[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 12th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 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 2046)
---------------------------------------
Vector Time (GMT): 2016/011/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4859875
05 A = 6786336
27 meter
Y = 4099771
16 meter E =
0016845
Z = 2343311
93 I = 51
96000
XDOT = -1715
888292 Wp = 54
21096
YDOT = -5147
118315 meter/sec RA = 123
08949 deg
ZDOT = 5428
945139 TA = 331
83435
MA = 331
92536
Ha = 221
767 n
mi
Hp = 213
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15944471
96 X = -4916741
14
Y = 13450692
80 feet Y = 4045106
75 meter
Z = 7688031
27 Z = 2319566
32
XDOT = -5629
554763 XDOT = -1684
575501
YDOT = -16886
871111 feet/sec YDOT = -5166
131712 meter/sec
ZDOT = 17811
499800 ZDOT = 5420
685696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20814945
51 X = -6344395
39
Y = -1862481
55 feet Y = -567684
38 meter
Z = 7584349
25 Z = 2311709
65
XDOT = 7792
347201 XDOT = 2375
107427
YDOT = -14458
499110 feet/sec YDOT = -4406
950529 meter/sec
ZDOT = 17776
623942 ZDOT = 5418
314978
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 16011
62957874
00016717 00000-0 10270-3 0 9004
2 25544 51
6429 123
7794 0005805 4
3594 355
7608 15
54379431 20474
Satellite: ISS
Catalog Number: 25544
Epoch time: 16011
62957874 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 123
7794 deg
Eccentricity:
0005805
Arg of perigee: 4
3594 deg
Mean anomaly: 355
7608 deg
Mean motion: 15
54379431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2047
Checksum: 322
Coasting Arc #2 (Orbit 2061)
---------------------------------------
Vector Time (GMT): 2016/012/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4875317
06 A = 6782512
00 meter
Y = -2779917
04 meter E =
0009761
Z = -3820414
42 I = 51
96310
XDOT = 331
666571 Wp = 42
91678
YDOT = 6382
329489 meter/sec RA = 118
12985 deg
ZDOT = -4220
219868 TA = 182
68289
MA = 182
68813
Ha = 221
771 n
mi
Hp = 213
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15995134
71 X = 4924598
07
Y = -9120462
74 feet Y = -2725122
35 meter
Z = -12534168
04 Z = -3796612
12
XDOT = 1088
144917 XDOT = 280
772828
YDOT = 20939
401212 feet/sec YDOT = 6385
753978 meter/sec
ZDOT = -13845
865710 ZDOT = -4218
732146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17884310
54 X = 5451137
85
Y = 4665561
54 feet Y = 1422063
16 meter
Z = -12430467
22 Z = -3788806
41
XDOT = -13411
479958 XDOT = -4087
819091
YDOT = 14528
729832 feet/sec YDOT = 4428
356853 meter/sec
ZDOT = -13840
573310 ZDOT = -4218
606745
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 16012
59395133
00016717 00000-0 10270-3 0 9016
2 25544 51
6420 118
9706 0005847 7
6472 352
4769 15
54383432 20626
Satellite: ISS
Catalog Number: 25544
Epoch time: 16012
59395133 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 118
9706 deg
Eccentricity:
0005847
Arg of perigee: 7
6472 deg
Mean anomaly: 352
4769 deg
Mean motion: 15
54383432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2062
Checksum: 306
Coasting Arc #3 (Orbit 2077)
---------------------------------------
Vector Time (GMT): 2016/013/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4601571
02 A = 6778603
67 meter
Y = 1130371
10 meter E =
0007801
Z = 4840076
50 I = 51
96518
XDOT = 910
148087 Wp = 73
29754
YDOT = -7183
628291 meter/sec RA = 113
15868 deg
ZDOT = 2541
802454 TA = 351
82899
MA = 351
84169
Ha = 221
956 n
mi
Hp = 213
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15097017
77 X = -4637379
77
Y = 3708566
59 feet Y = 1078713
00 meter
Z = 15879516
09 Z = 4817636
59
XDOT = 2986
050154 XDOT = 978
062744
YDOT = -23568
334288 feet/sec YDOT = -7173
070716 meter/sec
ZDOT = 8339
246895 ZDOT = 2546
388511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13617945
63 X = -4150749
83
Y = -7701432
34 feet Y = -2347396
58 meter
Z = 15782013
17 Z = 4810357
61
XDOT = 17711
225579 XDOT = 5398
381557
YDOT = -14177
095348 feet/sec YDOT = -4321
178662 meter/sec
ZDOT = 8360
440505 ZDOT = 2548
262266
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 16013
62260016
00016717 00000-0 10270-3 0 9023
2 25544 51
6424 113
8400 0005945 11
1108 349
0175 15
54433299 20787
Satellite: ISS
Catalog Number: 25544
Epoch time: 16013
62260016 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 113
8400 deg
Eccentricity:
0005945
Arg of perigee: 11
1108 deg
Mean anomaly: 349
0175 deg
Mean motion: 15
54433299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2078
Checksum: 274
Coasting Arc #4 (Orbit 2092)
---------------------------------------
Vector Time (GMT): 2016/014/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4152686
22 A = 6776639
86 meter
Y = 700526
57 meter E =
0017656
Z = -5323689
94 I = 51
96906
XDOT = -1965
112539 Wp = 66
71641
YDOT = 7379
103496 meter/sec RA = 108
18015 deg
ZDOT = -556
549769 TA = 197
95737
MA = 198
01983
Ha = 221
975 n
mi
Hp = 213
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13624298
62 X = 4170404
00
Y = 2298315
51 feet Y = 747063
72 meter
Z = -17466174
34 Z = -5303474
44
XDOT = -6447
219615 XDOT = -2044
777994
YDOT = 24209
657139 feet/sec YDOT = 7356
682872 meter/sec
ZDOT = -1825
950685 ZDOT = -566
289167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8628791
83 X = 2630055
75
Y = 10931497
49 feet Y = 3331920
44 meter
Z = -17378645
72 Z = -5297011
22
XDOT = -20237
456978 XDOT = -6168
376887
YDOT = 12974
414684 feet/sec YDOT = 3954
601596 meter/sec
ZDOT = -1869
534641 ZDOT = -569
834159
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 16014
58694774
00016717 00000-0 10270-3 0 9032
2 25544 51
6413 109
0306 0006082 14
6935 345
4393 15
54412995 20935
Satellite: ISS
Catalog Number: 25544
Epoch time: 16014
58694774 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 109
0306 deg
Eccentricity:
0006082
Arg of perigee: 14
6935 deg
Mean anomaly: 345
4393 deg
Mean motion: 15
54412995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2093
Checksum: 311
Coasting Arc #5 (Orbit 2108)
---------------------------------------
Vector Time (GMT): 2016/015/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3545023
18 A = 6777042
20 meter
Y = -2575734
85 meter E =
0010294
Z = 5166742
67 I = 51
98071
XDOT = 2845
122353 Wp = 33
90510
YDOT = -6963
028809 meter/sec RA = 103
19910 deg
ZDOT = -1509
352885 TA = 70
61220
MA = 70
50096
Ha = 222
035 n
mi
Hp = 213
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11630653
47 X = -3541054
79
Y = -8450573
66 feet Y = -2615355
44 meter
Z = 16951255
49 Z = 5149531
64
XDOT = 9334
390923 XDOT = 2930
104923
YDOT = -22844
582707 feet/sec YDOT = -6930
737609 meter/sec
ZDOT = -4951
945161 ZDOT = -1495
325673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3258486
56 X = -993186
70
Y = -14091669
85 feet Y = -4295140
97 meter
Z = 16877098
81 Z = 5144139
72
XDOT = 21074
294361 XDOT = 6423
444921
YDOT = -10768
032739 feet/sec YDOT = -3282
096379 meter/sec
ZDOT = -4889
832255 ZDOT = -1490
420871
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 16015
61556912
00016717 00000-0 10270-3 0 9049
2 25544 51
6417 103
8997 0006159 18
0538 342
0833 15
54487217 21098
Satellite: ISS
Catalog Number: 25544
Epoch time: 16015
61556912 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 103
8997 deg
Eccentricity:
0006159
Arg of perigee: 18
0538 deg
Mean anomaly: 342
0833 deg
Mean motion: 15
54487217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2109
Checksum: 311
Coasting Arc #6 (Orbit 2123)
---------------------------------------
Vector Time (GMT): 2016/016/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2882094
27 A = 6780033
06 meter
Y = 4255743
64 meter E =
0011359
Z = -4429627
85 I = 51
99653
XDOT = -3525
254079 Wp = 76
60027
YDOT = 5900
414868 meter/sec RA = 98
22437 deg
ZDOT = 3384
951894 TA = 227
45512
MA = 227
55107
Ha = 222
160 n
mi
Hp = 212
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9455689
87 X = 2855808
40
Y = 13962413
53 feet Y = 4287826
16 meter
Z = -14532899
76 Z = -4415691
28
XDOT = -11565
794221 XDOT = -3607
414511
YDOT = 19358
316495 feet/sec YDOT = 5860
533756 meter/sec
ZDOT = 11105
485218 ZDOT = 3367
627636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1732922
25 X = -528194
70
Y = 16825160
49 feet Y = 5128308
92 meter
Z = -14473257
85 Z = -4411448
99
XDOT = -20163
306758 XDOT = -6145
775900
YDOT = 7382
943353 feet/sec YDOT = 2250
321134 meter/sec
ZDOT = 11029
258101 ZDOT = 3361
717869
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 16016
57989191
00016717 00000-0 10270-3 0 9055
2 25544 51
6411 99
0897 0006368 23
7673 336
3773 15
54489526 21243
Satellite: ISS
Catalog Number: 25544
Epoch time: 16016
57989191 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 99
0897 deg
Eccentricity:
0006368
Arg of perigee: 23
7673 deg
Mean anomaly: 336
3773 deg
Mean motion: 15
54489526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2124
Checksum: 342
Coasting Arc #7 (Orbit 2139)
---------------------------------------
Vector Time (GMT): 2016/017/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2127094
33 A = 6784056
23 meter
Y = -5626350
29 meter E =
0016441
Z = 3129331
47 I = 52
01451
XDOT = 4071
785291 Wp = 73
50813
YDOT = -4275
995834 meter/sec RA = 93
26020 deg
ZDOT = -4894
513929 TA = 70
64832
MA = 70
47063
Ha = 222
162 n
mi
Hp = 212
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6978655
95 X = -2079221
89
Y = -18459154
50 feet Y = -5649869
24 meter
Z = 10266835
55 Z = 3119114
82
XDOT = 13358
875628 XDOT = 4143
073252
YDOT = -14028
857724 feet/sec YDOT = -4230
063777 meter/sec
ZDOT = -16058
116565 ZDOT = -4874
561201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6228462
88 X = 1898435
48
Y = -18749250
23 feet Y = -5714771
47 meter
Z = 10223590
45 Z = 3116150
37
XDOT = 17935
052262 XDOT = 5466
603929
YDOT = -2796
844589 feet/sec YDOT = -852
478231 meter/sec
ZDOT = -15970
781860 ZDOT = -4867
894311
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 16017
60848719
00016717 00000-0 10270-3 0 9061
2 25544 51
6416 93
9585 0006470 26
2129 333
9350 15
54526732 21406
Satellite: ISS
Catalog Number: 25544
Epoch time: 16017
60848719 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 93
9585 deg
Eccentricity:
0006470
Arg of perigee: 26
2129 deg
Mean anomaly: 333
9350 deg
Mean motion: 15
54526732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2140
Checksum: 311
Coasting Arc #8 (Orbit 2154)
---------------------------------------
Vector Time (GMT): 2016/018/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1358999
32 A = 6787292
81 meter
Y = 6472826
23 meter E =
0014862
Z = -1495406
93 I = 52
02612
XDOT = -4467
693768 Wp = 34
48911
YDOT = 2270
396880 meter/sec RA = 88
30762 deg
ZDOT = 5807
170930 TA = 309
26502
MA = 309
39678
Ha = 222
315 n
mi
Hp = 212
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4458659
20 X = 1293781
59
Y = 21236306
52 feet Y = 6487658
85 meter
Z = -4906190
71 Z = -1488963
49
XDOT = -14657
787952 XDOT = -4520
958472
YDOT = 7448
808663 feet/sec YDOT = 2220
138181 meter/sec
ZDOT = 19052
398065 ZDOT = 5785
338777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9630924
12 X = -2935505
67
Y = 19451658
74 feet Y = 5928865
58 meter
Z = -4879481
19 Z = -1487265
87
XDOT = -14799
221012 XDOT = -4510
802565
YDOT = -2605
025631 feet/sec YDOT = -794
011812 meter/sec
ZDOT = 18957
281904 ZDOT = 5778
179524
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 16018
57278494
00016717 00000-0 10270-3 0 9076
2 25544 51
6417 89
1485 0006564 30
5283 329
6251 15
54505270 21558
Satellite: ISS
Catalog Number: 25544
Epoch time: 16018
57278494 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 89
1485 deg
Eccentricity:
0006564
Arg of perigee: 30
5283 deg
Mean anomaly: 329
6251 deg
Mean motion: 15
54505270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2155
Checksum: 318
Coasting Arc #9 (Orbit 2170)
---------------------------------------
Vector Time (GMT): 2016/019/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -492994
96 A = 6788044
65 meter
Y = -6758373
19 meter E =
0011815
Z = -373673
13 I = 52
02792
XDOT = 4734
011952 Wp = 104
13153
YDOT = -20
997613 meter/sec RA = 83
36114 deg
ZDOT = -6027
788271 TA = 79
87360
MA = 79
74034
Ha = 222
328 n
mi
Hp = 212
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1617437
52 X = -415569
39
Y = -22173140
40 feet Y = -6763453
26 meter
Z = -1225961
72 Z = -375880
20
XDOT = 15531
535276 XDOT = 4763
175120
YDOT = -68
889808 feet/sec YDOT = 32
104562 meter/sec
ZDOT = -19776
208237 ZDOT = -6004
720940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12154429
19 X = 3704670
02
Y = -18614880
28 feet Y = -5673815
51 meter
Z = -1234230
38 Z = -376193
42
XDOT = 11142
029321 XDOT = 3396
090537
YDOT = 8544
714103 feet/sec YDOT = 2604
428858 meter/sec
ZDOT = -19676
159197 ZDOT = -5997
293323
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 16019
60135484
00016717 00000-0 10270-3 0 9083
2 25544 51
6424 84
0172 0006661 35
0364 325
1226 15
54547962 21716
Satellite: ISS
Catalog Number: 25544
Epoch time: 16019
60135484 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 84
0172 deg
Eccentricity:
0006661
Arg of perigee: 35
0364 deg
Mean anomaly: 325
1226 deg
Mean motion: 15
54547962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2171
Checksum: 293
Coasting Arc #10 (Orbit 2186)
---------------------------------------
Vector Time (GMT): 2016/020/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -402603
21 A = 6786215
82 meter
Y = 6410970
95 meter E =
0020104
Z = 2154214
51 I = 52
01632
XDOT = -4856
251706 Wp = 59
98501
YDOT = -2173
924264 meter/sec RA = 78
41309 deg
ZDOT = 5533
421377 TA = 323
80603
MA = 323
94191
Ha = 222
533 n
mi
Hp = 212
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1320876
69 X = -484726
49
Y = 21033369
25 feet Y = 6406009
48 meter
Z = 7067632
92 Z = 2152059
65
XDOT = -15932
584336 XDOT = -4858
460127
YDOT = -7132
297454 feet/sec YDOT = -2228
242714 meter/sec
ZDOT = 18154
269610 ZDOT = 5509
825684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13555829
78 X = -4131816
92
Y = 16141142
16 feet Y = 4919820
13 meter
Z = 7057037
70 Z = 2150985
09
XDOT = -7533
457267 XDOT = -2296
197775
YDOT = -14260
573201 feet/sec YDOT = -4346
622712 meter/sec
ZDOT = 18052
351015 ZDOT = 5502
356590
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 16020
62991313
00016717 00000-0 10270-3 0 9099
2 25544 51
6418 78
8866 0006891 39
1020 321
0630 15
54526204 21876
Satellite: ISS
Catalog Number: 25544
Epoch time: 16020
62991313 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 78
8866 deg
Eccentricity:
0006891
Arg of perigee: 39
1020 deg
Mean anomaly: 321
0630 deg
Mean motion: 15
54526204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2187
Checksum: 299
Coasting Arc #11 (Orbit 2201)
---------------------------------------
Vector Time (GMT): 2016/021/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1398855
01 A = 6782172
73 meter
Y = -5503957
84 meter E =
0011878
Z = -3721988
78 I = 51
99701
XDOT = 4764
116180 Wp = 58
91798
YDOT = 4140
056665 meter/sec RA = 73
45548 deg
ZDOT = -4335
914177 TA = 165
16140
MA = 165
12651
Ha = 222
426 n
mi
Hp = 212
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4589419
33 X = 1478377
22
Y = -18057604
46 feet Y = -5487870
09 meter
Z = -12211249
27 Z = -3715000
73
XDOT = 15630
302428 XDOT = 4738
528669
YDOT = 13582
863074 feet/sec YDOT = 4193
189321 meter/sec
ZDOT = -14225
440213 ZDOT = -4312
833557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14249624
90 X = 4343285
67
Y = -12035519
40 feet Y = -3668426
31 meter
Z = -12179857
15 Z = -3712420
46
XDOT = 4096
859221 XDOT = 1248
722691
YDOT = 19131
923565 feet/sec YDOT = 5831
410303 meter/sec
ZDOT = -14126
140213 ZDOT = -4305
647537
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 16021
59417145
00016717 00000-0 10270-3 0 9104
2 25544 51
6427 74
0763 0006777 42
5185 317
6492 15
54583279 22023
Satellite: ISS
Catalog Number: 25544
Epoch time: 16021
59417145 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 74
0763 deg
Eccentricity:
0006777
Arg of perigee: 42
5185 deg
Mean anomaly: 317
6492 deg
Mean motion: 15
54583279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2202
Checksum: 311
Coasting Arc #12 (Orbit 2217)
---------------------------------------
Vector Time (GMT): 2016/022/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2411454
31 A = 6778241
55 meter
Y = 4120669
01 meter E =
0011553
Z = 4801009
51 I = 51
97246
XDOT = -4449
655883 Wp = 83
98597
YDOT = -5675
222714 meter/sec RA = 68
48470 deg
ZDOT = 2631
789307 TA = 340
19292
MA = 340
23775
Ha = 222
616 n
mi
Hp = 211
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7911595
50 X = -2480674
23
Y = 13519255
29 feet Y = 4093315
28 meter
Z = 15751343
54 Z = 4789127
55
XDOT = -14598
608541 XDOT = -4398
647303
YDOT = -18619
497092 feet/sec YDOT = -5724
696625 meter/sec
ZDOT = 8634
479355 ZDOT = 2610
298018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14242702
44 X = -4341175
70
Y = 6644970
47 feet Y = 2025387
00 meter
Z = 15698988
03 Z = 4785051
55
XDOT = -1113
407414 XDOT = -339
366580
YDOT = -22601
066446 feet/sec YDOT = -6888
805053 meter/sec
ZDOT = 8542
378025 ZDOT = 2603
716822
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 16022
62270266
00016717 00000-0 10270-3 0 9111
2 25544 51
6412 68
9448 0006897 46
6119 313
5608 15
54590514 22185
Satellite: ISS
Catalog Number: 25544
Epoch time: 16022
62270266 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 68
9448 deg
Eccentricity:
0006897
Arg of perigee: 46
6119 deg
Mean anomaly: 313
5608 deg
Mean motion: 15
54590514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2218
Checksum: 310
Coasting Arc #13 (Orbit 2232)
---------------------------------------
Vector Time (GMT): 2016/023/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3432951
45 A = 6776101
36 meter
Y = -2448609
92 meter E =
0020577
Z = -5321727
88 I = 51
95328
XDOT = 3807
494815 Wp = 74
10366
YDOT = 6614
317759 meter/sec RA = 63
50420 deg
ZDOT = -583
596841 TA = 190
31919
MA = 190
36149
Ha = 222
501 n
mi
Hp = 212
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11262964
08 X = 3485927
38
Y = -8033497
11 feet Y = -2409924
00 meter
Z = -17459737
15 Z = -5304923
23
XDOT = 12491
780890 XDOT = 3736
083706
YDOT = 21700
517583 feet/sec YDOT = 6656
496422 meter/sec
ZDOT = -1914
687799 ZDOT = -565
274604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13918997
96 X = 4242510
58
Y = -458295
10 feet Y = -139688
35 meter
Z = -17386354
37 Z = -5299360
81
XDOT = -1519
107255 XDOT = -463
023891
YDOT = 23985
870584 feet/sec YDOT = 7310
893354 meter/sec
ZDOT = -1836
522883 ZDOT = -559
772175
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 16023
58693794
00016717 00000-0 10270-3 0 9123
2 25544 51
6418 64
1347 0006796 49
1790 310
9951 15
54597399 22335
Satellite: ISS
Catalog Number: 25544
Epoch time: 16023
58693794 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 64
1347 deg
Eccentricity:
0006796
Arg of perigee: 49
1790 deg
Mean anomaly: 310
9951 deg
Mean motion: 15
54597399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2233
Checksum: 342
Coasting Arc #14 (Orbit 2248)
---------------------------------------
Vector Time (GMT): 2016/024/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4349108
24 A = 6776665
66 meter
Y = 623727
26 meter E =
0011773
Z = 5152873
06 I = 51
93910
XDOT = -2841
704845 Wp = 53
35138
YDOT = -6959
762303 meter/sec RA = 58
51884 deg
ZDOT = -1546
713366 TA = 51
53142
MA = 51
42585
Ha = 222
661 n
mi
Hp = 211
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14268727
81 X = -4380789
54
Y = 2046349
26 feet Y = 574915
43 meter
Z = 16905751
52 Z = 5131669
73
XDOT = -9323
178626 XDOT = -2756
154774
YDOT = -22833
865823 feet/sec YDOT = -6991
061766 meter/sec
ZDOT = -5074
518917 ZDOT = -1560
309656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13239717
44 X = -4035465
87
Y = -5966545
40 feet Y = -1818603
04 meter
Z = 16813648
96 Z = 5124800
20
XDOT = 3941
566122 XDOT = 1201
389354
YDOT = -23294
886290 feet/sec YDOT = -7100
281341 meter/sec
ZDOT = -5132
110068 ZDOT = -1564
267149
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 16024
61544263
00016717 00000-0 10270-3 0 9135
2 25544 51
6404 59
0024 0006919 52
8516 307
3268 15
54641214 22493
Satellite: ISS
Catalog Number: 25544
Epoch time: 16024
61544263 = yrday
fracday
Element set: 913
Inclination: 51
6404 deg
RA of node: 59
0024 deg
Eccentricity:
0006919
Arg of perigee: 52
8516 deg
Mean anomaly: 307
3268 deg
Mean motion: 15
54641214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2249
Checksum: 292
Coasting Arc #15 (Orbit 2263)
---------------------------------------
Vector Time (GMT): 2016/025/13:40:37
923
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5072165
12 A = 6779888
57 meter
Y = 1100738
40 meter E =
0013870
Z = -4373485
45 I = 51
93242
XDOT = 1538
159126 Wp = 85
98976
YDOT = 6653
312254 meter/sec RA = 53
53974 deg
ZDOT = 3468
824750 TA = 219
07759
MA = 219
17786
Ha = 222
613 n
mi
Hp = 211
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16640961
69 X = 5080723
44
Y = 3611346
46 feet Y = 1157506
53 meter
Z = -14348705
53 Z = -4348825
93
XDOT = 5046
453826 XDOT = 1446
796165
YDOT = 21828
452277 feet/sec YDOT = 6670
002150 meter/sec
ZDOT = 11380
658629 ZDOT = 3476
074622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12405411
74 X = 3781169
50
Y = 11794966
50 feet Y = 3595105
79 meter
Z = -14241955
78 Z = -4340948
12
XDOT = -6261
005489 XDOT = -1908
354473
YDOT = 20321
579669 feet/sec YDOT = 6194
017483 meter/sec
ZDOT = 11410
776275 ZDOT = 3478
004609
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 16025
57965400
00016717 00000-0 10270-3 0 9142
2 25544 51
6406 54
1921 0006949 55
5524 304
6285 15
54630673 22642
Satellite: ISS
Catalog Number: 25544
Epoch time: 16025
57965400 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 54
1921 deg
Eccentricity:
0006949
Arg of perigee: 55
5524 deg
Mean anomaly: 304
6285 deg
Mean motion: 15
54630673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2264
Checksum: 308
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