[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 17th 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) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
There are no maneuvers
Coasting Arc #1 (Orbit 4)
---------------------------------------
Vector Time (GMT): 2016/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3454298
96 A = 6776362
72 meter
Y = 2652429
55 meter E =
0015775
Z = -5205428
64 I = 51
40671
XDOT = -5625
989479 Wp = 99
90255
YDOT = -5065
216627 meter/sec RA = 215
01722 deg
ZDOT = 1152
727226 TA = 181
20021
MA = 181
20400
Ha = 220
786 n
mi
Hp = 213
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11333001
83 X = -3458416
35
Y = 8702196
70 feet Y = 2613778
29 meter
Z = -17078177
97 Z = -5222218
94
XDOT = -18457
970733 XDOT = -5574
530337
YDOT = -16618
164786 feet/sec YDOT = -5127
842467 meter/sec
ZDOT = 3781
913472 ZDOT = 1125
522240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 388186
35 X = 118319
20
Y = 14195113
70 feet Y = 4326670
66 meter
Z = -17151599
89 Z = -5227807
65
XDOT = -23291
994587 XDOT = -7099
399950
YDOT = 5063
403105 feet/sec YDOT = 1543
325266 meter/sec
ZDOT = 3664
524759 ZDOT = 1116
947147
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16137
51417764
00016717 00000-0 10270-3 0 9000
2 25544 51
6421 216
0436 0001563 108
1993 251
9331 15
54612257 56
Satellite: ISS
Catalog Number: 25544
Epoch time: 16137
51417764 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 216
0436 deg
Eccentricity:
0001563
Arg of perigee: 108
1993 deg
Mean anomaly: 251
9331 deg
Mean motion: 15
54612257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 5
Checksum: 280
Coasting Arc #2 (Orbit 20)
---------------------------------------
Vector Time (GMT): 2016/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4869144
54 A = 6778999
73 meter
Y = -1343622
06 meter E =
0009801
Z = 4514518
62 I = 51
44355
XDOT = 4415
360009 Wp = 73
34990
YDOT = 5435
645948 meter/sec RA = 210
00155 deg
ZDOT = -3136
018836 TA = 48
20162
MA = 48
11793
Ha = 220
537 n
mi
Hp = 213
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15974883
65 X = 4861877
48
Y = -4408208
86 feet Y = -1289212
73 meter
Z = 14811412
80 Z = 4538154
37
XDOT = 14486
089269 XDOT = 4369
482738
YDOT = 17833
484080 feet/sec YDOT = 5484
764961 meter/sec
ZDOT = -10288
775710 ZDOT = -3114
681195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5561190
63 X = 1695050
90
Y = -15512631
67 feet Y = -4728250
13 meter
Z = 14914374
93 Z = 4545901
48
XDOT = 21829
759321 XDOT = 6653
710641
YDOT = -2004
178050 feet/sec YDOT = -610
873470 meter/sec
ZDOT = -10196
938578 ZDOT = -3108
026878
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16138
54268332
00016717 00000-0 10270-3 0 9010
2 25544 51
6427 210
9129 0001457 112
1474 247
9834 15
54660751 218
Satellite: ISS
Catalog Number: 25544
Epoch time: 16138
54268332 = yrday
fracday
Element set: 901
Inclination: 51
6427 deg
RA of node: 210
9129 deg
Eccentricity:
0001457
Arg of perigee: 112
1474 deg
Mean anomaly: 247
9834 deg
Mean motion: 15
54660751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 21
Checksum: 292
Coasting Arc #3 (Orbit 35)
---------------------------------------
Vector Time (GMT): 2016/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5938831
79 A = 6783121
67 meter
Y = 112014
85 meter E =
0006164
Z = -3281105
29 I = 51
48499
XDOT = -2703
043071 Wp = 92
81026
YDOT = -5401
259936 meter/sec RA = 204
99929 deg
ZDOT = 4715
515680 TA = 229
02233
MA = 229
07567
Ha = 220
690 n
mi
Hp = 213
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19484356
26 X = -5923704
52
Y = 367502
80 feet Y = 45687
54 meter
Z = -10764781
12 Z = -3309918
38
XDOT = -8868
251546 XDOT = -2665
350258
YDOT = -17720
669083 feet/sec YDOT = -5431
276511 meter/sec
ZDOT = 15470
851970 ZDOT = 4702
476193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10622970
92 X = -3237881
54
Y = 16254690
00 feet Y = 4954429
51 meter
Z = -10890052
86 Z = -3319288
11
XDOT = -18508
405877 XDOT = -5641
362111
YDOT = -1784
338961 feet/sec YDOT = -543
866515 meter/sec
ZDOT = 15415
071074 ZDOT = 4698
513663
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16139
50690088
00016717 00000-0 10270-3 0 9025
2 25544 51
6421 206
1034 0001594 112
6921 247
4401 15
54656363 363
Satellite: ISS
Catalog Number: 25544
Epoch time: 16139
50690088 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 206
1034 deg
Eccentricity:
0001594
Arg of perigee: 112
6921 deg
Mean anomaly: 247
4401 deg
Mean motion: 15
54656363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 36
Checksum: 282
Coasting Arc #4 (Orbit 51)
---------------------------------------
Vector Time (GMT): 2016/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6509043
66 A = 6786607
04 meter
Y = 1019072
43 meter E =
0015506
Z = 1597918
08 I = 51
52587
XDOT = 620
993516 Wp = 116
06220
YDOT = 5068
646043 meter/sec RA = 200
01112 deg
ZDOT = -5725
597636 TA = 46
41596
MA = 46
28735
Ha = 220
665 n
mi
Hp = 213
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21355130
12 X = 6489402
23
Y = 3343413
50 feet Y = 1091751
01 meter
Z = 5242513
40 Z = 1629490
30
XDOT = 2037
380303 XDOT = 592
081494
YDOT = 16629
416150 feet/sec YDOT = 5075
428953 meter/sec
ZDOT = -18784
769146 ZDOT = -5722
650993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14489875
08 X = 4416513
92
Y = -15993977
57 feet Y = -4874964
36 meter
Z = 5379604
50 Z = 1639703
45
XDOT = 13921
070547 XDOT = 4243
142303
YDOT = 6258
366471 feet/sec YDOT = 1907
550100 meter/sec
ZDOT = -18772
805354 ZDOT = -5721
951072
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16140
53539119
00016717 00000-0 10270-3 0 9038
2 25544 51
6418 200
9730 0001586 108
5997 251
5328 15
54673981 529
Satellite: ISS
Catalog Number: 25544
Epoch time: 16140
53539119 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 200
9730 deg
Eccentricity:
0001586
Arg of perigee: 108
5997 deg
Mean anomaly: 251
5328 deg
Mean motion: 15
54673981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 52
Checksum: 311
Coasting Arc #5 (Orbit 67)
---------------------------------------
Vector Time (GMT): 2016/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6490485
34 A = 6787892
48 meter
Y = -1951340
62 meter E =
0013336
Z = 253498
75 I = 51
55900
XDOT = 1596
335535 Wp = 53
92191
YDOT = -4502
548952 meter/sec RA = 195
03191 deg
ZDOT = 5999
953298 TA = 308
81331
MA = 308
93230
Ha = 220
770 n
mi
Hp = 213
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21294243
23 X = -6469413
98
Y = -6402036
15 feet Y = -2023803
74 meter
Z = 831688
83 Z = 222020
07
XDOT = 5237
321309 XDOT = 1617
419771
YDOT = -14772
142230 feet/sec YDOT = -4484
580090 meter/sec
ZDOT = 19684
886148 ZDOT = 6007
759023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16786526
77 X = -5116533
36
Y = 14589443
46 feet Y = 4446862
37 meter
Z = 695144
73 Z = 211880
12
XDOT = -8695
195931 XDOT = -2650
295720
YDOT = -10984
065733 feet/sec YDOT = -3347
943235 meter/sec
ZDOT = 19719
578675 ZDOT = 6010
527580
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 16141
56387700
00016717 00000-0 10270-3 0 9040
2 25544 51
6408 195
8425 0001576 108
8903 251
2420 15
54616938 686
Satellite: ISS
Catalog Number: 25544
Epoch time: 16141
56387700 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 195
8425 deg
Eccentricity:
0001576
Arg of perigee: 108
8903 deg
Mean anomaly: 251
2420 deg
Mean motion: 15
54616938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 68
Checksum: 310
Coasting Arc #6 (Orbit 82)
---------------------------------------
Vector Time (GMT): 2016/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5833400
34 A = 6785879
72 meter
Y = 2739984
78 meter E =
0008049
Z = -2118001
55 I = 51
58470
XDOT = -3765
569649 Wp = 134
10325
YDOT = 3771
053179 meter/sec RA = 190
05315 deg
ZDOT = -5511
146741 TA = 69
37895
MA = 69
29264
Ha = 220
749 n
mi
Hp = 213
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19138452
55 X = 5812616
12
Y = 8989451
37 feet Y = 2805101
68 meter
Z = -6948823
98 Z = -2089714
11
XDOT = -12354
231132 XDOT = -3780
687363
YDOT = 12372
221717 feet/sec YDOT = 3728
859928 meter/sec
ZDOT = -18081
190094 ZDOT = -5529
475741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17644470
42 X = 5378034
58
Y = -11723967
80 feet Y = -3573465
39 meter
Z = -6826272
71 Z = -2080647
92
XDOT = 3360
332774 XDOT = 1024
229429
YDOT = 15595
846571 feet/sec YDOT = 4753
614035 meter/sec
ZDOT = -18161
527182 ZDOT = -5535
633485
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 16142
52807132
00016717 00000-0 10270-3 0 9054
2 25544 51
6414 191
0319 0001694 112
7701 247
3631 15
54682139 837
Satellite: ISS
Catalog Number: 25544
Epoch time: 16142
52807132 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 191
0319 deg
Eccentricity:
0001694
Arg of perigee: 112
7701 deg
Mean anomaly: 247
3631 deg
Mean motion: 15
54682139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 83
Checksum: 285
Coasting Arc #7 (Orbit 98)
---------------------------------------
Vector Time (GMT): 2016/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4610765
87 A = 6782066
14 meter
Y = -3335954
77 meter E =
0013513
Z = 3678931
88 I = 51
60264
XDOT = 5603
282980 Wp = 97
28586
YDOT = -2949
947185 meter/sec RA = 185
06797 deg
ZDOT = 4332
274852 TA = 306
55870
MA = 306
68301
Ha = 220
796 n
mi
Hp = 213
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15127184
61 X = -4590990
68
Y = -10944733
50 feet Y = -3387405
16 meter
Z = 12069986
47 Z = 3656581
29
XDOT = 18383
474345 XDOT = 5614
808892
YDOT = -9678
304412 feet/sec YDOT = -2887
223467 meter/sec
ZDOT = 14213
500170 ZDOT = 4359
522417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17120463
92 X = -5218317
40
Y = 7604756
69 feet Y = 2317929
84 meter
Z = 11973339
95 Z = 3649474
02
XDOT = 1429
875214 XDOT = 435
825965
YDOT = -19426
626217 feet/sec YDOT = -5921
235671 meter/sec
ZDOT = 14332
500405 ZDOT = 4368
546123
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 16143
55653974
00016717 00000-0 10270-3 0 9062
2 25544 51
6404 185
9013 0001730 114
1460 245
9874 15
54682275 999
Satellite: ISS
Catalog Number: 25544
Epoch time: 16143
55653974 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 185
9013 deg
Eccentricity:
0001730
Arg of perigee: 114
1460 deg
Mean anomaly: 245
9874 deg
Mean motion: 15
54682275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 99
Checksum: 315
Coasting Arc #8 (Orbit 113)
---------------------------------------
Vector Time (GMT): 2016/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2907401
37 A = 6778016
43 meter
Y = 3809247
14 meter E =
0012483
Z = -4805192
73 I = 51
62160
XDOT = -6919
840800 Wp = 77
81319
YDOT = 2033
191397 meter/sec RA = 180
07182 deg
ZDOT = -2578
187688 TA = 166
77455
MA = 166
74179
Ha = 220
684 n
mi
Hp = 213
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9538718
40 X = 2887931
23
Y = 12497529
98 feet Y = 3841651
23 meter
Z = -15765068
03 Z = -4791116
03
XDOT = -22702
889764 XDOT = -6929
538248
YDOT = 6670
575449 feet/sec YDOT = 1955
755158 meter/sec
ZDOT = -8458
621022 ZDOT = -2611
826399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15615874
31 X = 4759718
49
Y = -2286177
47 feet Y = -696826
89 meter
Z = -15704478
23 Z = -4786724
96
XDOT = -5441
474676 XDOT = -1658
561481
YDOT = 21874
137754 feet/sec YDOT = 6667
237187 meter/sec
ZDOT = -8605
285941 ZDOT = -2622
891155
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 16144
52072377
00016717 00000-0 10270-3 0 9073
2 25544 51
6408 181
0909 0001682 120
2856 239
8463 15
54683502 1145
Satellite: ISS
Catalog Number: 25544
Epoch time: 16144
52072377 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 181
0909 deg
Eccentricity:
0001682
Arg of perigee: 120
2856 deg
Mean anomaly: 239
8463 deg
Mean motion: 15
54683502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 114
Checksum: 302
Coasting Arc #9 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2016/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -930967
09 A = 6775757
22 meter
Y = -4122989
61 meter E =
0004546
Z = 5292356
95 I = 51
64596
XDOT = 7582
711328 Wp = 115
27418
YDOT = -1057
573414 meter/sec RA = 175
06804 deg
ZDOT = 507
720288 TA = 329
87236
MA = 329
89850
Ha = 220
694 n
mi
Hp = 213
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3054353
97 X = -910501
88
Y = -13526868
80 feet Y = -4133286
41 meter
Z = 17363375
84 Z = 5287883
79
XDOT = 24877
661838 XDOT = 7591
507499
YDOT = -3469
729050 feet/sec YDOT = -972
729361 meter/sec
ZDOT = 1665
748977 ZDOT = 544
576889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13407557
92 X = -4086623
65
Y = -3632345
32 feet Y = -1107138
85 meter
Z = 17344611
16 Z = 5286637
48
XDOT = 8482
979560 XDOT = 2585
612170
YDOT = -22556
356802 feet/sec YDOT = -6875
177553 meter/sec
ZDOT = 1826
271698 ZDOT = 556
647614
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 16145
54917874
00016717 00000-0 10270-3 0 9087
2 25544 51
6402 175
9597 0001716 117
9370 242
1957 15
54709084 1303
Satellite: ISS
Catalog Number: 25544
Epoch time: 16145
54917874 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 175
9597 deg
Eccentricity:
0001716
Arg of perigee: 117
9370 deg
Mean anomaly: 242
1957 deg
Mean motion: 15
54709084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 130
Checksum: 324
Coasting Arc #10 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2016/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1123532
40 A = 6776548
35 meter
Y = 4307091
18 meter E =
0015027
Z = -5123116
34 I = 51
68182
XDOT = -7480
740532 Wp = 104
38827
YDOT = -3
658596 meter/sec RA = 170
06421 deg
ZDOT = 1637
879427 TA = 181
42887
MA = 181
43317
Ha = 220
607 n
mi
Hp = 213
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3686129
93 X = -1146725
78
Y = 14130876
56 feet Y = 4294397
92 meter
Z = -16808124
48 Z = -5128630
13
XDOT = -24543
111982 XDOT = -7488
099812
YDOT = -12
003269 feet/sec YDOT = -87
354526 meter/sec
ZDOT = 5373
620167 ZDOT = 1601
521685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10906474
40 X = 3324293
40
Y = 9668839
55 feet Y = 2947062
29 meter
Z = -16832843
87 Z = -5130650
81
XDOT = -10595
821662 XDOT = -3229
606442
YDOT = 21029
665183 feet/sec YDOT = 6409
841948 meter/sec
ZDOT = 5215
422611 ZDOT = 1589
660812
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 16146
51334899
00016717 00000-0 10270-3 0 9096
2 25544 51
6416 171
1494 0001535 120
9375 239
1929 15
54693993 1452
Satellite: ISS
Catalog Number: 25544
Epoch time: 16146
51334899 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 171
1494 deg
Eccentricity:
0001535
Arg of perigee: 120
9375 deg
Mean anomaly: 239
1929 deg
Mean motion: 15
54693993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 145
Checksum: 332
Coasting Arc #11 (Orbit 160)
---------------------------------------
Vector Time (GMT): 2016/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3034115
30 A = 6779716
14 meter
Y = -4296229
48 meter E =
0010996
Z = 4269912
17 I = 51
72263
XDOT = 6685
723943 Wp = 79
58260
YDOT = 1146
769975 meter/sec RA = 165
06926 deg
ZDOT = -3587
120450 TA = 47
01112
MA = 46
91901
Ha = 220
504 n
mi
Hp = 213
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9954446
53 X = 3061189
81
Y = -14095241
07 feet Y = -4262149
00 meter
Z = 14008898
20 Z = 4284716
58
XDOT = 21934
789840 XDOT = 6689
828352
YDOT = 3762
368684 feet/sec YDOT = 1221
557473 meter/sec
ZDOT = -11768
767882 ZDOT = -3554
632626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8248097
20 X = -2514020
03
Y = -15096556
98 feet Y = -4601430
57 meter
Z = 14074051
13 Z = 4289770
79
XDOT = 12042
830612 XDOT = 3670
654770
YDOT = -17449
498013 feet/sec YDOT = -5318
606994 meter/sec
ZDOT = -11627
581440 ZDOT = -3544
086823
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 16147
54179143
00016717 00000-0 10270-3 0 9101
2 25544 51
6397 166
0184 0001644 121
2860 238
8454 15
54745374 1611
Satellite: ISS
Catalog Number: 25544
Epoch time: 16147
54179143 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 166
0184 deg
Eccentricity:
0001644
Arg of perigee: 121
2860 deg
Mean anomaly: 238
8454 deg
Mean motion: 15
54745374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 161
Checksum: 306
Coasting Arc #12 (Orbit 175)
---------------------------------------
Vector Time (GMT): 2016/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4585310
86 A = 6783910
01 meter
Y = 4082316
13 meter E =
0005586
Z = -2889896
49 I = 51
76882
XDOT = -5261
184327 Wp = 80
62674
YDOT = -2333
989982 meter/sec RA = 160
08859 deg
ZDOT = 5059
950920 TA = 246
54068
MA = 246
59942
Ha = 220
519 n
mi
Hp = 213
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15043670
79 X = -4616581
63
Y = 13393425
62 feet Y = 4030865
52 meter
Z = -9481287
69 Z = -2912246
48
XDOT = -17261
103434 XDOT = -5259
273189
YDOT = -7657
447447 feet/sec YDOT = -2392
813776 meter/sec
ZDOT = 16600
888845 ZDOT = 5034
397762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5679299
37 X = 1731050
45
Y = 19276257
92 feet Y = 5875403
41 meter
Z = -9579255
51 Z = -2919757
08
XDOT = -12954
802689 XDOT = -3948
623860
YDOT = 11996
616095 feet/sec YDOT = 3656
568586 meter/sec
ZDOT = 16490
066635 ZDOT = 5026
172310
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 16148
50595073
00016717 00000-0 10270-3 0 9113
2 25544 51
6411 161
2083 0001637 125
3662 234
7644 15
54747974 1760
Satellite: ISS
Catalog Number: 25544
Epoch time: 16148
50595073 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 161
2083 deg
Eccentricity:
0001637
Arg of perigee: 125
3662 deg
Mean anomaly: 234
7644 deg
Mean motion: 15
54747974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 176
Checksum: 307
Coasting Arc #13 (Orbit 191)
---------------------------------------
Vector Time (GMT): 2016/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5655549
83 A = 6786987
48 meter
Y = -3574129
97 meter E =
0015280
Z = 1097178
71 I = 51
80794
XDOT = 3392
856530 Wp = 123
20696
YDOT = 3542
137742 meter/sec RA = 155
12111 deg
ZDOT = -5899
093003 TA = 44
91019
MA = 44
78667
Ha = 220
531 n
mi
Hp = 213
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18554953
49 X = 5689766
67
Y = -11726148
21 feet Y = -3510694
61 meter
Z = 3599667
70 Z = 1124734
92
XDOT = 11131
419063 XDOT = 3381
650643
YDOT = 11621
186816 feet/sec YDOT = 3580
016671 meter/sec
ZDOT = -19353
979669 ZDOT = -5882
638272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3026414
27 X = -922451
07
Y = -21719742
21 feet Y = -6620177
43 meter
Z = 3720224
93 Z = 1133924
56
XDOT = 13646
771696 XDOT = 4159
536013
YDOT = -5232
153262 feet/sec YDOT = -1594
760314 meter/sec
ZDOT = -19282
954163 ZDOT = -5877
444429
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 16149
53438031
00016717 00000-0 10270-3 0 9128
2 25544 51
6401 156
0766 0001608 124
1964 235
9341 15
54747846 1922
Satellite: ISS
Catalog Number: 25544
Epoch time: 16149
53438031 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 156
0766 deg
Eccentricity:
0001608
Arg of perigee: 124
1964 deg
Mean anomaly: 235
9341 deg
Mean motion: 15
54747846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 192
Checksum: 304
Coasting Arc #14 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2016/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6129553
96 A = 6787158
75 meter
Y = 2787423
84 meter E =
0013594
Z = 804018
37 I = 51
83667
XDOT = -1320
451767 Wp = 60
24492
YDOT = -4642
834292 meter/sec RA = 150
16181 deg
ZDOT = 5960
587371 TA = 308
42801
MA = 308
54996
Ha = 220
402 n
mi
Hp = 213
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20110085
16 X = -6164173
66
Y = 9145091
35 feet Y = 2718685
47 meter
Z = 2637855
56 Z = 774158
45
XDOT = -4332
190835 XDOT = -1297
390402
YDOT = -15232
395972 feet/sec YDOT = -4657
471858 meter/sec
ZDOT = 19555
732844 ZDOT = 5954
228664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 397725
87 X = 121226
85
Y = 22103423
30 feet Y = 6737123
42 meter
Z = 2507388
20 Z = 764251
92
XDOT = -14136
446850 XDOT = -4308
789000
YDOT = -1987
912960 feet/sec YDOT = -605
915870 meter/sec
ZDOT = 19528
840725 ZDOT = 5952
390653
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 16150
56280185
00016717 00000-0 10270-3 0 9139
2 25544 51
6392 150
9462 0001584 136
3892 223
7386 15
54791073 2088
Satellite: ISS
Catalog Number: 25544
Epoch time: 16150
56280185 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 150
9462 deg
Eccentricity:
0001584
Arg of perigee: 136
3892 deg
Mean anomaly: 223
7386 deg
Mean motion: 15
54791073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 311
Coasting Arc #15 (Orbit 222)
---------------------------------------
Vector Time (GMT): 2016/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6023643
08 A = 6784634
82 meter
Y = -1658713
87 meter E =
0006597
Z = -2643089
95 I = 51
85480
XDOT = -766
610659 Wp = 128
88635
YDOT = 5543
464599 meter/sec RA = 145
19910 deg
ZDOT = -5238
819657 TA = 80
81018
MA = 80
73557
Ha = 220
511 n
mi
Hp = 213
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19762608
52 X = 6054582
63
Y = -5441974
65 feet Y = -1591180
36 meter
Z = -8671554
97 Z = -2613753
30
XDOT = -2515
126835 XDOT = -803
093962
YDOT = 18187
219812 feet/sec YDOT = 5534
688120 meter/sec
ZDOT = -17187
728534 ZDOT = -5242
632026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2527115
09 X = 770264
68
Y = -20395911
24 feet Y = -6216673
74 meter
Z = -8543543
95 Z = -2604072
19
XDOT = 14406
718319 XDOT = 4391
167744
YDOT = 8974
199679 feet/sec YDOT = 2735
336062 meter/sec
ZDOT = -17205
274791 ZDOT = -5244
167756
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 16151
52694523
00016717 00000-0 10270-3 0 9142
2 25544 51
6388 146
1348 0001523 132
1139 228
0143 15
54752711 2236
Satellite: ISS
Catalog Number: 25544
Epoch time: 16151
52694523 = yrday
fracday
Element set: 914
Inclination: 51
6388 deg
RA of node: 146
1348 deg
Eccentricity:
0001523
Arg of perigee: 132
1139 deg
Mean anomaly: 228
0143 deg
Mean motion: 15
54752711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 223
Checksum: 282
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