[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 18th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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
050/12:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 213
7
Coasting Arc #1 (Orbit 2622)
---------------------------------------
Vector Time (GMT): 2016/048/14:39:04
880
Vector Time (MET): N/A
Weight (LBS) : 922145
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3526232
18 A = 6777338
27 meter
Y = 2365141
04 meter E =
0005466
Z = 5277936
52 I = 51
30099
XDOT = -3910
629440 Wp = 112
19669
YDOT = 6592
700940 meter/sec RA = 298
61901 deg
ZDOT = -343
332652 TA = 341
07995
MA = 341
10025
Ha = 221
973 n
mi
Hp = 213
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11569003
23 X = 3473885
01
Y = 7759649
08 feet Y = 2404281
24 meter
Z = 17316064
70 Z = 5294938
54
XDOT = -12830
149080 XDOT = -3982
392274
YDOT = 21629
596260 feet/sec YDOT = 6548
568424 meter/sec
ZDOT = -1126
419462 ZDOT = -362
503766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12199350
67 X = 3718362
08
Y = 6533620
11 feet Y = 1991447
41 meter
Z = 17389299
52 Z = 5300258
49
XDOT = -10038
548495 XDOT = -3059
749581
YDOT = 21950
944507 feet/sec YDOT = 6690
647886 meter/sec
ZDOT = -1210
771647 ZDOT = -369
043198
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 16048
65809445
00016717 00000-0 10270-3 0 9007
2 25544 51
6417 299
0882 0003811 137
9621 222
1824 15
54145293 26239
Satellite: ISS
Catalog Number: 25544
Epoch time: 16048
65809445 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 299
0882 deg
Eccentricity:
0003811
Arg of perigee: 137
9621 deg
Mean anomaly: 222
1824 deg
Mean motion: 15
54145293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2623
Checksum: 310
Coasting Arc #2 (Orbit 2637)
---------------------------------------
Vector Time (GMT): 2016/049/14:39:04
880
Vector Time (MET): N/A
Weight (LBS) : 922145
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2587581
87 A = 6778916
50 meter
Y = -3909049
25 meter E =
0015443
Z = -4911148
24 I = 51
29062
XDOT = 4486
326730 Wp = 114
48375
YDOT = -5785
482039 meter/sec RA = 293
59426 deg
ZDOT = 2240
525596 TA = 177
54557
MA = 177
53798
Ha = 221
995 n
mi
Hp = 213
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8489441
85 X = -2519821
85
Y = -12824964
73 feet Y = -3937606
67 meter
Z = -16112691
08 Z = -4923553
04
XDOT = 14718
919717 XDOT = 4539
804706
YDOT = -18981
240286 feet/sec YDOT = -5735
013836 meter/sec
ZDOT = 7350
805760 ZDOT = 2262
448767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9871441
41 X = -3008815
34
Y = -11721496
72 feet Y = -3572712
20 meter
Z = -16165714
22 Z = -4927309
70
XDOT = 11420
519474 XDOT = 3480
974336
YDOT = -19891
559733 feet/sec YDOT = -6062
947407 meter/sec
ZDOT = 7446
921298 ZDOT = 2269
821612
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 16049
62260279
00016717 00000-0 10270-3 0 9012
2 25544 51
6403 294
2780 0003791 141
8309 218
3112 15
54179999 26385
Satellite: ISS
Catalog Number: 25544
Epoch time: 16049
62260279 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 294
2780 deg
Eccentricity:
0003791
Arg of perigee: 141
8309 deg
Mean anomaly: 218
3112 deg
Mean motion: 15
54179999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2638
Checksum: 321
Coasting Arc #3 (Orbit 2651)
---------------------------------------
Vector Time (GMT): 2016/050/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -131238
07 A = 6786074
27 meter
Y = -6229759
29 meter E =
0006179
Z = -2693319
62 I = 51
30621
XDOT = 5169
996315 Wp = 91
63201
YDOT = -2331
551979 meter/sec RA = 289
04877 deg
ZDOT = 5151
156895 TA = 237
81465
MA = 237
87459
Ha = 221
902 n
mi
Hp = 213
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -430571
11 X = -48482
92
Y = -20438842
80 feet Y = -6230764
32 meter
Z = -8836350
46 Z = -2693755
76
XDOT = 16961
930167 XDOT = 5170
662538
YDOT = -7649
448749 feet/sec YDOT = -2273
733620 meter/sec
ZDOT = 16900
121046 ZDOT = 5176
272619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8526933
76 X = 2599009
41
Y = -18579836
64 feet Y = -5663134
21 meter
Z = -8837072
31 Z = -2693539
64
XDOT = 17147
598262 XDOT = 5226
587950
YDOT = -204
747483 feet/sec YDOT = -62
407033 meter/sec
ZDOT = 17009
415895 ZDOT = 5184
469965
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 16050
52280056
00016717 00000-0 10270-3 0 9029
2 25544 51
6428 289
7919 0003639 144
2490 215
8907 15
54189097 26524
Satellite: ISS
Catalog Number: 25544
Epoch time: 16050
52280056 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 289
7919 deg
Eccentricity:
0003639
Arg of perigee: 144
2490 deg
Mean anomaly: 215
8907 deg
Mean motion: 15
54189097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2652
Checksum: 327
Coasting Arc #4 (Orbit 2667)
---------------------------------------
Vector Time (GMT): 2016/051/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -794956
13 A = 6788700
30 meter
Y = 6650134
61 meter E =
0017144
Z = 1052942
39 I = 51
30505
XDOT = -4931
863282 Wp = 128
76998
YDOT = 348
014292 meter/sec RA = 284
05125 deg
ZDOT = -5867
371194 TA = 39
75224
MA = 39
62674
Ha = 221
888 n
mi
Hp = 213
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2608123
79 X = -874375
12
Y = 21818026
94 feet Y = 6640800
91 meter
Z = 3454535
39 Z = 1048887
39
XDOT = -16180
653811 XDOT = -4906
887853
YDOT = 1141
779174 feet/sec YDOT = 293
002129 meter/sec
ZDOT = -19249
905493 ZDOT = -5891
267729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11511401
44 X = -3508675
16
Y = 18720198
40 feet Y = 5705916
47 meter
Z = 3435728
88 Z = 1047210
16
XDOT = -13697
494984 XDOT = -4174
996471
YDOT = -4838
132079 feet/sec YDOT = -1474
662658 meter/sec
ZDOT = -19353
545112 ZDOT = -5898
960550
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 16051
55158514
00016717 00000-0 10270-3 0 9037
2 25544 51
6424 284
6628 0003815 148
0963 212
0422 15
54186599 26686
Satellite: ISS
Catalog Number: 25544
Epoch time: 16051
55158514 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 284
6628 deg
Eccentricity:
0003815
Arg of perigee: 148
0963 deg
Mean anomaly: 212
0422 deg
Mean motion: 15
54186599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2668
Checksum: 317
Coasting Arc #5 (Orbit 2683)
---------------------------------------
Vector Time (GMT): 2016/052/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1587185
83 A = 6788766
75 meter
Y = -6562366
14 meter E =
0013003
Z = 667134
02 I = 51
29806
XDOT = 4542
610038 Wp = 68
09008
YDOT = 1711
053547 meter/sec RA = 279
05578 deg
ZDOT = 5935
174466 TA = 299
14851
MA = 299
27858
Ha = 221
675 n
mi
Hp = 213
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5207302
60 X = 1657209
30
Y = -21530072
63 feet Y = -6544225
59 meter
Z = 2188759
92 Z = 675014
67
XDOT = 14903
576240 XDOT = 4494
309182
YDOT = 5613
692740 feet/sec YDOT = 1761
582518 meter/sec
ZDOT = 19472
357171 ZDOT = 5957
123311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13417821
78 X = 4089752
08
Y = -17620047
32 feet Y = -5370590
42 meter
Z = 2224115
29 Z = 677910
34
XDOT = 9984
314678 XDOT = 3043
219114
YDOT = 10109
103632 feet/sec YDOT = 3081
254787 meter/sec
ZDOT = 19567
179600 ZDOT = 5964
076342
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 16052
58035246
00016717 00000-0 10270-3 0 9048
2 25544 51
6414 279
5323 0003630 153
5109 206
6230 15
54255298 26845
Satellite: ISS
Catalog Number: 25544
Epoch time: 16052
58035246 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 279
5323 deg
Eccentricity:
0003630
Arg of perigee: 153
5109 deg
Mean anomaly: 206
6230 deg
Mean motion: 15
54255298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2684
Checksum: 297
Coasting Arc #6 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2016/053/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2318341
92 A = 6786617
00 meter
Y = 5921656
32 meter E =
0009020
Z = -2362213
01 I = 51
28557
XDOT = -4040
412236 Wp = 143
21297
YDOT = -3711
190534 meter/sec RA = 274
05809 deg
ZDOT = -5355
668508 TA = 63
29151
MA = 63
19920
Ha = 221
580 n
mi
Hp = 213
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7606108
67 X = -2372912
70
Y = 19428006
30 feet Y = 5895425
69 meter
Z = -7750042
68 Z = -2373607
88
XDOT = -13255
945657 XDOT = -3972
597564
YDOT = -12175
821963 feet/sec YDOT = -3755
994532 meter/sec
ZDOT = -17571
090907 ZDOT = -5375
130237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14479204
61 X = -4413261
57
Y = 14995610
68 feet Y = 4570662
13 meter
Z = -7800498
30 Z = -2377591
88
XDOT = -6319
680402 XDOT = -1926
238586
YDOT = -15255
737162 feet/sec YDOT = -4649
948687 meter/sec
ZDOT = -17654
778697 ZDOT = -5381
176547
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 16053
54481196
00016717 00000-0 10270-3 0 9055
2 25544 51
6403 274
7232 0003583 158
3174 201
8131 15
54235552 26995
Satellite: ISS
Catalog Number: 25544
Epoch time: 16053
54481196 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 274
7232 deg
Eccentricity:
0003583
Arg of perigee: 158
3174 deg
Mean anomaly: 201
8131 deg
Mean motion: 15
54235552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 304
Coasting Arc #7 (Orbit 2714)
---------------------------------------
Vector Time (GMT): 2016/054/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2939620
22 A = 6782864
64 meter
Y = -4810672
89 meter E =
0013370
Z = 3764430
63 I = 51
27126
XDOT = 3456
482490 Wp = 110
24962
YDOT = 5409
833405 meter/sec RA = 269
04997 deg
ZDOT = 4197
524534 TA = 295
13407
MA = 295
27271
Ha = 221
444 n
mi
Hp = 213
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9644423
29 X = 2974910
27
Y = -15783047
55 feet Y = -4777602
31 meter
Z = 12350494
19 Z = 3778796
60
XDOT = 11340
165648 XDOT = 3375
342154
YDOT = 17748
797262 feet/sec YDOT = 5448
032938 meter/sec
ZDOT = 13771
405950 ZDOT = 4214
117147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14733488
65 X = 4490767
34
Y = -11112183
99 feet Y = -3386993
68 meter
Z = 12413616
57 Z = 3783670
33
XDOT = 3060
109497 XDOT = 932
721375
YDOT = 19581
839097 feet/sec YDOT = 5968
544557 meter/sec
ZDOT = 13842
366170 ZDOT = 4219
153209
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 16054
57355426
00016717 00000-0 10270-3 0 9066
2 25544 51
6396 269
5921 0003433 161
4041 198
7238 15
54263606 27157
Satellite: ISS
Catalog Number: 25544
Epoch time: 16054
57355426 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 269
5921 deg
Eccentricity:
0003433
Arg of perigee: 161
4041 deg
Mean anomaly: 198
7238 deg
Mean motion: 15
54263606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2715
Checksum: 317
Coasting Arc #8 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2016/055/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3519495
45 A = 6779056
99 meter
Y = 3278023
40 meter E =
0011791
Z = -4787699
85 I = 51
25897
XDOT = -2755
688302 Wp = 89
13738
YDOT = -6676
303778 meter/sec RA = 264
03088 deg
ZDOT = -2550
656552 TA = 155
61812
MA = 155
56230
Ha = 221
370 n
mi
Hp = 213
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11546901
08 X = -3532633
36
Y = 10754669
94 feet Y = 3238591
95 meter
Z = -15707676
68 Z = -4804828
74
XDOT = -9040
972121 XDOT = -2668
437635
YDOT = -21903
883785 feet/sec YDOT = -6706
632214 meter/sec
ZDOT = -8368
295773 ZDOT = -2563
829934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14515384
70 X = -4424289
26
Y = 5995113
09 feet Y = 1827310
47 meter
Z = -15782496
10 Z = -4810504
81
XDOT = -197
334278 XDOT = -60
147488
YDOT = -22609
590356 feet/sec YDOT = -6891
403140 meter/sec
ZDOT = -8424
226555 ZDOT = -2567
704254
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 16055
53798656
00016717 00000-0 10270-3 0 9070
2 25544 51
6383 264
7819 0003507 165
1166 195
0091 15
54292368 27308
Satellite: ISS
Catalog Number: 25544
Epoch time: 16055
53798656 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 264
7819 deg
Eccentricity:
0003507
Arg of perigee: 165
1166 deg
Mean anomaly: 195
0091 deg
Mean motion: 15
54292368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 332
Coasting Arc #9 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2016/056/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4000937
82 A = 6777041
29 meter
Y = -1512376
06 meter E =
0005816
Z = 5254227
84 I = 51
25668
XDOT = 1954
529577 Wp = 144
05934
YDOT = 7391
080517 meter/sec RA = 259
00373 deg
ZDOT = 634
141589 TA = 299
82789
MA = 299
88570
Ha = 221
248 n
mi
Hp = 214
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13126436
40 X = 3992029
80
Y = -4961863
71 feet Y = -1467684
00 meter
Z = 17238280
32 Z = 5273641
70
XDOT = 6412
498612 XDOT = 1868
655075
YDOT = 24248
951826 feet/sec YDOT = 7412
457299 meter/sec
ZDOT = 2080
517023 ZDOT = 643
426471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13926148
21 X = 4244689
97
Y = -261616
31 feet Y = -79740
65 meter
Z = 17322692
79 Z = 5279956
76
XDOT = -2206
418196 XDOT = -672
516266
YDOT = 23968
157568 feet/sec YDOT = 7305
494427 meter/sec
ZDOT = 2119
483668 ZDOT = 646
018622
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 16056
56670213
00016717 00000-0 10270-3 0 9083
2 25544 51
6385 259
6512 0003503 167
9909 192
1328 15
54280983 27462
Satellite: ISS
Catalog Number: 25544
Epoch time: 16056
56670213 = yrday
fracday
Element set: 908
Inclination: 51
6385 deg
RA of node: 259
6512 deg
Eccentricity:
0003503
Arg of perigee: 167
9909 deg
Mean anomaly: 192
1328 deg
Mean motion: 15
54280983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 329
Coasting Arc #10 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2016/057/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4403644
16 A = 6777358
92 meter
Y = -358801
60 meter E =
0015407
Z = -5152798
83 I = 51
26444
XDOT = -999
928294 Wp = 113
11612
YDOT = -7466
826786 meter/sec RA = 253
97312 deg
ZDOT = 1371
828144 TA = 170
17654
MA = 170
14638
Ha = 221
220 n
mi
Hp = 213
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14447651
44 X = -4374274
85
Y = -1177170
61 feet Y = -407882
56 meter
Z = -16905507
96 Z = -5174119
01
XDOT = -3280
604638 XDOT = -923
021750
YDOT = -24497
463208 feet/sec YDOT = -7477
578453 meter/sec
ZDOT = 4500
748504 ZDOT = 1367
158597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13193869
55 X = -4021491
44
Y = -5736814
55 feet Y = -1748581
08 meter
Z = -16997862
44 Z = -5180948
47
XDOT = 4343
541189 XDOT = 1323
911354
YDOT = -23294
493789 feet/sec YDOT = -7100
161707 meter/sec
ZDOT = 4481
786404 ZDOT = 1366
048496
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 16057
53110774
00016717 00000-0 10270-3 0 9093
2 25544 51
6376 254
8400 0003539 171
7511 188
3700 15
54341478 27611
Satellite: ISS
Catalog Number: 25544
Epoch time: 16057
53110774 = yrday
fracday
Element set: 909
Inclination: 51
6376 deg
RA of node: 254
8400 deg
Eccentricity:
0003539
Arg of perigee: 171
7511 deg
Mean anomaly: 188
3700 deg
Mean motion: 15
54341478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 308
Coasting Arc #11 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2016/058/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4642708
23 A = 6780164
97 meter
Y = 2136656
34 meter E =
0008568
Z = 4447845
48 I = 51
28412
XDOT = -99
410138 Wp = 91
36915
YDOT = 6957
769991 meter/sec RA = 248
94973 deg
ZDOT = -3233
403473 TA = 31
34523
MA = 31
29419
Ha = 220
955 n
mi
Hp = 214
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15231982
39 X = 4596865
01
Y = 7010027
37 feet Y = 2188318
43 meter
Z = 14592668
89 Z = 4470286
78
XDOT = -326
148747 XDOT = -161
499903
YDOT = 22827
329366 feet/sec YDOT = 6956
310744 meter/sec
ZDOT = -10608
279110 ZDOT = -3234
038072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12266994
99 X = 3738980
07
Y = 11306488
09 feet Y = 3446217
57 meter
Z = 14689585
34 Z = 4477385
61
XDOT = -6404
695980 XDOT = -1952
151335
YDOT = 20758
395520 feet/sec YDOT = 6327
158955 meter/sec
ZDOT = -10612
210456 ZDOT = -3234
601747
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 16058
55979372
00016717 00000-0 10270-3 0 9105
2 25544 51
6380 249
7097 0003497 177
6066 182
5104 15
54350688 27778
Satellite: ISS
Catalog Number: 25544
Epoch time: 16058
55979372 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 249
7097 deg
Eccentricity:
0003497
Arg of perigee: 177
6066 deg
Mean anomaly: 182
5104 deg
Mean motion: 15
54350688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 347
Coasting Arc #12 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2016/059/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4694135
88 A = 6784029
56 meter
Y = -3668460
03 meter E =
0005593
Z = -3252576
74 I = 51
30949
XDOT = 1330
272157 Wp = 123
20837
YDOT = -5885
333274 meter/sec RA = 243
93589 deg
ZDOT = 4720
892643 TA = 198
91747
MA = 198
93825
Ha = 221
033 n
mi
Hp = 214
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15400708
26 X = -4636965
86
Y = -12035630
02 feet Y = -3720633
70 meter
Z = -10671183
52 Z = -3275240
23
XDOT = 4364
409963 XDOT = 1373
052630
YDOT = -19308
836201 feet/sec YDOT = -5870
217532 meter/sec
ZDOT = 15488
492924 ZDOT = 4727
459329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11190361
18 X = -3410822
09
Y = -15959976
19 feet Y = -4864600
74 meter
Z = -10768813
28 Z = -3282334
29
XDOT = 8508
246679 XDOT = 2593
313588
YDOT = -16429
768276 feet/sec YDOT = -5007
793370 meter/sec
ZDOT = 15517
949767 ZDOT = 4729
871089
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 16059
52417393
00016717 00000-0 10270-3 0 9114
2 25544 51
6378 244
8987 0003551 178
8841 181
2320 15
54380715 27921
Satellite: ISS
Catalog Number: 25544
Epoch time: 16059
52417393 = yrday
fracday
Element set: 911
Inclination: 51
6378 deg
RA of node: 244
8987 deg
Eccentricity:
0003551
Arg of perigee: 178
8841 deg
Mean anomaly: 181
2320 deg
Mean motion: 15
54380715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2792
Checksum: 329
Coasting Arc #13 (Orbit 2807)
---------------------------------------
Vector Time (GMT): 2016/060/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4454933
49 A = 6787243
97 meter
Y = 4834853
56 meter E =
0015416
Z = 1651254
62 I = 51
33571
XDOT = -2661
825625 Wp = 127
86321
YDOT = 4405
486196 meter/sec RA = 238
93528 deg
ZDOT = -5690
759714 TA = 33
95824
MA = 33
85966
Ha = 220
721 n
mi
Hp = 214
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14615923
53 X = 4392516
83
Y = 15862380
44 feet Y = 4884322
77 meter
Z = 5417502
04 Z = 1672743
32
XDOT = -8733
023705 XDOT = -2683
247940
YDOT = 14453
694870 feet/sec YDOT = 4375
599508 meter/sec
ZDOT = -18670
471503 ZDOT = -5703
742617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9696126
06 X = 2955379
22
Y = 19241005
62 feet Y = 5864658
51 meter
Z = 5509855
22 Z = 1679403
87
XDOT = -10828
210040 XDOT = -3300
438420
YDOT = 10844
492445 feet/sec YDOT = 3305
401297 meter/sec
ZDOT = -18727
491682 ZDOT = -5708
139465
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 16060
55282954
00016717 00000-0 10270-3 0 9123
2 25544 51
6379 239
7681 0003333 185
7696 174
3419 15
54435708 28082
Satellite: ISS
Catalog Number: 25544
Epoch time: 16060
55282954 = yrday
fracday
Element set: 912
Inclination: 51
6379 deg
RA of node: 239
7681 deg
Eccentricity:
0003333
Arg of perigee: 185
7696 deg
Mean anomaly: 174
3419 deg
Mean motion: 15
54435708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2808
Checksum: 339
Coasting Arc #14 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2016/061/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3915995
99 A = 6788439
83 meter
Y = -5539566
98 meter E =
0009884
Z = 118633
49 I = 51
35712
XDOT = 3974
146263 Wp = 60
25076
YDOT = -2673
226179 meter/sec RA = 233
94188 deg
ZDOT = 5986
446042 TA = 301
03198
MA = 301
12899
Ha = 220
818 n
mi
Hp = 214
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12847755
87 X = -3854336
40
Y = -18174432
35 feet Y = -5583013
48 meter
Z = 389217
50 Z = 99760
99
XDOT = 13038
537607 XDOT = 3974
664197
YDOT = -8770
427097 feet/sec YDOT = -2628
781169 meter/sec
ZDOT = 19640
571003 ZDOT = 6005
752827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7759973
33 X = -2365239
87
Y = -20861784
94 feet Y = -6358672
05 meter
Z = 308310
30 Z = 93972
98
XDOT = 13207
597121 XDOT = 4025
675602
YDOT = -4598
614482 feet/sec YDOT = -1401
657694 meter/sec
ZDOT = 19724
721355 ZDOT = 6012
095069
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 16061
58147258
00016717 00000-0 10270-3 0 9135
2 25544 51
6380 234
6369 0003544 185
8326 174
2787 15
54432843 28248
Satellite: ISS
Catalog Number: 25544
Epoch time: 16061
58147258 = yrday
fracday
Element set: 913
Inclination: 51
6380 deg
RA of node: 234
6369 deg
Eccentricity:
0003544
Arg of perigee: 185
8326 deg
Mean anomaly: 174
2787 deg
Mean motion: 15
54432843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 327
Coasting Arc #15 (Orbit 2838)
---------------------------------------
Vector Time (GMT): 2016/062/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2997955
68 A = 6786790
18 meter
Y = 5774046
76 meter E =
0009572
Z = -1915985
10 I = 51
37163
XDOT = -5184
937782 Wp = 156
00895
YDOT = 844
271284 meter/sec RA = 228
94985 deg
ZDOT = -5587
021714 TA = 45
19076
MA = 45
11298
Ha = 220
650 n
mi
Hp = 214
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9835812
60 X = 2942472
99
Y = 18943722
97 feet Y = 5807261
50 meter
Z = -6286040
35 Z = -1901557
17
XDOT = -17010
950728 XDOT = -5166
854171
YDOT = 2769
918911 feet/sec YDOT = 786
390496 meter/sec
ZDOT = -18330
123735 ZDOT = -5612
164770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5046107
41 X = 1538053
54
Y = 20758502
84 feet Y = 6327191
67 meter
Z = -6224428
69 Z = -1897205
86
XDOT = -15550
090208 XDOT = -4739
667495
YDOT = -1730
694921 feet/sec YDOT = -527
515812 meter/sec
ZDOT = -18439
284493 ZDOT = -5620
293913
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 16062
54580937
00016717 00000-0 10270-3 0 9148
2 25544 51
6380 229
8268 0003294 189
1831 170
9262 15
54475868 28393
Satellite: ISS
Catalog Number: 25544
Epoch time: 16062
54580937 = yrday
fracday
Element set: 914
Inclination: 51
6380 deg
RA of node: 229
8268 deg
Eccentricity:
0003294
Arg of perigee: 189
1831 deg
Mean anomaly: 170
9262 deg
Mean motion: 15
54475868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2839
Checksum: 345
Coasting Arc #16 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2016/063/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 906643
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1774959
34 A = 6783232
25 meter
Y = -5552593
05 meter E =
0012068
Z = 3462131
54 I = 51
38145
XDOT = 6125
281220 Wp = 107
46296
YDOT = 877
495426 meter/sec RA = 223
95079 deg
ZDOT = 4530
999048 TA = 293
34778
MA = 293
47470
Ha = 220
587 n
mi
Hp = 214
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5823357
41 X = -1729554
30
Y = -18217168
79 feet Y = -5572187
66 meter
Z = 11358699
29 Z = 3453620
07
XDOT = 20096
066996 XDOT = 6093
004215
YDOT = 2878
922002 feet/sec YDOT = 945
812287 meter/sec
ZDOT = 14865
482441 ZDOT = 4560
675320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1685038
66 X = -513599
78
Y = -19072336
79 feet Y = -5813248
25 meter
Z = 11322693
77 Z = 3451157
06
XDOT = 17463
239063 XDOT = 5322
795266
YDOT = 7391
146681 feet/sec YDOT = 2252
821508 meter/sec
ZDOT = 14994
031558 ZDOT = 4570
180819
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 16063
57442018
00016717 00000-0 10270-3 0 9150
2 25544 51
6379 224
6956 0003492 193
4955 166
6105 15
54488614 28552
Satellite: ISS
Catalog Number: 25544
Epoch time: 16063
57442018 = yrday
fracday
Element set: 915
Inclination: 51
6379 deg
RA of node: 224
6956 deg
Eccentricity:
0003492
Arg of perigee: 193
4955 deg
Mean anomaly: 166
6105 deg
Mean motion: 15
54488614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 336
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