[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 9th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14100 72 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 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 1501)
---------------------------------------
Vector Time (GMT): 2015/341/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 779604
69 A = 6781271
19 meter
Y = 5395192
12 meter E =
0002790
Z = 4031046
46 I = 51
31806
XDOT = -5489
201292 Wp = 93
11591
YDOT = 3692
429525 meter/sec RA = 298
08020 deg
ZDOT = -3878
192874 TA = 37
27361
MA = 37
25425
Ha = 219
029 n
mi
Hp = 217
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2557758
17 X = 699634
80
Y = 17700761
54 feet Y = 5403462
87 meter
Z = 13225218
05 Z = 4034639
66
XDOT = -18009
190589 XDOT = -5511
243898
YDOT = 12114
270095 feet/sec YDOT = 3630
922559 meter/sec
ZDOT = -12723
729901 ZDOT = -3904
912118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17174173
86 X = -5234688
19
Y = 4952265
32 feet Y = 1509450
47 meter
Z = 13239648
75 Z = 4035444
94
XDOT = -14166
093358 XDOT = -4317
825256
YDOT = -14781
254069 feet/sec YDOT = -4505
326240 meter/sec
ZDOT = -12839
895676 ZDOT = -3913
600202
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 15341
60477548
00016717 00000-0 10270-3 0 9002
2 25544 51
6425 298
6048 0008104 253
1186 106
9079 15
54523176 15020
Satellite: ISS
Catalog Number: 25544
Epoch time: 15341
60477548 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 298
6048 deg
Eccentricity:
0008104
Arg of perigee: 253
1186 deg
Mean anomaly: 106
9079 deg
Mean motion: 15
54523176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1502
Checksum: 306
Coasting Arc #2 (Orbit 1516)
---------------------------------------
Vector Time (GMT): 2015/342/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 391780
83 A = 6785258
22 meter
Y = -6249313
60 meter E =
0004094
Z = -2608567
37 I = 51
31719
XDOT = 5316
745968 Wp = 287
75523
YDOT = -1842
659833 meter/sec RA = 293
07188 deg
ZDOT = 5207
423839 TA = 42
73066
MA = 42
69884
Ha = 218
838 n
mi
Hp = 217
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1285370
18 X = 474304
69
Y = -20502997
39 feet Y = -6244470
89 meter
Z = -8558291
91 Z = -2606464
06
XDOT = 17443
392284 XDOT = 5311
659808
YDOT = -6045
471892 feet/sec YDOT = -1783
233201 meter/sec
ZDOT = 17084
723880 ZDOT = 5233
239476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20457095
66 X = 6235322
76
Y = -1925941
97 feet Y = -587027
11 meter
Z = -8547948
49 Z = -2605414
70
XDOT = 8573
818995 XDOT = 2613
300030
YDOT = 14665
153233 feet/sec YDOT = 4469
938706 meter/sec
ZDOT = 17196
610975 ZDOT = 5241
527025
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 15342
56905285
00016717 00000-0 10270-3 0 9013
2 25544 51
6424 293
7941 0008132 257
0879 102
9366 15
54538052 15170
Satellite: ISS
Catalog Number: 25544
Epoch time: 15342
56905285 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 293
7941 deg
Eccentricity:
0008132
Arg of perigee: 257
0879 deg
Mean anomaly: 102
9366 deg
Mean motion: 15
54538052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1517
Checksum: 317
Coasting Arc #3 (Orbit 1532)
---------------------------------------
Vector Time (GMT): 2015/343/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1421814
26 A = 6787761
02 meter
Y = 6574617
26 meter E =
0009680
Z = 859261
20 I = 51
31518
XDOT = -4883
818317 Wp = 162
35129
YDOT = -282
923079 meter/sec RA = 288
07348 deg
ZDOT = -5907
987227 TA = 8
30677
MA = 8
29076
Ha = 218
531 n
mi
Hp = 217
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4664744
95 X = -1499401
59
Y = 21570266
61 feet Y = 6558283
72 meter
Z = 2819098
43 Z = 852166
24
XDOT = -16023
025973 XDOT = -4851
592449
YDOT = -928
225326 feet/sec YDOT = -337
356537 meter/sec
ZDOT = -19383
160194 ZDOT = -5931
633938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22057495
03 X = -6723124
48
Y = -826054
95 feet Y = -251781
55 meter
Z = 2787132
84 Z = 849518
09
XDOT = -1933
612362 XDOT = -589
365048
YDOT = -14206
764240 feet/sec YDOT = -4330
221740 meter/sec
ZDOT = -19485
252744 ZDOT = -5939
105037
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 15343
59759878
00016717 00000-0 10270-3 0 9023
2 25544 51
6434 288
6632 0008066 260
2791 99
7451 15
54563175 15336
Satellite: ISS
Catalog Number: 25544
Epoch time: 15343
59759878 = yrday
fracday
Element set: 902
Inclination: 51
6434 deg
RA of node: 288
6632 deg
Eccentricity:
0008066
Arg of perigee: 260
2791 deg
Mean anomaly: 99
7451 deg
Mean motion: 15
54563175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1533
Checksum: 343
Coasting Arc #4 (Orbit 1548)
---------------------------------------
Vector Time (GMT): 2015/344/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2288554
89 A = 6787543
28 meter
Y = -6305761
42 meter E =
0007525
Z = 1001710
91 I = 51
30560
XDOT = 4256
751314 Wp = 25
07671
YDOT = 2480
042860 meter/sec RA = 283
07787 deg
ZDOT = 5877
119780 TA = 345
83085
MA = 345
85195
Ha = 218
173 n
mi
Hp = 217
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7508382
20 X = 2354031
38
Y = -20688193
64 feet Y = -6279803
28 meter
Z = 3286453
11 Z = 1012986
87
XDOT = 13965
719535 XDOT = 4200
153331
YDOT = 8136
623556 feet/sec YDOT = 2527
327682 meter/sec
ZDOT = 19281
889042 ZDOT = 5897
661234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21741666
32 X = 6626859
89
Y = 3368408
34 feet Y = 1026690
86 meter
Z = 3336420
88 Z = 1016941
08
XDOT = -5078
595865 XDOT = -1547
956020
YDOT = 13563
426453 feet/sec YDOT = 4134
132383 meter/sec
ZDOT = 19370
133625 ZDOT = 5904
016729
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 15344
62612666
00016717 00000-0 10270-3 0 9032
2 25544 51
6433 283
5319 0008085 264
7331 95
2900 15
54592383 15491
Satellite: ISS
Catalog Number: 25544
Epoch time: 15344
62612666 = yrday
fracday
Element set: 903
Inclination: 51
6433 deg
RA of node: 283
5319 deg
Eccentricity:
0008085
Arg of perigee: 264
7331 deg
Mean anomaly: 95
2900 deg
Mean motion: 15
54592383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1549
Checksum: 317
Coasting Arc #5 (Orbit 1563)
---------------------------------------
Vector Time (GMT): 2015/345/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2994671
12 A = 6784628
23 meter
Y = 5428776
50 meter E =
0004877
Z = -2747835
27 I = 51
29090
XDOT = -3497
500228 Wp = 235
59902
YDOT = -4519
381736 meter/sec RA = 278
07752 deg
ZDOT = -5113
265368 TA = 335
68312
MA = 335
70613
Ha = 217
311 n
mi
Hp = 216
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9825036
48 X = -3041806
40
Y = 17810946
54 feet Y = 5395024
84 meter
Z = -9015207
57 Z = -2762496
87
XDOT = -11474
738282 XDOT = -3421
864931
YDOT = -14827
367900 feet/sec YDOT = -4558
069688 meter/sec
ZDOT = -16775
805014 ZDOT = -5130
072413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19459194
54 X = -5931162
50
Y = -5825403
08 feet Y = -1775582
86 meter
Z = -9079622
92 Z = -2767469
07
XDOT = 11698
259020 XDOT = 3565
629349
YDOT = -12798
632234 feet/sec YDOT = -3901
023105 meter/sec
ZDOT = -16847
520800 ZDOT = -5135
124340
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 15345
59035516
00016717 00000-0 10270-3 0 9043
2 25544 51
6443 278
7219 0008106 268
1397 91
8828 15
54627716 15648
Satellite: ISS
Catalog Number: 25544
Epoch time: 15345
59035516 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 278
7219 deg
Eccentricity:
0008106
Arg of perigee: 268
1397 deg
Mean anomaly: 91
8828 deg
Mean motion: 15
54627716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 335
Coasting Arc #6 (Orbit 1579)
---------------------------------------
Vector Time (GMT): 2015/346/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3550119
06 A = 6780425
92 meter
Y = -4015457
03 meter E =
0003035
Z = 4152925
44 I = 51
27312
XDOT = 2643
559269 Wp = 141
44902
YDOT = 6171
237325 meter/sec RA = 273
06524 deg
ZDOT = 3703
319070 TA = 270
28125
MA = 270
31603
Ha = 217
216 n
mi
Hp = 216
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11647372
25 X = 3574583
60
Y = -13174071
62 feet Y = -3975620
88 meter
Z = 13625083
46 Z = 4170230
32
XDOT = 8673
094716 XDOT = 2556
365100
YDOT = 20246
841619 feet/sec YDOT = 6200
311447 meter/sec
ZDOT = 12149
996948 ZDOT = 3715
949853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15444283
26 X = 4707417
54
Y = 8284140
98 feet Y = 2525006
17 meter
Z = 13700637
41 Z = 4175954
28
XDOT = -17177
866891 XDOT = -5235
813828
YDOT = 11822
132922 feet/sec YDOT = 3603
386114 meter/sec
ZDOT = 12203
357025 ZDOT = 3719
583221
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 15346
61884961
00016717 00000-0 10270-3 0 9054
2 25544 51
6440 273
5906 0008056 271
9682 88
0549 15
54646522 15806
Satellite: ISS
Catalog Number: 25544
Epoch time: 15346
61884961 = yrday
fracday
Element set: 905
Inclination: 51
6440 deg
RA of node: 273
5906 deg
Eccentricity:
0008056
Arg of perigee: 271
9682 deg
Mean anomaly: 88
0549 deg
Mean motion: 15
54646522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 334
Coasting Arc #7 (Orbit 1594)
---------------------------------------
Vector Time (GMT): 2015/347/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3968907
67 A = 6776796
22 meter
Y = 2200773
44 meter E =
0006149
Z = -5038025
99 I = 51
26117
XDOT = -1707
620596 Wp = 50
25832
YDOT = -7247
682317 meter/sec RA = 268
04076 deg
ZDOT = -1818
396283 TA = 202
02171
MA = 202
04814
Ha = 217
901 n
mi
Hp = 217
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13021350
63 X = -3968749
44
Y = 7220385
29 feet Y = 2156391
86 meter
Z = -16528956
66 Z = -5057305
58
XDOT = -5602
429778 XDOT = -1617
615235
YDOT = -23778
485292 feet/sec YDOT = -7266
274633 meter/sec
ZDOT = -5965
867070 ZDOT = -1826
473656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10137488
35 X = -3089906
45
Y = -10777098
86 feet Y = -3284859
73 meter
Z = -16612688
35 Z = -5063547
41
XDOT = 20931
820443 XDOT = 6380
018871
YDOT = -10429
665861 feet/sec YDOT = -3178
962154 meter/sec
ZDOT = -5999
358982 ZDOT = -1828
604618
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 15347
58304658
00016717 00000-0 10270-3 0 9062
2 25544 51
6444 268
7803 0008086 275
8979 84
1252 15
54699641 15951
Satellite: ISS
Catalog Number: 25544
Epoch time: 15347
58304658 = yrday
fracday
Element set: 906
Inclination: 51
6444 deg
RA of node: 268
7803 deg
Eccentricity:
0008086
Arg of perigee: 275
8979 deg
Mean anomaly: 84
1252 deg
Mean motion: 15
54699641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 357
Coasting Arc #8 (Orbit 1610)
---------------------------------------
Vector Time (GMT): 2015/348/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4247959
78 A = 6775618
26 meter
Y = -169382
82 meter E =
0005979
Z = 5280908
08 I = 51
25915
XDOT = 687
544437 Wp = 288
74635
YDOT = 7628
511855 meter/sec RA = 263
00845 deg
ZDOT = -306
776551 TA = 164
20405
MA = 164
18539
Ha = 218
309 n
mi
Hp = 217
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13936875
90 X = 4223885
56
Y = -555717
91 feet Y = -122014
39 meter
Z = 17325813
93 Z = 5301485
29
XDOT = 2255
723219 XDOT = 603
679648
YDOT = 25027
926033 feet/sec YDOT = 7635
731541 meter/sec
ZDOT = -1006
484748 ZDOT = -303
639645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4120782
66 X = 1256014
55
Y = 13208872
23 feet Y = 4026064
25 meter
Z = 17414764
01 Z = 5308020
07
XDOT = -22621
577061 XDOT = -6895
056688
YDOT = 8375
195390 feet/sec YDOT = 2552
759555 meter/sec
ZDOT = -994
396646 ZDOT = -303
092098
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 15348
61150656
00016717 00000-0 10270-3 0 9075
2 25544 51
6440 263
6489 0008235 279
3095 80
7127 15
54734099 16114
Satellite: ISS
Catalog Number: 25544
Epoch time: 15348
61150656 = yrday
fracday
Element set: 907
Inclination: 51
6440 deg
RA of node: 263
6489 deg
Eccentricity:
0008235
Arg of perigee: 279
3095 deg
Mean anomaly: 80
7127 deg
Mean motion: 15
54734099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1611
Checksum: 323
Coasting Arc #9 (Orbit 1625)
---------------------------------------
Vector Time (GMT): 2015/349/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4366937
24 A = 6777491
07 meter
Y = -1850787
17 meter E =
0003722
Z = -4844892
82 I = 51
27022
XDOT = 419
015073 Wp = 116
47225
YDOT = -7268
991721 meter/sec RA = 257
97722 deg
ZDOT = 2398
936745 TA = 177
17807
MA = 177
17597
Ha = 218
403 n
mi
Hp = 216
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14327221
91 X = -4322382
19
Y = -6072136
39 feet Y = -1899371
68 meter
Z = -15895317
66 Z = -4865998
35
XDOT = 1374
721367 XDOT = 488
614510
YDOT = -23848
398035 feet/sec YDOT = -7263
917038 meter/sec
ZDOT = 7870
527379 ZDOT = 2401
140751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1912811
26 X = 583024
87
Y = -15348767
72 feet Y = -4678304
40 meter
Z = -15986173
21 Z = -4872585
59
XDOT = 22168
022240 XDOT = 6756
813179
YDOT = -5446
754600 feet/sec YDOT = -1660
170802 meter/sec
ZDOT = 7881
433378 ZDOT = 2402
260893
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 15349
57567413
00016717 00000-0 10270-3 0 9085
2 25544 51
6439 258
8380 0008235 283
2273 76
7961 15
54735857 16260
Satellite: ISS
Catalog Number: 25544
Epoch time: 15349
57567413 = yrday
fracday
Element set: 908
Inclination: 51
6439 deg
RA of node: 258
8380 deg
Eccentricity:
0008235
Arg of perigee: 283
2273 deg
Mean anomaly: 76
7961 deg
Mean motion: 15
54735857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1626
Checksum: 349
Coasting Arc #10 (Orbit 1641)
---------------------------------------
Vector Time (GMT): 2015/350/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284740
22 A = 6781338
11 meter
Y = 3659550
80 meter E =
0005271
Z = 3773200
17 I = 51
29063
XDOT = -1609
087184 Wp = 42
35525
YDOT = 6213
905763 meter/sec RA = 252
95598 deg
ZDOT = -4192
250259 TA = 92
16266
MA = 92
10230
Ha = 218
747 n
mi
Hp = 216
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14057546
66 X = 4225171
10
Y = 12006400
27 feet Y = 3707132
32 meter
Z = 12379265
64 Z = 3793869
99
XDOT = -5279
157429 XDOT = -1658
088760
YDOT = 20386
829931 feet/sec YDOT = 6195
638137 meter/sec
ZDOT = -13754
101901 ZDOT = -4200
185516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7395342
90 X = -2254100
52
Y = 16878229
47 feet Y = 5144484
34 meter
Z = 12467909
07 Z = 3800218
69
XDOT = -19781
634883 XDOT = -6029
442312
YDOT = 1536
286957 feet/sec YDOT = 468
260264 meter/sec
ZDOT = -13789
563144 ZDOT = -4203
058846
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 15350
60410268
00016717 00000-0 10270-3 0 9097
2 25544 51
6436 253
7064 0008229 287
6215 72
4039 15
54770617 16427
Satellite: ISS
Catalog Number: 25544
Epoch time: 15350
60410268 = yrday
fracday
Element set: 909
Inclination: 51
6436 deg
RA of node: 253
7064 deg
Eccentricity:
0008229
Arg of perigee: 287
6215 deg
Mean anomaly: 72
4039 deg
Mean motion: 15
54770617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1642
Checksum: 308
Coasting Arc #11 (Orbit 1656)
---------------------------------------
Vector Time (GMT): 2015/351/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3950809
66 A = 6785334
40 meter
Y = -5048915
66 meter E =
0008248
Z = -2205543
46 I = 51
31417
XDOT = 2839
139491 Wp = 333
82467
YDOT = -4599
520878 meter/sec RA = 247
94708 deg
ZDOT = 5442
893141 TA = 1
54535
MA = 1
54280
Ha = 218
851 n
mi
Hp = 216
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12961973
96 X = -3883344
17
Y = -16564683
94 feet Y = -5092718
92 meter
Z = -7236034
97 Z = -2224571
97
XDOT = 9314
762108 XDOT = 2863
922047
YDOT = -15090
291593 feet/sec YDOT = -4567
633399 meter/sec
ZDOT = 17857
260961 ZDOT = 5456
745067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11767086
91 X = 3586608
09
Y = -17399825
40 feet Y = -5303466
78 meter
Z = -7317340
15 Z = -2230325
28
XDOT = 15923
476185 XDOT = 4853
475541
YDOT = 3232
705131 feet/sec YDOT = 985
328524 meter/sec
ZDOT = 17917
983664 ZDOT = 5461
401421
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 15351
56823951
00016717 00000-0 10270-3 0 9102
2 25544 51
6435 248
8945 0008354 290
9588 69
0671 15
54776213 16576
Satellite: ISS
Catalog Number: 25544
Epoch time: 15351
56823951 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 248
8945 deg
Eccentricity:
0008354
Arg of perigee: 290
9588 deg
Mean anomaly: 69
0671 deg
Mean motion: 15
54776213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1657
Checksum: 342
Coasting Arc #12 (Orbit 1672)
---------------------------------------
Vector Time (GMT): 2015/352/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3316980
69 A = 6787433
34 meter
Y = 5908234
61 meter E =
0005489
Z = 333996
99 I = 51
33369
XDOT = -4037
395992 Wp = 158
43193
YDOT = 2605
900623 meter/sec RA = 242
94999 deg
ZDOT = -5974
642117 TA = 17
95283
MA = 17
93346
Ha = 219
070 n
mi
Hp = 216
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10882482
57 X = 3249044
41
Y = 19383971
82 feet Y = 5944947
42 meter
Z = 1095790
63 Z = 349945
38
XDOT = -13246
049842 XDOT = -4037
213236
YDOT = 8549
542726 feet/sec YDOT = 2560
753008 meter/sec
ZDOT = -19601
844216 ZDOT = -5994
254432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14794922
24 X = -4509492
30
Y = 16586855
27 feet Y = 5055673
49 meter
Z = 1163639
04 Z = 354677
18
XDOT = -11139
608353 XDOT = -3395
352626
YDOT = -8549
317781 feet/sec YDOT = -2605
832060 meter/sec
ZDOT = -19687
094030 ZDOT = -6000
626260
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 15352
59663809
00016717 00000-0 10270-3 0 9111
2 25544 51
6433 243
7629 0008241 293
5302 66
4984 15
54761801 16738
Satellite: ISS
Catalog Number: 25544
Epoch time: 15352
59663809 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 243
7629 deg
Eccentricity:
0008241
Arg of perigee: 293
5302 deg
Mean anomaly: 66
4984 deg
Mean motion: 15
54761801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 323
Coasting Arc #13 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2015/353/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2356520
58 A = 6786227
28 meter
Y = -6154771
99 meter E =
0011436
Z = 1585638
62 I = 51
34525
XDOT = 5095
649007 Wp = 25
54033
YDOT = -476
954100 meter/sec RA = 237
95401 deg
ZDOT = 5716
356960 TA = 351
88982
MA = 351
90829
Ha = 219
198 n
mi
Hp = 216
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7731366
72 X = -2295223
71
Y = -20192821
50 feet Y = -6180781
49 meter
Z = 5202226
46 Z = 1574339
77
XDOT = 16718
008552 XDOT = 5072
835757
YDOT = -1564
810038 feet/sec YDOT = -420
098934 meter/sec
ZDOT = 18754
451968 ZDOT = 5741
055231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16328982
61 X = 4977073
90
Y = -14190933
97 feet Y = -4325396
68 meter
Z = 5154507
88 Z = 1571094
00
XDOT = 6100
002527 XDOT = 1859
280770
YDOT = 13876
308234 feet/sec YDOT = 4229
498750 meter/sec
ZDOT = 18861
300060 ZDOT = 5748
924258
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 15353
62501815
00016717 00000-0 10270-3 0 9125
2 25544 51
6429 238
6296 0008458 298
1131 61
9167 15
54836527 16895
Satellite: ISS
Catalog Number: 25544
Epoch time: 15353
62501815 = yrday
fracday
Element set: 912
Inclination: 51
6429 deg
RA of node: 238
6296 deg
Eccentricity:
0008458
Arg of perigee: 298
1131 deg
Mean anomaly: 61
9167 deg
Mean motion: 15
54836527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 334
Coasting Arc #14 (Orbit 1703)
---------------------------------------
Vector Time (GMT): 2015/354/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1088696
67 A = 6782684
49 meter
Y = 5825046
67 meter E =
0004762
Z = -3301817
27 I = 51
35037
XDOT = -5866
556775 Wp = 326
68309
YDOT = -1560
171440 meter/sec RA = 232
95289 deg
ZDOT = -4679
676446 TA = 251
86919
MA = 251
92106
Ha = 219
406 n
mi
Hp = 216
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3571839
48 X = 1039517
71
Y = 19111045
50 feet Y = 5836946
36 meter
Z = -10832733
82 Z = -3296647
76
XDOT = -19247
233513 XDOT = -5825
942345
YDOT = -5118
672703 feet/sec YDOT = -1625
547855 meter/sec
ZDOT = -15353
269179 ZDOT = -4708
076562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16545668
00 X = -5043119
60
Y = 10231901
83 feet Y = 3118683
68 meter
Z = -10811441
85 Z = -3295327
47
XDOT = -1317
158108 XDOT = -401
469791
YDOT = -18507
005510 feet/sec YDOT = -5640
935279 meter/sec
ZDOT = -15475
758732 ZDOT = -4717
011261
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 15354
58911290
00016717 00000-0 10270-3 0 9134
2 25544 51
6422 233
8185 0008513 301
3178 58
7141 15
54830461 17047
Satellite: ISS
Catalog Number: 25544
Epoch time: 15354
58911290 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 233
8185 deg
Eccentricity:
0008513
Arg of perigee: 301
3178 deg
Mean anomaly: 58
7141 deg
Mean motion: 15
54830461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1704
Checksum: 295
Coasting Arc #15 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2015/355/13:31:53
160
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 435262
51 A = 6778373
42 meter
Y = -4979691
05 meter E =
0001834
Z = 4576518
20 I = 51
35580
XDOT = 6229
178040 Wp = 33
11890
YDOT = 3310
351240 meter/sec RA = 227
93872 deg
ZDOT = 3010
472735 TA = 26
71656
MA = 26
70711
Ha = 219
576 n
mi
Hp = 215
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1428026
60 X = 468683
18
Y = -16337569
06 feet Y = -4974637
08 meter
Z = 15014823
48 Z = 4578713
49
XDOT = 20436
935828 XDOT = 6177
074100
YDOT = 10860
732415 feet/sec YDOT = 3379
718506 meter/sec
ZDOT = 9876
879052 ZDOT = 3040
606660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15651405
29 X = 4770548
33
Y = -4865884
85 feet Y = -1483121
70 meter
Z = 15025212
95 Z = 4579684
91
XDOT = -2821
383887 XDOT = -859
957809
YDOT = 21814
321621 feet/sec YDOT = 6649
005230 meter/sec
ZDOT = 10006
561502 ZDOT = 3049
999946
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 15355
61746670
00016717 00000-0 10270-3 0 9148
2 25544 51
6420 228
6853 0008476 306
4003 53
6368 15
54833283 17208
Satellite: ISS
Catalog Number: 25544
Epoch time: 15355
61746670 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 228
6853 deg
Eccentricity:
0008476
Arg of perigee: 306
4003 deg
Mean anomaly: 53
6368 deg
Mean motion: 15
54833283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 310
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