[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 19th 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) : 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
233/21:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 212
9
237/07:36:05
457 1
3 4
0 4
0
N/A 3
8 -0
4 219
8
000/00:12:06
914 0
1 -0
0 215
5
239/10:11:00
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
Coasting Arc #1 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2016/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3646581
17 A = 6775339
41 meter
Y = 2431179
51 meter E =
0014704
Z = -5179974
03 I = 51
98794
XDOT = -2583
166708 Wp = 104
73106
YDOT = 7054
012006 meter/sec RA = 101
18100 deg
ZDOT = 1492
148309 TA = 179
58607
MA = 179
58486
Ha = 219
822 n
mi
Hp = 213
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11963848
98 X = 3644285
70
Y = 7976310
71 feet Y = 2471944
85 meter
Z = -16994665
47 Z = -5162265
92
XDOT = -8474
956392 XDOT = -2669
102552
YDOT = 23143
084009 feet/sec YDOT = 7024
644906 meter/sec
ZDOT = 4895
499701 ZDOT = 1479
390991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5878105
47 X = -1791646
55
Y = -13221724
07 feet Y = -4029981
50 meter
Z = -16917675
90 Z = -5156507
62
XDOT = 18667
380067 XDOT = 5689
817444
YDOT = -14490
648528 feet/sec YDOT = -4416
749671 meter/sec
ZDOT = 4838
523757 ZDOT = 1474
782041
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 16232
51354799
00016717 00000-0 10270-3 0 9004
2 25544 51
6431 102
0399 0001275 144
7815 215
3422 15
55069242 14835
Satellite: ISS
Catalog Number: 25544
Epoch time: 16232
51354799 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 102
0399 deg
Eccentricity:
0001275
Arg of perigee: 144
7815 deg
Mean anomaly: 215
3422 deg
Mean motion: 15
55069242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1483
Checksum: 293
Coasting Arc #2 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2016/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2909015
46 A = 6778673
93 meter
Y = -4347929
94 meter E =
0010183
Z = 4303542
81 I = 52
00500
XDOT = 3444
512072 Wp = 78
63080
YDOT = -5851
591689 meter/sec RA = 96
20168 deg
ZDOT = -3574
516044 TA = 47
64737
MA = 47
56118
Ha = 219
782 n
mi
Hp = 212
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9544013
96 X = -2881084
05
Y = -14264862
02 feet Y = -4380304
00 meter
Z = 14119234
95 Z = 4289479
92
XDOT = 11300
892625 XDOT = 3527
053254
YDOT = -19198
135463 feet/sec YDOT = -5812
611605 meter/sec
ZDOT = -11727
414844 ZDOT = -3557
582794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 732602
25 X = 223297
16
Y = 17197348
75 feet Y = 5241751
90 meter
Z = 14058512
60 Z = 4285034
64
XDOT = -18495
671985 XDOT = -5637
480821
YDOT = 10337
982240 feet/sec YDOT = 3151
016987 meter/sec
ZDOT = -11652
382370 ZDOT = -3551
646146
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 16233
54176398
00016717 00000-0 10270-3 0 9016
2 25544 51
6433 96
9068 0001062 147
9082 212
2136 15
55109240 14994
Satellite: ISS
Catalog Number: 25544
Epoch time: 16233
54176398 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 96
9068 deg
Eccentricity:
0001062
Arg of perigee: 147
9082 deg
Mean anomaly: 212
2136 deg
Mean motion: 15
55109240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1499
Checksum: 304
Coasting Arc #3 (Orbit 1504)
---------------------------------------
Vector Time (GMT): 2016/233/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3861104
79 A = 6775399
50 meter
Y = -2146003
72 meter E =
0004917
Z = 5133685
90 I = 51
99536
XDOT = 1840
528552 Wp = 72
80868
YDOT = -7264
308837 meter/sec RA = 94
31249 deg
ZDOT = -1649
659347 TA = 33
04005
MA = 33
00933
Ha = 219
892 n
mi
Hp = 212
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12667666
62 X = -3861757
57
Y = -7040694
62 feet Y = -2189184
43 meter
Z = 16842801
51 Z = 5114928
45
XDOT = 6038
479500 XDOT = 1929
636332
YDOT = -23833
034242 feet/sec YDOT = -7243
228712 meter/sec
ZDOT = -5412
268200 ZDOT = -1640
501642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3176181
08 X = 968099
99
Y = -14237131
38 feet Y = -4339477
65 meter
Z = 16761177
90 Z = 5108807
02
XDOT = 23542
281505 XDOT = 7175
687403
YDOT = -1081
626847 feet/sec YDOT = -329
679863 meter/sec
ZDOT = -5370
976992 ZDOT = -1637
073787
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 16233
92734445
00016717 00000-0 10270-3 0 9022
2 25544 51
6434 94
9789 0001546 157
8245 202
2975 15
55101750 15057
Satellite: ISS
Catalog Number: 25544
Epoch time: 16233
92734445 = yrday
fracday
Element set: 902
Inclination: 51
6434 deg
RA of node: 94
9789 deg
Eccentricity:
0001546
Arg of perigee: 157
8245 deg
Mean anomaly: 202
2975 deg
Mean motion: 15
55101750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1505
Checksum: 313
Coasting Arc #4 (Orbit 1519)
---------------------------------------
Vector Time (GMT): 2016/234/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3352117
55 A = 6779009
80 meter
Y = 4111624
30 meter E =
0009166
Z = -4230346
81 I = 52
00759
XDOT = -2814
650054 Wp = 117
72076
YDOT = 6093
171815 meter/sec RA = 89
33549 deg
ZDOT = 3693
803108 TA = 189
98921
MA = 190
00745
Ha = 219
788 n
mi
Hp = 212
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10997761
00 X = 3326440
22
Y = 13489581
02 feet Y = 4148966
01 meter
Z = -13879090
60 Z = -4214125
90
XDOT = -9234
416189 XDOT = -2900
519003
YDOT = 19990
721178 feet/sec YDOT = 6061
216684 meter/sec
ZDOT = 12118
776600 ZDOT = 3679
921320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9590686
22 X = -2923241
16
Y = 14590464
32 feet Y = 4447173
52 meter
Z = -13808902
48 Z = -4208953
48
XDOT = -20790
814780 XDOT = -6337
040345
YDOT = -2261
265885 feet/sec YDOT = -689
233842 meter/sec
ZDOT = 12057
026933 ZDOT = 3674
981809
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 16234
89129349
00016717 00000-0 10270-3 0 9031
2 25544 51
6421 90
1679 0001680 158
0827 202
0398 15
55096170 15200
Satellite: ISS
Catalog Number: 25544
Epoch time: 16234
89129349 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 90
1679 deg
Eccentricity:
0001680
Arg of perigee: 158
0827 deg
Mean anomaly: 202
0398 deg
Mean motion: 15
55096170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1520
Checksum: 305
Coasting Arc #5 (Orbit 1535)
---------------------------------------
Vector Time (GMT): 2016/235/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2662615
07 A = 6783500
84 meter
Y = -5621752
68 meter E =
0014370
Z = 2687905
96 I = 52
02179
XDOT = 3679
254011 Wp = 107
21278
YDOT = -4249
347677 meter/sec RA = 84
37119 deg
ZDOT = -5224
083779 TA = 42
57385
MA = 42
46254
Ha = 219
774 n
mi
Hp = 212
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8735613
75 X = -2612609
94
Y = -18444070
46 feet Y = -5651248
03 meter
Z = 8818589
09 Z = 2675093
56
XDOT = 12071
043342 XDOT = 3751
874058
YDOT = -13941
429387 feet/sec YDOT = -4207
798123 meter/sec
ZDOT = -17139
382477 ZDOT = -5206
034296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14762625
54 X = 4499648
27
Y = -14125396
01 feet Y = -4305420
70 meter
Z = 8763576
38 Z = 2671138
08
XDOT = 16026
143286 XDOT = 4884
768474
YDOT = 6126
565249 feet/sec YDOT = 1867
377088 meter/sec
ZDOT = -17059
728018 ZDOT = -5199
805100
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
91949970
00016717 00000-0 10270-3 0 9046
2 25544 51
6427 85
0350 0001506 162
0483 198
0723 15
55092441 15365
Satellite: ISS
Catalog Number: 25544
Epoch time: 16235
91949970 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 85
0350 deg
Eccentricity:
0001506
Arg of perigee: 162
0483 deg
Mean anomaly: 198
0723 deg
Mean motion: 15
55092441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1536
Checksum: 305
Coasting Arc #6 (Orbit 1550)
---------------------------------------
Vector Time (GMT): 2016/236/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1833059
36 A = 6786416
50 meter
Y = 6483008
29 meter E =
0009731
Z = -783375
84 I = 52
02703
XDOT = -4383
236646 Wp = 45
93852
YDOT = 1955
646979 meter/sec RA = 79
41900 deg
ZDOT = 5980
339881 TA = 305
63642
MA = 305
72701
Ha = 219
758 n
mi
Hp = 213
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6013974
28 X = 1764233
77
Y = 21269712
24 feet Y = 6503121
92 meter
Z = -2570130
70 Z = -774638
85
XDOT = -14380
697658 XDOT = -4433
829228
YDOT = 6416
164628 feet/sec YDOT = 1906
348147 meter/sec
ZDOT = 19620
537666 ZDOT = 5958
924300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18095765
92 X = -5515589
45
Y = 12700424
36 feet Y = 3871089
35 meter
Z = -2533099
70 Z = -772088
79
XDOT = -9912
518846 XDOT = -3021
335744
YDOT = -10263
782207 feet/sec YDOT = -3128
400817 meter/sec
ZDOT = 19526
569620 ZDOT = 5951
698420
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
88343812
00016717 00000-0 10270-3 0 9057
2 25544 51
6427 80
2230 0001263 162
7959 197
3237 15
55042564 15514
Satellite: ISS
Catalog Number: 25544
Epoch time: 16236
88343812 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 80
2230 deg
Eccentricity:
0001263
Arg of perigee: 162
7959 deg
Mean anomaly: 197
3237 deg
Mean motion: 15
55042564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1551
Checksum: 305
Coasting Arc #7 (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 = 4341920
36 A = 6778372
21 meter
Y = 1495699
79 meter E =
0010305
Z = -4995122
11 I = 51
99089
XDOT = -57
156357 Wp = 116
36578
YDOT = 7352
219412 meter/sec RA = 77
22949 deg
ZDOT = 2150
782200 TA = 174
51510
MA = 174
50380
Ha = 219
787 n
mi
Hp = 215
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14245145
53 X = 4349136
43
Y = 4907151
54 feet Y = 1544294
15 meter
Z = -16388195
90 Z = -4974012
77
XDOT = -187
520855 XDOT = -149
814027
YDOT = 24121
454764 feet/sec YDOT = 7351
062275 meter/sec
ZDOT = 7056
372046 ZDOT = 2150
279142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5476851
77 X = 1669344
42
Y = -14142689
85 feet Y = -4310691
87 meter
Z = -16296186
39 Z = -4967077
61
XDOT = 23062
065892 XDOT = 7029
317684
YDOT = 800
260362 feet/sec YDOT = 243
919358 meter/sec
ZDOT = 7052
847525 ZDOT = 2149
707926
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
33327771
00016717 00000-0 10270-3 0 9065
2 25544 51
6433 77
9781 0003027 246
7440 113
3394 15
54304663 15582
Satellite: ISS
Catalog Number: 25544
Epoch time: 16237
33327771 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 77
9781 deg
Eccentricity:
0003027
Arg of perigee: 246
7440 deg
Mean anomaly: 113
3394 deg
Mean motion: 15
54304663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1558
Checksum: 311
Coasting Arc #8 (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 = -4371113
60 A = 6781823
47 meter
Y = -3185776
40 meter E =
0007685
Z = 4085513
64 I = 51
99405
XDOT = 1106
954516 Wp = 80
57287
YDOT = -6517
246525 meter/sec RA = 72
26096 deg
ZDOT = -3890
205634 TA = 49
52662
MA = 49
45966
Ha = 219
861 n
mi
Hp = 215
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14340923
88 X = -4355010
14
Y = -10452022
30 feet Y = -3234566
94 meter
Z = 13403916
15 Z = 4064319
18
XDOT = 3631
740538 XDOT = 1198
646602
YDOT = -21382
042405 feet/sec YDOT = -6504
355265 meter/sec
ZDOT = -12763
141844 ZDOT = -3884
605432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10778204
16 X = -3285196
63
Y = 14184391
13 feet Y = 4323402
42 meter
Z = 13311844
33 Z = 4057450
15
XDOT = -20258
260947 XDOT = -6174
717937
YDOT = -3416
533765 feet/sec YDOT = -1041
359491 meter/sec
ZDOT = -12737
471279 ZDOT = -3882
381246
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
36199413
00016717 00000-0 10270-3 0 9070
2 25544 51
6430 72
8499 0003040 250
1612 109
9214 15
54306850 15744
Satellite: ISS
Catalog Number: 25544
Epoch time: 16238
36199413 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 72
8499 deg
Eccentricity:
0003040
Arg of perigee: 250
1612 deg
Mean anomaly: 109
9214 deg
Mean motion: 15
54306850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1574
Checksum: 298
Coasting Arc #9 (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 = 4221701
80 A = 6785621
46 meter
Y = 4552443
99 meter E =
0002131
Z = -2736201
36 I = 51
99761
XDOT = -2227
478472 Wp = 27
40221
YDOT = 5182
765835 meter/sec RA = 67
30072 deg
ZDOT = 5189
646682 TA = 301
81485
MA = 301
83560
Ha = 219
613 n
mi
Hp = 215
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13850727
71 X = 4183772
64
Y = 14935839
86 feet Y = 4599441
75 meter
Z = -8977038
58 Z = -2715785
78
XDOT = -7308
000235 XDOT = -2310
476797
YDOT = 17003
824917 feet/sec YDOT = 5157
392731 meter/sec
ZDOT = 17026
399875 ZDOT = 5178
624519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15013813
95 X = 4576210
49
Y = -13823417
84 feet Y = -4213377
76 meter
Z = -8888627
69 Z = -2709253
72
XDOT = 15954
915250 XDOT = 4863
058168
YDOT = 6419
610332 feet/sec YDOT = 1956
697229 meter/sec
ZDOT = 16977
259281 ZDOT = 5174
668629
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
32640980
00016717 00000-0 10270-3 0 9088
2 25544 51
6443 68
0406 0003171 255
2644 104
8157 15
54332393 15896
Satellite: ISS
Catalog Number: 25544
Epoch time: 16239
32640980 = yrday
fracday
Element set: 908
Inclination: 51
6443 deg
RA of node: 68
0406 deg
Eccentricity:
0003171
Arg of perigee: 255
2644 deg
Mean anomaly: 104
8157 deg
Mean motion: 15
54332393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1589
Checksum: 308
Coasting Arc #10 (Orbit 1590)
---------------------------------------
Vector Time (GMT): 2016/239/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2102175
23 A = 6788607
44 meter
Y = -6404840
06 meter E =
0009428
Z = -753937
54 I = 52
00499
XDOT = 4721
067323 Wp = 158
64518
YDOT = -848
944872 meter/sec RA = 66
81721 deg
ZDOT = -5983
597122 TA = 29
46299
MA = 29
40988
Ha = 219
609 n
mi
Hp = 215
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6896900
36 X = -2026736
17
Y = -21013254
77 feet Y = -6427926
20 meter
Z = -2473548
36 Z = -763965
92
XDOT = 15489
066019 XDOT = 4759
275064
YDOT = -2785
252205 feet/sec YDOT = -795
937245 meter/sec
ZDOT = -19631
224153 ZDOT = -5960
570723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12644572
46 X = -3854065
69
Y = 18139074
94 feet Y = 5528790
04 meter
Z = -2516207
43 Z = -766940
03
XDOT = -10298
808921 XDOT = -3139
076959
YDOT = -9874
105011 feet/sec YDOT = -3009
627207 meter/sec
ZDOT = -19530
403527 ZDOT = -5952
866995
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
45499759
00016717 00000-0 10270-3 0 9099
2 25544 51
6433 67
3994 0003336 255
7799 104
2983 15
54290792 15918
Satellite: ISS
Catalog Number: 25544
Epoch time: 16239
45499759 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 67
3994 deg
Eccentricity:
0003336
Arg of perigee: 255
7799 deg
Mean anomaly: 104
2983 deg
Mean motion: 15
54290792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1591
Checksum: 361
Coasting Arc #11 (Orbit 1606)
---------------------------------------
Vector Time (GMT): 2016/240/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1159114
00 A = 6786163
67 meter
Y = 6218600
82 meter E =
0010459
Z = 2443249
79 I = 51
98249
XDOT = -5359
416546 Wp = 72
33005
YDOT = -1117
607672 meter/sec RA = 61
86647 deg
ZDOT = 5371
377820 TA = 314
88533
MA = 314
97020
Ha = 219
484 n
mi
Hp = 215
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3802867
47 X = 1077621
77
Y = 20402233
66 feet Y = 6231107
22 meter
Z = 8015911
39 Z = 2448682
32
XDOT = -17583
387619 XDOT = -5372
612384
YDOT = -3666
691837 feet/sec YDOT = -1177
613903 meter/sec
ZDOT = 17622
630642 ZDOT = 5345
311401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13775241
25 X = 4198693
53
Y = -15511059
06 feet Y = -4727770
80 meter
Z = 8038504
22 Z = 2450136
09
XDOT = 6869
001401 XDOT = 2093
671627
YDOT = 15200
891596 feet/sec YDOT = 4633
231758 meter/sec
ZDOT = 17508
882402 ZDOT = 5336
707356
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
48370155
00016717 00000-0 10270-3 0 9104
2 25544 51
6420 62
2689 0003311 261
4567 98
6210 15
54342417 16078
Satellite: ISS
Catalog Number: 25544
Epoch time: 16240
48370155 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 62
2689 deg
Eccentricity:
0003311
Arg of perigee: 261
4567 deg
Mean anomaly: 98
6210 deg
Mean motion: 15
54342417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1607
Checksum: 286
Coasting Arc #12 (Orbit 1621)
---------------------------------------
Vector Time (GMT): 2016/241/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2468
53 A = 6782371
73 meter
Y = -5565409
71 meter E =
0003194
Z = -3880060
77 I = 51
95230
XDOT = 5759
219282 Wp = 63
63060
YDOT = 2889
386119 meter/sec RA = 56
90703 deg
ZDOT = -4149
344257 TA = 162
94076
MA = 162
93002
Ha = 219
488 n
mi
Hp = 215
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8098
85 X = 78612
86
Y = -18259218
21 feet Y = -5564984
10 meter
Z = -12729858
18 Z = -3879875
64
XDOT = 18895
076384 XDOT = 5746
636821
YDOT = 9479
613252 feet/sec YDOT = 2953
719066 meter/sec
ZDOT = -13613
334177 ZDOT = -4121
398497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14245563
34 X = -4342047
71
Y = 11424104
71 feet Y = 3482067
12 meter
Z = -12728006
95 Z = -3879496
52
XDOT = -3732
756193 XDOT = -1137
744088
YDOT = -19681
649929 feet/sec YDOT = -5998
966898 meter/sec
ZDOT = -13491
701690 ZDOT = -4112
270675
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
44810972
00016717 00000-0 10270-3 0 9118
2 25544 51
6406 57
4604 0003307 265
0031 95
0744 15
54327340 16224
Satellite: ISS
Catalog Number: 25544
Epoch time: 16241
44810972 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 57
4604 deg
Eccentricity:
0003307
Arg of perigee: 265
0031 deg
Mean anomaly: 95
0744 deg
Mean motion: 15
54327340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1622
Checksum: 276
Coasting Arc #13 (Orbit 1637)
---------------------------------------
Vector Time (GMT): 2016/242/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1287728
16 A = 6778806
72 meter
Y = 4539175
23 meter E =
0004508
Z = 4866189
18 I = 51
92218
XDOT = -5839
027789 Wp = 141
74696
YDOT = -4313
026524 meter/sec RA = 51
93409 deg
ZDOT = 2473
347067 TA = 284
04149
MA = 284
09160
Ha = 219
581 n
mi
Hp = 215
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4224829
91 X = -1362028
11
Y = 14892307
17 feet Y = 4524359
80 meter
Z = 15965187
58 Z = 4859753
13
XDOT = -19156
915317 XDOT = -5802
378715
YDOT = -14150
349488 feet/sec YDOT = -4378
117399 meter/sec
ZDOT = 8114
655730 ZDOT = 2445
072251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14197126
84 X = 4327284
26
Y = -6244712
06 feet Y = -1903388
24 meter
Z = 15936197
04 Z = 4857352
86
XDOT = 1030
276185 XDOT = 314
028181
YDOT = 22776
292111 feet/sec YDOT = 6942
213835 meter/sec
ZDOT = 7991
855441 ZDOT = 2435
917538
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
47680757
00016717 00000-0 10270-3 0 9129
2 25544 51
6411 52
3299 0003264 269
9882 90
0896 15
54303431 16388
Satellite: ISS
Catalog Number: 25544
Epoch time: 16242
47680757 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 52
3299 deg
Eccentricity:
0003264
Arg of perigee: 269
9882 deg
Mean anomaly: 90
0896 deg
Mean motion: 15
54303431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1638
Checksum: 321
Coasting Arc #14 (Orbit 1652)
---------------------------------------
Vector Time (GMT): 2016/243/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2656415
99 A = 6776780
42 meter
Y = -3267786
73 meter E =
0011608
Z = -5319440
03 I = 51
89384
XDOT = 5502
959844 Wp = 84
29933
YDOT = 5304
627736 meter/sec RA = 46
95103 deg
ZDOT = -510
458664 TA = 180
84180
MA = 180
84375
Ha = 219
484 n
mi
Hp = 215
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8715275
55 X = 2718598
87
Y = -10721085
07 feet Y = -3237733
59 meter
Z = -17452231
06 Z = -5306384
79
XDOT = 18054
330197 XDOT = 5445
712707
YDOT = 17403
634304 feet/sec YDOT = 5365
845394 meter/sec
ZDOT = -1674
733149 ZDOT = -483
866543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13884580
00 X = -4232019
99
Y = 355577
64 feet Y = 108380
06 meter
Z = -17394541
23 Z = -5301856
17
XDOT = 1338
814115 XDOT = 408
070542
YDOT = -24037
358901 feet/sec YDOT = -7326
586993 meter/sec
ZDOT = -1559
481640 ZDOT = -475
330004
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
44120412
00016717 00000-0 10270-3 0 9135
2 25544 51
6398 47
5197 0003178 272
5717 87
5072 15
54351654 16530
Satellite: ISS
Catalog Number: 25544
Epoch time: 16243
44120412 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 47
5197 deg
Eccentricity:
0003178
Arg of perigee: 272
5717 deg
Mean anomaly: 87
5072 deg
Mean motion: 15
54351654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1653
Checksum: 309
Coasting Arc #15 (Orbit 1668)
---------------------------------------
Vector Time (GMT): 2016/244/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3971426
21 A = 6777555
57 meter
Y = 1876734
46 meter E =
0003122
Z = 5161591
84 I = 51
87335
XDOT = -4728
450312 Wp = 12
23419
YDOT = -5845
816937 meter/sec RA = 41
96607 deg
ZDOT = -1509
501499 TA = 92
27435
MA = 92
23860
Ha = 219
635 n
mi
Hp = 215
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13029613
57 X = -4017189
55
Y = 6157265
29 feet Y = 1832067
89 meter
Z = 16934356
44 Z = 5142188
65
XDOT = -15513
288426 XDOT = -4655
397090
YDOT = -19179
189427 feet/sec YDOT = -5898
285302 meter/sec
ZDOT = -4952
432738 ZDOT = -1532
292802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13360316
10 X = 4072224
35
Y = 5662353
67 feet Y = 1725885
40 meter
Z = 16849180
34 Z = 5135630
17
XDOT = -3516
702219 XDOT = -1071
890836
YDOT = 23358
362455 feet/sec YDOT = 7119
628876 meter/sec
ZDOT = -5050
959135 ZDOT = -1539
532344
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
46989122
00016717 00000-0 10270-3 0 9140
2 25544 51
6397 42
3902 0003256 275
2501 84
8280 15
54327329 16694
Satellite: ISS
Catalog Number: 25544
Epoch time: 16244
46989122 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 42
3902 deg
Eccentricity:
0003256
Arg of perigee: 275
2501 deg
Mean anomaly: 84
8280 deg
Mean motion: 15
54327329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1669
Checksum: 318
Coasting Arc #16 (Orbit 1683)
---------------------------------------
Vector Time (GMT): 2016/245/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5110774
89 A = 6780444
97 meter
Y = -508713
77 meter E =
0005935
Z = -4432812
93 I = 51
85872
XDOT = 3499
922503 Wp = 117
06659
YDOT = 5933
952628 meter/sec RA = 36
98349 deg
ZDOT = 3355
040080 TA = 186
75723
MA = 186
76523
Ha = 219
510 n
mi
Hp = 215
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16767634
17 X = 5137616
01
Y = -1669008
45 feet Y = -451412
05 meter
Z = -14543349
52 Z = -4407921
18
XDOT = 11482
685378 XDOT = 3417
010307
YDOT = 19468
348518 feet/sec YDOT = 5972
627864 meter/sec
ZDOT = 11007
349345 ZDOT = 3371
839591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12702002
65 X = -3871570
41
Y = -11214013
02 feet Y = -3418031
17 meter
Z = -14434444
93 Z = -4399618
82
XDOT = 5675
406364 XDOT = 1729
863860
YDOT = -20686
497514 feet/sec YDOT = -6305
244442 meter/sec
ZDOT = 11079
658815 ZDOT = 3377
080007
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
43428037
00016717 00000-0 10270-3 0 9152
2 25544 51
6397 37
5799 0003185 277
6642 82
4149 15
54363221 16843
Satellite: ISS
Catalog Number: 25544
Epoch time: 16245
43428037 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 37
5799 deg
Eccentricity:
0003185
Arg of perigee: 277
6642 deg
Mean anomaly: 82
4149 deg
Mean motion: 15
54363221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1684
Checksum: 329
Coasting Arc #17 (Orbit 1699)
---------------------------------------
Vector Time (GMT): 2016/246/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5937486
40 A = 6784405
90 meter
Y = -761399
74 meter E =
0009614
Z = 3184391
47 I = 51
84639
XDOT = -1874
806866 Wp = 91
17737
YDOT = -5651
077741 meter/sec RA = 32
01066 deg
ZDOT = -4834
492586 TA = 52
14992
MA = 52
06298
Ha = 219
525 n
mi
Hp = 215
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19479942
25 X = -5943999
18
Y = -2498030
64 feet Y = -827832
74 meter
Z = 10447478
57 Z = 3155533
23
XDOT = -6150
941162 XDOT = -1787
992111
YDOT = -18540
281301 feet/sec YDOT = -5671
558233 meter/sec
ZDOT = -15861
196148 ZDOT = -4843
388318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11751535
17 X = 3581867
92
Y = 15818548
32 feet Y = 4821493
53 meter
Z = 10321485
64 Z = 3145988
82
XDOT = -8016
327440 XDOT = -2443
376604
YDOT = 16356
125308 feet/sec YDOT = 4985
346994 meter/sec
ZDOT = -15899
004069 ZDOT = -4846
016440
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
46295549
00016717 00000-0 10270-3 0 9167
2 25544 51
6403 32
4500 0003352 283
1529 76
9250 15
54378217 17008
Satellite: ISS
Catalog Number: 25544
Epoch time: 16246
46295549 = yrday
fracday
Element set: 916
Inclination: 51
6403 deg
RA of node: 32
4500 deg
Eccentricity:
0003352
Arg of perigee: 283
1529 deg
Mean anomaly: 76
9250 deg
Mean motion: 15
54378217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1700
Checksum: 299
Coasting Arc #18 (Orbit 1714)
---------------------------------------
Vector Time (GMT): 2016/247/10:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 910124
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6335021
85 A = 6787593
14 meter
Y = 1829573
53 meter E =
0007526
Z = -1591593
18 I = 51
82910
XDOT = -21
296890 Wp = 15
24733
YDOT = 5068
119048 meter/sec RA = 27
04667 deg
ZDOT = 5754
400639 TA = 327
38801
MA = 327
43447
Ha = 219
630 n
mi
Hp = 215
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20784192
41 X = 6321823
48
Y = 6002537
83 feet Y = 1900342
00 meter
Z = -5221762
41 Z = -1560851
74
XDOT = -69
871686 XDOT = -105
920502
YDOT = 16627
687164 feet/sec YDOT = 5067
408425 meter/sec
ZDOT = 18879
267189 ZDOT = 5754
091036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10434418
41 X = -3180410
73
Y = -18987301
04 feet Y = -5787329
36 meter
Z = -5087752
85 Z = -1550747
07
XDOT = 10535
411524 XDOT = 3211
193432
YDOT = -10835
936012 feet/sec YDOT = -3302
793296 meter/sec
ZDOT = 18876
946891 ZDOT = 5753
693412
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
42733615
00016717 00000-0 10270-3 0 9176
2 25544 51
6402 27
6408 0003048 285
4450 74
6366 15
54373842 17158
Satellite: ISS
Catalog Number: 25544
Epoch time: 16247
42733615 = yrday
fracday
Element set: 917
Inclination: 51
6402 deg
RA of node: 27
6408 deg
Eccentricity:
0003048
Arg of perigee: 285
4450 deg
Mean anomaly: 74
6366 deg
Mean motion: 15
54373842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1715
Checksum: 308
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