[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 4th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 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
132/13:26:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 213
5
135/07:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 213
1
Coasting Arc #1 (Orbit 3818)
---------------------------------------
Vector Time (GMT): 2016/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3200427
03 A = 6783341
74 meter
Y = -4894661
40 meter E =
0014021
Z = 3425030
34 I = 51
27632
XDOT = 3189
857169 Wp = 90
69731
YDOT = 5285
277919 meter/sec RA = 275
17058 deg
ZDOT = 4556
069982 TA = 309
67626
MA = 309
79983
Ha = 221
034 n
mi
Hp = 213
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10500088
67 X = 3238284
87
Y = -16058600
41 feet Y = -4858660
28 meter
Z = 11236976
18 Z = 3440669
65
XDOT = 10465
410659 XDOT = 3108
386970
YDOT = 17340
150653 feet/sec YDOT = 5320
493686 meter/sec
ZDOT = 14947
736163 ZDOT = 4571
367684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2980257
87 X = -908382
60
Y = -18912889
99 feet Y = -5764648
87 meter
Z = 11305786
04 Z = 3446003
59
XDOT = 17925
483889 XDOT = 5463
687489
YDOT = 6181
858850 feet/sec YDOT = 1884
230577 meter/sec
ZDOT = 15013
191026 ZDOT = 4576
020625
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 16125
55707577
00016717 00000-0 10270-3 0 9005
2 25544 51
6400 275
6799 0001678 91
6122 268
5223 15
54454875 38193
Satellite: ISS
Catalog Number: 25544
Epoch time: 16125
55707577 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 275
6799 deg
Eccentricity:
0001678
Arg of perigee: 91
6122 deg
Mean anomaly: 268
5223 deg
Mean motion: 15
54454875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3819
Checksum: 332
Coasting Arc #2 (Orbit 3833)
---------------------------------------
Vector Time (GMT): 2016/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3697559
82 A = 6779333
04 meter
Y = 3354948
98 meter E =
0011985
Z = -4597747
33 I = 51
26203
XDOT = -2359
185362 Wp = 72
90077
YDOT = -6656
818664 meter/sec RA = 270
15456 deg
ZDOT = -2963
122084 TA = 167
37878
MA = 167
34875
Ha = 221
124 n
mi
Hp = 213
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12131101
78 X = -3712466
53
Y = 11007050
45 feet Y = 3313516
94 meter
Z = -15084472
86 Z = -4615745
83
XDOT = -7740
109454 XDOT = -2270
177933
YDOT = -21839
956246 feet/sec YDOT = -6682
703051 meter/sec
ZDOT = -9721
529146 ZDOT = -2974
366297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1312220
35 X = -399964
76
Y = 16254670
47 feet Y = 4954423
56 meter
Z = -15163240
99 Z = -4621755
85
XDOT = -19313
680317 XDOT = -5886
809760
YDOT = -10663
329506 feet/sec YDOT = -3250
182833 meter/sec
ZDOT = -9769
138464 ZDOT = -2977
633404
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 16126
52141115
00016717 00000-0 10270-3 0 9014
2 25544 51
6410 270
8707 0001788 89
4782 270
6576 15
54457258 38349
Satellite: ISS
Catalog Number: 25544
Epoch time: 16126
52141115 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 270
8707 deg
Eccentricity:
0001788
Arg of perigee: 89
4782 deg
Mean anomaly: 270
6576 deg
Mean motion: 15
54457258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3834
Checksum: 317
Coasting Arc #3 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2016/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4060236
60 A = 6776683
63 meter
Y = -1525659
13 meter E =
0005233
Z = 5202896
91 I = 51
25417
XDOT = 1470
652960 Wp = 113
35670
YDOT = 7458
785611 meter/sec RA = 265
12789 deg
ZDOT = 1036
618801 TA = 326
65138
MA = 326
68434
Ha = 220
921 n
mi
Hp = 213
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13320986
21 X = 4051721
12
Y = -5005443
33 feet Y = -1480302
46 meter
Z = 17069871
74 Z = 5222600
29
XDOT = 4824
976902 XDOT = 1382
102090
YDOT = 24471
081400 feet/sec YDOT = 7474
736315 meter/sec
ZDOT = 3400
980319 ZDOT = 1043
547930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6043772
05 X = 1842141
72
Y = -12768636
82 feet Y = -3891880
50 meter
Z = 17155710
15 Z = 5229060
45
XDOT = 19504
513104 XDOT = 5944
975594
YDOT = 13852
759697 feet/sec YDOT = 4222
321156 meter/sec
ZDOT = 3429
713103 ZDOT = 1045
376554
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 16127
55002544
00016717 00000-0 10270-3 0 9021
2 25544 51
6410 265
7402 0001693 92
5824 267
5523 15
54479914 38509
Satellite: ISS
Catalog Number: 25544
Epoch time: 16127
55002544 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 265
7402 deg
Eccentricity:
0001693
Arg of perigee: 92
5824 deg
Mean anomaly: 267
5523 deg
Mean motion: 15
54479914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3850
Checksum: 304
Coasting Arc #4 (Orbit 3864)
---------------------------------------
Vector Time (GMT): 2016/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4322583
39 A = 6776645
79 meter
Y = -426807
87 meter E =
0016100
Z = -5215738
85 I = 51
25844
XDOT = -487
539063 Wp = 97
82102
YDOT = -7572
575700 meter/sec RA = 260
09871 deg
ZDOT = 1024
296452 TA = 182
05111
MA = 182
05772
Ha = 221
067 n
mi
Hp = 213
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14181704
05 X = -4292153
09
Y = -1400288
27 feet Y = -474975
60 meter
Z = -17112004
12 Z = -5236663
44
XDOT = -1599
537608 XDOT = -407
800094
YDOT = -24844
408463 feet/sec YDOT = -7577
581863 meter/sec
ZDOT = 3360
552663 ZDOT = 1022
121555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10955089
56 X = -3339111
30
Y = 8941590
81 feet Y = 2725396
88 meter
Z = -17202795
94 Z = -5243412
20
XDOT = -18036
151236 XDOT = -5497
418897
YDOT = -15651
345672 feet/sec YDOT = -4770
530161 meter/sec
ZDOT = 3352
478968 ZDOT = 1021
835590
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 16128
51434377
00016717 00000-0 10270-3 0 9032
2 25544 51
6416 260
9319 0001764 96
8588 263
2766 15
54491937 38659
Satellite: ISS
Catalog Number: 25544
Epoch time: 16128
51434377 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 260
9319 deg
Eccentricity:
0001764
Arg of perigee: 96
8588 deg
Mean anomaly: 263
2766 deg
Mean motion: 15
54491937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3865
Checksum: 345
Coasting Arc #5 (Orbit 3880)
---------------------------------------
Vector Time (GMT): 2016/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4420431
91 A = 6779297
71 meter
Y = 2312838
82 meter E =
0009964
Z = 4583532
87 I = 51
27456
XDOT = -591
687879 Wp = 71
31977
YDOT = 7047
162534 meter/sec RA = 255
07199 deg
ZDOT = -2976
883443 TA = 48
54455
MA = 48
45902
Ha = 220
996 n
mi
Hp = 213
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14502729
36 X = 4371975
39
Y = 7588053
89 feet Y = 2361999
89 meter
Z = 15037837
49 Z = 4604889
02
XDOT = -1941
233199 XDOT = -655
986352
YDOT = 23120
611988 feet/sec YDOT = 7040
186508 meter/sec
ZDOT = -9766
677961 ZDOT = -2979
913622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15475562
62 X = 4716951
49
Y = -5062523
88 feet Y = -1543057
28 meter
Z = 15130171
52 Z = 4611676
28
XDOT = 14925
485348 XDOT = 4549
287934
YDOT = 16310
617789 feet/sec YDOT = 4971
476302 meter/sec
ZDOT = -9781
107688 ZDOT = -2981
281623
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 16129
54293949
00016717 00000-0 10270-3 0 9045
2 25544 51
6426 255
8011 0001827 99
2241 260
9119 15
54470518 38811
Satellite: ISS
Catalog Number: 25544
Epoch time: 16129
54293949 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 255
8011 deg
Eccentricity:
0001827
Arg of perigee: 99
2241 deg
Mean anomaly: 260
9119 deg
Mean motion: 15
54470518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3881
Checksum: 320
Coasting Arc #6 (Orbit 3895)
---------------------------------------
Vector Time (GMT): 2016/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4345417
67 A = 6783208
50 meter
Y = -3928836
43 meter E =
0006637
Z = -3425725
28 I = 51
29697
XDOT = 1746
539910 Wp = 93
26540
YDOT = -5903
145990 meter/sec RA = 250
05761 deg
ZDOT = 4561
973190 TA = 226
43013
MA = 226
48526
Ha = 221
011 n
mi
Hp = 213
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14256619
65 X = -4284520
55
Y = -12889883
31 feet Y = -3977089
09 meter
Z = -11239256
16 Z = -3446686
84
XDOT = 5730
117815 XDOT = 1790
260146
YDOT = -19367
276870 feet/sec YDOT = -5883
370827 meter/sec
ZDOT = 14967
103643 ZDOT = 4570
563417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19104495
31 X = -5823050
17
Y = 1542604
09 feet Y = 470185
73 meter
Z = -11329598
67 Z = -3453261
68
XDOT = -10173
005336 XDOT = -3100
732026
YDOT = -15955
777352 feet/sec YDOT = -4863
320937 meter/sec
ZDOT = 15005
471354 ZDOT = 4573
667669
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 16130
50723514
00016717 00000-0 10270-3 0 9050
2 25544 51
6425 250
9927 0001684 97
0628 263
0717 15
54494649 38963
Satellite: ISS
Catalog Number: 25544
Epoch time: 16130
50723514 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 250
9927 deg
Eccentricity:
0001684
Arg of perigee: 97
0628 deg
Mean anomaly: 263
0717 deg
Mean motion: 15
54494649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3896
Checksum: 327
Coasting Arc #7 (Orbit 3911)
---------------------------------------
Vector Time (GMT): 2016/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4004341
90 A = 6786763
52 meter
Y = 5159954
67 meter E =
0015704
Z = 1816937
29 I = 51
32021
XDOT = -2967
182512 Wp = 113
07394
YDOT = 4294
087407 meter/sec RA = 245
05501 deg
ZDOT = -5622
736180 TA = 46
84734
MA = 46
71616
Ha = 220
979 n
mi
Hp = 213
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13137604
66 X = 3937518
40
Y = 16928985
15 feet Y = 5204360
15 meter
Z = 5961080
35 Z = 1836227
56
XDOT = -9734
850762 XDOT = -2987
666445
YDOT = 14088
213277 feet/sec YDOT = 4260
792193 meter/sec
ZDOT = -18447
297177 ZDOT = -5637
199656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21342282
08 X = 6505127
58
Y = 1642930
68 feet Y = 500765
27 meter
Z = 6043959
60 Z = 1842198
89
XDOT = 4115
551695 XDOT = 1254
420157
YDOT = 15024
676347 feet/sec YDOT = 4579
521351 meter/sec
ZDOT = -18510
887263 ZDOT = -5642
118438
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 16131
53580776
00016717 00000-0 10270-3 0 9066
2 25544 51
6418 245
8626 0001763 105
6797 254
4551 15
54517237 39123
Satellite: ISS
Catalog Number: 25544
Epoch time: 16131
53580776 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 245
8626 deg
Eccentricity:
0001763
Arg of perigee: 105
6797 deg
Mean anomaly: 254
4551 deg
Mean motion: 15
54517237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3912
Checksum: 323
Coasting Arc #8 (Orbit 3926)
---------------------------------------
Vector Time (GMT): 2016/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3399084
35 A = 6788119
81 meter
Y = -5869421
19 meter E =
0013073
Z = -20242
22 I = 51
34052
XDOT = 4140
805687 Wp = 51
75809
YDOT = -2409
546249 meter/sec RA = 240
06091 deg
ZDOT = 5988
565849 TA = 308
02293
MA = 308
14088
Ha = 220
951 n
mi
Hp = 213
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11151851
54 X = -3333100
06
Y = -19256631
21 feet Y = -5907063
07 meter
Z = -66411
50 Z = -36594
26
XDOT = 13585
320496 XDOT = 4138
352016
YDOT = -7905
335463 feet/sec YDOT = -2363
255022 meter/sec
ZDOT = 19647
525750 ZDOT = 6008
674902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21838146
67 X = -6656267
10
Y = -4273498
44 feet Y = -1302562
32 meter
Z = -136418
67 Z = -41580
41
XDOT = 2592
388827 XDOT = 790
160114
YDOT = -13742
619480 feet/sec YDOT = -4188
750417 meter/sec
ZDOT = 19735
310109 ZDOT = 6015
322521
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 16132
50008290
00016717 00000-0 10270-3 0 9071
2 25544 51
6430 241
0533 0001731 101
5264 258
6084 15
54543881 39278
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
50008290 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 241
0533 deg
Eccentricity:
0001731
Arg of perigee: 101
5264 deg
Mean anomaly: 258
6084 deg
Mean motion: 15
54543881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3927
Checksum: 283
Coasting Arc #9 (Orbit 3927)
---------------------------------------
Vector Time (GMT): 2016/132/13:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4669916
63 A = 6785874
69 meter
Y = -4351618
69 meter E =
0006792
Z = -2300827
09 I = 51
33367
XDOT = 2052
327495 Wp = 55
48497
YDOT = -5045
687692 meter/sec RA = 239
74329 deg
ZDOT = 5392
677698 TA = 278
77459
MA = 278
85151
Ha = 220
894 n
mi
Hp = 213
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15321248
80 X = -4609732
17
Y = -14276964
20 feet Y = -4403504
18 meter
Z = -7548645
30 Z = -2323366
55
XDOT = 6733
357923 XDOT = 2082
401628
YDOT = -16554
093478 feet/sec YDOT = -5022
569310 meter/sec
ZDOT = 17692
512132 ZDOT = 5402
720257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18571473
11 X = -5660585
01
Y = 9601902
64 feet Y = 2926659
93 meter
Z = -7645800
77 Z = -2330440
07
XDOT = -12675
225638 XDOT = -3863
408774
YDOT = -10431
222833 feet/sec YDOT = -3179
436719 meter/sec
ZDOT = 17737
027256 ZDOT = 5406
245908
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 16132
56436680
00016717 00000-0 10270-3 0 9086
2 25544 51
6428 240
7341 0001506 97
5082 262
6242 15
54522903 39284
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
56436680 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 240
7341 deg
Eccentricity:
0001506
Arg of perigee: 97
5082 deg
Mean anomaly: 262
6242 deg
Mean motion: 15
54522903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3928
Checksum: 304
Coasting Arc #10 (Orbit 3943)
---------------------------------------
Vector Time (GMT): 2016/133/13:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4220226
97 A = 6787961
94 meter
Y = 5285006
95 meter E =
0014509
Z = 495424
78 I = 51
35709
XDOT = -3475
221395 Wp = 126
53858
YDOT = 3344
768885 meter/sec RA = 234
74918 deg
ZDOT = -5964
152346 TA = 48
09435
MA = 47
97069
Ha = 220
921 n
mi
Hp = 213
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13845889
00 X = 4158408
47
Y = 17339261
65 feet Y = 5331854
67 meter
Z = 1625409
40 Z = 515775
73
XDOT = -11401
644998 XDOT = -3483
393730
YDOT = 10973
651196 feet/sec YDOT = 3305
861163 meter/sec
ZDOT = -19567
428956 ZDOT = -5981
053915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20846890
67 X = 6354132
28
Y = -7581139
55 feet Y = -2310731
34 meter
Z = 1712911
29 Z = 522095
36
XDOT = 6248
984323 XDOT = 1904
690422
YDOT = 12666
146651 feet/sec YDOT = 3860
641499 meter/sec
ZDOT = -19641
444604 ZDOT = -5986
712315
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 16133
59291549
00016717 00000-0 10270-3 0 9094
2 25544 51
6420 235
6040 0001691 101
7776 258
3567 15
54559884 39446
Satellite: ISS
Catalog Number: 25544
Epoch time: 16133
59291549 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 235
6040 deg
Eccentricity:
0001691
Arg of perigee: 101
7776 deg
Mean anomaly: 258
3567 deg
Mean motion: 15
54559884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3944
Checksum: 334
Coasting Arc #11 (Orbit 3959)
---------------------------------------
Vector Time (GMT): 2016/134/13:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3423870
87 A = 6787319
80 meter
Y = -5698175
64 meter E =
0015086
Z = 1336111
27 I = 51
37401
XDOT = 4791
290974 Wp = 64
07147
YDOT = -1509
139685 meter/sec RA = 229
75805 deg
ZDOT = 5797
302560 TA = 310
53774
MA = 310
66903
Ha = 220
908 n
mi
Hp = 213
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11233172
13 X = -3366388
25
Y = -18694801
98 feet Y = -5736142
27 meter
Z = 4383567
17 Z = 1319618
39
XDOT = 15719
458576 XDOT = 4779
649524
YDOT = -4951
245685 feet/sec YDOT = -1455
625495 meter/sec
ZDOT = 19020
021523 ZDOT = 5820
549253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21225836
28 X = -6469634
90
Y = 5075268
71 feet Y = 1546941
90 meter
Z = 4312883
04 Z = 1314566
75
XDOT = 372
999491 XDOT = 113
690245
YDOT = -14815
365014 feet/sec YDOT = -4515
723256 meter/sec
ZDOT = 19121
293006 ZDOT = 5828
170108
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 16134
62145309
00016717 00000-0 10270-3 0 9103
2 25544 51
6418 230
4736 0001674 101
5870 258
5471 15
54569157 39600
Satellite: ISS
Catalog Number: 25544
Epoch time: 16134
62145309 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 230
4736 deg
Eccentricity:
0001674
Arg of perigee: 101
5870 deg
Mean anomaly: 258
5471 deg
Mean motion: 15
54569157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3960
Checksum: 307
Coasting Arc #12 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2016/135/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3692751
09 A = 6776211
22 meter
Y = 2216119
63 meter E =
0016361
Z = -5245932
65 I = 51
35110
XDOT = -4774
457135 Wp = 97
74030
YDOT = -5924
469208 meter/sec RA = 225
95989 deg
ZDOT = 858
247341 TA = 180
51027
MA = 180
51194
Ha = 220
917 n
mi
Hp = 213
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12115325
08 X = -3691775
22
Y = 7270733
70 feet Y = 2174830
35 meter
Z = -17211065
13 Z = -5263868
81
XDOT = -15664
229444 XDOT = -4712
022409
YDOT = -19437
234936 feet/sec YDOT = -5977
511283 meter/sec
ZDOT = 2815
772117 ZDOT = 835
205669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13501831
06 X = -4115358
11
Y = 3826635
52 feet Y = 1166358
51 meter
Z = -17289385
53 Z = -5269804
71
XDOT = -9689
011355 XDOT = -2953
210661
YDOT = -21914
348618 feet/sec YDOT = -6679
493459 meter/sec
ZDOT = 2716
657222 ZDOT = 828
037121
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 16135
32856668
00016717 00000-0 10270-3 0 9119
2 25544 51
6396 226
9442 0001859 105
4885 254
6474 15
54600814 39711
Satellite: ISS
Catalog Number: 25544
Epoch time: 16135
32856668 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 226
9442 deg
Eccentricity:
0001859
Arg of perigee: 105
4885 deg
Mean anomaly: 254
6474 deg
Mean motion: 15
54600814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 334
Coasting Arc #13 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2016/136/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4883760
60 A = 6778726
13 meter
Y = -676323
21 meter E =
0009514
Z = 4645666
51 I = 51
38216
XDOT = 3587
818902 Wp = 72
28428
YDOT = 6146
057136 meter/sec RA = 220
93805 deg
ZDOT = -2869
247645 TA = 46
34789
MA = 46
26904
Ha = 220
833 n
mi
Hp = 213
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16022836
60 X = 4868393
62
Y = -2218908
17 feet Y = -621795
70 meter
Z = 15241688
01 Z = 4669353
45
XDOT = 11771
059391 XDOT = 3532
763174
YDOT = 20164
229448 feet/sec YDOT = 6185
870696 meter/sec
ZDOT = -9413
542141 ZDOT = -2851
952475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15975932
39 X = 4869464
19
Y = 1808963
18 feet Y = 551371
98 meter
Z = 15344742
95 Z = 4677077
65
XDOT = 6582
050050 XDOT = 2006
208855
YDOT = 21305
879620 feet/sec YDOT = 6494
032108 meter/sec
ZDOT = -9339
421546 ZDOT = -2846
655687
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 16136
35708658
00016717 00000-0 10270-3 0 9129
2 25544 51
6394 221
8122 0001921 108
3839 251
7523 15
54577632 39870
Satellite: ISS
Catalog Number: 25544
Epoch time: 16136
35708658 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 221
8122 deg
Eccentricity:
0001921
Arg of perigee: 108
3839 deg
Mean anomaly: 251
7523 deg
Mean motion: 15
54577632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3987
Checksum: 323
Coasting Arc #14 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2016/137/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5771887
52 A = 6782630
96 meter
Y = -743989
76 meter E =
0006968
Z = -3490753
99 I = 51
42126
XDOT = -1968
095691 Wp = 99
37942
YDOT = -5871
261922 meter/sec RA = 215
93027 deg
ZDOT = 4512
157676 TA = 219
47389
MA = 219
52468
Ha = 220
858 n
mi
Hp = 213
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18936638
84 X = -5746182
30
Y = -2440911
28 feet Y = -808391
10 meter
Z = -11452604
95 Z = -3518730
23
XDOT = -6457
006859 XDOT = -1924
213845
YDOT = -19262
670347 feet/sec YDOT = -5893
025141 meter/sec
ZDOT = 14803
666916 ZDOT = 4502
703617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17782826
03 X = -5420205
37
Y = -6747479
63 feet Y = -2056631
79 meter
Z = -11574070
84 Z = -3527776
79
XDOT = -2401
359480 XDOT = -731
934370
YDOT = -18958
713124 feet/sec YDOT = -5778
615760 meter/sec
ZDOT = 14763
566216 ZDOT = 4499
934983
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 16137
32131455
00016717 00000-0 10270-3 0 9133
2 25544 51
6402 217
0030 0001874 110
5063 249
6292 15
54617627 40023
Satellite: ISS
Catalog Number: 25544
Epoch time: 16137
32131455 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 217
0030 deg
Eccentricity:
0001874
Arg of perigee: 110
5063 deg
Mean anomaly: 249
6292 deg
Mean motion: 15
54617627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4002
Checksum: 270
Coasting Arc #15 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2016/138/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6206723
32 A = 6786349
10 meter
Y = 1990126
31 meter E =
0015733
Z = 1862573
14 I = 51
46008
XDOT = 18
814497 Wp = 113
77097
YDOT = 5227
035396 meter/sec RA = 210
93545 deg
ZDOT = -5616
302575 TA = 45
66348
MA = 45
53464
Ha = 220
771 n
mi
Hp = 213
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20363265
48 X = 6174960
23
Y = 6529285
81 feet Y = 2059356
41 meter
Z = 6110804
25 Z = 1892647
12
XDOT = 61
727354 XDOT = -12
354973
YDOT = 17149
066260 feet/sec YDOT = 5227
071566 meter/sec
ZDOT = -18426
189550 ZDOT = -5616
286837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18444122
94 X = 5621768
67
Y = 10746997
50 feet Y = 3275684
84 meter
Z = 6241190
32 Z = 1902314
81
XDOT = -2727
109952 XDOT = -831
223114
YDOT = 15440
111264 feet/sec YDOT = 4706
145913 meter/sec
ZDOT = -18426
997404 ZDOT = -5616
548809
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 16138
34981742
00016717 00000-0 10270-3 0 9149
2 25544 51
6400 211
8718 0001779 116
3505 243
7831 15
54626937 40180
Satellite: ISS
Catalog Number: 25544
Epoch time: 16138
34981742 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 211
8718 deg
Eccentricity:
0001779
Arg of perigee: 116
3505 deg
Mean anomaly: 243
7831 deg
Mean motion: 15
54626937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4018
Checksum: 313
Coasting Arc #16 (Orbit 4032)
---------------------------------------
Vector Time (GMT): 2016/139/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6110252
20 A = 6787822
56 meter
Y = -2944221
37 meter E =
0012695
Z = -33345
88 I = 51
49482
XDOT = 2053
037114 Wp = 53
05011
YDOT = -4310
718696 meter/sec RA = 205
95117 deg
ZDOT = 6001
225716 TA = 306
58993
MA = 306
70667
Ha = 220
780 n
mi
Hp = 213
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20046759
17 X = -6076713
06
Y = -9659518
92 feet Y = -3012362
74 meter
Z = -109402
48 Z = -62947
02
XDOT = 6735
686069 XDOT = 2071
936222
YDOT = -14142
777875 feet/sec YDOT = -4287
654712 meter/sec
ZDOT = 19689
060748 ZDOT = 6011
244840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17733657
21 X = -5405218
72
Y = -13440676
41 feet Y = -4096718
17 meter
Z = -237586
55 Z = -72416
38
XDOT = 8300
088587 XDOT = 2529
867001
YDOT = -11257
545234 feet/sec YDOT = -3431
299787 meter/sec
ZDOT = 19733
334697 ZDOT = 6014
720416
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 16139
31403110
00016717 00000-0 10270-3 0 9156
2 25544 51
6417 207
0620 0001806 115
2861 244
8480 15
54645538 40338
Satellite: ISS
Catalog Number: 25544
Epoch time: 16139
31403110 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 207
0620 deg
Eccentricity:
0001806
Arg of perigee: 115
2861 deg
Mean anomaly: 244
8480 deg
Mean motion: 15
54645538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4033
Checksum: 278
Coasting Arc #17 (Orbit 4048)
---------------------------------------
Vector Time (GMT): 2016/140/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5414592
29 A = 6786369
84 meter
Y = 3646104
99 meter E =
0009010
Z = -1845386
33 I = 51
51853
XDOT = -4083
955989 Wp = 137
13662
YDOT = 3227
084273 meter/sec RA = 200
96941 deg
ZDOT = -5629
433720 TA = 63
19863
MA = 63
10650
Ha = 220
792 n
mi
Hp = 213
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17764410
39 X = 5382382
46
Y = 11962286
71 feet Y = 3706474
53 meter
Z = -6054417
10 Z = -1819161
23
XDOT = -13398
805737 XDOT = -4092
392662
YDOT = 10587
546827 feet/sec YDOT = 3181
367771 meter/sec
ZDOT = -18469
270734 ZDOT = -5649
293304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15339405
97 X = 4675450
94
Y = 14991114
80 feet Y = 4569291
79 meter
Z = -5941014
05 Z = -1810821
08
XDOT = -13885
529266 XDOT = -4232
309320
YDOT = 6884
310410 feet/sec YDOT = 2098
337813 meter/sec
ZDOT = -18556
148386 ZDOT = -5655
914028
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 16140
34251866
00016717 00000-0 10270-3 0 9161
2 25544 51
6409 201
9315 0001810 117
3825 242
7513 15
54666808 40495
Satellite: ISS
Catalog Number: 25544
Epoch time: 16140
34251866 = yrday
fracday
Element set: 916
Inclination: 51
6409 deg
RA of node: 201
9315 deg
Eccentricity:
0001810
Arg of perigee: 117
3825 deg
Mean anomaly: 242
7513 deg
Mean motion: 15
54666808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4049
Checksum: 300
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