[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 20th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
361/06:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
5
362/01:03:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
4
364/11:45:00
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
3
Coasting Arc #1 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2017/354/15:32:15
084
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3285745
60 A = 6780895
45 meter
Y = -3968036
13 meter E =
0006964
Z = 4405973
86 I = 51
57339
XDOT = 6662
644995 Wp = 121
64797
YDOT = -1787
790731 meter/sec RA = 187
64776 deg
ZDOT = 3351
082459 TA = 294
41461
MA = 294
48725
Ha = 219
848 n
mi
Hp = 215
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10780005
25 X = -3262531
70
Y = -13018491
23 feet Y = -4004650
27 meter
Z = 14455294
80 Z = 4390068
74
XDOT = 21859
071507 XDOT = 6665
863539
YDOT = -5865
455154 feet/sec YDOT = -1713
266855 meter/sec
ZDOT = 10994
365023 ZDOT = 3383
454985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -437377
74 X = -133312
73
Y = -16956440
09 feet Y = -5168322
94 meter
Z = 14385166
50 Z = 4384598
75
XDOT = 19480
214783 XDOT = 5937
569466
YDOT = 8967
871681 feet/sec YDOT = 2733
407288 meter/sec
ZDOT = 11138
463331 ZDOT = 3395
003623
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 17354
70177205
00016717 00000-0 10270-3 0 9006
2 25544 51
6366 188
5191 0003004 261
1478 98
9334 15
54223743 10753
Satellite: ISS
Catalog Number: 25544
Epoch time: 17354
70177205 = yrday
fracday
Element set: 900
Inclination: 51
6366 deg
RA of node: 188
5191 deg
Eccentricity:
0003004
Arg of perigee: 261
1478 deg
Mean anomaly: 98
9334 deg
Mean motion: 15
54223743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 303
Coasting Arc #2 (Orbit 1089)
---------------------------------------
Vector Time (GMT): 2017/355/15:32:15
084
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1573412
58 A = 6777983
76 meter
Y = 4147202
52 meter E =
0010667
Z = -5134607
59 I = 51
59721
XDOT = -7446
468841 Wp = 75
82935
YDOT = 893
567541 meter/sec RA = 182
64914 deg
ZDOT = -1560
280312 TA = 179
10707
MA = 179
10517
Ha = 219
811 n
mi
Hp = 215
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5162114
77 X = 1551861
73
Y = 13606307
49 feet Y = 4164677
52 meter
Z = -16845825
42 Z = -5127016
42
XDOT = -24430
672049 XDOT = -7448
328499
YDOT = 2931
652037 feet/sec YDOT = 810
285794 meter/sec
ZDOT = -5119
029896 ZDOT = -1596
457111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4077589
06 X = -1242849
15
Y = 14009592
25 feet Y = 4270123
72 meter
Z = -16812657
71 Z = -5124498
07
XDOT = -20136
833830 XDOT = -6137
706951
YDOT = -12196
653953 feet/sec YDOT = -3717
540125 meter/sec
ZDOT = -5279
934143 ZDOT = -1609
323927
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 17355
66626477
00016717 00000-0 10270-3 0 9013
2 25544 51
6376 183
7109 0002909 267
0388 93
0432 15
54207356 10902
Satellite: ISS
Catalog Number: 25544
Epoch time: 17355
66626477 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 183
7109 deg
Eccentricity:
0002909
Arg of perigee: 267
0388 deg
Mean anomaly: 93
0432 deg
Mean motion: 15
54207356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1090
Checksum: 319
Coasting Arc #3 (Orbit 1105)
---------------------------------------
Vector Time (GMT): 2017/356/15:32:15
084
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 271910
90 A = 6777189
49 meter
Y = -4212854
36 meter E =
0000901
Z = 5302074
85 I = 51
62815
XDOT = 7658
651836 Wp = 336
59766
YDOT = -2
555293 meter/sec RA = 177
64631 deg
ZDOT = -394
009873 TA = 117
16444
MA = 117
15526
Ha = 219
835 n
mi
Hp = 215
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 892096
12 X = 293245
31
Y = -13821700
67 feet Y = -4209694
84 meter
Z = 17395258
68 Z = 5303447
15
XDOT = 25126
810484 XDOT = 7660
025094
YDOT = -8
383507 feet/sec YDOT = 83
096701 meter/sec
ZDOT = -1292
683312 ZDOT = -356
803513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8832140
34 X = 2692036
38
Y = -10658153
44 feet Y = -3248605
17 meter
Z = 17401934
71 Z = 5304109
70
XDOT = 19451
546903 XDOT = 5928
831496
YDOT = 14274
210832 feet/sec YDOT = 4350
779462 meter/sec
ZDOT = -1127
301037 ZDOT = -343
601356
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 17356
69505116
00016717 00000-0 10270-3 0 9024
2 25544 51
6384 178
5809 0002853 272
8885 87
1941 15
54196442 11064
Satellite: ISS
Catalog Number: 25544
Epoch time: 17356
69505116 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 178
5809 deg
Eccentricity:
0002853
Arg of perigee: 272
8885 deg
Mean anomaly: 87
1941 deg
Mean motion: 15
54196442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1106
Checksum: 332
Coasting Arc #4 (Orbit 1120)
---------------------------------------
Vector Time (GMT): 2017/357/15:32:15
084
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2086728
31 A = 6778789
41 meter
Y = 4187253
22 meter E =
0009448
Z = -4914394
36 I = 51
66633
XDOT = -7248
917455 Wp = 110
42548
YDOT = -904
606064 meter/sec RA = 172
64900 deg
ZDOT = 2307
619986 TA = 182
15448
MA = 182
15855
Ha = 219
818 n
mi
Hp = 215
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6846221
48 X = -2109524
72
Y = 13737707
40 feet Y = 4163790
88 meter
Z = -16123341
08 Z = -4924586
02
XDOT = -23782
537582 XDOT = -7249
472335
YDOT = -2967
867665 feet/sec YDOT = -985
671685 meter/sec
ZDOT = 7570
931714 ZDOT = 2272
405904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13456429
59 X = -4101519
74
Y = 7282741
04 feet Y = 2219779
47 meter
Z = -16169219
73 Z = -4928378
17
XDOT = -17164
265507 XDOT = -5231
668127
YDOT = -15255
634087 feet/sec YDOT = -4649
917270 meter/sec
ZDOT = 7414
506817 ZDOT = 2259
941678
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 17357
65953512
00016717 00000-0 10270-3 0 9039
2 25544 51
6382 173
7735 0002849 274
8704 85
2124 15
54216556 11212
Satellite: ISS
Catalog Number: 25544
Epoch time: 17357
65953512 = yrday
fracday
Element set: 903
Inclination: 51
6382 deg
RA of node: 173
7735 deg
Eccentricity:
0002849
Arg of perigee: 274
8704 deg
Mean anomaly: 85
2124 deg
Mean motion: 15
54216556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1121
Checksum: 315
Coasting Arc #5 (Orbit 1136)
---------------------------------------
Vector Time (GMT): 2017/358/15:32:15
084
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3717314
63 A = 6782338
41 meter
Y = -4033145
77 meter E =
0008218
Z = 3984495
21 I = 51
71103
XDOT = 6286
318193 Wp = 72
72638
YDOT = 1846
411963 meter/sec RA = 167
65986 deg
ZDOT = -3986
664114 TA = 58
78689
MA = 58
70637
Ha = 219
816 n
mi
Hp = 215
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12195914
15 X = 3742783
51
Y = -13232105
55 feet Y = -3991434
04 meter
Z = 13072490
84 Z = 4002614
25
XDOT = 20624
403521 XDOT = 6284
569005
YDOT = 6057
782032 feet/sec YDOT = 1916
700325 meter/sec
ZDOT = -13079
606673 ZDOT = -3956
131520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17470857
39 X = 5325117
33
Y = -4058436
86 feet Y = -1237011
56 meter
Z = 13153599
82 Z = 4009217
23
XDOT = 13354
015554 XDOT = 4070
303941
YDOT = 15437
305817 feet/sec YDOT = 4705
290813 meter/sec
ZDOT = -12944
104094 ZDOT = -3945
362928
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 17358
68831632
00016717 00000-0 10270-3 0 9042
2 25544 51
6389 168
6440 0002833 277
7908 82
2922 15
54187532 11377
Satellite: ISS
Catalog Number: 25544
Epoch time: 17358
68831632 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 168
6440 deg
Eccentricity:
0002833
Arg of perigee: 277
7908 deg
Mean anomaly: 82
2922 deg
Mean motion: 15
54187532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1137
Checksum: 333
Coasting Arc #6 (Orbit 1151)
---------------------------------------
Vector Time (GMT): 2017/359/15:32:15
084
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5004858
86 A = 6786106
17 meter
Y = 3741499
33 meter E =
0003859
Z = -2641990
58 I = 51
75665
XDOT = -4853
732723 Wp = 18
47586
YDOT = -2803
982035 meter/sec RA = 162
68407 deg
ZDOT = 5229
431165 TA = 311
79928
MA = 311
83224
Ha = 219
859 n
mi
Hp = 215
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16420140
61 X = -5033491
92
Y = 12275260
27 feet Y = 3685371
61 meter
Z = -8667948
09 Z = -2666371
85
XDOT = -15924
319957 XDOT = -4847
418960
YDOT = -9199
416125 feet/sec YDOT = -2858
224747 meter/sec
ZDOT = 17156
926394 ZDOT = 5205
868576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20418788
65 X = -6223646
78
Y = 1214872
87 feet Y = 370293
25 meter
Z = -8776873
61 Z = -2675191
08
XDOT = -8216
169206 XDOT = -2504
288374
YDOT = -15028
165646 feet/sec YDOT = -4580
584889 meter/sec
ZDOT = 17052
531494 ZDOT = 5197
611599
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 17359
65279370
00016717 00000-0 10270-3 0 9056
2 25544 51
6401 163
8358 0002973 286
5549 73
5277 15
54192348 11525
Satellite: ISS
Catalog Number: 25544
Epoch time: 17359
65279370 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 163
8358 deg
Eccentricity:
0002973
Arg of perigee: 286
5549 deg
Mean anomaly: 73
5277 deg
Mean motion: 15
54192348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1152
Checksum: 335
Coasting Arc #7 (Orbit 1167)
---------------------------------------
Vector Time (GMT): 2017/360/15:32:15
084
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5871581
62 A = 6788646
38 meter
Y = -3248484
51 meter E =
0010894
Z = 990822
07 I = 51
79540
XDOT = 3090
780411 Wp = 128
34829
YDOT = 3769
306850 meter/sec RA = 157
71983 deg
ZDOT = -5920
469497 TA = 40
93872
MA = 40
85697
Ha = 219
932 n
mi
Hp = 215
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19263719
24 X = 5902657
75
Y = -10657757
58 feet Y = -3182650
76 meter
Z = 3250728
56 Z = 1019419
63
XDOT = 10140
355678 XDOT = 3077
159937
YDOT = 12366
492289 feet/sec YDOT = 3803
794184 meter/sec
ZDOT = -19424
112523 ZDOT = -5905
488402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21955070
72 X = 6691905
56
Y = 1344441
15 feet Y = 409785
66 meter
Z = 3378351
58 Z = 1029721
56
XDOT = 2118
555134 XDOT = 645
735605
YDOT = 14343
864120 feet/sec YDOT = 4372
009784 meter/sec
ZDOT = -19358
002511 ZDOT = -5900
319165
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 17360
68156769
00016717 00000-0 10270-3 0 9068
2 25544 51
6393 158
7069 0002819 288
0708 72
0138 15
54209161 11689
Satellite: ISS
Catalog Number: 25544
Epoch time: 17360
68156769 = yrday
fracday
Element set: 906
Inclination: 51
6393 deg
RA of node: 158
7069 deg
Eccentricity:
0002819
Arg of perigee: 288
0708 deg
Mean anomaly: 72
0138 deg
Mean motion: 15
54209161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1168
Checksum: 331
Coasting Arc #8 (Orbit 1177)
---------------------------------------
Vector Time (GMT): 2017/361/06:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 872815
18 A = 6778895
97 meter
Y = -4648577
39 meter E =
0006100
Z = 4855379
99 I = 51
78310
XDOT = 7151
709047 Wp = 32
05239
YDOT = -1245
919835 meter/sec RA = 154
56468 deg
ZDOT = -2471
992151 TA = 82
20458
MA = 82
13532
Ha = 219
888 n
mi
Hp = 215
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2863566
86 X = 901146
93
Y = -15251238
16 feet Y = -4638658
79 meter
Z = 15929724
37 Z = 4859688
44
XDOT = 23463
612358 XDOT = 7177
117435
YDOT = -4087
663500 feet/sec YDOT = -1165
802346 meter/sec
ZDOT = -8110
210468 ZDOT = -2437
189759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1572192
18 X = 479204
18
Y = 15417435
68 feet Y = 4699234
40 meter
Z = 15949523
13 Z = 4861414
65
XDOT = -20340
443779 XDOT = -6199
767264
YDOT = 10325
954745 feet/sec YDOT = 3147
351006 meter/sec
ZDOT = -7955
254859 ZDOT = -2424
761681
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 17361
32454785
00016717 00000-0 10270-3 0 9070
2 25544 51
6398 155
5057 0003264 300
6943 59
3888 15
54267416 11781
Satellite: ISS
Catalog Number: 25544
Epoch time: 17361
32454785 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 155
5057 deg
Eccentricity:
0003264
Arg of perigee: 300
6943 deg
Mean anomaly: 59
3888 deg
Mean motion: 15
54267416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1178
Checksum: 335
Coasting Arc #9 (Orbit 1189)
---------------------------------------
Vector Time (GMT): 2017/362/01:03:30
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4013579
95 A = 6778536
91 meter
Y = -2244618
63 meter E =
0003159
Z = 4978417
78 I = 51
80174
XDOT = 5436
990760 Wp = 123
87139
YDOT = -4968
059696 meter/sec RA = 150
80137 deg
ZDOT = 2140
640494 TA = 305
31132
MA = 305
34085
Ha = 220
083 n
mi
Hp = 215
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13167913
23 X = -4012364
45
Y = -7364234
37 feet Y = -2289494
71 meter
Z = 16333391
67 Z = 4958923
87
XDOT = 17837
896195 XDOT = 5481
742665
YDOT = -16299
408452 feet/sec YDOT = -4907
009440 meter/sec
ZDOT = 7023
098735 ZDOT = 2167
160147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1931600
27 X = -588751
76
Y = 15056881
67 feet Y = 4589337
53 meter
Z = 16246993
73 Z = 4952083
69
XDOT = -20624
768884 XDOT = -6286
429556
YDOT = -10361
694589 feet/sec YDOT = -3158
244511 meter/sec
ZDOT = 7141
740744 ZDOT = 2176
802579
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 17362
09612570
00016717 00000-0 10270-3 0 9084
2 25544 51
6375 151
6574 0003186 301
8014 58
2828 15
54259513 11907
Satellite: ISS
Catalog Number: 25544
Epoch time: 17362
09612570 = yrday
fracday
Element set: 908
Inclination: 51
6375 deg
RA of node: 151
6574 deg
Eccentricity:
0003186
Arg of perigee: 301
8014 deg
Mean anomaly: 58
2828 deg
Mean motion: 15
54259513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1190
Checksum: 305
Coasting Arc #10 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2017/363/01:03:30
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2541333
65 A = 6777092
71 meter
Y = 3340906
54 meter E =
0012599
Z = -5331354
96 I = 51
82504
XDOT = -6244
958808 Wp = 79
15106
YDOT = 4430
662900 meter/sec RA = 145
81257 deg
ZDOT = -198
428709 TA = 188
94924
MA = 188
97172
Ha = 220
157 n
mi
Hp = 215
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8337708
82 X = 2529683
01
Y = 10960979
47 feet Y = 3369260
71 meter
Z = -17491322
05 Z = -5319037
98
XDOT = -20488
710000 XDOT = -6293
075662
YDOT = 14536
295605 feet/sec YDOT = 4360
558475 meter/sec
ZDOT = -651
012826 ZDOT = -228
881399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6850817
49 X = 2088129
17
Y = -12025983
37 feet Y = -3665519
73 meter
Z = -17436996
02 Z = -5314796
39
XDOT = 20435
738611 XDOT = 6228
813129
YDOT = 12791
961215 feet/sec YDOT = 3898
989778 meter/sec
ZDOT = -787
097272 ZDOT = -239
907249
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 17363
06059454
00016717 00000-0 10270-3 0 9099
2 25544 51
6378 146
8477 0003170 308
5585 51
5283 15
54225774 12058
Satellite: ISS
Catalog Number: 25544
Epoch time: 17363
06059454 = yrday
fracday
Element set: 909
Inclination: 51
6378 deg
RA of node: 146
8477 deg
Eccentricity:
0003170
Arg of perigee: 308
5585 deg
Mean anomaly: 51
5283 deg
Mean motion: 15
54225774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 321
Coasting Arc #11 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2017/364/01:03:30
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -981574
51 A = 6778048
47 meter
Y = -4361281
51 meter E =
0005583
Z = 5094460
73 I = 51
85481
XDOT = 6561
785895 Wp = 21
71289
YDOT = -3552
323864 meter/sec RA = 140
82656 deg
ZDOT = -1771
115541 TA = 85
39602
MA = 85
33225
Ha = 220
279 n
mi
Hp = 215
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3220388
80 X = -957478
96
Y = -14308666
38 feet Y = -4372123
90 meter
Z = 16714109
99 Z = 5089750
65
XDOT = 21528
168946 XDOT = 6609
624474
YDOT = -11654
605852 feet/sec YDOT = -3478
677838 meter/sec
ZDOT = -5810
746527 ZDOT = -1739
124503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11765801
41 X = -3586216
27
Y = 8795127
82 feet Y = 2680754
96 meter
Z = 16693769
92 Z = 5088261
07
XDOT = -18692
627190 XDOT = -5697
512768
YDOT = -14212
813437 feet/sec YDOT = -4332
065536 meter/sec
ZDOT = -5667
916399 ZDOT = -1727
580918
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 17364
08935740
00016717 00000-0 10270-3 0 9105
2 25544 51
6377 141
7190 0003168 314
2896 45
7997 15
54228827 12216
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
08935740 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 141
7190 deg
Eccentricity:
0003168
Arg of perigee: 314
2896 deg
Mean anomaly: 45
7997 deg
Mean motion: 15
54228827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1221
Checksum: 325
Coasting Arc #12 (Orbit 1227)
---------------------------------------
Vector Time (GMT): 2017/364/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3502314
96 A = 6777304
11 meter
Y = -2428144
18 meter E =
0000703
Z = 5269104
42 I = 51
86328
XDOT = 5216
943914 Wp = 94
24645
YDOT = -5547
580448 meter/sec RA = 138
63020 deg
ZDOT = 911
015846 TA = 347
06659
MA = 347
06840
Ha = 220
257 n
mi
Hp = 215
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11490534
66 X = -3500497
24
Y = -7966352
30 feet Y = -2467299
85 meter
Z = 17287088
00 Z = 5252095
41
XDOT = 17115
957723 XDOT = 5274
165446
YDOT = -18200
723254 feet/sec YDOT = -5488
921162 meter/sec
ZDOT = 2988
897132 ZDOT = 936
496570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7032179
51 X = 2143408
32
Y = -12191904
48 feet Y = -3716092
48 meter
Z = 17211754
24 Z = 5246142
69
XDOT = 18593
694804 XDOT = 5667
358176
YDOT = 15106
092380 feet/sec YDOT = 4604
336957 meter/sec
ZDOT = 3103
055671 ZDOT = 945
811368
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 17364
53943983
00016717 00000-0 10270-3 0 9114
2 25544 51
6373 139
4704 0002897 308
0648 52
0243 15
54245188 12282
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
53943983 = yrday
fracday
Element set: 911
Inclination: 51
6373 deg
RA of node: 139
4704 deg
Eccentricity:
0002897
Arg of perigee: 308
0648 deg
Mean anomaly: 52
0243 deg
Mean motion: 15
54245188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1228
Checksum: 320
Coasting Arc #13 (Orbit 1242)
---------------------------------------
Vector Time (GMT): 2017/365/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2150046
95 A = 6777329
99 meter
Y = 3716920
62 meter E =
0012077
Z = -5253900
55 I = 51
88882
XDOT = -5811
091630 Wp = 90
69648
YDOT = 4873
990501 meter/sec RA = 133
64625 deg
ZDOT = 1072
066302 TA = 189
53833
MA = 189
56129
Ha = 220
216 n
mi
Hp = 215
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7053959
80 X = 2133844
33
Y = 12194621
46 feet Y = 3740873
97 meter
Z = -17237206
54 Z = -5243495
22
XDOT = -19065
261254 XDOT = -5870
369565
YDOT = 15990
782482 feet/sec YDOT = 4808
675325 meter/sec
ZDOT = 3517
277894 ZDOT = 1043
694534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11453710
74 X = -3491091
03
Y = 8297917
02 feet Y = 2529205
11 meter
Z = -17191437
24 Z = -5239950
07
XDOT = -17134
186777 XDOT = -5222
500130
YDOT = -16640
027156 feet/sec YDOT = -5071
880277 meter/sec
ZDOT = 3390
324298 ZDOT = 1033
370846
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 17365
50390049
00016717 00000-0 10270-3 0 9122
2 25544 51
6386 134
6626 0002841 312
1132 47
9779 15
54258523 12430
Satellite: ISS
Catalog Number: 25544
Epoch time: 17365
50390049 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 134
6626 deg
Eccentricity:
0002841
Arg of perigee: 312
1132 deg
Mean anomaly: 47
9779 deg
Mean motion: 15
54258523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1243
Checksum: 306
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