[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 5th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14800 38 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 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 1455)
---------------------------------------
Vector Time (GMT): 2015/338/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1699682
00 A = 6783857
87 meter
Y = 5683089
82 meter E =
0007071
Z = 3281944
73 I = 51
38176
XDOT = -5988
009932 Wp = 127
73476
YDOT = 926
898888 meter/sec RA = 312
88002 deg
ZDOT = -4703
457387 TA = 13
97714
MA = 13
95758
Ha = 219
758 n
mi
Hp = 216
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5576384
52 X = -1779047
97
Y = 18645307
82 feet Y = 5663639
04 meter
Z = 10767535
19 Z = 3273495
26
XDOT = -19645
701877 XDOT = -5975
081877
YDOT = 3041
006850 feet/sec YDOT = 860
009372 meter/sec
ZDOT = -15431
290641 ZDOT = -4732
514800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19421801
34 X = -5919765
05
Y = 1531982
51 feet Y = 466948
27 meter
Z = 10729866
93 Z = 3270463
44
XDOT = -9836
580259 XDOT = -2998
189663
YDOT = -15681
604742 feet/sec YDOT = -4779
753125 meter/sec
ZDOT = -15557
008574 ZDOT = -4741
776213
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 15338
64755711
00016717 00000-0 10270-3 0 9003
2 25544 51
6425 313
3539 0008078 241
8879 118
1458 15
54448920 14560
Satellite: ISS
Catalog Number: 25544
Epoch time: 15338
64755711 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 313
3539 deg
Eccentricity:
0008078
Arg of perigee: 241
8879 deg
Mean anomaly: 118
1458 deg
Mean motion: 15
54448920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1456
Checksum: 327
Coasting Arc #2 (Orbit 1470)
---------------------------------------
Vector Time (GMT): 2015/339/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2891007
99 A = 6787191
90 meter
Y = -5903449
26 meter E =
0003821
Z = -1680853
90 I = 51
37155
XDOT = 5075
563955 Wp = 317
15680
YDOT = 867
120083 meter/sec RA = 307
88238 deg
ZDOT = 5679
437508 TA = 24
35439
MA = 24
33634
Ha = 219
554 n
mi
Hp = 216
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9484934
36 X = 2964971
99
Y = -19368271
86 feet Y = -5870706
51 meter
Z = -5514612
53 Z = -1666630
26
XDOT = 16652
112713 XDOT = 5037
901504
YDOT = 2844
882161 feet/sec YDOT = 923
667692 meter/sec
ZDOT = 18633
325156 ZDOT = 5704
002413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21533625
51 X = 6563449
06
Y = 1443590
88 feet Y = 440006
50 meter
Z = -5451963
31 Z = -1661758
42
XDOT = 3756
165006 XDOT = 1144
879094
YDOT = 14803
439403 feet/sec YDOT = 4512
088330 meter/sec
ZDOT = 18739
264813 ZDOT = 5711
727915
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 15339
61188310
00016717 00000-0 10270-3 0 9017
2 25544 51
6420 308
5438 0008088 245
6943 114
3365 15
54459887 14710
Satellite: ISS
Catalog Number: 25544
Epoch time: 15339
61188310 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 308
5438 deg
Eccentricity:
0008088
Arg of perigee: 245
6943 deg
Mean anomaly: 114
3365 deg
Mean motion: 15
54459887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1471
Checksum: 321
Coasting Arc #3 (Orbit 1486)
---------------------------------------
Vector Time (GMT): 2015/340/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3768630
64 A = 6788287
26 meter
Y = 5635288
23 meter E =
0011419
Z = -130569
54 I = 51
35756
XDOT = -3919
187604 Wp = 176
21366
YDOT = -2758
815572 meter/sec RA = 302
89055 deg
ZDOT = -5990
115835 TA = 5
19907
MA = 5
18722
Ha = 219
317 n
mi
Hp = 217
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12364273
77 X = -3830731
46
Y = 18488478
43 feet Y = 5592797
69 meter
Z = -428377
75 Z = -149027
73
XDOT = -12858
227047 XDOT = -3858
948460
YDOT = -9051
232192 feet/sec YDOT = -2802
305531 meter/sec
ZDOT = -19652
611006 ZDOT = -6009
008491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21871847
25 X = -6666539
04
Y = -4030578
48 feet Y = -1228520
32 meter
Z = -509257
17 Z = -155221
59
XDOT = 2978
025996 XDOT = 907
702324
YDOT = -13681
234693 feet/sec YDOT = -4170
040334 meter/sec
ZDOT = -19733
662135 ZDOT = -6014
820219
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 15340
64047981
00016717 00000-0 10270-3 0 9021
2 25544 51
6430 303
4130 0008078 248
7936 111
2354 15
54484332 14873
Satellite: ISS
Catalog Number: 25544
Epoch time: 15340
64047981 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 303
4130 deg
Eccentricity:
0008078
Arg of perigee: 248
7936 deg
Mean anomaly: 111
2354 deg
Mean motion: 15
54484332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1487
Checksum: 298
Coasting Arc #4 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2015/341/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4320275
02 A = 6786568
14 meter
Y = -4860664
05 meter E =
0005984
Z = 1929740
18 I = 51
33535
XDOT = 2633
783301 Wp = 60
46571
YDOT = 4558
141322 meter/sec RA = 297
89638 deg
ZDOT = 5574
484746 TA = 320
90100
MA = 320
94423
Ha = 219
081 n
mi
Hp = 217
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14174130
64 X = 4364932
97
Y = -15947060
53 feet Y = -4812102
26 meter
Z = 6331168
58 Z = 1950835
81
XDOT = 8641
021329 XDOT = 2555
538158
YDOT = 14954
531896 feet/sec YDOT = 4587
156305 meter/sec
ZDOT = 18288
991949 ZDOT = 5587
089468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20350891
39 X = 6202951
69
Y = 6315151
09 feet Y = 1924858
05 meter
Z = 6423278
05 Z = 1957815
15
XDOT = -9660
425164 XDOT = -2944
497590
YDOT = 12441
189878 feet/sec YDOT = 3792
074675 meter/sec
ZDOT = 18342
519094 ZDOT = 5590
799820
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
66905736
00016717 00000-0 10270-3 0 9036
2 25544 51
6427 298
2819 0008044 253
1740 106
8531 15
54519348 15032
Satellite: ISS
Catalog Number: 25544
Epoch time: 15341
66905736 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 298
2819 deg
Eccentricity:
0008044
Arg of perigee: 253
1740 deg
Mean anomaly: 106
8531 deg
Mean motion: 15
54519348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 312
Coasting Arc #5 (Orbit 1517)
---------------------------------------
Vector Time (GMT): 2015/342/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4563099
42 A = 6782754
77 meter
Y = 3585882
11 meter E =
0002983
Z = -3507098
38 I = 51
30994
XDOT = -1330
065888 Wp = 242
65894
YDOT = -6077
837606 meter/sec RA = 292
89313 deg
ZDOT = -4482
220666 TA = 338
84148
MA = 338
85382
Ha = 218
618 n
mi
Hp = 217
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14970798
63 X = -4585822
08
Y = 11764705
09 feet Y = 3534727
67 meter
Z = -11506228
29 Z = -3529320
34
XDOT = -4363
733229 XDOT = -1240
229903
YDOT = -19940
412093 feet/sec YDOT = -6092
208722 meter/sec
ZDOT = -14705
448378 ZDOT = -4488
464102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17001008
19 X = -5181907
30
Y = -8441790
80 feet Y = -2573057
84 meter
Z = -11602942
54 Z = -3536576
88
XDOT = 15589
643318 XDOT = 4751
723283
YDOT = -11141
497510 feet/sec YDOT = -3395
928441 meter/sec
ZDOT = -14731
195288 ZDOT = -4490
068324
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
63333139
00016717 00000-0 10270-3 0 9047
2 25544 51
6436 293
4718 0008024 256
8364 103
1894 15
54564311 15185
Satellite: ISS
Catalog Number: 25544
Epoch time: 15342
63333139 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 293
4718 deg
Eccentricity:
0008024
Arg of perigee: 256
8364 deg
Mean anomaly: 103
1894 deg
Mean motion: 15
54564311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1518
Checksum: 306
Coasting Arc #6 (Orbit 1533)
---------------------------------------
Vector Time (GMT): 2015/343/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4540547
29 A = 6778696
84 meter
Y = -1917647
56 meter E =
0005003
Z = 4656613
36 I = 51
28480
XDOT = 92
972141 Wp = 188
03464
YDOT = 7120
952138 meter/sec RA = 287
87647 deg
ZDOT = 2837
337952 TA = 233
62501
MA = 233
67118
Ha = 218
564 n
mi
Hp = 217
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14896808
71 X = 4539033
05
Y = -6291494
61 feet Y = -1866880
97 meter
Z = 15277602
89 Z = 4678666
94
XDOT = 305
026709 XDOT = -
445909
YDOT = 23362
703865 feet/sec YDOT = 7121
469271 meter/sec
ZDOT = 9308
851548 ZDOT = 2837
563224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12192503
29 X = 3716275
00
Y = 10483743
64 feet Y = 3195445
06 meter
Z = 15373254
28 Z = 4685767
90
XDOT = -20075
243980 XDOT = -6118
934365
YDOT = 9676
088617 feet/sec YDOT = 2949
271810 meter/sec
ZDOT = 9308
398839 ZDOT = 2837
199966
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
66187294
00016717 00000-0 10270-3 0 9051
2 25544 51
6435 288
3405 0008032 260
1934 99
8312 15
54583124 15347
Satellite: ISS
Catalog Number: 25544
Epoch time: 15343
66187294 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 288
3405 deg
Eccentricity:
0008032
Arg of perigee: 260
1934 deg
Mean anomaly: 99
8312 deg
Mean motion: 15
54583124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 312
Coasting Arc #7 (Orbit 1548)
---------------------------------------
Vector Time (GMT): 2015/344/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4305915
12 A = 6776121
68 meter
Y = -13083
00 meter E =
0006516
Z = -5237804
96 I = 51
26849
XDOT = 1036
317477 Wp = 82
86321
YDOT = -7548
480052 meter/sec RA = 282
84883 deg
ZDOT = -833
183856 TA = 179
12720
MA = 179
12607
Ha = 217
870 n
mi
Hp = 217
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14127018
11 X = -4280005
22
Y = -42923
22 feet Y = -61089
24 meter
Z = -17184399
47 Z = -5258659
56
XDOT = 3399
991723 XDOT = 1124
696748
YDOT = -24765
354500 feet/sec YDOT = -7536
397033 meter/sec
ZDOT = -2733
542834 ZDOT = -827
935579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6382088
09 X = -1945260
45
Y = -12479545
95 feet Y = -3803765
60 meter
Z = -17274488
50 Z = -5265264
09
XDOT = 22669
237190 XDOT = 6909
583495
YDOT = -7843
209206 feet/sec YDOT = -2390
610166 meter/sec
ZDOT = -2709
367359 ZDOT = -825
815171
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
62611358
00016717 00000-0 10270-3 0 9062
2 25544 51
6443 283
5302 0008017 264
2186 95
8053 15
54627917 15499
Satellite: ISS
Catalog Number: 25544
Epoch time: 15344
62611358 = yrday
fracday
Element set: 906
Inclination: 51
6443 deg
RA of node: 283
5302 deg
Eccentricity:
0008017
Arg of perigee: 264
2186 deg
Mean anomaly: 95
8053 deg
Mean motion: 15
54627917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1549
Checksum: 315
Coasting Arc #8 (Orbit 1564)
---------------------------------------
Vector Time (GMT): 2015/345/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3907512
65 A = 6776321
66 meter
Y = 2003634
36 meter E =
0005153
Z = 5165427
39 I = 51
26329
XDOT = -2036
780456 Wp = 294
30665
YDOT = 7278
253698 meter/sec RA = 277
81735 deg
ZDOT = -1281
341533 TA = 168
07330
MA = 168
06109
Ha = 217
450 n
mi
Hp = 217
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12819923
39 X = 3859725
20
Y = 6573603
53 feet Y = 2047063
04 meter
Z = 16946940
27 Z = 5184293
61
XDOT = -6682
350577 XDOT = -2111
791968
YDOT = 23878
785100 feet/sec YDOT = 7255
057787 meter/sec
ZDOT = -4203
876420 ZDOT = -1291
417375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 225173
57 X = 68632
90
Y = 14309307
57 feet Y = 4361476
95 meter
Z = 17028050
32 Z = 5190149
74
XDOT = -23140
577584 XDOT = -7053
248048
YDOT = 5424
427963 feet/sec YDOT = 1653
365643 meter/sec
ZDOT = -4248
845831 ZDOT = -1295
048209
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
65461825
00016717 00000-0 10270-3 0 9079
2 25544 51
6442 278
3992 0008185 268
2081 91
8134 15
54672719 15653
Satellite: ISS
Catalog Number: 25544
Epoch time: 15345
65461825 = yrday
fracday
Element set: 907
Inclination: 51
6442 deg
RA of node: 278
3992 deg
Eccentricity:
0008185
Arg of perigee: 268
2081 deg
Mean anomaly: 91
8134 deg
Mean motion: 15
54672719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1565
Checksum: 336
Coasting Arc #9 (Orbit 1579)
---------------------------------------
Vector Time (GMT): 2015/346/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3379606
92 A = 6779313
40 meter
Y = -3849753
98 meter E =
0003091
Z = -4442601
45 I = 51
27013
XDOT = 2913
005476 Wp = 168
21822
YDOT = -6305
115895 meter/sec RA = 272
79014 deg
ZDOT = 3245
148214 TA = 134
65691
MA = 134
63172
Ha = 217
222 n
mi
Hp = 216
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11087949
23 X = -3314726
28
Y = -12630426
45 feet Y = -3887183
76 meter
Z = -14575464
07 Z = -4458861
78
XDOT = 9557
104579 XDOT = 2967
530552
YDOT = -20686
075770 feet/sec YDOT = -6272
236202 meter/sec
ZDOT = 10646
811725 ZDOT = 3259
430889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5652210
07 X = 1722793
63
Y = -15763630
78 feet Y = -4804754
66 meter
Z = -14644961
90 Z = -4463784
39
XDOT = 21534
883197 XDOT = 6563
832398
YDOT = -2235
991821 feet/sec YDOT = -681
530307 meter/sec
ZDOT = 10709
757238 ZDOT = 3264
334006
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
61882671
00016717 00000-0 10270-3 0 9083
2 25544 51
6445 273
5886 0008158 271
8621 88
1597 15
54666297 15808
Satellite: ISS
Catalog Number: 25544
Epoch time: 15346
61882671 = yrday
fracday
Element set: 908
Inclination: 51
6445 deg
RA of node: 273
5886 deg
Eccentricity:
0008158
Arg of perigee: 271
8621 deg
Mean anomaly: 88
1597 deg
Mean motion: 15
54666297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 355
Coasting Arc #10 (Orbit 1595)
---------------------------------------
Vector Time (GMT): 2015/347/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2733962
77 A = 6783450
84 meter
Y = 5347653
98 meter E =
0004830
Z = 3148901
98 I = 51
28322
XDOT = -3672
991649 Wp = 91
95996
YDOT = 4711
819088 meter/sec RA = 267
77475 deg
ZDOT = -4806
660548 TA = 51
51863
MA = 51
47532
Ha = 218
053 n
mi
Hp = 217
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8969694
11 X = 2658664
61
Y = 17544796
52 feet Y = 5377805
64 meter
Z = 10331043
23 Z = 3162000
66
XDOT = -12050
497536 XDOT = -3702
058429
YDOT = 15458
724043 feet/sec YDOT = 4670
583209 meter/sec
ZDOT = -15769
883688 ZDOT = -4824
573377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10678785
24 X = -3254893
74
Y = 16525368
61 feet Y = 5036932
35 meter
Z = 10386601
46 Z = 3165836
13
XDOT = -18166
037073 XDOT = -5537
008100
YDOT = -1765
210476 feet/sec YDOT = -538
036153 meter/sec
ZDOT = -15848
197736 ZDOT = -4830
530670
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
64729788
00016717 00000-0 10270-3 0 9097
2 25544 51
6442 268
4578 0008062 275
6871 84
3363 15
54688163 15961
Satellite: ISS
Catalog Number: 25544
Epoch time: 15347
64729788 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 268
4578 deg
Eccentricity:
0008062
Arg of perigee: 275
6871 deg
Mean anomaly: 84
3363 deg
Mean motion: 15
54688163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1596
Checksum: 362
Coasting Arc #11 (Orbit 1610)
---------------------------------------
Vector Time (GMT): 2015/348/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1970558
18 A = 6786691
91 meter
Y = -6325012
49 meter E =
0008538
Z = -1446351
33 I = 51
29648
XDOT = 4312
847870 Wp = 339
65059
YDOT = -2660
856390 meter/sec RA = 262
77019 deg
ZDOT = 5757
771844 TA = 4
48744
MA = 4
47979
Ha = 218
274 n
mi
Hp = 217
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6465085
89 X = -1892658
08
Y = -20751353
31 feet Y = -6346612
88 meter
Z = -4745247
13 Z = -1455735
21
XDOT = 14149
763354 XDOT = 4314
312682
YDOT = -8729
843800 feet/sec YDOT = -2612
619582 meter/sec
ZDOT = 18890
327572 ZDOT = 5778
726078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14414243
07 X = 4393461
29
Y = -16256406
51 feet Y = -4954952
70 meter
Z = -4784580
90 Z = -1458340
26
XDOT = 13548
662041 XDOT = 4129
632190
YDOT = 6424
443595 feet/sec YDOT = 1958
170408 meter/sec
ZDOT = 18981
385883 ZDOT = 5785
526417
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
61147197
00016717 00000-0 10270-3 0 9105
2 25544 51
6441 263
6465 0008217 279
3720 80
6503 15
54725204 16119
Satellite: ISS
Catalog Number: 25544
Epoch time: 15348
61147197 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 263
6465 deg
Eccentricity:
0008217
Arg of perigee: 279
3720 deg
Mean anomaly: 80
6503 deg
Mean motion: 15
54725204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1611
Checksum: 298
Coasting Arc #12 (Orbit 1626)
---------------------------------------
Vector Time (GMT): 2015/349/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1075675
88 A = 6787574
97 meter
Y = 6681802
49 meter E =
0006667
Z = -454097
99 I = 51
30361
XDOT = -4807
489668 Wp = 185
30019
YDOT = 368
666264 meter/sec RA = 257
77366 deg
ZDOT = -5962
845149 TA = 359
62049
MA = 359
62099
Ha = 218
538 n
mi
Hp = 217
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3529120
33 X = 1003084
20
Y = 21921924
19 feet Y = 6693425
56 meter
Z = -1489822
79 Z = -449048
43
XDOT = -15772
603898 XDOT = -4782
289784
YDOT = 1209
534988 feet/sec YDOT = 315
047068 meter/sec
ZDOT = -19563
140252 ZDOT = -5986
137633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16665561
01 X = -5079663
00
Y = 14674649
69 feet Y = 4472833
23 meter
Z = -1469270
30 Z = -447833
59
XDOT = -8288
771018 XDOT = -2526
417406
YDOT = -11382
283840 feet/sec YDOT = -3469
320114 meter/sec
ZDOT = -19663
868667 ZDOT = -5993
547170
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
63990902
00016717 00000-0 10270-3 0 9119
2 25544 51
6436 258
5153 0008225 281
8067 78
2163 15
54702468 16270
Satellite: ISS
Catalog Number: 25544
Epoch time: 15349
63990902 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 258
5153 deg
Eccentricity:
0008225
Arg of perigee: 281
8067 deg
Mean anomaly: 78
2163 deg
Mean motion: 15
54702468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1627
Checksum: 323
Coasting Arc #13 (Orbit 1642)
---------------------------------------
Vector Time (GMT): 2015/350/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -47016
91 A = 6785223
34 meter
Y = -6376896
04 meter E =
0008409
Z = 2301459
35 I = 51
30325
XDOT = 5112
776677 Wp = 38
42648
YDOT = 1909
225471 meter/sec RA = 252
77356 deg
ZDOT = 5390
385878 TA = 347
35579
MA = 347
37687
Ha = 218
710 n
mi
Hp = 216
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -154254
94 X = 13115
05
Y = -20921574
93 feet Y = -6377085
72 meter
Z = 7550719
65 Z = 2301376
65
XDOT = 16774
201697 XDOT = 5064
862948
YDOT = 6263
863093 feet/sec YDOT = 1966
131718 meter/sec
ZDOT = 17684
993039 ZDOT = 5415
106329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17398696
49 X = 5303122
69
Y = -11619327
68 feet Y = -3541571
08 meter
Z = 7551559
05 Z = 2301715
20
XDOT = 3026
947304 XDOT = 922
613538
YDOT = 16104
309157 feet/sec YDOT = 4908
593431 meter/sec
ZDOT = 17791
471483 ZDOT = 5422
840508
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
66832680
00016717 00000-0 10270-3 0 9123
2 25544 51
6428 253
3824 0008349 287
2020 72
8219 15
54768079 16435
Satellite: ISS
Catalog Number: 25544
Epoch time: 15350
66832680 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 253
3824 deg
Eccentricity:
0008349
Arg of perigee: 287
2020 deg
Mean anomaly: 72
8219 deg
Mean motion: 15
54768079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1643
Checksum: 322
Coasting Arc #14 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2015/351/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1097748
35 A = 6781117
06 meter
Y = 5472556
15 meter E =
0004874
Z = -3853059
98 I = 51
29906
XDOT = -5152
803644 Wp = 338
26326
YDOT = -3924
399606 meter/sec RA = 247
76478 deg
ZDOT = -4099
714214 TA = 248
45110
MA = 248
50305
Ha = 218
904 n
mi
Hp = 216
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3601536
58 X = -1140145
60
Y = 17954580
53 feet Y = 5460043
50 meter
Z = -12641272
91 Z = -3858495
36
XDOT = -16905
523766 XDOT = -5088
622300
YDOT = -12875
326792 feet/sec YDOT = -3981
662636 meter/sec
ZDOT = -13450
505950 ZDOT = -4124
589681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16831859
64 X = -5130350
82
Y = 7169819
64 feet Y = 2185361
03 meter
Z = -12665780
51 Z = -3860529
90
XDOT = 1731
375081 XDOT = 527
723125
YDOT = -19920
323671 feet/sec YDOT = -6071
714655 meter/sec
ZDOT = -13557
291391 ZDOT = -4132
262416
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
63245390
00016717 00000-0 10270-3 0 9138
2 25544 51
6419 248
5713 0008428 290
0898 69
9348 15
54779526 16586
Satellite: ISS
Catalog Number: 25544
Epoch time: 15351
63245390 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 248
5713 deg
Eccentricity:
0008428
Arg of perigee: 290
0898 deg
Mean anomaly: 69
9348 deg
Mean motion: 15
54779526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 348
Coasting Arc #15 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2015/352/14:36:25
397
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2316272
52 A = 6777174
68 meter
Y = -4072872
27 meter E =
0001905
Z = 4898261
62 I = 51
29891
XDOT = 4861
371498 Wp = 269
34762
YDOT = 5482
050395 meter/sec RA = 242
74257 deg
ZDOT = 2260
202786 TA = 158
46483
MA = 158
45681
Ha = 219
023 n
mi
Hp = 216
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7599319
31 X = 2337850
36
Y = -13362441
83 feet Y = -4046849
69 meter
Z = 16070412
12 Z = 4909565
87
XDOT = 15949
381555 XDOT = 4788
729363
YDOT = 17985
729643 feet/sec YDOT = 5536
007224 meter/sec
ZDOT = 7415
363470 ZDOT = 2283
642072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15240177
36 X = 4645206
06
Y = -1563508
18 feet Y = -476557
29 meter
Z = 16120021
33 Z = 4913382
50
XDOT = -5664
760619 XDOT = -1726
619037
YDOT = 22245
911198 feet/sec YDOT = 6780
553733 meter/sec
ZDOT = 7515
669014 ZDOT = 2290
775915
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
66084143
00016717 00000-0 10270-3 0 9140
2 25544 51
6420 243
4382 0008298 294
7871 65
2418 15
54784848 16749
Satellite: ISS
Catalog Number: 25544
Epoch time: 15352
66084143 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 243
4382 deg
Eccentricity:
0008298
Arg of perigee: 294
7871 deg
Mean anomaly: 65
2418 deg
Mean motion: 15
54784848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1674
Checksum: 333
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