[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 18th 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 1451)
---------------------------------------
Vector Time (GMT): 2016/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4597088
03 A = 6777563
11 meter
Y = -1782028
85 meter E =
0011018
Z = -4660904
72 I = 51
97744
XDOT = -254
887108 Wp = 76
34103
YDOT = 7063
201307 meter/sec RA = 111
14990 deg
ZDOT = -2955
225857 TA = 164
35584
MA = 164
32177
Ha = 219
943 n
mi
Hp = 212
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15082309
82 X = 4639313
66
Y = -5846551
34 feet Y = -1730385
16 meter
Z = -15291682
14 Z = -4638471
08
XDOT = -836
243792 XDOT = -319
495758
YDOT = 23173
232636 feet/sec YDOT = 7059
989664 meter/sec
ZDOT = -9695
622890 ZDOT = -2956
621114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15819497
11 X = -4821782
72
Y = -3794750
66 feet Y = -1156640
00 meter
Z = -15193325
94 Z = -4630925
75
XDOT = 13504
192443 XDOT = 4116
077857
YDOT = -17491
610267 feet/sec YDOT = -5331
442809 meter/sec
ZDOT = -9702
920569 ZDOT = -2957
450189
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 16230
52136046
00016717 00000-0 10270-3 0 9006
2 25544 51
6442 111
9842 0001304 132
6114 227
5150 15
55050953 14528
Satellite: ISS
Catalog Number: 25544
Epoch time: 16230
52136046 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 111
9842 deg
Eccentricity:
0001304
Arg of perigee: 132
6114 deg
Mean anomaly: 227
5150 deg
Mean motion: 15
55050953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 258
Coasting Arc #2 (Orbit 1467)
---------------------------------------
Vector Time (GMT): 2016/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4219903
09 A = 6774880
07 meter
Y = -295743
86 meter E =
0004598
Z = 5288925
59 I = 51
97846
XDOT = 1522
246265 Wp = 124
74450
YDOT = -7478
535860 meter/sec RA = 106
16735 deg
ZDOT = 793
341557 TA = 317
69611
MA = 317
73156
Ha = 220
089 n
mi
Hp = 212
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13844826
41 X = -4241973
17
Y = -970288
24 feet Y = -343056
79 meter
Z = 17352118
07 Z = 5268373
19
XDOT = 4994
246276 XDOT = 1601
906379
YDOT = -24535
878806 feet/sec YDOT = -7461
067641 meter/sec
ZDOT = 2602
826631 ZDOT = 800
929922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11093071
41 X = 3381168
16
Y = 8524806
95 feet Y = 2598361
16 meter
Z = 17262332
18 Z = 5261558
85
XDOT = -17092
951816 XDOT = -5209
931713
YDOT = 16881
886794 feet/sec YDOT = 5145
599095 meter/sec
ZDOT = 2637
272048 ZDOT = 803
840520
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 16231
54958933
00016717 00000-0 10270-3 0 9017
2 25544 51
6435 106
8518 0001413 137
4090 222
7173 15
55048808 14685
Satellite: ISS
Catalog Number: 25544
Epoch time: 16231
54958933 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 106
8518 deg
Eccentricity:
0001413
Arg of perigee: 137
4090 deg
Mean anomaly: 222
7173 deg
Mean motion: 15
55048808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1468
Checksum: 306
Coasting Arc #3 (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 = 3646837
86 A = 6775341
57 meter
Y = 2430451
24 meter E =
0014695
Z = -5180130
15 I = 51
98801
XDOT = -2582
712025 Wp = 104
55043
YDOT = 7054
322731 meter/sec RA = 101
18106 deg
ZDOT = 1491
494403 TA = 179
76002
MA = 179
75932
Ha = 219
821 n
mi
Hp = 213
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11964691
13 X = 3644551
27
Y = 7973921
39 feet Y = 2471219
51 meter
Z = -16995177
65 Z = -5162420
76
XDOT = -8473
464650 XDOT = -2668
648201
YDOT = 23144
103447 feet/sec YDOT = 7024
960714 meter/sec
ZDOT = 4893
354339 ZDOT = 1478
739293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5880104
64 X = -1792255
90
Y = -13220166
14 feet Y = -4029506
64 meter
Z = -16918182
41 Z = -5156662
00
XDOT = 18666
774008 XDOT = 5689
632718
YDOT = -14492
172393 feet/sec YDOT = -4417
214145 meter/sec
ZDOT = 4836
387993 ZDOT = 1474
131060
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
51354911
00016717 00000-0 10270-3 0 9022
2 25544 51
6432 102
0398 0001238 143
4866 216
6372 15
55068255 14837
Satellite: ISS
Catalog Number: 25544
Epoch time: 16232
51354911 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 102
0398 deg
Eccentricity:
0001238
Arg of perigee: 143
4866 deg
Mean anomaly: 216
6372 deg
Mean motion: 15
55068255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1483
Checksum: 293
Coasting Arc #4 (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 = -2909567
26 A = 6778676
51 meter
Y = -4347005
95 meter E =
0010195
Z = 4304133
39 I = 52
00506
XDOT = 3443
893651 Wp = 78
37255
YDOT = -5852
486585 meter/sec RA = 96
20175 deg
ZDOT = -3573
603188 TA = 47
89520
MA = 47
80857
Ha = 219
784 n
mi
Hp = 212
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9545824
33 X = -2881649
01
Y = -14261830
55 feet Y = -4379386
25 meter
Z = 14121172
52 Z = 4290067
78
XDOT = 11298
863683 XDOT = 3526
440451
YDOT = -19201
071474 feet/sec YDOT = -5813
513385 meter/sec
ZDOT = -11724
419907 ZDOT = -3556
672928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 735743
35 X = 224254
57
Y = 17195721
76 feet Y = 5241255
99 meter
Z = 14060438
15 Z = 4285621
55
XDOT = -18495
584343 XDOT = -5637
454108
YDOT = 10341
326899 feet/sec YDOT = 3152
036439 meter/sec
ZDOT = -11649
400350 ZDOT = -3550
737227
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
54176597
00016717 00000-0 10270-3 0 9039
2 25544 51
6434 96
9067 0001026 146
2869 213
8350 15
55107639 14994
Satellite: ISS
Catalog Number: 25544
Epoch time: 16233
54176597 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 96
9067 deg
Eccentricity:
0001026
Arg of perigee: 146
2869 deg
Mean anomaly: 213
8350 deg
Mean motion: 15
55107639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1499
Checksum: 327
Coasting Arc #5 (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 = -3861462
59 A = 6775403
42 meter
Y = -2144584
94 meter E =
0004935
Z = 5134021
46 I = 51
99543
XDOT = 1839
543261 Wp = 72
33261
YDOT = -7264
849636 meter/sec RA = 94
31257 deg
ZDOT = -1648
339484 TA = 33
50337
MA = 33
47216
Ha = 219
893 n
mi
Hp = 212
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12668840
50 X = -3862132
84
Y = -7036039
84 feet Y = -2187769
75 meter
Z = 16843902
44 Z = 5115262
23
XDOT = 6035
246919 XDOT = 1928
650750
YDOT = -23834
808516 feet/sec YDOT = -7243
780531 meter/sec
ZDOT = -5407
937940 ZDOT = -1639
186565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3171381
77 X = 966637
16
Y = -14236960
38 feet Y = -4339425
52 meter
Z = 16762270
81 Z = 5109140
14
XDOT = 23543
082924 XDOT = 7175
931675
YDOT = -1084
903881 feet/sec YDOT = -330
678703 meter/sec
ZDOT = -5366
667563 ZDOT = -1635
760273
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
92734688
00016717 00000-0 10270-3 0 9043
2 25544 51
6435 94
9789 0001506 156
9229 203
1992 15
55099915 15054
Satellite: ISS
Catalog Number: 25544
Epoch time: 16233
92734688 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 94
9789 deg
Eccentricity:
0001506
Arg of perigee: 156
9229 deg
Mean anomaly: 203
1992 deg
Mean motion: 15
55099915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1505
Checksum: 341
Coasting Arc #6 (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 = 3353030
94 A = 6779012
36 meter
Y = 4109616
75 meter E =
0009161
Z = -4231564
17 I = 52
00764
XDOT = -2813
266210 Wp = 117
44129
YDOT = 6094
883390 meter/sec RA = 89
33559 deg
ZDOT = 3692
049812 TA = 190
24734
MA = 190
26603
Ha = 219
791 n
mi
Hp = 212
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11000757
67 X = 3327381
89
Y = 13482994
57 feet Y = 4146968
83 meter
Z = -13883084
55 Z = -4215338
75
XDOT = -9229
876016 XDOT = -2899
145883
YDOT = 19996
336583 feet/sec YDOT = 6062
943675 meter/sec
ZDOT = 12113
024317 ZDOT = 3678
174720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9583499
21 X = -2921050
56
Y = 14591396
00 feet Y = 4447457
50 meter
Z = -13812876
39 Z = -4210164
72
XDOT = -20794
750535 XDOT = -6338
239963
YDOT = -2255
752682 feet/sec YDOT = -687
553418 meter/sec
ZDOT = 12051
303622 ZDOT = 3673
237344
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
89129726
00016717 00000-0 10270-3 0 9052
2 25544 51
6422 90
1679 0001642 157
1516 202
9710 15
55093792 15208
Satellite: ISS
Catalog Number: 25544
Epoch time: 16234
89129726 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 90
1679 deg
Eccentricity:
0001642
Arg of perigee: 157
1516 deg
Mean anomaly: 202
9710 deg
Mean motion: 15
55093792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1520
Checksum: 304
Coasting Arc #7 (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 = -2664320
04 A = 6783503
78 meter
Y = -5619810
14 meter E =
0014367
Z = 2690343
44 I = 52
02184
XDOT = 3677
647670 Wp = 106
99370
YDOT = -4252
687910 meter/sec RA = 84
37131 deg
ZDOT = -5222
455511 TA = 42
76282
MA = 42
65113
Ha = 219
779 n
mi
Hp = 212
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8741207
49 X = -2614348
34
Y = -18437697
31 feet Y = -5649324
75 meter
Z = 8826586
08 Z = 2677522
68
XDOT = 12065
773195 XDOT = 3750
297279
YDOT = -13952
388156 feet/sec YDOT = -4211
156154 meter/sec
ZDOT = -17134
040392 ZDOT = -5204
413759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14754804
50 X = 4497264
41
Y = -14128761
60 feet Y = -4306446
53 meter
Z = 8771536
46 Z = 2673564
31
XDOT = 16034
644062 XDOT = 4887
359510
YDOT = 6118
666404 feet/sec YDOT = 1864
969520 meter/sec
ZDOT = -17054
419138 ZDOT = -5198
186953
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
91950524
00016717 00000-0 10270-3 0 9065
2 25544 51
6428 85
0350 0001469 160
9941 199
1267 15
55089540 15361
Satellite: ISS
Catalog Number: 25544
Epoch time: 16235
91950524 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 85
0350 deg
Eccentricity:
0001469
Arg of perigee: 160
9941 deg
Mean anomaly: 199
1267 deg
Mean motion: 15
55089540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1536
Checksum: 320
Coasting Arc #8 (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 = 1835898
67 A = 6786424
04 meter
Y = 6481718
65 meter E =
0009763
Z = -787275
43 I = 52
02709
XDOT = -4381
722010 Wp = 45
81036
YDOT = 1961
034762 meter/sec RA = 79
41912 deg
ZDOT = 5979
709925 TA = 305
72233
MA = 305
81311
Ha = 219
766 n
mi
Hp = 213
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6023289
59 X = 1767106
23
Y = 21265481
14 feet Y = 6501864
21 meter
Z = -2582924
62 Z = -778524
57
XDOT = -14375
728378 XDOT = -4432
371892
YDOT = 6433
841084 feet/sec YDOT = 1911
752548 meter/sec
ZDOT = 19618
470881 ZDOT = 5958
301562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18088674
08 X = -5513427
86
Y = 12707903
47 feet Y = 3873368
98 meter
Z = -2545832
75 Z = -775969
82
XDOT = -9927
021779 XDOT = -3025
756238
YDOT = -10253
772033 feet/sec YDOT = -3125
349716 meter/sec
ZDOT = 19524
533423 ZDOT = 5951
077787
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
88344566
00016717 00000-0 10270-3 0 9076
2 25544 51
6428 80
2230 0001227 161
4371 198
6828 15
55039096 15515
Satellite: ISS
Catalog Number: 25544
Epoch time: 16236
88344566 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 80
2230 deg
Eccentricity:
0001227
Arg of perigee: 161
4371 deg
Mean anomaly: 198
6828 deg
Mean motion: 15
55039096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1551
Checksum: 315
Coasting Arc #9 (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
50 A = 6778376
27 meter
Y = 1490242
87 meter E =
0010313
Z = -4996735
26 I = 51
99094
XDOT = -53
080022 Wp = 116
07613
YDOT = 7353
616781 meter/sec RA = 77
22969 deg
ZDOT = 2146
061165 TA = 174
75658
MA = 174
74577
Ha = 219
794 n
mi
Hp = 215
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14245277
23 X = 4349245
43
Y = 4889248
27 feet Y = 1538838
07 meter
Z = -16393488
39 Z = -4975625
56
XDOT = -174
147054 XDOT = -145
730688
YDOT = 24126
039307 feet/sec YDOT = 7352
505267 meter/sec
ZDOT = 7040
883086 ZDOT = 2145
577925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5458969
06 X = 1663893
77
Y = -14143573
12 feet Y = -4310961
09 meter
Z = -16301476
31 Z = -4968689
98
XDOT = 23067
120915 XDOT = 7030
858455
YDOT = 788
285211 feet/sec YDOT = 240
269332 meter/sec
ZDOT = 7037
444951 ZDOT = 2145
013221
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
33328630
00016717 00000-0 10270-3 0 9082
2 25544 51
6434 77
9781 0002994 247
2947 112
7889 15
54300950 15580
Satellite: ISS
Catalog Number: 25544
Epoch time: 16237
33328630 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 77
9781 deg
Eccentricity:
0002994
Arg of perigee: 247
2947 deg
Mean anomaly: 112
7889 deg
Mean motion: 15
54300950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1558
Checksum: 336
Coasting Arc #10 (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 = -4372160
43 A = 6781822
78 meter
Y = -3179605
00 meter E =
0007699
Z = 4089221
21 I = 51
99408
XDOT = 1101
635640 Wp = 80
21719
YDOT = -6521
111826 meter/sec RA = 72
26118 deg
ZDOT = -3885
204799 TA = 49
82067
MA = 49
75328
Ha = 219
870 n
mi
Hp = 215
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14344358
37 X = -4356143
92
Y = -10431774
95 feet Y = -3228407
74 meter
Z = 13416080
08 Z = 4068021
45
XDOT = 3614
290157 XDOT = 1193
347052
YDOT = -21394
723840 feet/sec YDOT = -6508
279937 meter/sec
ZDOT = -12746
734904 ZDOT = -3879
630387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10758041
40 X = -3279051
02
Y = 14188366
59 feet Y = 4324614
14 meter
Z = 13323983
98 Z = 4061150
32
XDOT = -20271
049408 XDOT = -6178
615860
YDOT = -3400
742680 feet/sec YDOT = -1036
546369 meter/sec
ZDOT = -12721
176380 ZDOT = -3877
414561
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
36200537
00016717 00000-0 10270-3 0 9092
2 25544 51
6431 72
8500 0003007 250
7046 109
3782 15
54302716 15749
Satellite: ISS
Catalog Number: 25544
Epoch time: 16238
36200537 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 72
8500 deg
Eccentricity:
0003007
Arg of perigee: 250
7046 deg
Mean anomaly: 109
3782 deg
Mean motion: 15
54302716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1574
Checksum: 285
Coasting Arc #11 (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 = 4224388
51 A = 6785620
93 meter
Y = 4546156
15 meter E =
0002155
Z = -2742509
80 I = 51
99763
XDOT = -2220
957796 Wp = 27
88744
YDOT = 5189
798565 meter/sec RA = 67
30094 deg
ZDOT = 5185
405634 TA = 301
25093
MA = 301
27204
Ha = 219
627 n
mi
Hp = 215
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13859542
36 X = 4186560
11
Y = 14915210
47 feet Y = 4593184
51 meter
Z = -8997735
55 Z = -2722080
92
XDOT = -7286
606941 XDOT = -2304
014646
YDOT = 17026
898178 feet/sec YDOT = 5164
498053 meter/sec
ZDOT = 17012
485677 ZDOT = 5174
415005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14993233
86 X = 4569937
68
Y = -13832483
20 feet Y = -4216140
88 meter
Z = -8909265
37 Z = -2715544
09
XDOT = 15977
447887 XDOT = 4869
926116
YDOT = 6399
759651 feet/sec YDOT = 1950
646742 meter/sec
ZDOT = 16963
481640 ZDOT = 5170
469204
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
32642386
00016717 00000-0 10270-3 0 9103
2 25544 51
6444 68
0407 0003138 255
7859 104
2945 15
54327603 15891
Satellite: ISS
Catalog Number: 25544
Epoch time: 16239
32642386 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 68
0407 deg
Eccentricity:
0003138
Arg of perigee: 255
7859 deg
Mean anomaly: 104
2945 deg
Mean motion: 15
54327603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1589
Checksum: 318
Coasting Arc #12 (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 = -2107984
26 A = 6788626
31 meter
Y = -6403832
26 meter E =
0009420
Z = -746567
48 I = 52
00508
XDOT = 4717
717110 Wp = 158
33964
YDOT = -859
031895 meter/sec RA = 66
81740 deg
ZDOT = -5984
761144 TA = 29
68869
MA = 29
63526
Ha = 219
622 n
mi
Hp = 215
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6915958
86 X = -2032591
84
Y = -21009948
35 feet Y = -6426983
62 meter
Z = -2449368
38 Z = -756624
19
XDOT = 15478
074507 XDOT = 4756
043550
YDOT = -2818
346111 feet/sec YDOT = -806
061069 meter/sec
ZDOT = -19635
043125 ZDOT = -5961
750731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12630369
06 X = -3849736
49
Y = 18152431
80 feet Y = 5532861
21 meter
Z = -2492151
50 Z = -759607
78
XDOT = -10317
670698 XDOT = -3144
826029
YDOT = -9846
469537 feet/sec YDOT = -3001
203915 meter/sec
ZDOT = -19534
290522 ZDOT = -5954
051751
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
45501205
00016717 00000-0 10270-3 0 9112
2 25544 51
6434 67
3995 0003302 256
2662 103
8123 15
54285929 15915
Satellite: ISS
Catalog Number: 25544
Epoch time: 16239
45501205 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 67
3995 deg
Eccentricity:
0003302
Arg of perigee: 256
2662 deg
Mean anomaly: 103
8123 deg
Mean motion: 15
54285929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1591
Checksum: 301
Coasting Arc #13 (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 = 1167243
56 A = 6786195
73 meter
Y = 6220282
75 meter E =
0010503
Z = 2435071
22 I = 51
98262
XDOT = -5357
160823 Wp = 72
05102
YDOT = -1105
539035 meter/sec RA = 61
86672 deg
ZDOT = 5376
156903 TA = 315
06574
MA = 315
15069
Ha = 219
501 n
mi
Hp = 215
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3829539
25 X = 1085771
65
Y = 20407751
81 feet Y = 6232880
17 meter
Z = 7989078
81 Z = 2440543
29
XDOT = -17575
986951 XDOT = -5370
514997
YDOT = -3627
096573 feet/sec YDOT = -1165
520927 meter/sec
ZDOT = 17638
310050 ZDOT = 5350
101057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13763071
22 X = 4194984
11
Y = -15535614
19 feet Y = -4735255
21 meter
Z = 8011844
19 Z = 2442010
11
XDOT = 6893
932854 XDOT = 2101
270734
YDOT = 15171
660842 feet/sec YDOT = 4624
322225 meter/sec
ZDOT = 17524
605786 ZDOT = 5341
499843
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
48371940
00016717 00000-0 10270-3 0 9129
2 25544 51
6421 62
2690 0003279 261
9496 98
1284 15
54337198 16076
Satellite: ISS
Catalog Number: 25544
Epoch time: 16240
48371940 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 62
2690 deg
Eccentricity:
0003279
Arg of perigee: 261
9496 deg
Mean anomaly: 98
1284 deg
Mean motion: 15
54337198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1607
Checksum: 319
Coasting Arc #14 (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 = -13015
01 A = 6782413
74 meter
Y = -5570734
97 meter E =
0003201
Z = -3872470
14 I = 51
95246
XDOT = 5759
151574 Wp = 63
57701
YDOT = 2876
370698 meter/sec RA = 56
90739 deg
ZDOT = -4158
419721 TA = 162
87554
MA = 162
86474
Ha = 219
508 n
mi
Hp = 215
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -42700
16 X = 68089
84
Y = -18276689
55 feet Y = -5570427
17 meter
Z = -12704954
52 Z = -3872336
17
XDOT = 18894
854244 XDOT = 5746
758744
YDOT = 9436
911739 feet/sec YDOT = 2940
703948 meter/sec
ZDOT = -13643
109321 ZDOT = -4130
473829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14237289
42 X = -4339525
81
Y = 11462118
98 feet Y = 3493653
86 meter
Z = -12703326
02 Z = -3871973
77
XDOT = -3763
171471 XDOT = -1147
014664
YDOT = -19655
378569 feet/sec YDOT = -5990
959388 meter/sec
ZDOT = -13521
473818 ZDOT = -4121
345220
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
44813111
00016717 00000-0 10270-3 0 9138
2 25544 51
6407 57
4605 0003273 265
4978 94
5801 15
54321412 16224
Satellite: ISS
Catalog Number: 25544
Epoch time: 16241
44813111 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 57
4605 deg
Eccentricity:
0003273
Arg of perigee: 265
4978 deg
Mean anomaly: 94
5801 deg
Mean motion: 15
54321412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1622
Checksum: 286
Coasting Arc #15 (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 = -1275020
58 A = 6778847
43 meter
Y = 4548540
60 meter E =
0004532
Z = 4860784
38 I = 51
92232
XDOT = -5842
587156 Wp = 140
85736
YDOT = -4300
420600 meter/sec RA = 51
93458 deg
ZDOT = 2486
933219 TA = 284
78975
MA = 284
83995
Ha = 219
603 n
mi
Hp = 215
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4183138
40 X = -1349399
95
Y = 14923033
48 feet Y = 4533866
84 meter
Z = 15947455
32 Z = 4854409
87
XDOT = -19168
593033 XDOT = -5806
144775
YDOT = -14108
991469 feet/sec YDOT = -4365
552433 meter/sec
ZDOT = 8159
229722 ZDOT = 2458
640611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14193840
14 X = 4326282
48
Y = -6296489
40 feet Y = -1919169
97 meter
Z = 15918732
03 Z = 4852029
52
XDOT = 1065
893467 XDOT = 324
884329
YDOT = 22759
148162 feet/sec YDOT = 6936
988360 meter/sec
ZDOT = 8036
349275 ZDOT = 2449
479259
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
47683310
00016717 00000-0 10270-3 0 9149
2 25544 51
6412 52
3301 0003232 270
5012 89
5771 15
54296968 16382
Satellite: ISS
Catalog Number: 25544
Epoch time: 16242
47683310 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 52
3301 deg
Eccentricity:
0003232
Arg of perigee: 270
5012 deg
Mean anomaly: 89
5771 deg
Mean motion: 15
54296968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1638
Checksum: 295
Coasting Arc #16 (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 = 2642335
42 A = 6776806
87 meter
Y = -3281368
51 meter E =
0011637
Z = -5318150
98 I = 51
89393
XDOT = 5511
532760 Wp = 84
01802
YDOT = 5293
962150 meter/sec RA = 46
95165 deg
ZDOT = -527
835896 TA = 180
95715
MA = 180
95938
Ha = 219
509 n
mi
Hp = 215
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8669079
45 X = 2704664
96
Y = -10765644
73 feet Y = -3251472
01 meter
Z = -17448001
89 Z = -5305163
78
XDOT = 18082
456563 XDOT = 5454
488661
YDOT = 17368
642223 feet/sec YDOT = 5355
276810 meter/sec
ZDOT = -1731
745067 ZDOT = -501
201637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13887961
10 X = -4233050
54
Y = 419691
75 feet Y = 127922
05 meter
Z = -17390606
95 Z = -5300657
00
XDOT = 1298
380917 XDOT = 395
746504
YDOT = -24035
711008 feet/sec YDOT = -7326
084715 meter/sec
ZDOT = -1616
307329 ZDOT = -492
650474
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
44123384
00016717 00000-0 10270-3 0 9158
2 25544 51
6399 47
5199 0003144 273
0697 87
0093 15
54344478 16533
Satellite: ISS
Catalog Number: 25544
Epoch time: 16243
44123384 = yrday
fracday
Element set: 915
Inclination: 51
6399 deg
RA of node: 47
5199 deg
Eccentricity:
0003144
Arg of perigee: 273
0697 deg
Mean anomaly: 87
0093 deg
Mean motion: 15
54344478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1653
Checksum: 325
Coasting Arc #17 (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 = -3957402
70 A = 6777558
52 meter
Y = 1894015
30 meter E =
0003119
Z = 5166041
45 I = 51
87335
XDOT = -4743
433488 Wp = 12
26881
YDOT = -5838
714240 meter/sec RA = 41
96675 deg
ZDOT = -1489
895484 TA = 92
04745
MA = 92
01173
Ha = 219
662 n
mi
Hp = 215
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12983604
64 X = -4003381
93
Y = 6213960
95 feet Y = 1849504
34 meter
Z = 16948954
89 Z = 5146705
85
XDOT = -15562
445827 XDOT = -4670
553812
YDOT = -19155
886615 feet/sec YDOT = -5891
351125 meter/sec
ZDOT = -4888
108543 ZDOT = -1512
759992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13371832
00 X = 4075734
39
Y = 5590312
12 feet Y = 1703927
13 meter
Z = 16864071
02 Z = 5140168
85
XDOT = -3471
494267 XDOT = -1058
111453
YDOT = 23378
838599 feet/sec YDOT = 7125
870005 meter/sec
ZDOT = -4986
956303 ZDOT = -1520
024281
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
46992589
00016717 00000-0 10270-3 0 9163
2 25544 51
6398 42
3905 0003220 275
7146 84
3639 15
54319499 16691
Satellite: ISS
Catalog Number: 25544
Epoch time: 16244
46992589 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 42
3905 deg
Eccentricity:
0003220
Arg of perigee: 275
7146 deg
Mean anomaly: 84
3639 deg
Mean motion: 15
54319499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1669
Checksum: 348
Coasting Arc #18 (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 = 5098803
63 A = 6780426
11 meter
Y = -528955
45 meter E =
0006026
Z = -4444277
15 I = 51
85864
XDOT = 3522
083426 Wp = 116
66163
YDOT = 5931
692610 meter/sec RA = 36
98416 deg
ZDOT = 3335
660182 TA = 186
94083
MA = 186
94917
Ha = 219
538 n
mi
Hp = 215
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16728358
38 X = 5125927
68
Y = -1735418
15 feet Y = -471786
02 meter
Z = -14580961
79 Z = -4419442
86
XDOT = 11555
391819 XDOT = 3439
288993
YDOT = 19460
933760 feet/sec YDOT = 5970
616320 meter/sec
ZDOT = 10943
767001 ZDOT = 3352
567630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12724079
63 X = -3878299
47
Y = -11140210
75 feet Y = -3395536
24 meter
Z = -14472304
55 Z = -4411158
43
XDOT = 5625
578206 XDOT = 1714
676237
YDOT = -20733
394357 feet/sec YDOT = -6319
538600 meter/sec
ZDOT = 11016
548721 ZDOT = 3357
844050
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
43431999
00016717 00000-0 10270-3 0 9175
2 25544 51
6398 37
5802 0003148 278
1088 81
9708 15
54354951 16843
Satellite: ISS
Catalog Number: 25544
Epoch time: 16245
43431999 = yrday
fracday
Element set: 917
Inclination: 51
6398 deg
RA of node: 37
5802 deg
Eccentricity:
0003148
Arg of perigee: 278
1088 deg
Mean anomaly: 81
9708 deg
Mean motion: 15
54354951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1684
Checksum: 342
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