[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 16th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24322 131 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 ET - UTC (sec) : 68 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
352/04:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (Orbit 3303)
---------------------------------------
Vector Time (GMT): 2016/349/13:33:12
318
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2808562
42 A = 6778536
93 meter
Y = -3334082
25 meter E =
0003601
Z = 5189996
00 I = 51
30706
XDOT = 4812
629731 Wp = 3
47206
YDOT = 5856
897557 meter/sec RA = 237
64006 deg
ZDOT = 1161
642109 TA = 75
35760
MA = 75
31768
Ha = 221
625 n
mi
Hp = 215
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9214443
64 X = 2820425
45
Y = -10938590
04 feet Y = -3302609
31 meter
Z = 17027545
95 Z = 5203667
73
XDOT = 15789
467621 XDOT = 4741
135949
YDOT = 19215
543165 feet/sec YDOT = 5910
315730 meter/sec
ZDOT = 3811
161775 ZDOT = 1184
847749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13032275
36 X = 3972237
53
Y = 5714527
83 feet Y = 1741788
08 meter
Z = 17088007
94 Z = 5208424
82
XDOT = -13675
149010 XDOT = -4168
185418
YDOT = 19523
725758 feet/sec YDOT = 5950
831611 meter/sec
ZDOT = 3911
771111 ZDOT = 1192
307835
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 16349
61502299
00016717 00000-0 10270-3 0 9004
2 25544 51
6428 238
3919 0006617 332
0814 27
9983 15
53880306 33041
Satellite: ISS
Catalog Number: 25544
Epoch time: 16349
61502299 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 238
3919 deg
Eccentricity:
0006617
Arg of perigee: 332
0814 deg
Mean anomaly: 27
9983 deg
Mean motion: 15
53880306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3304
Checksum: 319
Coasting Arc #2 (Orbit 3318)
---------------------------------------
Vector Time (GMT): 2016/350/13:33:12
318
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3812221
35 A = 6778123
36 meter
Y = 1950958
37 meter E =
0012743
Z = -5263734
63 I = 51
32210
XDOT = -4189
848895 Wp = 68
26209
YDOT = -6376
670403 meter/sec RA = 232
61986 deg
ZDOT = 676
962794 TA = 208
20353
MA = 208
27261
Ha = 221
764 n
mi
Hp = 215
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12507287
88 X = -3808185
29
Y = 6400782
06 feet Y = 1908350
73 meter
Z = -17269470
56 Z = -5282243
34
XDOT = -13746
223409 XDOT = -4121
520310
YDOT = -20920
834657 feet/sec YDOT = -6423
142138 meter/sec
ZDOT = 2221
006541 ZDOT = 656
774869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9757748
13 X = -2974161
63
Y = -9968454
34 feet Y = -3038384
88 meter
Z = -17350883
09 Z = -5288549
17
XDOT = 15228
875749 XDOT = 4641
761328
YDOT = -18586
980044 feet/sec YDOT = -5665
311517 meter/sec
ZDOT = 2133
681878 ZDOT = 650
346236
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 16350
57970085
00016717 00000-0 10270-3 0 9014
2 25544 51
6408 233
5846 0006670 335
3407 24
7426 15
53911924 33192
Satellite: ISS
Catalog Number: 25544
Epoch time: 16350
57970085 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 233
5846 deg
Eccentricity:
0006670
Arg of perigee: 335
3407 deg
Mean anomaly: 24
7426 deg
Mean motion: 15
53911924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3319
Checksum: 310
Coasting Arc #3 (Orbit 3334)
---------------------------------------
Vector Time (GMT): 2016/351/13:33:12
318
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4738058
49 A = 6779904
36 meter
Y = -529170
48 meter E =
0010417
Z = 4821343
82 I = 51
34911
XDOT = 3249
977531 Wp = 19
89146
YDOT = 6489
756639 meter/sec RA = 227
60365 deg
ZDOT = -2470
350697 TA = 94
53484
MA = 94
41584
Ha = 221
791 n
mi
Hp = 215
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15544811
32 X = 4720203
86
Y = -1736123
63 feet Y = -476286
64 meter
Z = 15818057
15 Z = 4844316
51
XDOT = 10662
655943 XDOT = 3189
165657
YDOT = 21291
852490 feet/sec YDOT = 6525
760297 meter/sec
ZDOT = -8104
825121 ZDOT = -2454
710311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6438202
71 X = 1962364
18
Y = 14142414
91 feet Y = 4310608
06 meter
Z = 15918789
62 Z = 4852047
08
XDOT = -15886
852944 XDOT = -4842
312777
YDOT = 16320
398368 feet/sec YDOT = 4974
457423 meter/sec
ZDOT = -8037
417985 ZDOT = -2449
805002
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 16351
60868482
00016717 00000-0 10270-3 0 9027
2 25544 51
6412 228
4575 0006787 337
6749 22
4107 15
53937163 33354
Satellite: ISS
Catalog Number: 25544
Epoch time: 16351
60868482 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 228
4575 deg
Eccentricity:
0006787
Arg of perigee: 337
6749 deg
Mean anomaly: 22
4107 deg
Mean motion: 15
53937163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3335
Checksum: 325
Coasting Arc #4 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2016/352/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2625470
90 A = 6778082
84 meter
Y = -3339544
30 meter E =
0005353
Z = 5280919
21 I = 51
35374
XDOT = 5694
293403 Wp = 6
17415
YDOT = 5120
858828 meter/sec RA = 224
43361 deg
ZDOT = 412
527894 TA = 79
90690
MA = 79
84651
Ha = 221
929 n
mi
Hp = 215
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8613749
69 X = 2636967
25
Y = -10956510
19 feet Y = -3310120
70 meter
Z = 17325850
44 Z = 5293700
60
XDOT = 18682
064970 XDOT = 5634
603571
YDOT = 16800
717939 feet/sec YDOT = 5184
202462 meter/sec
ZDOT = 1353
437974 ZDOT = 440
044534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11937492
28 X = -3638547
65
Y = 7055120
82 feet Y = 2150400
82 meter
Z = 17382417
58 Z = 5298160
88
XDOT = -10660
407872 XDOT = -3249
292319
YDOT = -21625
449085 feet/sec YDOT = -6591
436881 meter/sec
ZDOT = 1473
125195 ZDOT = 449
008559
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 16352
25179919
00016717 00000-0 10270-3 0 9030
2 25544 51
6382 225
2513 0006530 342
4111 17
6814 15
53898350 33456
Satellite: ISS
Catalog Number: 25544
Epoch time: 16352
25179919 = yrday
fracday
Element set: 903
Inclination: 51
6382 deg
RA of node: 225
2513 deg
Eccentricity:
0006530
Arg of perigee: 342
4111 deg
Mean anomaly: 17
6814 deg
Mean motion: 15
53898350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 300
Coasting Arc #5 (Orbit 3359)
---------------------------------------
Vector Time (GMT): 2016/353/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3859599
16 A = 6778674
75 meter
Y = 2152872
74 meter E =
0012663
Z = -5149613
70 I = 51
37949
XDOT = -5022
436415 Wp = 72
47136
YDOT = -5604
594408 meter/sec RA = 219
41768 deg
ZDOT = 1427
842981 TA = 211
29377
MA = 211
36920
Ha = 222
137 n
mi
Hp = 215
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12662726
89 X = -3858371
95
Y = 7063230
78 feet Y = 2109719
31 meter
Z = -16895058
07 Z = -5168359
34
XDOT = -16477
809759 XDOT = -4966
326894
YDOT = -18387
776929 feet/sec YDOT = -5660
445033 meter/sec
ZDOT = 4684
524215 ZDOT = 1403
581421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14235473
32 X = 4338972
27
Y = -2188747
97 feet Y = -667130
38 meter
Z = -16977560
19 Z = -5174760
35
XDOT = 8815
556544 XDOT = 2686
981635
YDOT = 21984
771579 feet/sec YDOT = 6700
958377 meter/sec
ZDOT = 4579
156885 ZDOT = 1395
727019
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 16353
21646349
00016717 00000-0 10270-3 0 9044
2 25544 51
6382 220
4443 0006635 346
2850 13
8121 15
53895357 33603
Satellite: ISS
Catalog Number: 25544
Epoch time: 16353
21646349 = yrday
fracday
Element set: 904
Inclination: 51
6382 deg
RA of node: 220
4443 deg
Eccentricity:
0006635
Arg of perigee: 346
2850 deg
Mean anomaly: 13
8121 deg
Mean motion: 15
53895357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3360
Checksum: 301
Coasting Arc #6 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2016/354/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4979896
40 A = 6781199
39 meter
Y = -945134
87 meter E =
0012084
Z = 4504008
17 I = 51
41339
XDOT = 3957
781167 Wp = 34
80202
YDOT = 5760
265724 meter/sec RA = 214
40736 deg
ZDOT = -3153
274676 TA = 87
01177
MA = 86
87349
Ha = 222
163 n
mi
Hp = 214
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16338242
79 X = 4968216
71
Y = -3100836
18 feet Y = -889511
84 meter
Z = 14776929
70 Z = 4528170
61
XDOT = 12984
846347 XDOT = 3908
391344
YDOT = 18898
509594 feet/sec YDOT = 5804
248290 meter/sec
ZDOT = -10345
389356 ZDOT = -3134
168637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16339093
86 X = -4980155
81
Y = -2538129
12 feet Y = -773621
76 meter
Z = 14882974
36 Z = 4536330
59
XDOT = -6128
310732 XDOT = -1867
909111
YDOT = -20992
845911 feet/sec YDOT = -6398
619434 meter/sec
ZDOT = -10262
619240 ZDOT = -3128
046344
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 16354
24543592
00016717 00000-0 10270-3 0 9055
2 25544 51
6377 215
3164 0006694 349
2384 10
8624 15
53924370 33760
Satellite: ISS
Catalog Number: 25544
Epoch time: 16354
24543592 = yrday
fracday
Element set: 905
Inclination: 51
6377 deg
RA of node: 215
3164 deg
Eccentricity:
0006694
Arg of perigee: 349
2384 deg
Mean anomaly: 10
8624 deg
Mean motion: 15
53924370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 319
Coasting Arc #7 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2016/355/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5839659
98 A = 6784821
28 meter
Y = -137192
08 meter E =
0007668
Z = -3448796
42 I = 51
45336
XDOT = -2554
119019 Wp = 33
75299
YDOT = -5609
380121 meter/sec RA = 209
40773 deg
ZDOT = 4559
019579 TA = 285
70053
MA = 285
78511
Ha = 222
305 n
mi
Hp = 214
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19158989
44 X = -5820939
21
Y = -450105
24 feet Y = -202390
27 meter
Z = -11314948
89 Z = -3477118
35
XDOT = -8379
655575 XDOT = -2513
349244
YDOT = -18403
478088 feet/sec YDOT = -5637
714215 meter/sec
ZDOT = 14957
413318 ZDOT = 4546
711212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17938904
39 X = 5467778
06
Y = 6530028
24 feet Y = 1990352
61 meter
Z = -11439055
03 Z = -3486623
97
XDOT = 2623
594535 XDOT = 799
671614
YDOT = 18838
300734 feet/sec YDOT = 5741
914064 meter/sec
ZDOT = 14904
393734 ZDOT = 4542
859210
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 16355
21009423
00016717 00000-0 10270-3 0 9064
2 25544 51
6385 210
5093 0006741 353
0359 7
0699 15
53904940 33913
Satellite: ISS
Catalog Number: 25544
Epoch time: 16355
21009423 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 210
5093 deg
Eccentricity:
0006741
Arg of perigee: 353
0359 deg
Mean anomaly: 7
0699 deg
Mean motion: 15
53904940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 301
Coasting Arc #8 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2016/356/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6377867
66 A = 6788078
92 meter
Y = 1125338
53 meter E =
0012759
Z = 2026101
69 I = 51
49394
XDOT = 848
248212 Wp = 81
95416
YDOT = 5227
448894 meter/sec RA = 204
41905 deg
ZDOT = -5541
872556 TA = 75
61647
MA = 75
47488
Ha = 222
475 n
mi
Hp = 214
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20924762
67 X = 6354967
94
Y = 3692055
55 feet Y = 1196532
02 meter
Z = 6647315
25 Z = 2057028
04
XDOT = 2782
966575 XDOT = 816
650382
YDOT = 17150
422882 feet/sec YDOT = 5236
758105 meter/sec
ZDOT = -18181
996574 ZDOT = -5537
828555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18776443
81 X = -5723060
07
Y = -9854139
35 feet Y = -3003541
67 meter
Z = 6782688
45 Z = 2067363
44
XDOT = 1720
300829 XDOT = 524
347693
YDOT = -15851
338394 feet/sec YDOT = -4831
487943 meter/sec
ZDOT = -18165
127358 ZDOT = -5536
730819
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 16356
23905849
00016717 00000-0 10270-3 0 9075
2 25544 51
6393 205
3810 0006837 356
7899 3
3209 15
53936141 34078
Satellite: ISS
Catalog Number: 25544
Epoch time: 16356
23905849 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 205
3810 deg
Eccentricity:
0006837
Arg of perigee: 356
7899 deg
Mean anomaly: 3
3209 deg
Mean motion: 15
53936141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 327
Coasting Arc #9 (Orbit 3421)
---------------------------------------
Vector Time (GMT): 2016/357/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6487959
74 A = 6789783
53 meter
Y = -1918643
44 meter E =
0016806
Z = -440548
11 I = 51
52874
XDOT = 989
164722 Wp = 26
62335
YDOT = -4695
909400 meter/sec RA = 199
44008 deg
ZDOT = 5987
046016 TA = 328
61600
MA = 328
71618
Ha = 222
530 n
mi
Hp = 214
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21285957
16 X = -6463882
79
Y = -6294761
96 feet Y = -1991061
53 meter
Z = -1445367
83 Z = -472006
51
XDOT = 3245
291084 XDOT = 1012
519662
YDOT = -15406
526903 feet/sec YDOT = -4684
717554 meter/sec
ZDOT = 19642
539423 ZDOT = 5991
907652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18574747
73 X = 5661583
11
Y = 12135817
84 feet Y = 3698997
28 meter
Z = -1582959
36 Z = -482486
01
XDOT = -6522
341093 XDOT = -1988
009565
YDOT = 12507
581342 feet/sec YDOT = 3812
310793 meter/sec
ZDOT = 19664
617623 ZDOT = 5993
775451
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 16357
20370978
00016717 00000-0 10270-3 0 9083
2 25544 51
6387 200
5743 0006808
4595 359
6563 15
53939260 34229
Satellite: ISS
Catalog Number: 25544
Epoch time: 16357
20370978 = yrday
fracday
Element set: 908
Inclination: 51
6387 deg
RA of node: 200
5743 deg
Eccentricity:
0006808
Arg of perigee:
4595 deg
Mean anomaly: 359
6563 deg
Mean motion: 15
53939260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3422
Checksum: 326
Coasting Arc #10 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2016/358/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6154379
41 A = 6789252
30 meter
Y = 2592805
74 meter E =
0006079
Z = -1226285
13 I = 51
55886
XDOT = -2864
169863 Wp = 94
20576
YDOT = 4048
473894 meter/sec RA = 194
46453 deg
ZDOT = -5840
004070 TA = 99
12569
MA = 99
05690
Ha = 222
672 n
mi
Hp = 214
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20191533
50 X = 6130885
34
Y = 8506580
52 feet Y = 2661496
85 meter
Z = -4023245
18 Z = -1196445
66
XDOT = -9396
882754 XDOT = -2880
859873
YDOT = 13282
394664 feet/sec YDOT = 4016
351790 meter/sec
ZDOT = -19160
118340 ZDOT = -5853
957815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17163262
90 X = -5231362
53
Y = -13657035
04 feet Y = -4162664
28 meter
Z = -3892844
70 Z = -1186539
07
XDOT = 11522
630643 XDOT = 3512
097820
YDOT = -9026
410113 feet/sec YDOT = -2751
249803 meter/sec
ZDOT = -19221
953623 ZDOT = -5858
851464
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 16358
23266823
00016717 00000-0 10270-3 0 9091
2 25544 51
6398 195
4464 0006878 3
3889 356
7309 15
53947398 34382
Satellite: ISS
Catalog Number: 25544
Epoch time: 16358
23266823 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 195
4464 deg
Eccentricity:
0006878
Arg of perigee: 3
3889 deg
Mean anomaly: 356
7309 deg
Mean motion: 15
53947398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 367
Coasting Arc #11 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2016/359/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5362972
30 A = 6786719
89 meter
Y = -3102704
80 meter E =
0016989
Z = 2744075
98 I = 51
58193
XDOT = 4590
220613 Wp = 56
47486
YDOT = -3370
799519 meter/sec RA = 189
48686 deg
ZDOT = 5145
940593 TA = 334
64645
MA = 334
72972
Ha = 222
810 n
mi
Hp = 214
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17595053
49 X = -5341208
01
Y = -10179477
71 feet Y = -3162555
64 meter
Z = 9002873
94 Z = 2718076
67
XDOT = 15059
778913 XDOT = 4602
575846
YDOT = -11059
053539 feet/sec YDOT = -3319
399816 meter/sec
ZDOT = 16883
007195 ZDOT = 5168
268540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14490991
54 X = 4416854
22
Y = 14326532
33 feet Y = 4366727
06 meter
Z = 8889378
40 Z = 2709482
53
XDOT = -16222
390835 XDOT = -4944
584726
YDOT = 5843
513077 feet/sec YDOT = 1781
102786 meter/sec
ZDOT = 16981
458262 ZDOT = 5175
948478
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 16359
26162196
00016717 00000-0 10270-3 0 9105
2 25544 51
6398 190
3187 0006866 7
3291 352
7961 15
53955518 34547
Satellite: ISS
Catalog Number: 25544
Epoch time: 16359
26162196 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 190
3187 deg
Eccentricity:
0006866
Arg of perigee: 7
3291 deg
Mean anomaly: 352
7961 deg
Mean motion: 15
53955518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 336
Coasting Arc #12 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2016/360/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4179072
38 A = 6783040
85 meter
Y = 3528994
10 meter E =
0012005
Z = -4025030
90 I = 51
60154
XDOT = -6017
548612 Wp = 41
98589
YDOT = 2646
766413 meter/sec RA = 184
50264 deg
ZDOT = -3925
328677 TA = 187
14988
MA = 187
16702
Ha = 222
892 n
mi
Hp = 214
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13710867
38 X = 4158851
52
Y = 11578064
62 feet Y = 3575614
53 meter
Z = -13205481
97 Z = -4004778
87
XDOT = -19742
613557 XDOT = -6027
630649
YDOT = 8683
616841 feet/sec YDOT = 2579
418056 meter/sec
ZDOT = -12878
374926 ZDOT = -3954
584710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10656899
20 X = -3248222
88
Y = -14518698
40 feet Y = -4425299
27 meter
Z = -13117244
95 Z = -3998136
26
XDOT = 20098
194382 XDOT = 6125
929648
YDOT = -2994
988589 feet/sec YDOT = -912
872522 meter/sec
ZDOT = -13007
103609 ZDOT = -3964
565180
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 16360
22626345
00016717 00000-0 10270-3 0 9115
2 25544 51
6395 185
5114 0007052 11
3550 348
7760 15
53966642 34699
Satellite: ISS
Catalog Number: 25544
Epoch time: 16360
22626345 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 185
5114 deg
Eccentricity:
0007052
Arg of perigee: 11
3550 deg
Mean anomaly: 348
7760 deg
Mean motion: 15
53966642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 308
Coasting Arc #13 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2016/361/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2668611
39 A = 6779631
13 meter
Y = -3851648
66 meter E =
0008105
Z = 4892058
78 I = 51
62266
XDOT = 7053
221350 Wp = 67
64365
YDOT = -1913
828213 meter/sec RA = 179
51176 deg
ZDOT = 2340
633246 TA = 359
45897
MA = 359
45985
Ha = 222
900 n
mi
Hp = 213
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8755286
71 X = -2649106
40
Y = -12636642
60 feet Y = -3881382
24 meter
Z = 16050061
61 Z = 4879142
39
XDOT = 23140
489995 XDOT = 7062
728290
YDOT = -6278
963952 feet/sec YDOT = -1834
901396 meter/sec
ZDOT = 7679
242932 ZDOT = 2374
918905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5856216
81 X = 1784974
88
Y = 14277243
57 feet Y = 4351703
84 meter
Z = 15994039
52 Z = 4874983
25
XDOT = -22864
983404 XDOT = -6969
246941
YDOT = 606
965649 feet/sec YDOT = 185
003130 meter/sec
ZDOT = 7829
930929 ZDOT = 2386
562947
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 16361
25521023
00016717 00000-0 10270-3 0 9127
2 25544 51
6394 180
3842 0006852 13
5292 346
6043 15
53989465 34850
Satellite: ISS
Catalog Number: 25544
Epoch time: 16361
25521023 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 180
3842 deg
Eccentricity:
0006852
Arg of perigee: 13
5292 deg
Mean anomaly: 346
6043 deg
Mean motion: 15
53989465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 311
Coasting Arc #14 (Orbit 3499)
---------------------------------------
Vector Time (GMT): 2016/362/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 990682
64 A = 6777923
01 meter
Y = 4120929
80 meter E =
0018546
Z = -5304471
99 I = 51
64988
XDOT = -7552
283949 Wp = 65
45926
YDOT = 1138
498303 meter/sec RA = 174
51467 deg
ZDOT = -519
929516 TA = 199
53688
MA = 199
60805
Ha = 223
035 n
mi
Hp = 213
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3250271
12 X = 970294
45
Y = 13520110
88 feet Y = 4131894
79 meter
Z = -17403123
33 Z = -5299708
64
XDOT = -24777
834479 XDOT = -7561
928045
YDOT = 3735
230653 feet/sec YDOT = 1053
989714 meter/sec
ZDOT = -1705
805498 ZDOT = -556
639796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -540109
96 X = -164625
52
Y = -13920105
77 feet Y = -4242848
24 meter
Z = -17382902
49 Z = -5298308
68
XDOT = 23992
842432 XDOT = 7313
018373
YDOT = 1425
503795 feet/sec YDOT = 434
493557 meter/sec
ZDOT = -1867
026121 ZDOT = -569
069562
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 16362
21984630
00016717 00000-0 10270-3 0 9132
2 25544 51
6402 175
5761 0007041 17
8257 342
3141 15
53972622 35002
Satellite: ISS
Catalog Number: 25544
Epoch time: 16362
21984630 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 175
5761 deg
Eccentricity:
0007041
Arg of perigee: 17
8257 deg
Mean anomaly: 342
3141 deg
Mean motion: 15
53972622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3500
Checksum: 288
Coasting Arc #15 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2016/363/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 773313
23 A = 6778307
56 meter
Y = -4303017
07 meter E =
0010917
Z = 5176453
49 I = 51
68341
XDOT = 7543
155664 Wp = 34
02758
YDOT = -298
604844 meter/sec RA = 169
51906 deg
ZDOT = -1364
857493 TA = 69
13714
MA = 69
02028
Ha = 223
043 n
mi
Hp = 213
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2537116
88 X = 796228
39
Y = -14117510
07 feet Y = -4294241
77 meter
Z = 16983115
12 Z = 5180265
24
XDOT = 24747
886037 XDOT = 7552
563960
YDOT = -979
674685 feet/sec YDOT = -214
199460 meter/sec
ZDOT = -4477
878913 ZDOT = -1328
192164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5020222
28 X = -1530163
75
Y = 13414399
78 feet Y = 4088709
05 meter
Z = 17000544
07 Z = 5181765
83
XDOT = -23545
401375 XDOT = -7176
638339
YDOT = -3298
085762 feet/sec YDOT = -1005
256540 meter/sec
ZDOT = -4316
967365 ZDOT = -1315
811653
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 16363
24878530
00016717 00000-0 10270-3 0 9148
2 25544 51
6399 170
4487 0007113 20
8057 339
3384 15
53996827 35163
Satellite: ISS
Catalog Number: 25544
Epoch time: 16363
24878530 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 170
4487 deg
Eccentricity:
0007113
Arg of perigee: 20
8057 deg
Mean anomaly: 339
3384 deg
Mean motion: 15
53996827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 335
Coasting Arc #16 (Orbit 3530)
---------------------------------------
Vector Time (GMT): 2016/364/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2401276
45 A = 6780856
85 meter
Y = 4406173
46 meter E =
0012796
Z = -4569924
07 I = 51
72410
XDOT = -6980
246356 Wp = 76
98735
YDOT = -603
142247 meter/sec RA = 164
52920 deg
ZDOT = 3096
368316 TA = 223
95349
MA = 224
05534
Ha = 223
166 n
mi
Hp = 213
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7878203
58 X = -2428170
47
Y = 14455949
67 feet Y = 4379170
87 meter
Z = -14993189
21 Z = -4581653
61
XDOT = -22901
070722 XDOT = -6988
023741
YDOT = -1978
813146 feet/sec YDOT = -681
243862 meter/sec
ZDOT = 10158
688701 ZDOT = 3062
441430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10122362
86 X = 3085296
20
Y = -12923255
32 feet Y = -3939008
22 meter
Z = -15045382
59 Z = -4585832
61
XDOT = 21354
696795 XDOT = 6508
911583
YDOT = 5111
285282 feet/sec YDOT = 1557
919754 meter/sec
ZDOT = 10009
915781 ZDOT = 3051
022330
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 16364
21341482
00016717 00000-0 10270-3 0 9158
2 25544 51
6406 165
6410 0007105 24
9458 335
2037 15
53980353 35319
Satellite: ISS
Catalog Number: 25544
Epoch time: 16364
21341482 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 165
6410 deg
Eccentricity:
0007105
Arg of perigee: 24
9458 deg
Mean anomaly: 335
2037 deg
Mean motion: 15
53980353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3531
Checksum: 291
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