[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 19th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23680 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 3 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 3511)
---------------------------------------
Vector Time (GMT): 2014/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3182380
44 A = 6786184
87 meter
Y = 2770981
60 meter E =
0007386
Z = 5308924
12 I = 51
93911
XDOT = -4378
054487 Wp = 59
06118
YDOT = -6263
301001 meter/sec RA = 58
85207 deg
ZDOT = 647
769351 TA = 24
79826
MA = 24
76277
Ha = 227
693 n
mi
Hp = 217
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10440880
72 X = -3238919
22
Y = 9091146
97 feet Y = 2735078
20 meter
Z = 17417730
06 Z = 5293326
85
XDOT = -14363
695823 XDOT = -4310
838123
YDOT = -20548
887798 feet/sec YDOT = -6311
883395 meter/sec
ZDOT = 2125
227528 ZDOT = 626
664446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1550738
95 X = -472665
23
Y = -13841499
28 feet Y = -4218888
98 meter
Z = 17350687
89 Z = 5288489
67
XDOT = 24067
936289 XDOT = 7335
906981
YDOT = -156
318104 feet/sec YDOT = -47
645758 meter/sec
ZDOT = 2036
387530 ZDOT = 620
690919
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 14321
54941222
00016717 00000-0 10270-3 0 9007
2 25544 51
6466 59
2887 0006214 36
6715 323
4861 15
51139101 35125
Satellite: ISS
Catalog Number: 25544
Epoch time: 14321
54941222 = yrday
fracday
Element set: 900
Inclination: 51
6466 deg
RA of node: 59
2887 deg
Eccentricity:
0006214
Arg of perigee: 36
6715 deg
Mean anomaly: 323
4861 deg
Mean motion: 15
51139101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3512
Checksum: 286
Coasting Arc #2 (Orbit 3526)
---------------------------------------
Vector Time (GMT): 2014/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3489759
76 A = 6786072
66 meter
Y = -2328551
48 meter E =
0019421
Z = -5350040
85 I = 51
92182
XDOT = 4405
435052 Wp = 76
24596
YDOT = 6251
853719 meter/sec RA = 53
90458 deg
ZDOT = 157
516456 TA = 195
22371
MA = 195
28223
Ha = 227
661 n
mi
Hp = 217
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11449343
03 X = 3541528
14
Y = -7639604
59 feet Y = -2289237
42 meter
Z = -17552627
47 Z = -5332961
91
XDOT = 14453
527073 XDOT = 4334
432762
YDOT = 20511
331099 feet/sec YDOT = 6300
721158 meter/sec
ZDOT = 516
786274 ZDOT = 178
745267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21215
78 X = 6466
57
Y = 13857046
43 feet Y = 4223627
75 meter
Z = -17479346
65 Z = -5327704
86
XDOT = -24067
541330 XDOT = -7335
786598
YDOT = 780
799008 feet/sec YDOT = 237
987538 meter/sec
ZDOT = 606
142972 ZDOT = 184
752378
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 14322
51581400
00016717 00000-0 10270-3 0 9014
2 25544 51
6467 54
4940 0006358 39
6826 320
4789 15
51144436 35277
Satellite: ISS
Catalog Number: 25544
Epoch time: 14322
51581400 = yrday
fracday
Element set: 901
Inclination: 51
6467 deg
RA of node: 54
4940 deg
Eccentricity:
0006358
Arg of perigee: 39
6826 deg
Mean anomaly: 320
4789 deg
Mean motion: 15
51144436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3527
Checksum: 305
Coasting Arc #3 (Orbit 3542)
---------------------------------------
Vector Time (GMT): 2014/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3845706
07 A = 6786157
80 meter
Y = 1868372
33 meter E =
0009969
Z = 5264464
08 I = 51
90411
XDOT = -4383
211484 Wp = 47
88576
YDOT = -6214
509967 meter/sec RA = 48
95392 deg
ZDOT = -988
690295 TA = 51
58775
MA = 51
49828
Ha = 227
724 n
mi
Hp = 217
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12617145
90 X = -3891886
52
Y = 6129830
48 feet Y = 1825109
02 meter
Z = 17271863
78 Z = 5245669
52
XDOT = -14380
615104 XDOT = -4308
590756
YDOT = -20388
812228 feet/sec YDOT = -6263
108667 meter/sec
ZDOT = -3243
734564 ZDOT = -1009
802487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1639945
42 X = 499855
36
Y = -14030412
42 feet Y = -4276469
71 meter
Z = 17191351
81 Z = 5239924
03
XDOT = 23886
205732 XDOT = 7280
515507
YDOT = -1322
598478 feet/sec YDOT = -403
128016 meter/sec
ZDOT = -3332
586149 ZDOT = -1015
772258
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 14323
54661261
00016717 00000-0 10270-3 0 9023
2 25544 51
6471 49
3779 0006403 42
9703 317
1948 15
51223440 35438
Satellite: ISS
Catalog Number: 25544
Epoch time: 14323
54661261 = yrday
fracday
Element set: 902
Inclination: 51
6471 deg
RA of node: 49
3779 deg
Eccentricity:
0006403
Arg of perigee: 42
9703 deg
Mean anomaly: 317
1948 deg
Mean motion: 15
51223440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3543
Checksum: 295
Coasting Arc #4 (Orbit 3557)
---------------------------------------
Vector Time (GMT): 2014/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4238318
19 A = 6786873
06 meter
Y = -1475582
93 meter E =
0017613
Z = -5105994
94 I = 51
88498
XDOT = 4274
164739 Wp = 85
03448
YDOT = 6086
632026 meter/sec RA = 44
00407 deg
ZDOT = 1795
680038 TA = 202
28270
MA = 202
35933
Ha = 227
699 n
mi
Hp = 217
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13905243
42 X = 4279307
43
Y = -4841151
35 feet Y = -1427958
11 meter
Z = -16751951
91 Z = -5085305
70
XDOT = 14022
850193 XDOT = 4197
061871
YDOT = 19969
265177 feet/sec YDOT = 6133
997393 meter/sec
ZDOT = 5891
338706 ZDOT = 1816
256607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3167786
54 X = -965541
34
Y = 14481558
37 feet Y = 4413978
99 meter
Z = -16663433
89 Z = -5079014
65
XDOT = -23275
916736 XDOT = -7094
499421
YDOT = 1761
202351 feet/sec YDOT = 536
814477 meter/sec
ZDOT = 5977
915681 ZDOT = 1822
068700
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 14324
51296246
00016717 00000-0 10270-3 0 9039
2 25544 51
6467 44
5831 0006587 46
7187 313
4513 15
51240645 35589
Satellite: ISS
Catalog Number: 25544
Epoch time: 14324
51296246 = yrday
fracday
Element set: 903
Inclination: 51
6467 deg
RA of node: 44
5831 deg
Eccentricity:
0006587
Arg of perigee: 46
7187 deg
Mean anomaly: 313
4513 deg
Mean motion: 15
51240645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3558
Checksum: 312
Coasting Arc #5 (Orbit 3573)
---------------------------------------
Vector Time (GMT): 2014/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4661762
13 A = 6787889
16 meter
Y = 1078432
68 meter E =
0014004
Z = 4807946
45 I = 51
86622
XDOT = -4079
362950 Wp = 55
38929
YDOT = -5946
350579 meter/sec RA = 39
05159 deg
ZDOT = -2608
400007 TA = 60
30330
MA = 60
16398
Ha = 227
738 n
mi
Hp = 217
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15294495
18 X = -4696831
01
Y = 3538164
95 feet Y = 1026105
62 meter
Z = 15774102
54 Z = 4785214
53
XDOT = -13383
736714 XDOT = -3999
895185
YDOT = -19509
024210 feet/sec YDOT = -5991
524262 meter/sec
ZDOT = -8557
742806 ZDOT = -2628
024622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4742196
65 X = 1445421
54
Y = -15066762
43 feet Y = -4592349
19 meter
Z = 15676949
51 Z = 4778334
21
XDOT = 22474
524583 XDOT = 6850
235093
YDOT = -1961
612761 feet/sec YDOT = -597
899569 meter/sec
ZDOT = -8640
273407 ZDOT = -2633
555334
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 14325
54370630
00016717 00000-0 10270-3 0 9044
2 25544 51
6471 39
4667 0006588 49
2423 310
9299 15
51303331 35749
Satellite: ISS
Catalog Number: 25544
Epoch time: 14325
54370630 = yrday
fracday
Element set: 904
Inclination: 51
6471 deg
RA of node: 39
4667 deg
Eccentricity:
0006588
Arg of perigee: 49
2423 deg
Mean anomaly: 310
9299 deg
Mean motion: 15
51303331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3574
Checksum: 307
Coasting Arc #6 (Orbit 3588)
---------------------------------------
Vector Time (GMT): 2014/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5085227
70 A = 6789263
52 meter
Y = -772371
09 meter E =
0013930
Z = -4442938
56 I = 51
84524
XDOT = 3790
230364 Wp = 86
14526
YDOT = 5744
199326 meter/sec RA = 34
10037 deg
ZDOT = 3349
543597 TA = 217
62258
MA = 217
72010
Ha = 227
725 n
mi
Hp = 217
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16683817
91 X = 5115069
48
Y = -2534025
88 feet Y = -715337
72 meter
Z = -14576570
07 Z = -4418162
18
XDOT = 12435
138989 XDOT = 3709
444284
YDOT = 18845
798314 feet/sec YDOT = 5786
132284 meter/sec
ZDOT = 10989
316264 ZDOT = 3367
760490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6035972
82 X = -1839764
51
Y = 15855966
36 feet Y = 4832898
55 meter
Z = -14470757
58 Z = -4410686
91
XDOT = -21334
566382 XDOT = -6502
775833
YDOT = 1947
531491 feet/sec YDOT = 593
607598 meter/sec
ZDOT = 11065
871300 ZDOT = 3372
877572
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 14326
51000516
00016717 00000-0 10270-3 0 9056
2 25544 51
6461 34
6714 0006783 53
8634 306
3144 15
51332887 35892
Satellite: ISS
Catalog Number: 25544
Epoch time: 14326
51000516 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 34
6714 deg
Eccentricity:
0006783
Arg of perigee: 53
8634 deg
Mean anomaly: 306
3144 deg
Mean motion: 15
51332887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3589
Checksum: 302
Coasting Arc #7 (Orbit 3604)
---------------------------------------
Vector Time (GMT): 2014/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5509646
19 A = 6790899
87 meter
Y = 467410
89 meter E =
0017559
Z = 3932445
43 I = 51
82507
XDOT = -3387
201334 Wp = 71
02631
YDOT = -5549
006200 meter/sec RA = 29
14745 deg
ZDOT = -4065
769301 TA = 61
47702
MA = 61
30034
Ha = 227
730 n
mi
Hp = 216
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18076267
04 X = -5533566
36
Y = 1533500
28 feet Y = 405664
47 meter
Z = 12901723
86 Z = 3905621
70
XDOT = -11112
865268 XDOT = -3305
148684
YDOT = -18205
400917 feet/sec YDOT = -5586
425053 meter/sec
ZDOT = -13339
138126 ZDOT = -4082
025231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7300457
99 X = 2225179
60
Y = -16695728
34 feet Y = -5088858
00 meter
Z = 12787239
73 Z = 3897550
67
XDOT = 20044
240040 XDOT = 6109
484364
YDOT = -1555
742189 feet/sec YDOT = -474
190219 meter/sec
ZDOT = -13407
359909 ZDOT = -4086
563300
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 14327
54069504
00016717 00000-0 10270-3 0 9063
2 25544 51
6465 29
5545 0006788 55
6722 304
5071 15
51382549 36052
Satellite: ISS
Catalog Number: 25544
Epoch time: 14327
54069504 = yrday
fracday
Element set: 906
Inclination: 51
6465 deg
RA of node: 29
5545 deg
Eccentricity:
0006788
Arg of perigee: 55
6722 deg
Mean anomaly: 304
5071 deg
Mean motion: 15
51382549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3605
Checksum: 319
Coasting Arc #8 (Orbit 3619)
---------------------------------------
Vector Time (GMT): 2014/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5892405
16 A = 6792539
92 meter
Y = -263028
37 meter E =
0011380
Z = -3374057
38 I = 51
80204
XDOT = 2901
788184 Wp = 70
50708
YDOT = 5331
163117 meter/sec RA = 24
19543 deg
ZDOT = 4668
574719 TA = 250
30784
MA = 250
43065
Ha = 227
742 n
mi
Hp = 216
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19332037
93 X = 5911298
83
Y = -862953
96 feet Y = -197029
81 meter
Z = -11069742
07 Z = -3345386
54
XDOT = 9520
302441 XDOT = 2819
279381
YDOT = 17490
692642 feet/sec YDOT = 5363
151148 meter/sec
ZDOT = 15316
846190 ZDOT = 4682
471387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8181115
58 X = -2493604
03
Y = 17613486
32 feet Y = 5368590
63 meter
Z = -10947420
57 Z = -3336773
79
XDOT = -18582
351708 XDOT = -5663
900801
YDOT = 890
928187 feet/sec YDOT = 271
554911 meter/sec
ZDOT = 15375
043712 ZDOT = 4686
313324
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 14328
50694377
00016717 00000-0 10270-3 0 9073
2 25544 51
6455 24
7582 0006940 60
5655 299
6188 15
51409035 36209
Satellite: ISS
Catalog Number: 25544
Epoch time: 14328
50694377 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 24
7582 deg
Eccentricity:
0006940
Arg of perigee: 60
5655 deg
Mean anomaly: 299
6188 deg
Mean motion: 15
51409035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3620
Checksum: 326
Coasting Arc #9 (Orbit 3635)
---------------------------------------
Vector Time (GMT): 2014/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6238242
73 A = 6794165
26 meter
Y = 53599
23 meter E =
0019462
Z = 2674943
73 I = 51
77937
XDOT = -2290
497174 Wp = 88
70289
YDOT = -5141
487673 meter/sec RA = 19
24259 deg
ZDOT = -5205
506594 TA = 61
19047
MA = 60
99520
Ha = 227
713 n
mi
Hp = 216
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20466675
63 X = -6251372
63
Y = 175850
49 feet Y = -16234
44 meter
Z = 8776062
09 Z = 2644606
94
XDOT = -7514
754508 XDOT = -2207
546625
YDOT = -16868
397876 feet/sec YDOT = -5166
637348 meter/sec
ZDOT = -17078
433707 ZDOT = -5216
432507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8991566
49 X = 2740629
47
Y = -18447810
23 feet Y = -5622892
56 meter
Z = 8646677
41 Z = 2635507
27
XDOT = 17057
507334 XDOT = 5199
128235
YDOT = 236
001330 feet/sec YDOT = 71
933206 meter/sec
ZDOT = -17123
996221 ZDOT = -5219
394048
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 14329
53758062
00016717 00000-0 10270-3 0 9080
2 25544 51
6459 19
6407 0007025 62
4636 297
7228 15
51460269 36364
Satellite: ISS
Catalog Number: 25544
Epoch time: 14329
53758062 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 19
6407 deg
Eccentricity:
0007025
Arg of perigee: 62
4636 deg
Mean anomaly: 297
7228 deg
Mean motion: 15
51460269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3636
Checksum: 328
Coasting Arc #10 (Orbit 3650)
---------------------------------------
Vector Time (GMT): 2014/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6503966
48 A = 6795517
75 meter
Y = 62921
78 meter E =
0013721
Z = -1959314
61 I = 51
75375
XDOT = 1628
215346 Wp = 52
67729
YDOT = 4969
365194 meter/sec RA = 14
28994 deg
ZDOT = 5599
527973 TA = 285
77579
MA = 285
92706
Ha = 227
766 n
mi
Hp = 216
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21338472
72 X = 6512297
29
Y = 206436
28 feet Y = 135700
04 meter
Z = -6428197
53 Z = -1927698
73
XDOT = 5341
913864 XDOT = 1545
324788
YDOT = 16303
691583 feet/sec YDOT = 4987
109160 meter/sec
ZDOT = 18371
154766 ZDOT = 5607
236636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9386999
69 X = -2861157
51
Y = 19208652
68 feet Y = 5854797
34 meter
Z = -6293381
95 Z = -1918222
82
XDOT = -15566
349032 XDOT = -4744
623185
YDOT = -1616
119284 feet/sec YDOT = -492
593158 meter/sec
ZDOT = 18403
029624 ZDOT = 5609
243429
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 14330
50377987
00016717 00000-0 10270-3 0 9093
2 25544 51
6455 14
8436 0007123 66
5866 293
6033 15
51466274 36516
Satellite: ISS
Catalog Number: 25544
Epoch time: 14330
50377987 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 14
8436 deg
Eccentricity:
0007123
Arg of perigee: 66
5866 deg
Mean anomaly: 293
6033 deg
Mean motion: 15
51466274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3651
Checksum: 323
Coasting Arc #11 (Orbit 3666)
---------------------------------------
Vector Time (GMT): 2014/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6694181
42 A = 6796408
72 meter
Y = -203513
11 meter E =
0018845
Z = 1121930
35 I = 51
72716
XDOT = -851
416624 Wp = 104
73942
YDOT = -4841
884796 meter/sec RA = 9
33639 deg
ZDOT = -5880
505272 TA = 63
11184
MA = 62
91936
Ha = 227
698 n
mi
Hp = 216
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21962537
46 X = -6696858
17
Y = -667693
94 feet Y = -278386
81 meter
Z = 3680873
86 Z = 1089404
24
XDOT = -2793
361626 XDOT = -768
644478
YDOT = -15885
448805 feet/sec YDOT = -4850
942824 meter/sec
ZDOT = -19292
996299 ZDOT = -5884
440524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9726792
17 X = 2964726
25
Y = -19727898
57 feet Y = -6013063
48 meter
Z = 3542207
11 Z = 1079664
73
XDOT = 14125
519966 XDOT = 4305
458486
YDOT = 3449
904772 feet/sec YDOT = 1051
530974 meter/sec
ZDOT = -19308
804361 ZDOT = -5885
323569
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 14331
53436484
00016717 00000-0 10270-3 0 9107
2 25544 51
6459 9
7257 0007260 69
8507 290
3425 15
51528147 36678
Satellite: ISS
Catalog Number: 25544
Epoch time: 14331
53436484 = yrday
fracday
Element set: 910
Inclination: 51
6459 deg
RA of node: 9
7257 deg
Eccentricity:
0007260
Arg of perigee: 69
8507 deg
Mean anomaly: 290
3425 deg
Mean motion: 15
51528147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3667
Checksum: 319
Coasting Arc #12 (Orbit 3681)
---------------------------------------
Vector Time (GMT): 2014/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6777599
47 A = 6796875
12 meter
Y = 274836
18 meter E =
0018311
Z = -308717
98 I = 51
69770
XDOT = 68
573276 Wp = 54
28549
YDOT = 4762
770286 meter/sec RA = 4
38213 deg
ZDOT = 6005
952188 TA = 302
39316
MA = 302
57022
Ha = 227
768 n
mi
Hp = 216
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22236218
74 X = 6775522
12
Y = 901693
50 feet Y = 350616
09 meter
Z = -1012854
28 Z = -275798
21
XDOT = 224
977938 XDOT = -13
865380
YDOT = 15625
886765 feet/sec YDOT = 4763
076013 meter/sec
ZDOT = 19704
567546 ZDOT = 6006
085200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9703285
14 X = -2957561
31
Y = 20034303
14 feet Y = 6106455
60 meter
Z = -872527
56 Z = -265946
40
XDOT = -12908
423178 XDOT = -3934
487385
YDOT = -5437
030091 feet/sec YDOT = -1657
206772 meter/sec
ZDOT = 19704
177596 ZDOT = 6005
833331
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 14332
50051500
00016717 00000-0 10270-3 0 9118
2 25544 51
6459 4
9286 0007352 72
8097 287
3859 15
51525681 36821
Satellite: ISS
Catalog Number: 25544
Epoch time: 14332
50051500 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 4
9286 deg
Eccentricity:
0007352
Arg of perigee: 72
8097 deg
Mean anomaly: 287
3859 deg
Mean motion: 15
51525681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3682
Checksum: 313
Coasting Arc #13 (Orbit 3697)
---------------------------------------
Vector Time (GMT): 2014/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6755730
30 A = 6796551
81 meter
Y = -399652
42 meter E =
0015601
Z = -591076
60 I = 51
66625
XDOT = 791
152944 Wp = 114
11676
YDOT = -4731
802249 meter/sec RA = 359
42550 deg
ZDOT = -5973
916192 TA = 72
25172
MA = 72
08151
Ha = 227
659 n
mi
Hp = 216
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22164469
49 X = -6747887
91
Y = -1311195
59 feet Y = -475155
52 meter
Z = -1939227
70 Z = -623876
18
XDOT = 2595
646142 XDOT = 873
025833
YDOT = -15524
285595 feet/sec YDOT = -4722
497208 meter/sec
ZDOT = -19599
462572 ZDOT = -5969
874051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9701072
13 X = 2956886
78
Y = -19957716
83 feet Y = -6083112
09 meter
Z = -2079010
33 Z = -633682
35
XDOT = 11842
973679 XDOT = 3609
738377
YDOT = 7754
751853 feet/sec YDOT = 2363
648365 meter/sec
ZDOT = -19581
276179 ZDOT = -5968
372979
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 14333
53104866
00016717 00000-0 10270-3 0 9127
2 25544 51
6462 359
8105 0007396 77
4627 282
7351 15
51587441 36980
Satellite: ISS
Catalog Number: 25544
Epoch time: 14333
53104866 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 359
8105 deg
Eccentricity:
0007396
Arg of perigee: 77
4627 deg
Mean anomaly: 282
7351 deg
Mean motion: 15
51587441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3698
Checksum: 331
Coasting Arc #14 (Orbit 3713)
---------------------------------------
Vector Time (GMT): 2014/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6618366
69 A = 6795768
65 meter
Y = 489265
54 meter E =
0021095
Z = 1421238
97 I = 51
63211
XDOT = -1608
745254 Wp = 67
39417
YDOT = 4762
245697 meter/sec RA = 354
46664 deg
ZDOT = 5791
407334 TA = 308
09696
MA = 308
28700
Ha = 227
674 n
mi
Hp = 215
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21713801
49 X = 6605499
72
Y = 1605201
90 feet Y = 563204
46 meter
Z = 4662857
51 Z = 1453359
14
XDOT = -5278
035611 XDOT = -1690
011312
YDOT = 15624
165674 feet/sec YDOT = 4743
801240 meter/sec
ZDOT = 19000
680231 ZDOT = 5783
394838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9458172
31 X = -2882850
92
Y = 19578400
79 feet Y = 5967496
56 meter
Z = 4799717
43 Z = 1462953
87
XDOT = -11123
205811 XDOT = -3390
353131
YDOT = -10070
451603 feet/sec YDOT = -3069
473649 meter/sec
ZDOT = 18965
559819 ZDOT = 5780
702633
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 14334
56155680
00016717 00000-0 10270-3 0 9132
2 25544 51
6457 354
6934 0007500 80
1483 280
0515 15
51607786 37142
Satellite: ISS
Catalog Number: 25544
Epoch time: 14334
56155680 = yrday
fracday
Element set: 913
Inclination: 51
6457 deg
RA of node: 354
6934 deg
Eccentricity:
0007500
Arg of perigee: 80
1483 deg
Mean anomaly: 280
0515 deg
Mean motion: 15
51607786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3714
Checksum: 308
Coasting Arc #15 (Orbit 3728)
---------------------------------------
Vector Time (GMT): 2014/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6364212
96 A = 6794235
38 meter
Y = -665265
79 meter E =
0011977
Z = -2287841
91 I = 51
59631
XDOT = 2443
813165 Wp = 105
81221
YDOT = -4824
083936 meter/sec RA = 349
50327 deg
ZDOT = -5422
188290 TA = 99
63064
MA = 99
49531
Ha = 227
579 n
mi
Hp = 215
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20879963
76 X = -6345187
04
Y = -2182630
54 feet Y = -736328
14 meter
Z = -7506043
02 Z = -2318712
58
XDOT = 8017
759728 XDOT = 2523
915172
YDOT = -15827
047034 feet/sec YDOT = -4796
307697 meter/sec
ZDOT = -17789
331661 ZDOT = -5410
121916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9361680
63 X = 2853440
26
Y = -18737782
24 feet Y = -5711276
03 meter
Z = -7637532
13 Z = -2327919
79
XDOT = 10597
939264 XDOT = 3230
251888
YDOT = 12489
164053 feet/sec YDOT = 3806
697203 meter/sec
ZDOT = -17736
916034 ZDOT = -5406
212007
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 14335
52763236
00016717 00000-0 10270-3 0 9142
2 25544 51
6456 349
8950 0007440 84
5301 275
6699 15
51654172 37295
Satellite: ISS
Catalog Number: 25544
Epoch time: 14335
52763236 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 349
8950 deg
Eccentricity:
0007440
Arg of perigee: 84
5301 deg
Mean anomaly: 275
6699 deg
Mean motion: 15
51654172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3729
Checksum: 331
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