum: 311
Coasting Arc #14 (Orbit 4040)
---------------------------------------
Vector Time (GMT): 2014/355/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4201920
29 A = 6790568
33 meter
Y = 4423268
71 meter E =
0017613
Z = 2957699
25 I = 51
31357
XDOT = -2202
010031 Wp = 117
29404
YDOT = 5421
151122 meter/sec RA = 249
31291 deg
ZDOT = -4964
183072 TA = 28
72898
MA = 28
63208
Ha = 225
453 n
mi
Hp = 216
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13785827
73 X = 4137778
42
Y = 14512036
46 feet Y = 4469898
34 meter
Z = 9703737
70 Z = 2977956
29
XDOT = -7224
442360 XDOT = -2238
352551
YDOT = 17785
928879 feet/sec YDOT = 5396
324171 meter/sec
ZDOT = -16286
689868 ZDOT = -4974
967792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6561056
60 X = -1999810
05
Y = 18866167
25 feet Y = 5750407
78 meter
Z = 9789333
15 Z = 2983788
74
XDOT = -17690
007161 XDOT = -5391
914183
YDOT = 2348
329130 feet/sec YDOT = 715
770719 meter/sec
ZDOT = -16333
670708 ZDOT = -4978
502832
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 14355
61666002
00016717 00000-0 10270-3 0 9136
2 25544 51
6468 250
0756 0006909 157
8158 202
3294 15
52406907 40416
Satellite: ISS
Catalog Number: 25544
Epoch time: 14355
61666002 = yrday
fracday
Element set: 913
Inclination: 51
6468 deg
RA of node: 250
0756 deg
Eccentricity:
0006909
Arg of perigee: 157
8158 deg
Mean anomaly: 202
3294 deg
Mean motion: 15
52406907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4041
Checksum: 306
Coasting Arc #15 (Orbit 4055)
---------------------------------------
Vector Time (GMT): 2014/356/13:52:47
713
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4151700
06 A = 6792626
93 meter
Y = -5007846
20 meter E =
0006520
Z = -1964199
08 I = 51
33137
XDOT = 2779
838302 Wp = 102
05441
YDOT = -4477
846809 meter/sec RA = 244
32316 deg
ZDOT = 5555
200775 TA = 236
21609
MA = 236
27820
Ha = 225
397 n
mi
Hp = 216
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13621063
18 X = -4085851
19
Y = -16429941
60 feet Y = -5053904
80 meter
Z = -6444222
70 Z = -1984207
96
XDOT = 9120
204403 XDOT = 2802
718795
YDOT = -14691
098456 feet/sec YDOT = -4446
633531 meter/sec
ZDOT = 18225
724327 ZDOT = 5568
759851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7990816
94 X = 2435601
00
Y = -19761772
27 feet Y = -6023388
19 meter
Z = -6528671
43 Z = -1989939
05
XDOT = 15763
530138 XDOT = 4804
723986
YDOT = 348
879512 feet/sec YDOT = 106
338475 meter/sec
ZDOT = 18284
366853 ZDOT = 5573
075017
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 14356
58226114
00016717 00000-0 10270-3 0 9140
2 25544 51
6457 245
2740 0006835 162
7880 197
3505 15
52417234 40567
Satellite: ISS
Catalog Number: 25544
Epoch time: 14356
58226114 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 245
2740 deg
Eccentricity:
0006835
Arg of perigee: 162
7880 deg
Mean anomaly: 197
3505 deg
Mean motion: 15
52417234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4056
Checksum: 311
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