[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 24th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
237/07:36:04
457 1
3 4
0 4
0
N/A 3
8 -0
4 219
8
000/00:12:08
914 0
1 -0
0 215
5
239/10:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 215
6
246/19:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2016/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1143254
51 A = 6786253
83 meter
Y = -6619350
86 meter E =
0014520
Z = 911976
07 I = 52
03098
XDOT = 4555
037210 Wp = 127
71443
YDOT = -1615
353105 meter/sec RA = 86
28293 deg
ZDOT = -5958
593563 TA = 42
46001
MA = 42
34777
Ha = 219
757 n
mi
Hp = 213
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3750835
01 X = -1073580
24
Y = -21717030
38 feet Y = -6631745
86 meter
Z = 2992047
49 Z = 906592
19
XDOT = 14944
347802 XDOT = 4601
706053
YDOT = -5299
714913 feet/sec YDOT = -1564
155136 meter/sec
ZDOT = -19549
191479 ZDOT = -5936
353005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7459089
02 X = -2273530
33
Y = 20741106
91 feet Y = 6321889
39 meter
Z = 2969679
32 Z = 905158
26
XDOT = -14208
394231 XDOT = -4330
718562
YDOT = -2298
249378 feet/sec YDOT = -700
506410 meter/sec
ZDOT = -19451
684044 ZDOT = -5928
873296
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 16235
53392154
00016717 00000-0 10270-3 0 9006
2 25544 51
6420 86
9610 0001217 156
5941 203
5268 15
55068396 15305
Satellite: ISS
Catalog Number: 25544
Epoch time: 16235
53392154 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 86
9610 deg
Eccentricity:
0001217
Arg of perigee: 156
5941 deg
Mean anomaly: 203
5268 deg
Mean motion: 15
55068396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1530
Checksum: 295
Coasting Arc #2 (Orbit 1545)
---------------------------------------
Vector Time (GMT): 2016/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 147585
10 A = 6785989
14 meter
Y = 6688008
80 meter E =
0013350
Z = 1104180
32 I = 52
02685
XDOT = -4804
140899 Wp = 61
86481
YDOT = -878
499596 meter/sec RA = 81
33368 deg
ZDOT = 5915
097609 TA = 310
05779
MA = 310
17481
Ha = 219
643 n
mi
Hp = 213
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 484203
09 X = 67423
51
Y = 21942286
07 feet Y = 6689211
05 meter
Z = 3622638
83 Z = 1104702
13
XDOT = -15761
617122 XDOT = -4822
693123
YDOT = -2882
216523 feet/sec YDOT = -932
326080 meter/sec
ZDOT = 19406
488219 ZDOT = 5891
715384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10113818
15 X = 3082691
77
Y = -19478223
01 feet Y = -5936962
37 meter
Z = 3623726
49 Z = 1104511
83
XDOT = 11141
462221 XDOT = 3395
917685
YDOT = 9405
798758 feet/sec YDOT = 2866
887461 meter/sec
ZDOT = 19304
430906 ZDOT = 5883
990540
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 16236
56212402
00016717 00000-0 10270-3 0 9018
2 25544 51
6415 81
8269 0001192 164
3789 195
7401 15
55100983 15469
Satellite: ISS
Catalog Number: 25544
Epoch time: 16236
56212402 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 81
8269 deg
Eccentricity:
0001192
Arg of perigee: 164
3789 deg
Mean anomaly: 195
7401 deg
Mean motion: 15
55100983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1546
Checksum: 301
Coasting Arc #3 (Orbit 1557)
---------------------------------------
Vector Time (GMT): 2016/237/07:42:08
914
Vector Time (MET): N/A
Weight (LBS) : 929563
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4341960
34 A = 6778374
72 meter
Y = 1495708
34 meter E =
0010310
Z = -4995092
56 I = 51
99070
XDOT = -57
112460 Wp = 116
39953
YDOT = 7352
199762 meter/sec RA = 77
22870 deg
ZDOT = 2150
832615 TA = 174
48197
MA = 174
47060
Ha = 219
790 n
mi
Hp = 215
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14245276
70 X = 4349176
17
Y = 4907179
59 feet Y = 1544303
15 meter
Z = -16388098
93 Z = -4973983
02
XDOT = -187
376836 XDOT = -149
770158
YDOT = 24121
390296 feet/sec YDOT = 7351
043116 meter/sec
ZDOT = 7056
537451 ZDOT = 2150
329770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5476885
04 X = 1669354
56
Y = -14142819
16 feet Y = -4310731
28 meter
Z = -16296088
58 Z = -4967047
80
XDOT = 23061
997790 XDOT = 7029
296927
YDOT = 800
112522 feet/sec YDOT = 243
874297 meter/sec
ZDOT = 7053
013863 ZDOT = 2149
758626
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 16237
33327761
00016717 00000-0 10270-3 0 9020
2 25544 51
6431 77
9774 0003027 246
5903 113
4932 15
54303859 15589
Satellite: ISS
Catalog Number: 25544
Epoch time: 16237
33327761 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 77
9774 deg
Eccentricity:
0003027
Arg of perigee: 246
5903 deg
Mean anomaly: 113
4932 deg
Mean motion: 15
54303859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1558
Checksum: 313
Coasting Arc #4 (Orbit 1573)
---------------------------------------
Vector Time (GMT): 2016/238/07:42:08
914
Vector Time (MET): N/A
Weight (LBS) : 929563
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4371193
81 A = 6781824
04 meter
Y = -3185565
52 meter E =
0007684
Z = 4085586
84 I = 51
99386
XDOT = 1106
755336 Wp = 80
62863
YDOT = -6517
357592 meter/sec RA = 72
26016 deg
ZDOT = -3890
084131 TA = 49
46942
MA = 49
40252
Ha = 219
863 n
mi
Hp = 215
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14341187
05 X = -4355093
06
Y = -10451330
46 feet Y = -3234356
98 meter
Z = 13404156
31 Z = 4064391
99
XDOT = 3631
087060 XDOT = 1198
448088
YDOT = -21382
406799 feet/sec YDOT = -6504
468556 meter/sec
ZDOT = -12762
743213 ZDOT = -3884
484895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10777518
53 X = -3284987
65
Y = 14184671
61 feet Y = 4323487
91 meter
Z = 13312082
72 Z = 4057522
81
XDOT = -20258
619768 XDOT = -6174
827305
YDOT = -3415
936228 feet/sec YDOT = -1041
177362 meter/sec
ZDOT = -12737
076850 ZDOT = -3882
261024
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 16238
36199437
00016717 00000-0 10270-3 0 9032
2 25544 51
6427 72
8492 0003042 250
0186 110
0640 15
54306571 15746
Satellite: ISS
Catalog Number: 25544
Epoch time: 16238
36199437 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 72
8492 deg
Eccentricity:
0003042
Arg of perigee: 250
0186 deg
Mean anomaly: 110
0640 deg
Mean motion: 15
54306571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1574
Checksum: 292
Coasting Arc #5 (Orbit 1588)
---------------------------------------
Vector Time (GMT): 2016/239/07:42:08
914
Vector Time (MET): N/A
Weight (LBS) : 929563
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4221824
74 A = 6785620
53 meter
Y = 4552273
57 meter E =
0002124
Z = -2736304
24 I = 51
99742
XDOT = -2227
304314 Wp = 27
50336
YDOT = 5182
925131 meter/sec RA = 67
29990 deg
ZDOT = 5189
555492 TA = 301
71235
MA = 301
73306
Ha = 219
614 n
mi
Hp = 215
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13851131
03 X = 4183897
97
Y = 14935280
75 feet Y = 4599272
72 meter
Z = -8977376
11 Z = -2715888
05
XDOT = -7307
428852 XDOT = -2310
303990
YDOT = 17004
347542 feet/sec YDOT = 5157
553968 meter/sec
ZDOT = 17026
100695 ZDOT = 5178
534172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15013257
11 X = 4576040
77
Y = -13823826
51 feet Y = -4213502
32 meter
Z = -8888962
55 Z = -2709355
79
XDOT = 15955
411296 XDOT = 4863
209363
YDOT = 6419
080609 feet/sec YDOT = 1956
535770 meter/sec
ZDOT = 16976
963755 ZDOT = 5174
578553
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 16239
32641004
00016717 00000-0 10270-3 0 9042
2 25544 51
6441 68
0398 0003173 255
1356 104
9446 15
54332639 15890
Satellite: ISS
Catalog Number: 25544
Epoch time: 16239
32641004 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 68
0398 deg
Eccentricity:
0003173
Arg of perigee: 255
1356 deg
Mean anomaly: 104
9446 deg
Mean motion: 15
54332639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1589
Checksum: 306
Coasting Arc #6 (Orbit 1590)
---------------------------------------
Vector Time (GMT): 2016/239/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2380562
16 A = 6788793
01 meter
Y = -6339136
59 meter E =
0010154
Z = -393336
66 I = 52
00546
XDOT = 4548
930544 Wp = 154
49368
YDOT = -1338
389583 meter/sec RA = 66
81647 deg
ZDOT = -6027
779209 TA = 29
72625
MA = 29
66859
Ha = 219
624 n
mi
Hp = 215
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7810243
31 X = -2307588
76
Y = -20797692
24 feet Y = -6365349
62 meter
Z = -1290474
59 Z = -404723
35
XDOT = 14924
312809 XDOT = 4592
838790
YDOT = -4391
041940 feet/sec YDOT = -1287
275033 meter/sec
ZDOT = -19776
178506 ZDOT = -6005
575143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12000089
56 X = -3657627
30
Y = 18692617
06 feet Y = 5697509
68 meter
Z = -1339083
89 Z = -408152
77
XDOT = -11160
696851 XDOT = -3401
780400
YDOT = -8559
493230 feet/sec YDOT = -2608
933536 meter/sec
ZDOT = -19678
862551 ZDOT = -5998
117305
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 16239
45499795
00016717 00000-0 10270-3 0 9055
2 25544 51
6432 67
3986 0003320 255
3620 104
7165 15
54288699 15910
Satellite: ISS
Catalog Number: 25544
Epoch time: 16239
45499795 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 67
3986 deg
Eccentricity:
0003320
Arg of perigee: 255
3620 deg
Mean anomaly: 104
7165 deg
Mean motion: 15
54288699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1591
Checksum: 339
Coasting Arc #7 (Orbit 1606)
---------------------------------------
Vector Time (GMT): 2016/240/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1477786
54 A = 6786778
15 meter
Y = 6271270
99 meter E =
0010672
Z = 2115640
27 I = 51
98444
XDOT = -5258
239119 Wp = 66
49121
YDOT = -638
218946 meter/sec RA = 61
86691 deg
ZDOT = 5546
810680 TA = 316
83609
MA = 316
91970
Ha = 219
477 n
mi
Hp = 215
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4848381
05 X = 1397273
02
Y = 20575036
06 feet Y = 6287346
46 meter
Z = 6941076
99 Z = 2122623
19
XDOT = -17251
440678 XDOT = -5277
655290
YDOT = -2093
894180 feet/sec YDOT = -697
128519 meter/sec
ZDOT = 18198
197770 ZDOT = 5521
220630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13335630
82 X = 4064700
28
Y = -16388758
42 feet Y = -4995293
57 meter
Z = 6970437
95 Z = 2124589
49
XDOT = 7777
265259 XDOT = 2370
510451
YDOT = 14045
821839 feet/sec YDOT = 4281
166496 meter/sec
ZDOT = 18086
442913 ZDOT = 5512
747800
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 16240
48370114
00016717 00000-0 10270-3 0 9064
2 25544 51
6418 62
2681 0003314 260
8996 99
1782 15
54348418 16076
Satellite: ISS
Catalog Number: 25544
Epoch time: 16240
48370114 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 62
2681 deg
Eccentricity:
0003314
Arg of perigee: 260
8996 deg
Mean anomaly: 99
1782 deg
Mean motion: 15
54348418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1607
Checksum: 314
Coasting Arc #8 (Orbit 1621)
---------------------------------------
Vector Time (GMT): 2016/241/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -347387
47 A = 6783177
51 meter
Y = -5725675
09 meter E =
0002137
Z = -3622687
48 I = 51
95490
XDOT = 5745
887427 Wp = 76
19415
YDOT = 2457
643446 meter/sec RA = 56
90966 deg
ZDOT = -4436
996834 TA = 146
49654
MA = 146
48302
Ha = 219
483 n
mi
Hp = 215
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1139722
66 X = -265738
51
Y = -18785023
28 feet Y = -5729103
41 meter
Z = -11885457
60 Z = -3624176
46
XDOT = 18851
336703 XDOT = 5739
531084
YDOT = 8063
134665 feet/sec YDOT = 2521
862110 meter/sec
ZDOT = -14557
076226 ZDOT = -4409
100698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13994559
34 X = -4265541
69
Y = 12577721
87 feet Y = 3833689
63 meter
Z = -11890895
30 Z = -3624344
89
XDOT = -4639
773625 XDOT = -1414
203001
YDOT = -18804
479386 feet/sec YDOT = -5731
605317 meter/sec
ZDOT = -14435
579858 ZDOT = -4399
964741
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 16241
44810880
00016717 00000-0 10270-3 0 9071
2 25544 51
6405 57
4596 0003311 264
9563 95
1212 15
54328892 16220
Satellite: ISS
Catalog Number: 25544
Epoch time: 16241
44810880 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 57
4596 deg
Eccentricity:
0003311
Arg of perigee: 264
9563 deg
Mean anomaly: 95
1212 deg
Mean motion: 15
54328892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1622
Checksum: 305
Coasting Arc #9 (Orbit 1637)
---------------------------------------
Vector Time (GMT): 2016/242/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -935640
82 A = 6779431
64 meter
Y = 4786676
38 meter E =
0005213
Z = 4707156
11 I = 51
92413
XDOT = -5924
077103 Wp = 132
83426
YDOT = -3956
453354 meter/sec RA = 51
93875 deg
ZDOT = 2840
323070 TA = 289
07220
MA = 289
12866
Ha = 219
557 n
mi
Hp = 215
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3069687
74 X = -1011962
06
Y = 15704318
83 feet Y = 4775786
92 meter
Z = 15443425
56 Z = 4702425
47
XDOT = -19435
948502 XDOT = -5893
191581
YDOT = -12980
490005 feet/sec YDOT = -4022
527514 meter/sec
ZDOT = 9318
645243 ZDOT = 2811
621097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14109144
75 X = 4300467
32
Y = -7592546
63 feet Y = -2314208
21 meter
Z = 15421844
10 Z = 4700578
08
XDOT = 1911
216737 XDOT = 582
538862
YDOT = 22262
404459 feet/sec YDOT = 6785
580879 meter/sec
ZDOT = 9193
910452 ZDOT = 2802
303906
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 16242
47680545
00016717 00000-0 10270-3 0 9089
2 25544 51
6409 52
3290 0003284 270
2009 89
8767 15
54307418 16386
Satellite: ISS
Catalog Number: 25544
Epoch time: 16242
47680545 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 52
3290 deg
Eccentricity:
0003284
Arg of perigee: 270
2009 deg
Mean anomaly: 89
8767 deg
Mean motion: 15
54307418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1638
Checksum: 319
Coasting Arc #10 (Orbit 1652)
---------------------------------------
Vector Time (GMT): 2016/243/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2322055
78 A = 6776959
80 meter
Y = -3576881
54 meter E =
0011341
Z = -5276871
35 I = 51
89429
XDOT = 5692
232818 Wp = 80
29650
YDOT = 5044
435693 meter/sec RA = 46
95697 deg
ZDOT = -914
303034 TA = 180
97813
MA = 180
98035
Ha = 219
479 n
mi
Hp = 215
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7618293
25 X = 2387513
12
Y = -11735175
67 feet Y = -3550549
13 meter
Z = -17312570
04 Z = -5265432
35
XDOT = 18675
304521 XDOT = 5639
842815
YDOT = 16549
985870 feet/sec YDOT = 5107
797059 meter/sec
ZDOT = -2999
681869 ZDOT = -886
779673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13939391
40 X = -4248726
50
Y = 1788414
56 feet Y = 545108
76 meter
Z = -17261887
56 Z = -5261423
33
XDOT = 495
073269 XDOT = 150
898333
YDOT = -23948
257833 feet/sec YDOT = -7299
428988 meter/sec
ZDOT = -2880
310177 ZDOT = -877
918542
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 16243
44120063
00016717 00000-0 10270-3 0 9092
2 25544 51
6396 47
5189 0003191 272
6016 87
4772 15
54352014 16534
Satellite: ISS
Catalog Number: 25544
Epoch time: 16243
44120063 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 47
5189 deg
Eccentricity:
0003191
Arg of perigee: 272
6016 deg
Mean anomaly: 87
4772 deg
Mean motion: 15
54352014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1653
Checksum: 300
Coasting Arc #11 (Orbit 1668)
---------------------------------------
Vector Time (GMT): 2016/244/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3681068
27 A = 6777204
32 meter
Y = 2220387
80 meter E =
0002459
Z = 5239674
90 I = 51
87200
XDOT = -5019
546653 Wp =
22238
YDOT = -5689
943099 meter/sec RA = 41
97168 deg
ZDOT = -1112
825726 TA = 100
42183
MA = 100
39412
Ha = 219
634 n
mi
Hp = 215
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12076995
65 X = -3731075
30
Y = 7284736
87 feet Y = 2178944
48 meter
Z = 17190534
46 Z = 5221671
84
XDOT = -16468
328915 XDOT = -4950
141665
YDOT = -18667
792318 feet/sec YDOT = -5745
687061 meter/sec
ZDOT = -3651
003039 ZDOT = -1137
039954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13545500
46 X = 4128668
54
Y = 4260823
64 feet Y = 1298699
04 meter
Z = 17111414
01 Z = 5215558
99
XDOT = -2702
725294 XDOT = -823
790670
YDOT = 23707
094466 feet/sec YDOT = 7225
922393 meter/sec
ZDOT = -3755
779251 ZDOT = -1144
761516
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 16244
46988598
00016717 00000-0 10270-3 0 9102
2 25544 51
6394 42
3893 0003244 275
3347 84
7436 15
54327233 16692
Satellite: ISS
Catalog Number: 25544
Epoch time: 16244
46988598 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 42
3893 deg
Eccentricity:
0003244
Arg of perigee: 275
3347 deg
Mean anomaly: 84
7436 deg
Mean motion: 15
54327233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1669
Checksum: 338
Coasting Arc #12 (Orbit 1683)
---------------------------------------
Vector Time (GMT): 2016/245/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4891722
04 A = 6779710
78 meter
Y = -859598
06 meter E =
0007025
Z = -4621797
04 I = 51
85611
XDOT = 3878
390882 Wp = 115
29675
YDOT = 5882
144578 meter/sec RA = 36
98741 deg
ZDOT = 3011
537200 TA = 184
68329
MA = 184
68986
Ha = 219
499 n
mi
Hp = 215
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16048956
83 X = 4923421
11
Y = -2820203
61 feet Y = -804718
79 meter
Z = -15163376
12 Z = -4597957
54
XDOT = 12724
379534 XDOT = 3797
698454
YDOT = 19298
374601 feet/sec YDOT = 5925
064476 meter/sec
ZDOT = 9880
371391 ZDOT = 3030
180586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13015328
29 X = -3967072
06
Y = -9963842
00 feet Y = -3036979
04 meter
Z = -15059004
65 Z = -4589984
62
XDOT = 4889
756890 XDOT = 1490
397900
YDOT = -21438
383646 feet/sec YDOT = -6534
419335 meter/sec
ZDOT = 9960
750740 ZDOT = 3036
036825
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 16245
43427283
00016717 00000-0 10270-3 0 9110
2 25544 51
6395 37
5790 0003186 277
7151 82
3640 15
54366876 16843
Satellite: ISS
Catalog Number: 25544
Epoch time: 16245
43427283 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 37
5790 deg
Eccentricity:
0003186
Arg of perigee: 277
7151 deg
Mean anomaly: 82
3640 deg
Mean motion: 15
54366876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1684
Checksum: 327
Coasting Arc #13 (Orbit 1699)
---------------------------------------
Vector Time (GMT): 2016/246/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5813452
42 A = 6783630
11 meter
Y = -425686
94 meter E =
0009163
Z = 3462888
02 I = 51
84361
XDOT = -2319
221955 Wp = 84
65685
YDOT = -5695
949389 meter/sec RA = 32
01224 deg
ZDOT = -4582
431379 TA = 54
83662
MA = 54
75082
Ha = 219
538 n
mi
Hp = 215
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19073006
64 X = -5825081
26
Y = -1396610
71 feet Y = -490761
49 meter
Z = 11361181
16 Z = 3434619
84
XDOT = -7608
995914 XDOT = -2233
096795
YDOT = -18687
497995 feet/sec YDOT = -5721
403455 meter/sec
ZDOT = -15034
223683 ZDOT = -4593
487614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12202645
66 X = 3719366
40
Y = 14819446
71 feet Y = 4516967
36 meter
Z = 11237703
48 Z = 3425252
02
XDOT = -7261
027036 XDOT = -2213
161041
YDOT = 17443
555379 feet/sec YDOT = 5316
795680 meter/sec
ZDOT = -15081
466518 ZDOT = -4596
830995
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 16246
46294542
00016717 00000-0 10270-3 0 9125
2 25544 51
6401 32
4490 0003341 282
8123 77
2657 15
54377087 17007
Satellite: ISS
Catalog Number: 25544
Epoch time: 16246
46294542 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 32
4490 deg
Eccentricity:
0003341
Arg of perigee: 282
8123 deg
Mean anomaly: 77
2657 deg
Mean motion: 15
54377087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1700
Checksum: 296
Coasting Arc #14 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2016/246/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 421215
34 A = 6777490
73 meter
Y = -4418402
62 meter E =
0010931
Z = -5131750
95 I = 51
81589
XDOT = 7026
734682 Wp = 69
89267
YDOT = 2573
854603 meter/sec RA = 30
03325 deg
ZDOT = -1638
481739 TA = 184
31283
MA = 184
32226
Ha = 219
573 n
mi
Hp = 215
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1381940
09 X = 495519
34
Y = -14496071
57 feet Y = -4413277
45 meter
Z = -16836453
23 Z = -5129523
81
XDOT = 23053
591478 XDOT = 7005
389911
YDOT = 8444
404865 feet/sec YDOT = 2652
312718 meter/sec
ZDOT = -5375
596258 ZDOT = -1604
400093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14530726
09 X = 4428965
31
Y = -1122431
56 feet Y = -342117
14 meter
Z = -16825877
50 Z = -5128527
46
XDOT = -4266
521063 XDOT = -1300
435620
YDOT = 23165
158742 feet/sec YDOT = 7060
740385 meter/sec
ZDOT = -5227
121980 ZDOT = -1593
226779
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 16246
84869721
00016717 00000-0 10270-3 0 9135
2 25544 51
6439 30
5286 0003090 286
0825 73
9987 15
54370431 17067
Satellite: ISS
Catalog Number: 25544
Epoch time: 16246
84869721 = yrday
fracday
Element set: 913
Inclination: 51
6439 deg
RA of node: 30
5286 deg
Eccentricity:
0003090
Arg of perigee: 286
0825 deg
Mean anomaly: 73
9987 deg
Mean motion: 15
54370431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1706
Checksum: 326
Coasting Arc #15 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2016/247/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2166087
58 A = 6776649
71 meter
Y = 3605857
84 meter E =
0001979
Z = 5313395
87 I = 51
78310
XDOT = -6805
011105 Wp = 353
08754
YDOT = -3515
365610 meter/sec RA = 25
04238 deg
ZDOT = -386
613812 TA = 100
60243
MA = 100
58014
Ha = 219
738 n
mi
Hp = 215
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7106586
56 X = -2232058
26
Y = 11830242
25 feet Y = 3581266
97 meter
Z = 17432401
15 Z = 5302712
95
XDOT = -22326
151920 XDOT = -6763
317640
YDOT = -11533
351738 feet/sec YDOT = -3591
230728 meter/sec
ZDOT = -1268
418017 ZDOT = -419
568966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13014818
73 X = -3966916
75
Y = -4766790
02 feet Y = -1452917
60 meter
Z = 17385022
88 Z = 5298954
97
XDOT = 6600
286395 XDOT = 2011
767293
YDOT = -23192
566444 feet/sec YDOT = -7069
094252 meter/sec
ZDOT = -1411
775468 ZDOT = -430
309163
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 16247
87736301
00016717 00000-0 10270-3 0 9147
2 25544 51
6422 25
3992 0002964 292
0633 68
0205 15
54389100 17227
Satellite: ISS
Catalog Number: 25544
Epoch time: 16247
87736301 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 25
3992 deg
Eccentricity:
0002964
Arg of perigee: 292
0633 deg
Mean anomaly: 68
0205 deg
Mean motion: 15
54389100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 298
Coasting Arc #16 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2016/248/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3828800
70 A = 6778544
00 meter
Y = -2712893
05 meter E =
0008704
Z = -4899806
62 I = 51
76074
XDOT = 5978
404295 Wp = 103
77772
YDOT = 4166
875822 meter/sec RA = 20
05142 deg
ZDOT = 2366
052438 TA = 189
36645
MA = 189
38269
Ha = 219
686 n
mi
Hp = 215
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12561682
10 X = 3882653
49
Y = -8900567
76 feet Y = -2669776
30 meter
Z = -16075481
03 Z = -4881076
19
XDOT = 19614
187320 XDOT = 5919
871668
YDOT = 13670
852433 feet/sec YDOT = 4233
403345 meter/sec
ZDOT = 7762
639233 ZDOT = 2394
951297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11388344
74 X = 3471167
48
Y = 10486333
77 feet Y = 3196234
53 meter
Z = -15993106
71 Z = -4874698
92
XDOT = -8440
996314 XDOT = -2572
815676
YDOT = 21189
996398 feet/sec YDOT = 6458
710902 meter/sec
ZDOT = 7888
131036 ZDOT = 2404
302340
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 16248
84173075
00016717 00000-0 10270-3 0 9159
2 25544 51
6433 20
5909 0003222 295
6902 64
3918 15
54376176 17375
Satellite: ISS
Catalog Number: 25544
Epoch time: 16248
84173075 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 20
5909 deg
Eccentricity:
0003222
Arg of perigee: 295
6902 deg
Mean anomaly: 64
3918 deg
Mean motion: 15
54376176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1737
Checksum: 318
Coasting Arc #17 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2016/249/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5248420
02 A = 6782078
30 meter
Y = 1777101
63 meter E =
0009115
Z = 3906073
94 I = 51
74161
XDOT = -4600
173222 Wp = 67
55298
YDOT = -4576
606237 meter/sec RA = 15
06576 deg
ZDOT = -4087
870441 TA = 65
24520
MA = 65
15037
Ha = 219
789 n
mi
Hp = 215
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17219225
80 X = -5286875
98
Y = 5830385
91 feet Y = 1718195
68 meter
Z = 12815203
22 Z = 3880484
84
XDOT = -15092
431832 XDOT = -4528
797439
YDOT = -15015
112327 feet/sec YDOT = -4627
649819 meter/sec
ZDOT = -13411
648429 ZDOT = -4110
043064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9640512
23 X = -2938428
13
Y = -15505412
08 feet Y = -4726049
60 meter
Z = 12703042
59 Z = 3871887
38
XDOT = 10048
203316 XDOT = 3062
692371
YDOT = -17343
702366 feet/sec YDOT = -5286
360481 meter/sec
ZDOT = -13507
656299 ZDOT = -4117
133640
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 16249
87038209
00016717 00000-0 10270-3 0 9163
2 25544 51
6424 15
4611 0003202 302
9106 57
1738 15
54434983 17533
Satellite: ISS
Catalog Number: 25544
Epoch time: 16249
87038209 = yrday
fracday
Element set: 916
Inclination: 51
6424 deg
RA of node: 15
4611 deg
Eccentricity:
0003202
Arg of perigee: 302
9106 deg
Mean anomaly: 57
1738 deg
Mean motion: 15
54434983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 300
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