[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 8th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10 7639 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
070/23:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
4
077/03:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
1
078/21:26:42
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 214
9
079/03:12:07
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 214
9
080/10:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 214
8
Coasting Arc #1 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2016/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5539955
53 A = 6789101
09 meter
Y = -3666047
15 meter E =
0012037
Z = 1371564
45 I = 51
50325
XDOT = 3693
559533 Wp = 59
08784
YDOT = -3400
834051 meter/sec RA = 204
04314 deg
ZDOT = 5797
019687 TA = 315
88459
MA = 315
98055
Ha = 220
709 n
mi
Hp = 215
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18175707
11 X = -5505211
49
Y = -12027713
74 feet Y = -3727804
16 meter
Z = 4499883
36 Z = 1344738
09
XDOT = 12117
977471 XDOT = 3703
155061
YDOT = -11157
592032 feet/sec YDOT = -3359
475793 meter/sec
ZDOT = 19019
093462 ZDOT = 5814
985513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14410688
03 X = -4392377
71
Y = -16382403
95 feet Y = -4993356
72 meter
Z = 4384072
13 Z = 1336265
18
XDOT = 13307
719415 XDOT = 4056
192878
YDOT = -6566
770593 feet/sec YDOT = -2001
551677 meter/sec
ZDOT = 19097
569086 ZDOT = 5820
939057
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 16067
56171306
00016717 00000-0 10270-3 0 9006
2 25544 51
6413 204
8357 0001784 247
6331 112
4633 15
53947653 29174
Satellite: ISS
Catalog Number: 25544
Epoch time: 16067
56171306 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 204
8357 deg
Eccentricity:
0001784
Arg of perigee: 247
6331 deg
Mean anomaly: 112
4633 deg
Mean motion: 15
53947653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2917
Checksum: 304
Coasting Arc #2 (Orbit 2931)
---------------------------------------
Vector Time (GMT): 2016/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4625752
56 A = 6786344
94 meter
Y = 4033016
62 meter E =
0003547
Z = -2895456
65 I = 51
52333
XDOT = -5252
445123 Wp = 137
17837
YDOT = 2416
302930 meter/sec RA = 199
06113 deg
ZDOT = -5031
817853 TA = 75
84950
MA = 75
81009
Ha = 220
685 n
mi
Hp = 215
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15176353
55 X = 4594375
25
Y = 13231681
82 feet Y = 4084568
98 meter
Z = -9499529
70 Z = -2873063
07
XDOT = -17232
431506 XDOT = -5254
632414
YDOT = 7927
503050 feet/sec YDOT = 2357
553608 meter/sec
ZDOT = -16508
588758 ZDOT = -5057
338204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11518422
05 X = 3510815
04
Y = 16569546
09 feet Y = 5050397
65 meter
Z = -9402992
68 Z = -2866032
17
XDOT = -17340
322689 XDOT = -5285
330356
YDOT = 2634
403358 feet/sec YDOT = 802
966144 meter/sec
ZDOT = -16619
691936 ZDOT = -5065
682102
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 16068
52636125
00016717 00000-0 10270-3 0 9019
2 25544 51
6409 200
0289 0001764 254
3350 105
7608 15
53956748 29324
Satellite: ISS
Catalog Number: 25544
Epoch time: 16068
52636125 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 200
0289 deg
Eccentricity:
0001764
Arg of perigee: 254
3350 deg
Mean anomaly: 105
7608 deg
Mean motion: 15
53956748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2932
Checksum: 307
Coasting Arc #3 (Orbit 2947)
---------------------------------------
Vector Time (GMT): 2016/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3350120
14 A = 6782540
62 meter
Y = -4213725
41 meter E =
0008859
Z = 4120726
99 I = 51
54300
XDOT = 6508
752796 Wp = 108
54505
YDOT = -1465
995122 meter/sec RA = 194
07195 deg
ZDOT = 3783
050175 TA = 302
37064
MA = 302
45635
Ha = 220
574 n
mi
Hp = 215
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10991207
80 X = -3322768
73
Y = -13824558
45 feet Y = -4251035
09 meter
Z = 13519445
51 Z = 4104520
24
XDOT = 21354
175841 XDOT = 6506
285944
YDOT = -4809
695283 feet/sec YDOT = -1393
223104 meter/sec
ZDOT = 12411
581940 ZDOT = 3814
661963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7617361
71 X = -2321771
85
Y = -15993122
13 feet Y = -4874703
63 meter
Z = 13449770
16 Z = 4099489
94
XDOT = 20643
572125 XDOT = 6292
160784
YDOT = 747
188138 feet/sec YDOT = 227
742944 meter/sec
ZDOT = 12548
977442 ZDOT = 3824
928324
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 16069
55529832
00016717 00000-0 10270-3 0 9020
2 25544 51
6422 194
9011 0001880 259
5654 100
5286 15
54011433 29482
Satellite: ISS
Catalog Number: 25544
Epoch time: 16069
55529832 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 194
9011 deg
Eccentricity:
0001880
Arg of perigee: 259
5654 deg
Mean anomaly: 100
5286 deg
Mean motion: 15
54011433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2948
Checksum: 306
Coasting Arc #4 (Orbit 2962)
---------------------------------------
Vector Time (GMT): 2016/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1767793
97 A = 6779296
78 meter
Y = 4273803
95 meter E =
0010658
Z = -4966511
88 I = 51
56431
XDOT = -7334
389203 Wp = 72
22060
YDOT = 547
990856 meter/sec RA = 189
07570 deg
ZDOT = -2139
669145 TA = 176
89022
MA = 176
88359
Ha = 220
538 n
mi
Hp = 215
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5799848
97 X = 1743996
88
Y = 14021666
51 feet Y = 4293438
74 meter
Z = -16294330
30 Z = -4957982
92
XDOT = -24062
956702 XDOT = -7329
578337
YDOT = 1797
870262 feet/sec YDOT = 465
999394 meter/sec
ZDOT = -7019
911892 ZDOT = -2175
285952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2794014
99 X = 851615
77
Y = 14954006
86 feet Y = 4557981
29 meter
Z = -16257974
62 Z = -4955430
66
XDOT = -22761
100056 XDOT = -6937
583297
YDOT = -3545
305449 feet/sec YDOT = -1080
609101 meter/sec
ZDOT = -7174
556810 ZDOT = -2186
804916
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 16070
51991172
00016717 00000-0 10270-3 0 9039
2 25544 51
6431 190
0945 0001789 267
3863 92
7084 15
54005152 29638
Satellite: ISS
Catalog Number: 25544
Epoch time: 16070
51991172 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node: 190
0945 deg
Eccentricity:
0001789
Arg of perigee: 267
3863 deg
Mean anomaly: 92
7084 deg
Mean motion: 15
54005152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2963
Checksum: 311
Coasting Arc #5 (Orbit 2969)
---------------------------------------
Vector Time (GMT): 2016/070/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6260992
01 A = 6787258
98 meter
Y = 1140345
29 meter E =
0005022
Z = -2353665
20 I = 51
60377
XDOT = -2866
913590 Wp = 28
45279
YDOT = -4637
622773 meter/sec RA = 186
72079 deg
ZDOT = 5388
426373 TA = 305
27758
MA = 305
32456
Ha = 220
540 n
mi
Hp = 215
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20541312
38 X = -6261845
26
Y = 3741290
34 feet Y = 1070325
58 meter
Z = -7721998
70 Z = -2384081
66
XDOT = -9405
884483 XDOT = -2841
016019
YDOT = -15215
297811 feet/sec YDOT = -4669
536851 meter/sec
ZDOT = 17678
564216 ZDOT = 5374
563319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20215460
31 X = 6161672
30
Y = 5021869
17 feet Y = 1530665
72 meter
Z = -7854172
55 Z = -2393951
79
XDOT = 2782
676978 XDOT = 848
159943
YDOT = 16308
864031 feet/sec YDOT = 4970
941757 meter/sec
ZDOT = 17619
114127 ZDOT = 5370
305986
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 16070
97005904
00016717 00000-0 10270-3 0 9049
2 25544 51
6410 187
8544 0001803 289
1263 70
9694 15
54003707 29704
Satellite: ISS
Catalog Number: 25544
Epoch time: 16070
97005904 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 187
8544 deg
Eccentricity:
0001803
Arg of perigee: 289
1263 deg
Mean anomaly: 70
9694 deg
Mean motion: 15
54003707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2970
Checksum: 307
Coasting Arc #6 (Orbit 2985)
---------------------------------------
Vector Time (GMT): 2016/071/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6734007
26 A = 6789332
15 meter
Y = -371805
55 meter E =
0011581
Z = 729198
24 I = 51
64296
XDOT = 912
953629 Wp = 129
19825
YDOT = 4743
530970 meter/sec RA = 181
74818 deg
ZDOT = -5956
090389 TA = 42
92267
MA = 42
83235
Ha = 220
561 n
mi
Hp = 215
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22093199
68 X = 6734122
27
Y = -1219834
48 feet Y = -296500
66 meter
Z = 2392382
67 Z = 761910
66
XDOT = 2995
254689 XDOT = 888
774534
YDOT = 15562
765650 feet/sec YDOT = 4753
604174 meter/sec
ZDOT = -19540
978967 ZDOT = -5951
714904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20757904
50 X = -6327009
29
Y = -7616239
35 feet Y = -2321429
75 meter
Z = 2534415
59 Z = 772489
87
XDOT = 2736
278477 XDOT = 834
017680
YDOT = -14012
079366 feet/sec YDOT = -4270
881791 meter/sec
ZDOT = -19522
717859 ZDOT = -5950
524403
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 16071
99895408
00016717 00000-0 10270-3 0 9059
2 25544 51
6411 182
7265 0001783 293
6562 66
4403 15
54040871 29866
Satellite: ISS
Catalog Number: 25544
Epoch time: 16071
99895408 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 182
7265 deg
Eccentricity:
0001783
Arg of perigee: 293
6562 deg
Mean anomaly: 66
4403 deg
Mean motion: 15
54040871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2986
Checksum: 329
Coasting Arc #7 (Orbit 3001)
---------------------------------------
Vector Time (GMT): 2016/072/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6704612
01 A = 6789116
82 meter
Y = -376387
26 meter E =
0012678
Z = 951775
37 I = 51
67432
XDOT = 1112
877079 Wp = 47
79302
YDOT = -4749
073052 meter/sec RA = 176
78027 deg
ZDOT = 5919
276025 TA = 322
51162
MA = 322
59997
Ha = 220
496 n
mi
Hp = 215
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21996758
57 X = -6704528
17
Y = -1234866
34 feet Y = -451362
10 meter
Z = 3122622
61 Z = 919206
29
XDOT = 3651
171518 XDOT = 1137
146380
YDOT = -15580
948333 feet/sec YDOT = -4736
491685 meter/sec
ZDOT = 19420
196931 ZDOT = 5924
741642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19897168
47 X = 6064656
95
Y = 9505131
28 feet Y = 2897164
01 meter
Z = 2981311
95 Z = 908703
88
XDOT = -8486
729323 XDOT = -2586
755098
YDOT = 11621
060083 feet/sec YDOT = 3542
099113 meter/sec
ZDOT = 19444
653416 ZDOT = 5926
730361
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 16073
02782765
00016717 00000-0 10270-3 0 9067
2 25544 51
6409 177
5986 0001874 296
6311 63
4649 15
54082352 30020
Satellite: ISS
Catalog Number: 25544
Epoch time: 16073
02782765 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 177
5986 deg
Eccentricity:
0001874
Arg of perigee: 296
6311 deg
Mean anomaly: 63
4649 deg
Mean motion: 15
54082352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3002
Checksum: 321
Coasting Arc #8 (Orbit 3016)
---------------------------------------
Vector Time (GMT): 2016/073/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6169795
38 A = 6786628
44 meter
Y = 1165911
13 meter E =
0003319
Z = -2574021
36 I = 51
69902
XDOT = -3072
050015 Wp = 132
15140
YDOT = 4644
294476 meter/sec RA = 171
81033 deg
ZDOT = -5266
423788 TA = 76
75225
MA = 76
71523
Ha = 220
526 n
mi
Hp = 215
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20242110
84 X = 6168802
80
Y = 3825167
75 feet Y = 1234900
06 meter
Z = -8444951
98 Z = -2544052
60
XDOT = -10078
904248 XDOT = -3098
173344
YDOT = 15237
186602 feet/sec YDOT = 4609
794145 meter/sec
ZDOT = -17278
293267 ZDOT = -5281
410972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17512858
06 X = -5337919
14
Y = -10947701
46 feet Y = -3336859
40 meter
Z = -8315035
11 Z = -2534422
70
XDOT = 14030
054810 XDOT = 4276
360706
YDOT = -9286
938515 feet/sec YDOT = -2830
658859 meter/sec
ZDOT = -17344
073837 ZDOT = -5286
473706
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 16073
99237680
00016717 00000-0 10270-3 0 9075
2 25544 51
6417 172
7905 0001923 306
2933 53
8042 15
54120028 30179
Satellite: ISS
Catalog Number: 25544
Epoch time: 16073
99237680 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 172
7905 deg
Eccentricity:
0001923
Arg of perigee: 306
2933 deg
Mean anomaly: 53
8042 deg
Mean motion: 15
54120028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3017
Checksum: 298
Coasting Arc #9 (Orbit 3032)
---------------------------------------
Vector Time (GMT): 2016/074/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5174557
76 A = 6782901
20 meter
Y = -1962160
81 meter E =
0009682
Z = 3914044
50 I = 51
71760
XDOT = 4765
434760 Wp = 93
38709
YDOT = -4418
433072 meter/sec RA = 166
83443 deg
ZDOT = 4075
869239 TA = 313
97222
MA = 314
05203
Ha = 220
627 n
mi
Hp = 215
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16976895
54 X = -5171244
50
Y = -6437535
48 feet Y = -2020007
26 meter
Z = 12841353
34 Z = 3888916
10
XDOT = 15634
628479 XDOT = 4794
689839
YDOT = -14496
171496 feet/sec YDOT = -4364
978853 meter/sec
ZDOT = 13372
274405 ZDOT = 4099
089933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13755312
75 X = 4192619
33
Y = 11967894
59 feet Y = 3647814
27 meter
Z = 12732559
49 Z = 3880884
13
XDOT = -18746
408622 XDOT = -5713
905348
YDOT = 7178
981061 feet/sec YDOT = 2188
153427 meter/sec
ZDOT = 13473
778737 ZDOT = 4106
807759
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 16075
02120951
00016717 00000-0 10270-3 0 9084
2 25544 51
6410 167
6624 0001886 310
4590 49
6398 15
54141191 30336
Satellite: ISS
Catalog Number: 25544
Epoch time: 16075
02120951 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 167
6624 deg
Eccentricity:
0001886
Arg of perigee: 310
4590 deg
Mean anomaly: 49
6398 deg
Mean motion: 15
54141191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3033
Checksum: 294
Coasting Arc #10 (Orbit 3047)
---------------------------------------
Vector Time (GMT): 2016/075/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3809906
53 A = 6779206
99 meter
Y = 2794491
37 meter E =
0010956
Z = -4871727
75 I = 51
73756
XDOT = -6055
733224 Wp = 63
53636
YDOT = 4007
525645 meter/sec RA = 161
84960 deg
ZDOT = -2436
555301 TA = 182
56115
MA = 182
56676
Ha = 220
489 n
mi
Hp = 215
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12499693
34 X = 3802039
29
Y = 9168278
78 feet Y = 2837051
85 meter
Z = -15983358
74 Z = -4853239
65
XDOT = -19867
891154 XDOT = -6088
260631
YDOT = 13148
050015 feet/sec YDOT = 3939
624319 meter/sec
ZDOT = -7993
947839 ZDOT = -2466
051728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8848941
55 X = -2697157
39
Y = -12827387
14 feet Y = -3909787
60 meter
Z = -15903515
30 Z = -4847391
46
XDOT = 22119
383649 XDOT = 6741
988136
YDOT = -5186
320680 feet/sec YDOT = -1580
790543 meter/sec
ZDOT = -8122
654951 ZDOT = -2475
785229
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 16075
98572171
00016717 00000-0 10270-3 0 9095
2 25544 51
6418 162
8544 0001959 315
8342 44
2654 15
54190011 30484
Satellite: ISS
Catalog Number: 25544
Epoch time: 16075
98572171 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 162
8544 deg
Eccentricity:
0001959
Arg of perigee: 315
8342 deg
Mean anomaly: 44
2654 deg
Mean motion: 15
54190011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3048
Checksum: 313
Coasting Arc #11 (Orbit 3063)
---------------------------------------
Vector Time (GMT): 2016/076/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2198240
51 A = 6777135
61 meter
Y = -3603355
00 meter E =
0001229
Z = 5301135
53 I = 51
76167
XDOT = 6858
036225 Wp = 74
33417
YDOT = -3392
248959 meter/sec RA = 156
85904 deg
ZDOT = 538
244009 TA = 10
54124
MA = 10
53867
Ha = 220
461 n
mi
Hp = 215
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7212075
15 X = -2183533
92
Y = -11822030
85 feet Y = -3627854
45 meter
Z = 17392176
95 Z = 5290493
20
XDOT = 22500
118848 XDOT = 6892
844959
YDOT = -11129
425720 feet/sec YDOT = -3315
363163 meter/sec
ZDOT = 1765
892417 ZDOT = 571
643195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3222335
38 X = 982167
83
Y = 13526896
48 feet Y = 4122998
05 meter
Z = 17346523
77 Z = 5287220
44
XDOT = -23864
087443 XDOT = -7273
773853
YDOT = 3234
540842 feet/sec YDOT = 985
888049 meter/sec
ZDOT = 1911
470806 ZDOT = 582
616302
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 16077
01451265
00016717 00000-0 10270-3 0 9103
2 25544 51
6421 157
7258 0002081 316
1762 43
9225 15
54239186 30645
Satellite: ISS
Catalog Number: 25544
Epoch time: 16077
01451265 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 157
7258 deg
Eccentricity:
0002081
Arg of perigee: 316
1762 deg
Mean anomaly: 43
9225 deg
Mean motion: 15
54239186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3064
Checksum: 292
Coasting Arc #12 (Orbit 3066)
---------------------------------------
Vector Time (GMT): 2016/077/03:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2315684
22 A = 6781220
30 meter
Y = -4726472
62 meter E =
0009036
Z = 4271930
44 I = 51
78033
XDOT = 6775
067689 Wp = 60
48609
YDOT = 61
803887 meter/sec RA = 155
83105 deg
ZDOT = -3594
122206 TA = 66
17917
MA = 66
08447
Ha = 220
323 n
mi
Hp = 215
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7597389
19 X = 2347613
71
Y = -15506799
94 feet Y = -4700398
16 meter
Z = 14015519
82 Z = 4283257
36
XDOT = 22227
912364 XDOT = 6791
331577
YDOT = 202
768657 feet/sec YDOT = 137
657781 meter/sec
ZDOT = -11791
739520 ZDOT = -3561
171448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8115768
91 X = 2473686
36
Y = 15195831
40 feet Y = 4631689
41 meter
Z = 14065452
91 Z = 4287150
05
XDOT = -12183
352576 XDOT = -3713
485865
YDOT = 17319
434483 feet/sec YDOT = 5278
963630 meter/sec
ZDOT = -11648
646099 ZDOT = -3550
507331
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 16077
20740719
00016717 00000-0 10270-3 0 9110
2 25544 51
6411 156
7621 0002252 315
4191 44
6780 15
54235187 30679
Satellite: ISS
Catalog Number: 25544
Epoch time: 16077
20740719 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 156
7621 deg
Eccentricity:
0002252
Arg of perigee: 315
4191 deg
Mean anomaly: 44
6780 deg
Mean motion: 15
54235187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3067
Checksum: 293
Coasting Arc #13 (Orbit 3081)
---------------------------------------
Vector Time (GMT): 2016/078/03:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3719666
82 A = 6785075
35 meter
Y = 4799244
07 meter E =
0004210
Z = -3026896
12 I = 51
82024
XDOT = -5697
720871 Wp = 45
81534
YDOT = -1290
767940 meter/sec RA = 150
85651 deg
ZDOT = 4962
342841 TA = 279
60463
MA = 279
65219
Ha = 220
436 n
mi
Hp = 214
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12203631
31 X = -3758353
52
Y = 15745551
40 feet Y = 4757431
64 meter
Z = -9930761
53 Z = -3045059
60
XDOT = -18693
309945 XDOT = -5706
968364
YDOT = -4234
802954 feet/sec YDOT = -1354
534805 meter/sec
ZDOT = 16280
652366 ZDOT = 4934
642746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5909698
31 X = -1801276
04
Y = -18982576
94 feet Y = -5785889
45 meter
Z = -10010408
05 Z = -3051172
37
XDOT = 12882
179245 XDOT = 3926
488234
YDOT = -12520
485606 feet/sec YDOT = -3816
244013 meter/sec
ZDOT = 16160
540996 ZDOT = 4925
732896
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 16078
17188070
00016717 00000-0 10270-3 0 9124
2 25544 51
6393 151
9532 0002032 320
3264 39
7740 15
54232982 30826
Satellite: ISS
Catalog Number: 25544
Epoch time: 16078
17188070 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 151
9532 deg
Eccentricity:
0002032
Arg of perigee: 320
3264 deg
Mean anomaly: 39
7740 deg
Mean motion: 15
54232982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3082
Checksum: 294
Coasting Arc #14 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2016/078/21:26:42
000
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3122709
25 A = 6777201
34 meter
Y = -2911946
21 meter E =
0001764
Z = 5261554
90 I = 51
81657
XDOT = 5976
250530 Wp = 94
62314
YDOT = -4716
230925 meter/sec RA = 147
27149 deg
ZDOT = 936
326342 TA = 346
44039
MA = 346
44513
Ha = 220
517 n
mi
Hp = 214
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10245109
10 X = -3115473
12
Y = -9553629
28 feet Y = -2946825
33 meter
Z = 17262319
21 Z = 5246403
67
XDOT = 19607
121161 XDOT = 6023
996215
YDOT = -15473
198573 feet/sec YDOT = -4649
133446 meter/sec
ZDOT = 3071
936818 ZDOT = 965
473643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1229159
28 X = 374647
75
Y = 14034791
05 feet Y = 4277804
31 meter
Z = 17196963
84 Z = 5241634
58
XDOT = -23876
954753 XDOT = -7277
695809
YDOT = -1830
637796 feet/sec YDOT = -557
978400 meter/sec
ZDOT = 3199
289223 ZDOT = 975
143355
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 16078
94344902
00016717 00000-0 10270-3 0 9138
2 25544 51
6415 148
1093 0002157 324
3457 35
7551 15
54286173 30947
Satellite: ISS
Catalog Number: 25544
Epoch time: 16078
94344902 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 148
1093 deg
Eccentricity:
0002157
Arg of perigee: 324
3457 deg
Mean anomaly: 35
7551 deg
Mean motion: 15
54286173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3094
Checksum: 309
Coasting Arc #15 (Orbit 3096)
---------------------------------------
Vector Time (GMT): 2016/079/03:12:07
000
Vector Time (MET): N/A
Weight (LBS) : 905198
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4767020
46 A = 6788006
02 meter
Y = 4597456
80 meter E =
0009102
Z = -1467086
73 I = 51
85770
XDOT = -4288
777296 Wp = 24
74793
YDOT = -2603
030647 meter/sec RA = 146
05545 deg
ZDOT = 5799
401590 TA = 319
29030
MA = 319
35829
Ha = 220
418 n
mi
Hp = 214
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15639830
91 X = -4810949
68
Y = 15083519
70 feet Y = 4543903
01 meter
Z = -4813276
67 Z = -1490350
70
XDOT = -14070
791655 XDOT = -4287
521464
YDOT = -8540
126794 feet/sec YDOT = -2650
982867 meter/sec
ZDOT = 19026
908104 ZDOT = 5778
571414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 642843
48 X = 195938
69
Y = -21695932
19 feet Y = -6612920
13 meter
Z = -4915057
31 Z = -1498109
47
XDOT = 14540
044100 XDOT = 4431
805442
YDOT = -3843
877692 feet/sec YDOT = -1171
613921 meter/sec
ZDOT = 18936
833854 ZDOT = 5771
946959
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 16079
13633900
00016717 00000-0 10270-3 0 9140
2 25544 51
6402 147
1459 0002165 322
8022 37
2980 15
54255232 30976
Satellite: ISS
Catalog Number: 25544
Epoch time: 16079
13633900 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 147
1459 deg
Eccentricity:
0002165
Arg of perigee: 322
8022 deg
Mean anomaly: 37
2980 deg
Mean motion: 15
54255232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3097
Checksum: 290
Coasting Arc #16 (Orbit 3112)
---------------------------------------
Vector Time (GMT): 2016/080/03:12:07
000
Vector Time (MET): N/A
Weight (LBS) : 905198
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5421262
98 A = 6788808
27 meter
Y = -4068072
67 meter E =
0009377
Z = -303844
84 I = 51
88716
XDOT = 2631
583556 Wp = 133
87040
YDOT = 3947
705625 meter/sec RA = 141
10041 deg
ZDOT = -6023
000862 TA = 49
39261
MA = 49
31107
Ha = 220
496 n
mi
Hp = 214
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17786295
86 X = 5467826
19
Y = -13346695
13 feet Y = -4007188
20 meter
Z = -996866
27 Z = -277396
35
XDOT = 8633
804317 XDOT = 2616
500559
YDOT = 12951
790108 feet/sec YDOT = 3977
048572 meter/sec
ZDOT = -19760
501516 ZDOT = -6010
254618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3039942
10 X = -926574
35
Y = 22033210
27 feet Y = 6715722
49 meter
Z = -881323
29 Z = -268627
34
XDOT = -13758
836016 XDOT = -4193
693218
YDOT = -2668
463687 feet/sec YDOT = -813
347732 meter/sec
ZDOT = -19705
751870 ZDOT = -6006
313170
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 16080
16507840
00016717 00000-0 10270-3 0 9159
2 25544 51
6406 142
0164 0002259 330
3119 29
7906 15
54296518 31137
Satellite: ISS
Catalog Number: 25544
Epoch time: 16080
16507840 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 142
0164 deg
Eccentricity:
0002259
Arg of perigee: 330
3119 deg
Mean anomaly: 29
7906 deg
Mean motion: 15
54296518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3113
Checksum: 290
Coasting Arc #17 (Orbit 3117)
---------------------------------------
Vector Time (GMT): 2016/080/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905198
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4555831
83 A = 6778781
92 meter
Y = -1156263
35 meter E =
0005352
Z = 4881124
17 I = 51
86412
XDOT = 4121
159383 Wp = 112
66696
YDOT = -5999
917524 meter/sec RA = 139
62181 deg
ZDOT = 2421
102537 TA = 313
65342
MA = 313
69778
Ha = 220
530 n
mi
Hp = 214
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14946954
83 X = -4566273
75
Y = -3793514
91 feet Y = -1207267
37 meter
Z = 16014186
91 Z = 4858968
13
XDOT = 13520
864116 XDOT = 4176
185113
YDOT = -19684
768779 feet/sec YDOT = -5953
523967 meter/sec
ZDOT = 7943
249793 ZDOT = 2441
256382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11826762
57 X = -3604797
23
Y = -10049760
84 feet Y = -3063167
10 meter
Z = 15918115
18 Z = 4851841
51
XDOT = 20046
193704 XDOT = 6110
079841
YDOT = -10847
479039 feet/sec YDOT = -3306
311611 meter/sec
ZDOT = 8031
755480 ZDOT = 2448
079070
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 16080
48655554
00016717 00000-0 10270-3 0 9161
2 25544 51
6434 140
4129 0001881 323
8443 36
2582 15
54317427 31189
Satellite: ISS
Catalog Number: 25544
Epoch time: 16080
48655554 = yrday
fracday
Element set: 916
Inclination: 51
6434 deg
RA of node: 140
4129 deg
Eccentricity:
0001881
Arg of perigee: 323
8443 deg
Mean anomaly: 36
2582 deg
Mean motion: 15
54317427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3118
Checksum: 304
Coasting Arc #18 (Orbit 3132)
---------------------------------------
Vector Time (GMT): 2016/081/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905198
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3345985
20 A = 6776967
38 meter
Y = 2555407
99 meter E =
0013992
Z = -5322535
31 I = 51
88031
XDOT = -5101
100645 Wp = 79
15135
YDOT = 5692
940560 meter/sec RA = 134
63886 deg
ZDOT = -472
025340 TA = 186
34649
MA = 186
36423
Ha = 220
503 n
mi
Hp = 214
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10977641
74 X = 3343015
68
Y = 8383884
47 feet Y = 2592807
59 meter
Z = -17462386
18 Z = -5306289
10
XDOT = -16735
894506 XDOT = -5162
088522
YDOT = 18677
626508 feet/sec YDOT = 5635
555584 meter/sec
ZDOT = -1548
639566 ZDOT = -496
954007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6459207
81 X = 1968766
54
Y = 12309460
66 feet Y = 3751923
61 meter
Z = -17392207
48 Z = -5301144
84
XDOT = -22193
395060 XDOT = -6764
546814
YDOT = 9296
214344 feet/sec YDOT = 2833
486132 meter/sec
ZDOT = -1657
852627 ZDOT = -505
313481
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 16081
45098153
00016717 00000-0 10270-3 0 9176
2 25544 51
6421 135
6051 0001968 330
0377 30
0663 15
54291293 31338
Satellite: ISS
Catalog Number: 25544
Epoch time: 16081
45098153 = yrday
fracday
Element set: 917
Inclination: 51
6421 deg
RA of node: 135
6051 deg
Eccentricity:
0001968
Arg of perigee: 330
0377 deg
Mean anomaly: 30
0663 deg
Mean motion: 15
54291293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3133
Checksum: 288
Coasting Arc #19 (Orbit 3148)
---------------------------------------
Vector Time (GMT): 2016/082/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905198
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2008401
08 A = 6777415
85 meter
Y = -3911261
25 meter E =
0005345
Z = 5156143
37 I = 51
90447
XDOT = 5661
568836 Wp = 33
66743
YDOT = -4941
172929 meter/sec RA = 129
65468 deg
ZDOT = -1537
822500 TA = 71
12082
MA = 71
06286
Ha = 220
484 n
mi
Hp = 214
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6589242
40 X = -1989561
32
Y = -12832221
95 feet Y = -3933614
35 meter
Z = 16916480
88 Z = 5146433
51
XDOT = 18574
700904 XDOT = 5723
871522
YDOT = -16211
197272 feet/sec YDOT = -4877
513395 meter/sec
ZDOT = -5045
349408 ZDOT = -1510
168041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -838965
87 X = -255716
80
Y = -14449382
01 feet Y = -4404171
64 meter
Z = 16874917
98 Z = 5143475
00
XDOT = 22568
727482 XDOT = 6878
948136
YDOT = -7081
006539 feet/sec YDOT = -2158
290793 meter/sec
ZDOT = -4924
400728 ZDOT = -1500
957342
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 16082
47968768
00016717 00000-0 10270-3 0 9188
2 25544 51
6422 130
4758 0001979 332
7858 27
3191 15
54361674 31494
Satellite: ISS
Catalog Number: 25544
Epoch time: 16082
47968768 = yrday
fracday
Element set: 918
Inclination: 51
6422 deg
RA of node: 130
4758 deg
Eccentricity:
0001979
Arg of perigee: 332
7858 deg
Mean anomaly: 27
3191 deg
Mean motion: 15
54361674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3149
Checksum: 346
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