[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 30th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
153/12:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
9
154/09:16:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
0
156/19:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
1
157/11:12:41
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
2
159/13:07:21
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 214
3
164/10:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
7
Coasting Arc #1 (Orbit 3575)
---------------------------------------
Vector Time (GMT): 2018/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4183137
12 A = 6777563
51 meter
Y = 506948
25 meter E =
0017225
Z = -5323140
46 I = 51
98181
XDOT = -1648
805805 Wp = 94
15048
YDOT = 7453
002930 meter/sec RA = 105
93156 deg
ZDOT = -588
761298 TA = 170
26434
MA = 170
23092
Ha = 222
120 n
mi
Hp = 213
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13724203
15 X = 4203014
70
Y = 1663216
03 feet Y = 553838
84 meter
Z = -17464371
59 Z = -5302771
63
XDOT = -5409
467864 XDOT = -1729
164854
YDOT = 24452
109350 feet/sec YDOT = 7434
115613 meter/sec
ZDOT = -1931
631554 ZDOT = -596
964885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6920983
21 X = 2109515
68
Y = -12099289
30 feet Y = -3687863
38 meter
Z = -17373298
61 Z = -5295381
42
XDOT = 19536
719999 XDOT = 5954
792256
YDOT = 13989
612018 feet/sec YDOT = 4264
033743 meter/sec
ZDOT = -1969
360475 ZDOT = -600
261073
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 18150
51713072
00016717 00000-0 10270-3 0 9008
2 25544 51
6380 106
8032 0003494 133
3371 226
8074 15
54099358 35765
Satellite: ISS
Catalog Number: 25544
Epoch time: 18150
51713072 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 106
8032 deg
Eccentricity:
0003494
Arg of perigee: 133
3371 deg
Mean anomaly: 226
8074 deg
Mean motion: 15
54099358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3576
Checksum: 297
Coasting Arc #2 (Orbit 3591)
---------------------------------------
Vector Time (GMT): 2018/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3706288
59 A = 6777993
24 meter
Y = -2252175
01 meter E =
0005910
Z = 5203768
22 I = 51
99200
XDOT = 2453
121689 Wp = 90
96923
YDOT = -7145
074038 meter/sec RA = 100
95701 deg
ZDOT = -1343
960626 TA = 11
88168
MA = 11
86774
Ha = 222
207 n
mi
Hp = 213
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12159739
47 X = -3706106
08
Y = -7389025
62 feet Y = -2293621
01 meter
Z = 17072730
37 Z = 5185764
31
XDOT = 8048
299504 XDOT = 2539
365849
YDOT = -23441
843956 feet/sec YDOT = -7117
159129 meter/sec
ZDOT = -4409
319638 ZDOT = -1331
835654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11437651
71 X = -3486196
24
Y = 8623859
08 feet Y = 2628552
25 meter
Z = 16992476
68 Z = 5179306
89
XDOT = -18098
303094 XDOT = -5516
362783
YDOT = -15416
266883 feet/sec YDOT = -4698
878146 meter/sec
ZDOT = -4354
064480 ZDOT = -1327
118853
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 18151
54597554
00016717 00000-0 10270-3 0 9018
2 25544 51
6386 101
6756 0003477 137
1598 222
9826 15
54105649 35922
Satellite: ISS
Catalog Number: 25544
Epoch time: 18151
54597554 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 101
6756 deg
Eccentricity:
0003477
Arg of perigee: 137
1598 deg
Mean anomaly: 222
9826 deg
Mean motion: 15
54105649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3592
Checksum: 334
Coasting Arc #3 (Orbit 3606)
---------------------------------------
Vector Time (GMT): 2018/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3183545
28 A = 6780636
78 meter
Y = 3880747
88 meter E =
0012862
Z = -4571657
36 I = 52
00682
XDOT = -3118
265933 Wp = 118
23297
YDOT = 6251
201772 meter/sec RA = 95
98602 deg
ZDOT = 3135
795850 TA = 183
07092
MA = 183
07883
Ha = 221
982 n
mi
Hp = 213
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10444702
35 X = 3162119
91
Y = 12732112
48 feet Y = 3916229
34 meter
Z = -14998875
86 Z = -4556244
20
XDOT = -10230
531275 XDOT = -3203
168951
YDOT = 20509
192166 feet/sec YDOT = 6215
856004 meter/sec
ZDOT = 10288
044126 ZDOT = 3120
442989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15659421
34 X = 4772991
63
Y = -5294251
15 feet Y = -1613687
75 meter
Z = -14930445
41 Z = -4550799
76
XDOT = 15085
325797 XDOT = 4598
007303
YDOT = 15809
616269 feet/sec YDOT = 4818
771039 meter/sec
ZDOT = 10218
449528 ZDOT = 3114
583416
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 18152
51051430
00016717 00000-0 10270-3 0 9025
2 25544 51
6393 96
8675 0003390 141
7330 218
4064 15
54105838 36075
Satellite: ISS
Catalog Number: 25544
Epoch time: 18152
51051430 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 96
8675 deg
Eccentricity:
0003390
Arg of perigee: 141
7330 deg
Mean anomaly: 218
4064 deg
Mean motion: 15
54105838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3607
Checksum: 294
Coasting Arc #4 (Orbit 3622)
---------------------------------------
Vector Time (GMT): 2018/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2591974
39 A = 6784361
27 meter
Y = -5232107
16 meter E =
0014624
Z = 3439564
95 I = 52
02233
XDOT = 3697
910517 Wp = 100
26471
YDOT = -4881
223955 meter/sec RA = 91
02466 deg
ZDOT = -4624
341412 TA = 39
65188
MA = 39
54503
Ha = 221
989 n
mi
Hp = 213
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8503853
00 X = -2549982
54
Y = -17165705
89 feet Y = -5260858
08 meter
Z = 11284661
92 Z = 3427075
27
XDOT = 12132
252352 XDOT = 3774
681534
YDOT = -16014
514287 feet/sec YDOT = -4839
441481 meter/sec
ZDOT = -15171
723794 ZDOT = -4606
192403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19062313
15 X = -5810193
05
Y = 2201552
20 feet Y = 671033
11 meter
Z = 11229512
66 Z = 3422755
46
XDOT = -10715
598106 XDOT = -3266
114303
YDOT = -15575
954368 feet/sec YDOT = -4747
550891 meter/sec
ZDOT = -15089
793945 ZDOT = -4599
369194
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 18153
53935313
00016717 00000-0 10270-3 0 9030
2 25544 51
6398 91
7390 0003326 143
1230 217
0152 15
54127066 36230
Satellite: ISS
Catalog Number: 25544
Epoch time: 18153
53935313 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 91
7390 deg
Eccentricity:
0003326
Arg of perigee: 143
1230 deg
Mean anomaly: 217
0152 deg
Mean motion: 15
54127066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3623
Checksum: 284
Coasting Arc #5 (Orbit 3622)
---------------------------------------
Vector Time (GMT): 2018/153/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3570959
30 A = 6780866
72 meter
Y = -3624737
11 meter E =
0010867
Z = -4491831
20 I = 52
01098
XDOT = 2451
244563 Wp = 86
75574
YDOT = 6472
950744 meter/sec RA = 90
98661 deg
ZDOT = -3280
938274 TA = 150
35415
MA = 150
29252
Ha = 221
962 n
mi
Hp = 213
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11715745
75 X = 3633045
71
Y = -11892182
11 feet Y = -3584456
41 meter
Z = -14736979
00 Z = -4474334
37
XDOT = 8042
140956 XDOT = 2394
617184
YDOT = 21236
715039 feet/sec YDOT = 6500
046078 meter/sec
ZDOT = -10764
233181 ZDOT = -3269
167588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8757432
28 X = -2669265
36
Y = -14293610
88 feet Y = -4356692
59 meter
Z = -14658148
31 Z = -4467803
60
XDOT = 21510
839682 XDOT = 6556
503935
YDOT = -2214
673081 feet/sec YDOT = -675
032355 meter/sec
ZDOT = -10712
480023 ZDOT = -3265
163911
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 18153
53935327
00016717 00000-0 10270-3 0 9046
2 25544 51
6400 91
7389 0003378 142
2574 217
8816 15
54132793 36238
Satellite: ISS
Catalog Number: 25544
Epoch time: 18153
53935327 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 91
7389 deg
Eccentricity:
0003378
Arg of perigee: 142
2574 deg
Mean anomaly: 217
8816 deg
Mean motion: 15
54132793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3623
Checksum: 318
Coasting Arc #6 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2018/154/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3515918
80 A = 6779834
90 meter
Y = 3329703
85 meter E =
0010860
Z = 4740658
15 I = 52
00517
XDOT = -2561
736667 Wp = 126
67064
YDOT = -6675
826148 meter/sec RA = 86
67503 deg
ZDOT = 2778
287558 TA = 295
91427
MA = 296
02616
Ha = 221
933 n
mi
Hp = 213
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11535166
65 X = -3575918
78
Y = 10924225
24 feet Y = 3290050
33 meter
Z = 15553340
40 Z = 4723433
72
XDOT = -8404
647857 XDOT = -2500
390825
YDOT = -21902
316758 feet/sec YDOT = -6704
130607 meter/sec
ZDOT = 9115
116661 ZDOT = 2765
991647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4607290
30 X = -1404302
08
Y = 15283285
73 feet Y = 4658345
49 meter
Z = 15475762
27 Z = 4717012
34
XDOT = -17175
400001 XDOT = -5235
061920
YDOT = -14388
595562 feet/sec YDOT = -4385
643927 meter/sec
ZDOT = 9061
049480 ZDOT = 2761
807882
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 18154
43958453
00016717 00000-0 10270-3 0 9052
2 25544 51
6378 87
2520 0003396 149
5186 210
6164 15
54144770 36378
Satellite: ISS
Catalog Number: 25544
Epoch time: 18154
43958453 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 87
2520 deg
Eccentricity:
0003396
Arg of perigee: 149
5186 deg
Mean anomaly: 210
6164 deg
Mean motion: 15
54144770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 324
Coasting Arc #7 (Orbit 3651)
---------------------------------------
Vector Time (GMT): 2018/155/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3938735
55 A = 6777665
83 meter
Y = -1618270
02 meter E =
0016026
Z = -5286570
30 I = 51
99507
XDOT = 1803
656789 Wp = 94
33627
YDOT = 7384
288498 meter/sec RA = 81
70186 deg
ZDOT = -920
168844 TA = 166
91184
MA = 166
87020
Ha = 221
869 n
mi
Hp = 214
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12922360
72 X = 3982218
11
Y = -5309284
84 feet Y = -1573980
61 meter
Z = -17344390
76 Z = -5267331
87
XDOT = 5917
509151 XDOT = 1725
419296
YDOT = 24226
668302 feet/sec YDOT = 7404
020887 meter/sec
ZDOT = -3018
926655 ZDOT = -911
596459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8436041
31 X = 2571305
39
Y = -11269297
22 feet Y = -3434881
79 meter
Z = -17258040
16 Z = -5260250
64
XDOT = 16750
667250 XDOT = 5105
603378
YDOT = 17087
420472 feet/sec YDOT = 5208
245760 meter/sec
ZDOT = -2981
639130 ZDOT = -908
803607
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 18155
40411834
00016717 00000-0 10270-3 0 9068
2 25544 51
6382 82
4430 0003411 151
3338 208
8003 15
54116540 36520
Satellite: ISS
Catalog Number: 25544
Epoch time: 18155
40411834 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 82
4430 deg
Eccentricity:
0003411
Arg of perigee: 151
3338 deg
Mean anomaly: 208
8003 deg
Mean motion: 15
54116540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3652
Checksum: 272
Coasting Arc #8 (Orbit 3667)
---------------------------------------
Vector Time (GMT): 2018/156/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4264774
10 A = 6777704
98 meter
Y = -170280
47 meter E =
0004625
Z = 5260946
97 I = 51
99024
XDOT = -958
970260 Wp = 102
66417
YDOT = -7543
293215 meter/sec RA = 76
72656 deg
ZDOT = -1021
773676 TA = 357
06564
MA = 357
06835
Ha = 221
929 n
mi
Hp = 214
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13992041
01 X = -4288107
91
Y = -558662
95 feet Y = -218103
13 meter
Z = 17260324
70 Z = 5240173
48
XDOT = -3146
227888 XDOT = -869
584580
YDOT = -24748
337318 feet/sec YDOT = -7553
517187 meter/sec
ZDOT = -3352
275840 ZDOT = -1026
215710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12257427
34 X = -3736063
85
Y = 7003229
85 feet Y = 2134584
46 meter
Z = 17167363
55 Z = 5232612
41
XDOT = -15254
604011 XDOT = -4649
603302
YDOT = -18437
715752 feet/sec YDOT = -5619
815761 meter/sec
ZDOT = -3371
040603 ZDOT = -1027
493176
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 18156
43294997
00016717 00000-0 10270-3 0 9072
2 25544 51
6389 77
3146 0003310 154
7313 205
4002 15
54124416 36682
Satellite: ISS
Catalog Number: 25544
Epoch time: 18156
43294997 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 77
3146 deg
Eccentricity:
0003310
Arg of perigee: 154
7313 deg
Mean anomaly: 205
4002 deg
Mean motion: 15
54124416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3668
Checksum: 308
Coasting Arc #9 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2018/156/19:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4062321
62 A = 6783777
03 meter
Y = 4042335
44 meter E =
0007970
Z = -3639682
78 I = 52
00649
XDOT = -1949
014246 Wp = 121
30096
YDOT = 5940
267840 meter/sec RA = 74
59964 deg
ZDOT = 4425
206662 TA = 195
83341
MA = 195
85835
Ha = 221
836 n
mi
Hp = 214
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13327826
82 X = 4034496
86
Y = 13262255
37 feet Y = 4087607
90 meter
Z = -11941216
48 Z = -3620016
60
XDOT = -6394
403693 XDOT = -2036
790419
YDOT = 19489
067717 feet/sec YDOT = 5917
981393 meter/sec
ZDOT = 14518
394561 ZDOT = 4415
526420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14573649
01 X = -4442048
22
Y = -11966933
22 feet Y = -3647521
25 meter
Z = -11853788
43 Z = -3613034
71
XDOT = 3790
624222 XDOT = 1155
382263
YDOT = -18943
472715 feet/sec YDOT = -5773
970483 meter/sec
ZDOT = 14474
178560 ZDOT = 4411
729625
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 18156
81876085
00016717 00000-0 10270-3 0 9089
2 25544 51
6381 75
3875 0003710 156
8007 203
3314 15
54136786 36741
Satellite: ISS
Catalog Number: 25544
Epoch time: 18156
81876085 = yrday
fracday
Element set: 908
Inclination: 51
6381 deg
RA of node: 75
3875 deg
Eccentricity:
0003710
Arg of perigee: 156
8007 deg
Mean anomaly: 203
3314 deg
Mean motion: 15
54136786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 324
Coasting Arc #10 (Orbit 3684)
---------------------------------------
Vector Time (GMT): 2018/157/11:12:41
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -94903
61 A = 6786319
09 meter
Y = 6236262
32 meter E =
0014468
Z = 2662422
07 I = 52
01047
XDOT = -5097
992518 Wp = 90
41781
YDOT = -2324
013423 meter/sec RA = 71
39739 deg
ZDOT = 5237
287222 TA = 299
45973
MA = 299
60401
Ha = 221
702 n
mi
Hp = 214
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -311363
56 X = -177564
81
Y = 20460178
21 feet Y = 6234738
61 meter
Z = 8734980
53 Z = 2661760
86
XDOT = -16725
697236 XDOT = -5097
065884
YDOT = -7624
715954 feet/sec YDOT = -2381
017989 meter/sec
ZDOT = 17182
700859 ZDOT = 5212
524940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17912403
61 X = 5459700
62
Y = 9895942
20 feet Y = 3016283
18 meter
Z = 8731085
23 Z = 2661234
78
XDOT = -13892
239560 XDOT = -4234
354618
YDOT = 10012
162776 feet/sec YDOT = 3051
707214 meter/sec
ZDOT = 17072
207737 ZDOT = 5203
608918
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 18157
52608066
00016717 00000-0 10270-3 0 9091
2 25544 51
6396 71
8659 0003250 158
2862 201
8429 15
54132273 36851
Satellite: ISS
Catalog Number: 25544
Epoch time: 18157
52608066 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 71
8659 deg
Eccentricity:
0003250
Arg of perigee: 158
2862 deg
Mean anomaly: 201
8429 deg
Mean motion: 15
54132273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3685
Checksum: 326
Coasting Arc #11 (Orbit 3699)
---------------------------------------
Vector Time (GMT): 2018/158/11:12:41
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1084467
95 A = 6782448
49 meter
Y = -5362752
58 meter E =
0007664
Z = -4014166
52 I = 51
98743
XDOT = 5157
132815 Wp = 96
71630
YDOT = 4024
021105 meter/sec RA = 66
43975 deg
ZDOT = -3990
053323 TA = 131
94413
MA = 131
87878
Ha = 221
602 n
mi
Hp = 214
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3557965
73 X = 1163853
90
Y = -17594332
63 feet Y = -5350181
10 meter
Z = -13169837
67 Z = -4008706
17
XDOT = 16919
727084 XDOT = 5131
133470
YDOT = 13202
168981 feet/sec YDOT = 4081
546686 meter/sec
ZDOT = -13090
726124 ZDOT = -3965
064465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14042418
03 X = -4280129
01
Y = -11211366
11 feet Y = -3417224
39 meter
Z = -13144582
56 Z = -4006468
76
XDOT = 18649
257299 XDOT = 5684
293625
YDOT = -8169
387092 feet/sec YDOT = -2490
029186 meter/sec
ZDOT = -12979
481942 ZDOT = -3956
146096
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 18158
49060486
00016717 00000-0 10270-3 0 9108
2 25544 51
6407 67
0577 0003188 162
1449 197
9816 15
54155722 37002
Satellite: ISS
Catalog Number: 25544
Epoch time: 18158
49060486 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 67
0577 deg
Eccentricity:
0003188
Arg of perigee: 162
1449 deg
Mean anomaly: 197
9816 deg
Mean motion: 15
54155722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3700
Checksum: 324
Coasting Arc #12 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2018/159/11:12:41
000
Vector Time (MET): N/A
Weight (LBS) : 907753
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2119069
07 A = 6779016
23 meter
Y = 4155044
20 meter E =
0009236
Z = 4916238
50 I = 51
96218
XDOT = -4989
131204 Wp = 135
84822
YDOT = -5332
635605 meter/sec RA = 61
47124 deg
ZDOT = 2347
381536 TA = 291
23830
MA = 291
33693
Ha = 221
554 n
mi
Hp = 214
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6952326
34 X = -2189255
08
Y = 13632034
77 feet Y = 4130954
46 meter
Z = 16129391
41 Z = 4905774
61
XDOT = -16368
540697 XDOT = -4940
531830
YDOT = -17495
523638 feet/sec YDOT = -5388
155972 meter/sec
ZDOT = 7701
382993 ZDOT = 2323
263482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9177566
93 X = 2797322
40
Y = 12307262
78 feet Y = 3751253
70 meter
Z = 16081916
21 Z = 4901768
06
XDOT = -22013
903749 XDOT = -6709
837863
YDOT = 6453
302748 feet/sec YDOT = 1966
966678 meter/sec
ZDOT = 7594
247568 ZDOT = 2314
726659
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 18159
51942605
00016717 00000-0 10270-3 0 9115
2 25544 51
6410 61
9290 0003236 167
8200 192
3031 15
54166857 37168
Satellite: ISS
Catalog Number: 25544
Epoch time: 18159
51942605 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 61
9290 deg
Eccentricity:
0003236
Arg of perigee: 167
8200 deg
Mean anomaly: 192
3031 deg
Mean motion: 15
54166857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 297
Coasting Arc #13 (Orbit 3716)
---------------------------------------
Vector Time (GMT): 2018/159/13:07:21
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4580307
43 A = 6786902
05 meter
Y = -4372504
10 meter E =
0015642
Z = 2418374
02 I = 51
98803
XDOT = 1998
896607 Wp = 116
34435
YDOT = -5084
858874 meter/sec RA = 61
03848 deg
ZDOT = -5387
674039 TA = 36
73021
MA = 36
62311
Ha = 221
636 n
mi
Hp = 214
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15027255
36 X = -4542819
75
Y = -14345485
90 feet Y = -4423514
86 meter
Z = 7934297
96 Z = 2396214
99
XDOT = 6558
059735 XDOT = 2081
778997
YDOT = -16682
607854 feet/sec YDOT = -5062
041951 meter/sec
ZDOT = -17676
095927 ZDOT = -5377
763146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13582561
30 X = -4139964
68
Y = 15769557
98 feet Y = 4806561
27 meter
Z = 7835784
80 Z = 2388347
21
XDOT = -15843
406675 XDOT = -4829
070355
YDOT = -4852
300123 feet/sec YDOT = -1478
981078 meter/sec
ZDOT = -17630
952382 ZDOT = -5373
914286
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 18159
58372832
00016717 00000-0 10270-3 0 9122
2 25544 51
6422 61
6096 0003230 166
5407 193
5833 15
54132139 37171
Satellite: ISS
Catalog Number: 25544
Epoch time: 18159
58372832 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 61
6096 deg
Eccentricity:
0003230
Arg of perigee: 166
5407 deg
Mean anomaly: 193
5833 deg
Mean motion: 15
54132139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3717
Checksum: 307
Coasting Arc #14 (Orbit 3731)
---------------------------------------
Vector Time (GMT): 2018/160/13:07:21
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4256872
88 A = 6788955
70 meter
Y = 5225962
60 meter E =
0008599
Z = -789290
70 I = 51
97836
XDOT = -3247
792691 Wp = 55
11202
YDOT = 3540
003721 meter/sec RA = 56
08839 deg
ZDOT = 5973
131120 TA = 296
39795
MA = 296
48618
Ha = 221
395 n
mi
Hp = 214
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13966118
38 X = 4201952
35
Y = 17145546
60 feet Y = 5273258
89 meter
Z = -2589536
40 Z = -768744
97
XDOT = -10655
487832 XDOT = -3316
151218
YDOT = 11614
185435 feet/sec YDOT = 3503
301885 meter/sec
ZDOT = 19596
886875 ZDOT = 5957
188606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16176559
16 X = 4930615
23
Y = -15093207
59 feet Y = -4600409
67 meter
Z = -2498389
07 Z = -761508
99
XDOT = 11207
268988 XDOT = 3415
975588
YDOT = 8808
277283 feet/sec YDOT = 2684
762916 meter/sec
ZDOT = 19524
977726 ZDOT = 5951
213211
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 18160
54824451
00016717 00000-0 10270-3 0 9130
2 25544 51
6421 56
8010 0003116 172
2192 187
9010 15
54170597 37321
Satellite: ISS
Catalog Number: 25544
Epoch time: 18160
54824451 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 56
8010 deg
Eccentricity:
0003116
Arg of perigee: 172
2192 deg
Mean anomaly: 187
9010 deg
Mean motion: 15
54170597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3732
Checksum: 285
Coasting Arc #15 (Orbit 3747)
---------------------------------------
Vector Time (GMT): 2018/161/13:07:21
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3602312
86 A = 6788956
49 meter
Y = -5666270
56 meter E =
0012572
Z = -958393
12 I = 51
95856
XDOT = 4480
726855 Wp = 149
82841
YDOT = -1850
845000 meter/sec RA = 51
14154 deg
ZDOT = -5943
314359 TA = 40
50754
MA = 40
41403
Ha = 221
401 n
mi
Hp = 214
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11818611
76 X = -3534027
92
Y = -18590126
51 feet Y = -5706172
19 meter
Z = -3144334
38 Z = -975726
91
XDOT = 14700
547423 XDOT = 4529
960344
YDOT = -6072
326114 feet/sec YDOT = -1800
462481 meter/sec
ZDOT = -19499
062858 ZDOT = -5921
428887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17537466
82 X = -5345419
89
Y = 13312456
63 feet Y = 4057636
78 meter
Z = -3221021
92 Z = -981767
48
XDOT = -6323
275404 XDOT = -1927
334343
YDOT = -12989
928681 feet/sec YDOT = -3959
330262 meter/sec
ZDOT = -19400
815286 ZDOT = -5913
368499
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 18161
57706157
00016717 00000-0 10270-3 0 9147
2 25544 51
6420 51
6729 0003263 177
7267 182
3901 15
54116005 37485
Satellite: ISS
Catalog Number: 25544
Epoch time: 18161
57706157 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 51
6729 deg
Eccentricity:
0003263
Arg of perigee: 177
7267 deg
Mean anomaly: 182
3901 deg
Mean motion: 15
54116005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3748
Checksum: 306
Coasting Arc #16 (Orbit 3763)
---------------------------------------
Vector Time (GMT): 2018/162/13:07:21
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2662652
99 A = 6786399
61 meter
Y = 5683287
64 meter E =
0013139
Z = 2570080
44 I = 51
92917
XDOT = -5550
179890 Wp = 88
87602
YDOT = 198
310859 meter/sec RA = 46
18808 deg
ZDOT = 5288
528209 TA = 299
89898
MA = 300
02944
Ha = 221
187 n
mi
Hp = 214
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8735738
15 X = 2586418
75
Y = 18645956
81 feet Y = 5712636
66 meter
Z = 8432022
45 Z = 2582830
46
XDOT = -18209
251609 XDOT = -5577
674181
YDOT = 650
626177 feet/sec YDOT = 136
090486 meter/sec
ZDOT = 17350
814335 ZDOT = 5261
500237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17676267
68 X = 5387726
39
Y = -10515904
20 feet Y = -3205247
60 meter
Z = 8488177
01 Z = 2587196
35
XDOT = 1729
731862 XDOT = 527
222272
YDOT = 16875
596725 feet/sec YDOT = 5143
681882 meter/sec
ZDOT = 17229
813238 ZDOT = 5251
647075
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 18162
60587331
00016717 00000-0 10270-3 0 9154
2 25544 51
6422 46
5436 0002966 182
6375 177
4762 15
54161139 37645
Satellite: ISS
Catalog Number: 25544
Epoch time: 18162
60587331 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 46
5436 deg
Eccentricity:
0002966
Arg of perigee: 182
6375 deg
Mean anomaly: 177
4762 deg
Mean motion: 15
54161139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3764
Checksum: 323
Coasting Arc #17 (Orbit 3778)
---------------------------------------
Vector Time (GMT): 2018/163/13:07:21
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1399557
22 A = 6782614
37 meter
Y = -5340150
30 meter E =
0006153
Z = -3945012
93 I = 51
89191
XDOT = 6358
081357 Wp = 99
13109
YDOT = 1331
931093 meter/sec RA = 41
22444 deg
ZDOT = -4064
943987 TA = 128
50796
MA = 128
45277
Ha = 221
121 n
mi
Hp = 214
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4591723
15 X = -1320575
15
Y = -17520178
14 feet Y = -5355358
87 meter
Z = -12942955
82 Z = -3951620
59
XDOT = 20859
846971 XDOT = 6362
460382
YDOT = 4369
852667 feet/sec YDOT = 1403
056662 meter/sec
ZDOT = -13336
430405 ZDOT = -4034
047408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16867481
92 X = -5141208
49
Y = 6541002
15 feet Y = 1993697
46 meter
Z = -12971661
93 Z = -3953762
56
XDOT = 2344
602951 XDOT = 714
634979
YDOT = -20086
766215 feet/sec YDOT = -6122
446342 meter/sec
ZDOT = -13198
364244 ZDOT = -4022
861422
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 18163
57038161
00016717 00000-0 10270-3 0 9164
2 25544 51
6411 41
7350 0002980 187
0008 173
1104 15
54159302 37791
Satellite: ISS
Catalog Number: 25544
Epoch time: 18163
57038161 = yrday
fracday
Element set: 916
Inclination: 51
6411 deg
RA of node: 41
7350 deg
Eccentricity:
0002980
Arg of perigee: 187
0008 deg
Mean anomaly: 173
1104 deg
Mean motion: 15
54159302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3779
Checksum: 289
Coasting Arc #18 (Orbit 3792)
---------------------------------------
Vector Time (GMT): 2018/164/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -77398
39 A = 6779333
56 meter
Y = -4778277
09 meter E =
0010546
Z = -4817837
01 I = 51
85915
XDOT = 6759
395241 Wp = 86
18932
YDOT = 2502
172563 meter/sec RA = 36
73209 deg
ZDOT = -2594
422860 TA = 158
32606
MA = 158
28140
Ha = 221
070 n
mi
Hp = 214
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -253931
73 X = -557
93
Y = -15676762
11 feet Y = -4778712
13 meter
Z = -15806551
86 Z = -4818027
19
XDOT = 22176
493574 XDOT = 6743
515333
YDOT = 8209
227569 feet/sec YDOT = 2577
672440 meter/sec
ZDOT = -8511
886023 ZDOT = -2561
625907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14015748
14 X = -4272000
03
Y = -7027235
94 feet Y = -2141901
51 meter
Z = -15806618
62 Z = -4817857
36
XDOT = 16943
421332 XDOT = 5164
354822
YDOT = -15007
673531 feet/sec YDOT = -4574
338892 meter/sec
ZDOT = -8365
508839 ZDOT = -2549
807094
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 18164
47058887
00016717 00000-0 10270-3 0 9172
2 25544 51
6421 37
2484 0002970 187
9997 172
1109 15
54186638 37937
Satellite: ISS
Catalog Number: 25544
Epoch time: 18164
47058887 = yrday
fracday
Element set: 917
Inclination: 51
6421 deg
RA of node: 37
2484 deg
Eccentricity:
0002970
Arg of perigee: 187
9997 deg
Mean anomaly: 172
1109 deg
Mean motion: 15
54186638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3793
Checksum: 353
Coasting Arc #19 (Orbit 3808)
---------------------------------------
Vector Time (GMT): 2018/165/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922985
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1496563
85 A = 6777321
00 meter
Y = 3963454
16 meter E =
0004776
Z = 5288599
97 I = 51
82573
XDOT = -6773
877196 Wp = 154
36436
YDOT = -3525
233843 meter/sec RA = 31
74796 deg
ZDOT = 720
617800 TA = 288
74595
MA = 288
79778
Ha = 221
029 n
mi
Hp = 214
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4909986
38 X = -1566462
35
Y = 13003458
53 feet Y = 3946326
75 meter
Z = 17351049
76 Z = 5281161
12
XDOT = -22224
006548 XDOT = -6737
454008
YDOT = -11565
727830 feet/sec YDOT = -3600
780481 meter/sec
ZDOT = 2364
231628 ZDOT = 687
800367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9452364
65 X = 2881080
74
Y = 10248302
20 feet Y = 3123682
51 meter
Z = 17317099
42 Z = 5278251
90
XDOT = -19445
624820 XDOT = -5927
026445
YDOT = 14162
926016 feet/sec YDOT = 4316
859850 meter/sec
ZDOT = 2217
934869 ZDOT = 676
026548
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 18165
49939316
00016717 00000-0 10270-3 0 9181
2 25544 51
6425 32
1194 0003058 192
8388 167
2688 15
54189313 38098
Satellite: ISS
Catalog Number: 25544
Epoch time: 18165
49939316 = yrday
fracday
Element set: 918
Inclination: 51
6425 deg
RA of node: 32
1194 deg
Eccentricity:
0003058
Arg of perigee: 192
8388 deg
Mean anomaly: 167
2688 deg
Mean motion: 15
54189313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3809
Checksum: 343
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