[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 30th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21226 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 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
There are no maneuvers
Coasting Arc #1 (Orbit 1394)
---------------------------------------
Vector Time (GMT): 2015/334/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4399789
21 A = 6778919
56 meter
Y = -1983814
48 meter E =
0005315
Z = -4763695
43 I = 51
46523
XDOT = 5129
477140 Wp = 111
85644
YDOT = -5047
519298 meter/sec RA = 332
44866 deg
ZDOT = -2639
925803 TA = 132
04483
MA = 131
99959
Ha = 220
524 n
mi
Hp = 215
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14435003
97 X = -4354138
38
Y = -6508577
69 feet Y = -2032760
34 meter
Z = -15628922
01 Z = -4784958
05
XDOT = 16828
993243 XDOT = 5198
362316
YDOT = -16560
102684 feet/sec YDOT = -4989
772807 meter/sec
ZDOT = -8661
173893 ZDOT = -2614
840647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7349080
24 X = -2239999
66
Y = -13923184
87 feet Y = -4243786
75 meter
Z = -15720371
15 Z = -4791569
13
XDOT = 22473
572973 XDOT = 6849
945042
YDOT = -2222
525915 feet/sec YDOT = -677
425899 meter/sec
ZDOT = -8551
731528 ZDOT = -2606
567770
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 15334
72582026
00016717 00000-0 10270-3 0 9005
2 25544 51
6433 332
9101 0008105 226
4249 133
6231 15
54359913 13958
Satellite: ISS
Catalog Number: 25544
Epoch time: 15334
72582026 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 332
9101 deg
Eccentricity:
0008105
Arg of perigee: 226
4249 deg
Mean anomaly: 133
6231 deg
Mean motion: 15
54359913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1395
Checksum: 287
Coasting Arc #2 (Orbit 1410)
---------------------------------------
Vector Time (GMT): 2015/335/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2933354
40 A = 6776655
20 meter
Y = 3106918
73 meter E =
0007532
Z = 5263616
32 I = 51
43026
XDOT = -6114
228744 Wp = 208
69179
YDOT = 4570
512608 meter/sec RA = 327
43566 deg
ZDOT = 703
526540 TA = 234
53226
MA = 234
60258
Ha = 220
312 n
mi
Hp = 216
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9623866
13 X = 2872825
30
Y = 10193302
91 feet Y = 3139382
81 meter
Z = 17269082
40 Z = 5277719
12
XDOT = -20059
805591 XDOT = -6168
300390
YDOT = 14995
120104 feet/sec YDOT = 4501
836909 meter/sec
ZDOT = 2308
157938 ZDOT = 673
693533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1519445
10 X = 463126
87
Y = 13861020
21 feet Y = 4224838
96 meter
Z = 17329363
40 Z = 5281989
96
XDOT = -24045
813973 XDOT = -7329
164099
YDOT = -112
240680 feet/sec YDOT = -34
210959 meter/sec
ZDOT = 2178
311524 ZDOT = 663
949353
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 15335
75449351
00016717 00000-0 10270-3 0 9013
2 25544 51
6433 327
7807 0008256 230
5612 129
4810 15
54417883 14116
Satellite: ISS
Catalog Number: 25544
Epoch time: 15335
75449351 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 327
7807 deg
Eccentricity:
0008256
Arg of perigee: 230
5612 deg
Mean anomaly: 129
4810 deg
Mean motion: 15
54417883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1411
Checksum: 303
Coasting Arc #3 (Orbit 1425)
---------------------------------------
Vector Time (GMT): 2015/336/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1311781
63 A = 6777120
91 meter
Y = -4194165
90 meter E =
0010218
Z = -5166888
90 I = 51
40587
XDOT = 6570
016187 Wp = 135
43651
YDOT = -3709
466517 meter/sec RA = 322
41641 deg
ZDOT = 1337
580782 TA = 147
50042
MA = 147
43746
Ha = 220
168 n
mi
Hp = 216
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4303745
49 X = -1239685
03
Y = -13760386
79 feet Y = -4208431
87 meter
Z = -16951735
23 Z = -5173086
29
XDOT = 21555
171218 XDOT = 6604
510557
YDOT = -12170
165739 feet/sec YDOT = -3635
803421 meter/sec
ZDOT = 4388
388392 ZDOT = 1369
580474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4642235
55 X = 1414953
40
Y = -13617680
68 feet Y = -4150669
07 meter
Z = -16977638
80 Z = -5174784
31
XDOT = 23586
323952 XDOT = 7189
111541
YDOT = 2373
471704 feet/sec YDOT = 723
434175 meter/sec
ZDOT = 4527
406541 ZDOT = 1379
953514
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 15336
71885292
00016717 00000-0 10270-3 0 9029
2 25544 51
6438 322
9706 0008100 233
7989 126
2415 15
54425693 14266
Satellite: ISS
Catalog Number: 25544
Epoch time: 15336
71885292 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 322
9706 deg
Eccentricity:
0008100
Arg of perigee: 233
7989 deg
Mean anomaly: 126
2415 deg
Mean motion: 15
54425693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1426
Checksum: 319
Coasting Arc #4 (Orbit 1441)
---------------------------------------
Vector Time (GMT): 2015/337/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -276565
29 A = 6779905
87 meter
Y = 5095111
76 meter E =
0002040
Z = 4462255
06 I = 51
39044
XDOT = -6501
106030 Wp = 121
35129
YDOT = 2474
975436 meter/sec RA = 317
40149 deg
ZDOT = -3228
866370 TA = 1
25047
MA = 1
24996
Ha = 219
916 n
mi
Hp = 216
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -907366
44 X = -355195
62
Y = 16716245
92 feet Y = 5091579
29 meter
Z = 14639944
42 Z = 4460720
65
XDOT = -21329
088025 XDOT = -6512
613915
YDOT = 8119
998149 feet/sec YDOT = 2402
211488 meter/sec
ZDOT = -10593
393601 ZDOT = -3260
475581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10361072
47 X = -3158054
89
Y = 13157856
58 feet Y = 4010514
68 meter
Z = 14632264
07 Z = 4459914
09
XDOT = -21133
253940 XDOT = -6441
415801
YDOT = -4708
195142 feet/sec YDOT = -1435
057879 meter/sec
ZDOT = -10730
460253 ZDOT = -3270
644285
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 15337
74747606
00016717 00000-0 10270-3 0 9030
2 25544 51
6434 317
8408 0008061 237
4731 122
5644 15
54465429 14428
Satellite: ISS
Catalog Number: 25544
Epoch time: 15337
74747606 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 317
8408 deg
Eccentricity:
0008061
Arg of perigee: 237
4731 deg
Mean anomaly: 122
5644 deg
Mean motion: 15
54465429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1442
Checksum: 312
Coasting Arc #5 (Orbit 1456)
---------------------------------------
Vector Time (GMT): 2015/338/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1728002
22 A = 6783828
02 meter
Y = -5713513
46 meter E =
0004064
Z = -3224781
74 I = 51
38174
XDOT = 5948
437674 Wp = 218
39257
YDOT = -886
319697 meter/sec RA = 312
39371 deg
ZDOT = 4751
458861 TA = 104
13723
MA = 104
09206
Ha = 219
707 n
mi
Hp = 216
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5669298
62 X = 1807428
61
Y = -18745122
89 feet Y = -5693745
64 meter
Z = -10579992
58 Z = -3216194
55
XDOT = 19515
871633 XDOT = 5934
825613
YDOT = -2907
873021 feet/sec YDOT = -819
876530 meter/sec
ZDOT = 15588
775791 ZDOT = 4780
322384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15196965
94 X = 4632035
22
Y = -12384712
58 feet Y = -3774860
39 meter
Z = -10541723
90 Z = -3213117
44
XDOT = 16846
959661 XDOT = 5134
953305
YDOT = 7279
388349 feet/sec YDOT = 2218
757569 meter/sec
ZDOT = 15713
647266 ZDOT = 4789
519687
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 15338
71178541
00016717 00000-0 10270-3 0 9045
2 25544 51
6440 313
0302 0008076 240
8529 119
1816 15
54515078 14570
Satellite: ISS
Catalog Number: 25544
Epoch time: 15338
71178541 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 313
0302 deg
Eccentricity:
0008076
Arg of perigee: 240
8529 deg
Mean anomaly: 119
1816 deg
Mean motion: 15
54515078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1457
Checksum: 299
Coasting Arc #6 (Orbit 1472)
---------------------------------------
Vector Time (GMT): 2015/339/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2919181
37 A = 6787157
28 meter
Y = 5909135
02 meter E =
0011195
Z = 1588858
25 I = 51
37185
XDOT = -5028
021456 Wp = 152
58011
YDOT = -944
996276 meter/sec RA = 307
39665 deg
ZDOT = -5717
018779 TA = 9
96290
MA = 9
94072
Ha = 219
550 n
mi
Hp = 216
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9577366
69 X = -2992759
96
Y = 19386925
90 feet Y = 5876079
37 meter
Z = 5212789
55 Z = 1574498
69
XDOT = -16496
133387 XDOT = -4989
309144
YDOT = -3100
381482 feet/sec YDOT = -1001
006359 meter/sec
ZDOT = -18756
623292 ZDOT = -5741
350188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18584570
62 X = -5664577
13
Y = 11083675
59 feet Y = 3378304
32 meter
Z = 5149552
77 Z = 1569583
68
XDOT = -11272
102687 XDOT = -3435
736899
YDOT = -10127
541072 feet/sec YDOT = -3086
874519 meter/sec
ZDOT = -18861
538184 ZDOT = -5748
996838
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 15339
74035719
00016717 00000-0 10270-3 0 9059
2 25544 51
6438 307
8997 0008086 243
8730 116
1591 15
54516837 14735
Satellite: ISS
Catalog Number: 25544
Epoch time: 15339
74035719 = yrday
fracday
Element set: 905
Inclination: 51
6438 deg
RA of node: 307
8997 deg
Eccentricity:
0008086
Arg of perigee: 243
8730 deg
Mean anomaly: 116
1591 deg
Mean motion: 15
54516837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1473
Checksum: 338
Coasting Arc #7 (Orbit 1488)
---------------------------------------
Vector Time (GMT): 2015/340/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3799530
96 A = 6787968
52 meter
Y = -5614893
76 meter E =
0005761
Z = 248868
41 I = 51
35693
XDOT = 3844
320112 Wp = 18
31205
YDOT = 2867
975065 meter/sec RA = 302
40392 deg
ZDOT = 5981
869004 TA = 344
37994
MA = 344
39771
Ha = 219
213 n
mi
Hp = 216
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12465652
77 X = 3860826
77
Y = -18421567
44 feet Y = -5572062
17 meter
Z = 816497
41 Z = 267474
75
XDOT = 12612
598792 XDOT = 3782
905939
YDOT = 9409
367010 feet/sec YDOT = 2910
621230 meter/sec
ZDOT = 19625
554474 ZDOT = 6000
395119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20302636
36 X = 6188243
56
Y = -9077986
85 feet Y = -2766970
39 meter
Z = 898012
00 Z = 273714
06
XDOT = 4982
229197 XDOT = 1518
583459
YDOT = 13101
419255 feet/sec YDOT = 3993
312589 meter/sec
ZDOT = 19705
000202 ZDOT = 6006
084062
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 15340
76890013
00016717 00000-0 10270-3 0 9060
2 25544 51
6441 302
7680 0008107 248
8701 111
1586 15
54585497 14893
Satellite: ISS
Catalog Number: 25544
Epoch time: 15340
76890013 = yrday
fracday
Element set: 906
Inclination: 51
6441 deg
RA of node: 302
7680 deg
Eccentricity:
0008107
Arg of perigee: 248
8701 deg
Mean anomaly: 111
1586 deg
Mean motion: 15
54585497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1489
Checksum: 317
Coasting Arc #8 (Orbit 1503)
---------------------------------------
Vector Time (GMT): 2015/341/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4344142
12 A = 6786110
44 meter
Y = 4776085
36 meter E =
0008275
Z = -2071865
13 I = 51
33473
XDOT = -2532
942831 Wp = 205
53169
YDOT = -4695
091155 meter/sec RA = 297
40943 deg
ZDOT = -5511
372980 TA = 357
50624
MA = 357
51037
Ha = 218
989 n
mi
Hp = 217
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14252434
79 X = -4387162
13
Y = 15669571
37 feet Y = 4727265
84 meter
Z = -6797457
78 Z = -2093072
72
XDOT = -8310
179893 XDOT = -2453
480352
YDOT = -15403
842371 feet/sec YDOT = -4722
971661 meter/sec
ZDOT = -18081
932350 ZDOT = -5523
484889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20233105
71 X = -6167050
62
Y = 6166171
49 feet Y = 1879449
07 meter
Z = -6890033
34 Z = -2100082
16
XDOT = 1314
376259 XDOT = 400
621884
YDOT = -15952
409056 feet/sec YDOT = -4862
294280 meter/sec
ZDOT = -18133
303412 ZDOT = -5527
030880
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 15341
73313592
00016717 00000-0 10270-3 0 9071
2 25544 51
6443 297
9579 0008262 251
6416 108
3838 15
54592021 15041
Satellite: ISS
Catalog Number: 25544
Epoch time: 15341
73313592 = yrday
fracday
Element set: 907
Inclination: 51
6443 deg
RA of node: 297
9579 deg
Eccentricity:
0008262
Arg of perigee: 251
6416 deg
Mean anomaly: 108
3838 deg
Mean motion: 15
54592021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1504
Checksum: 316
Coasting Arc #9 (Orbit 1519)
---------------------------------------
Vector Time (GMT): 2015/342/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4572022
60 A = 6782114
66 meter
Y = -3439995
11 meter E =
0004907
Z = 3640611
51 I = 51
30801
XDOT = 1204
261480 Wp = 125
75450
YDOT = 6203
034092 meter/sec RA = 292
40373 deg
ZDOT = 4341
912384 TA = 277
70082
MA = 277
75654
Ha = 218
701 n
mi
Hp = 217
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15000074
15 X = 4592464
68
Y = -11286073
18 feet Y = -3388753
65 meter
Z = 11944263
47 Z = 3662871
28
XDOT = 3950
989107 XDOT = 1113
716443
YDOT = 20351
161720 feet/sec YDOT = 6215
994417 meter/sec
ZDOT = 14245
119369 ZDOT = 4347
542974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18560872
11 X = 5657353
82
Y = -2355581
18 feet Y = -717981
14 meter
Z = 12041111
50 Z = 3670130
79
XDOT = -6958
840567 XDOT = -2121
054605
YDOT = 18218
383556 feet/sec YDOT = 5552
963308 meter/sec
ZDOT = 14268
194372 ZDOT = 4348
945645
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 15342
76162811
00016717 00000-0 10270-3 0 9082
2 25544 51
6443 292
8258 0008044 256
4730 103
5527 15
54645486 15203
Satellite: ISS
Catalog Number: 25544
Epoch time: 15342
76162811 = yrday
fracday
Element set: 908
Inclination: 51
6443 deg
RA of node: 292
8258 deg
Eccentricity:
0008044
Arg of perigee: 256
4730 deg
Mean anomaly: 103
5527 deg
Mean motion: 15
54645486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1520
Checksum: 309
Coasting Arc #10 (Orbit 1534)
---------------------------------------
Vector Time (GMT): 2015/343/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4525481
29 A = 6777909
66 meter
Y = 1685987
57 meter E =
0003429
Z = -4759008
25 I = 51
28303
XDOT = 62
508211 Wp = 50
55727
YDOT = -7207
202407 meter/sec RA = 287
38489 deg
ZDOT = -2611
879661 TA = 193
54700
MA = 193
55621
Ha = 218
206 n
mi
Hp = 217
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14847379
56 X = -4520880
29
Y = 5531455
27 feet Y = 1635406
74 meter
Z = -15613544
12 Z = -4780981
15
XDOT = 205
079433 XDOT = 155
783968
YDOT = -23645
677189 feet/sec YDOT = -7205
981664 meter/sec
ZDOT = -8569
158993 ZDOT = -2611
349994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15583991
01 X = -4750000
46
Y = -2279745
84 feet Y = -694866
53 meter
Z = -15708800
73 Z = -4788042
46
XDOT = 11481
346881 XDOT = 3499
514529
YDOT = -19444
115096 feet/sec YDOT = -5926
566281 meter/sec
ZDOT = -8565
428550 ZDOT = -2610
742622
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 15343
72581353
00016717 00000-0 10270-3 0 9096
2 25544 51
6440 288
0150 0008235 260
2264 99
7959 15
54711260 15350
Satellite: ISS
Catalog Number: 25544
Epoch time: 15343
72581353 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 288
0150 deg
Eccentricity:
0008235
Arg of perigee: 260
2264 deg
Mean anomaly: 99
7959 deg
Mean motion: 15
54711260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1535
Checksum: 310
Coasting Arc #11 (Orbit 1550)
---------------------------------------
Vector Time (GMT): 2015/344/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4257444
88 A = 6775669
23 meter
Y = 307250
64 meter E =
0005866
Z = 5267013
64 I = 51
26747
XDOT = -1212
156705 Wp = 249
57873
YDOT = 7550
037509 meter/sec RA = 282
35518 deg
ZDOT = 537
859271 TA = 195
25189
MA = 195
26958
Ha = 218
134 n
mi
Hp = 217
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13967995
02 X = 4228107
25
Y = 1008040
15 feet Y = 354695
68 meter
Z = 17280228
47 Z = 5287624
47
XDOT = -3976
892076 XDOT = -1299
105730
YDOT = 24770
464267 feet/sec YDOT = 7535
996163 meter/sec
ZDOT = 1764
630153 ZDOT = 531
760276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11774924
38 X = 3588996
95
Y = 7374900
27 feet Y = 2247869
60 meter
Z = 17369206
31 Z = 5294134
08
XDOT = -14575
017104 XDOT = -4442
465213
YDOT = 19168
646861 feet/sec YDOT = 5842
603563 meter/sec
ZDOT = 1736
780068 ZDOT = 529
370565
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 15344
75425419
00016717 00000-0 10270-3 0 9102
2 25544 51
6444 282
8835 0008151 263
2722 96
7504 15
54738027 15516
Satellite: ISS
Catalog Number: 25544
Epoch time: 15344
75425419 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 282
8835 deg
Eccentricity:
0008151
Arg of perigee: 263
2722 deg
Mean anomaly: 96
7504 deg
Mean motion: 15
54738027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1551
Checksum: 312
Coasting Arc #12 (Orbit 1565)
---------------------------------------
Vector Time (GMT): 2015/345/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3815699
57 A = 6776299
26 meter
Y = -2345166
16 meter E =
0005954
Z = -5090268
98 I = 51
26324
XDOT = 2230
272536 Wp = 123
88191
YDOT = -7152
148699 meter/sec RA = 277
32117 deg
ZDOT = 1621
385663 TA = 161
86287
MA = 161
84163
Ha = 217
457 n
mi
Hp = 216
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12518699
39 X = -3764464
96
Y = -7694114
71 feet Y = -2387548
86 meter
Z = -16700357
54 Z = -5108680
83
XDOT = 7317
167113 XDOT = 2302
207714
YDOT = -23465
054787 feet/sec YDOT = -7126
806267 meter/sec
ZDOT = 5319
506770 ZDOT = 1632
393993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7585278
75 X = -2311992
96
Y = -12479310
34 feet Y = -3803693
79 meter
Z = -16779437
93 Z = -5114372
68
XDOT = 16203
172514 XDOT = 4938
726982
YDOT = -17075
413458 feet/sec YDOT = -5204
586022 meter/sec
ZDOT = 5368
479041 ZDOT = 1636
312412
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 15345
71839220
00016717 00000-0 10270-3 0 9119
2 25544 51
6434 278
0715 0008253 267
0041 93
0167 15
54794379 15661
Satellite: ISS
Catalog Number: 25544
Epoch time: 15345
71839220 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 278
0715 deg
Eccentricity:
0008253
Arg of perigee: 267
0041 deg
Mean anomaly: 93
0167 deg
Mean motion: 15
54794379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1566
Checksum: 314
Coasting Arc #13 (Orbit 1581)
---------------------------------------
Vector Time (GMT): 2015/346/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3232205
21 A = 6779525
43 meter
Y = 4192211
36 meter E =
0003212
Z = 4236480
69 I = 51
27179
XDOT = -3114
428719 Wp = 21
86311
YDOT = 6022
563644 meter/sec RA = 272
29499 deg
ZDOT = -3579
681962 TA = 104
91564
MA = 104
88008
Ha = 217
483 n
mi
Hp = 217
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10604347
81 X = 3164507
35
Y = 13753974
28 feet Y = 4227977
07 meter
Z = 13899214
85 Z = 4252018
16
XDOT = -10217
941992 XDOT = -3164
154218
YDOT = 19759
067074 feet/sec YDOT = 5987
458373 meter/sec
ZDOT = -11744
363391 ZDOT = -3594
931481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3444363
61 X = 1049842
03
Y = 16967990
05 feet Y = 5171843
37 meter
Z = 13965523
53 Z = 4256691
57
XDOT = -16521
695931 XDOT = -5035
812920
YDOT = 13085
415119 feet/sec YDOT = 3988
434528 meter/sec
ZDOT = -11811
430161 ZDOT = -3600
123913
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 15346
74678026
00016717 00000-0 10270-3 0 9129
2 25544 51
6437 272
9401 0008373 271
1363 88
8831 15
54856535 15826
Satellite: ISS
Catalog Number: 25544
Epoch time: 15346
74678026 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 272
9401 deg
Eccentricity:
0008373
Arg of perigee: 271
1363 deg
Mean anomaly: 88
8831 deg
Mean motion: 15
54856535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1582
Checksum: 329
Coasting Arc #14 (Orbit 1596)
---------------------------------------
Vector Time (GMT): 2015/347/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2521615
11 A = 6783832
55 meter
Y = -5633013
76 meter E =
0005078
Z = -2808624
43 I = 51
28422
XDOT = 3866
480231 Wp = 303
74149
YDOT = -4260
797564 meter/sec RA = 267
27944 deg
ZDOT = 5070
289653 TA = 24
19481
MA = 24
17097
Ha = 217
543 n
mi
Hp = 217
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8273015
45 X = -2444794
72
Y = -18481016
29 feet Y = -5660782
33 meter
Z = -9214647
08 Z = -2820687
89
XDOT = 12685
302594 XDOT = 3889
208595
YDOT = -13978
994633 feet/sec YDOT = -4217
433430 meter/sec
ZDOT = 16634
808574 ZDOT = 5089
127056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 343770
47 X = 104781
24
Y = -20222005
22 feet Y = -6163667
19 meter
Z = -9265678
34 Z = -2824178
76
XDOT = 15824
221077 XDOT = 4823
222584
YDOT = -7396
455064 feet/sec YDOT = -2254
439504 meter/sec
ZDOT = 16717
029681 ZDOT = 5095
350647
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 15347
71087249
00016717 00000-0 10270-3 0 9139
2 25544 51
6421 268
1278 0008346 273
8760 86
1439 15
54854658 15973
Satellite: ISS
Catalog Number: 25544
Epoch time: 15347
71087249 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 268
1278 deg
Eccentricity:
0008346
Arg of perigee: 273
8760 deg
Mean anomaly: 86
1439 deg
Mean motion: 15
54854658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1597
Checksum: 346
Coasting Arc #15 (Orbit 1612)
---------------------------------------
Vector Time (GMT): 2015/348/16:55:24
188
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1679330
69 A = 6786630
04 meter
Y = 6496120
61 meter E =
0007119
Z = 987426
84 I = 51
29641
XDOT = -4475
876377 Wp = 155
21595
YDOT = 2052
164905 meter/sec RA = 262
27748 deg
ZDOT = -5879
588256 TA = 14
03145
MA = 14
01169
Ha = 218
011 n
mi
Hp = 217
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5509615
12 X = 1601768
13
Y = 21312731
66 feet Y = 6514466
23 meter
Z = 3239589
36 Z = 995396
83
XDOT = -14684
633784 XDOT = -4469
930807
YDOT = 6732
824493 feet/sec YDOT = 2002
146442 meter/sec
ZDOT = -19289
987717 ZDOT = -5901
316498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3635598
37 X = -1108130
38
Y = 21706097
07 feet Y = 6616018
39 meter
Z = 3272782
21 Z = 997544
02
XDOT = -14456
649729 XDOT = -4406
386837
YDOT = 505
779412 feet/sec YDOT = 154
161565 meter/sec
ZDOT = -19384
273913 ZDOT = -5908
326689
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 15348
73921138
00016717 00000-0 10270-3 0 9147
2 25544 51
6420 262
9962 0008298 278
1609 81
8603 15
54911936 16137
Satellite: ISS
Catalog Number: 25544
Epoch time: 15348
73921138 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 262
9962 deg
Eccentricity:
0008298
Arg of perigee: 278
1609 deg
Mean anomaly: 81
8603 deg
Mean motion: 15
54911936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1613
Checksum: 328
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