[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 20th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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
080/17:44:25
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
3
082/19:41:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
3
086/11:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
4
087/13:50:30
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
090/15:00:00
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
092/20:30:37
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
3
Coasting Arc #1 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2018/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1649187
18 A = 6789388
86 meter
Y = 6579999
47 meter E =
0010077
Z = -121965
56 I = 52
02353
XDOT = -4602
401077 Wp = 44
56310
YDOT = -1047
239110 meter/sec RA = 104
87475 deg
ZDOT = 6042
603631 TA = 314
13013
MA = 314
21297
Ha = 220
653 n
mi
Hp = 215
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5410719
11 X = -1722051
51
Y = 21587924
77 feet Y = 6561149
70 meter
Z = -400149
48 Z = -130154
63
XDOT = -15099
741066 XDOT = -4619
700310
YDOT = -3435
823852 feet/sec YDOT = -1098
802219 meter/sec
ZDOT = 19824
815062 ZDOT = 6020
204880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6858994
01 X = -2090621
38
Y = 21171614
54 feet Y = 6453108
11 meter
Z = -437533
42 Z = -133360
19
XDOT = -13418
580448 XDOT = -4089
983321
YDOT = -3958
714211 feet/sec YDOT = -1206
616091 meter/sec
ZDOT = 19724
963068 ZDOT = 6012
168743
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 18078
50025958
00016717 00000-0 10270-3 0 9005
2 25544 51
6391 105
8286 0001768 224
2402 135
8609 15
54104562 24567
Satellite: ISS
Catalog Number: 25544
Epoch time: 18078
50025958 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 105
8286 deg
Eccentricity:
0001768
Arg of perigee: 224
2402 deg
Mean anomaly: 135
8609 deg
Mean motion: 15
54104562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 306
Coasting Arc #2 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2018/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2342138
50 A = 6788341
16 meter
Y = -6164232
86 meter E =
0008453
Z = -1593845
40 I = 52
02714
XDOT = 4043
342437 Wp = 155
28417
YDOT = 3023
617978 meter/sec RA = 99
93025 deg
ZDOT = -5770
729563 TA = 42
05525
MA = 41
99040
Ha = 220
639 n
mi
Hp = 215
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7684181
43 X = 2418636
65
Y = -20223861
08 feet Y = -6137613
92 meter
Z = -5229151
57 Z = -1582281
49
XDOT = 13265
559177 XDOT = 4037
262286
YDOT = 9920
006490 feet/sec YDOT = 3068
798700 meter/sec
ZDOT = -18932
839774 ZDOT = -5751
103477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8732387
42 X = 2661631
68
Y = -19807625
05 feet Y = -6037364
11 meter
Z = -5176739
07 Z = -1577870
07
XDOT = 11426
627666 XDOT = 3482
836113
YDOT = 9946
864915 feet/sec YDOT = 3031
804426 meter/sec
ZDOT = -18845
618624 ZDOT = -5744
144557
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 18079
52910183
00016717 00000-0 10270-3 0 9012
2 25544 51
6388 100
6995 0001899 226
5920 133
5075 15
54104466 24721
Satellite: ISS
Catalog Number: 25544
Epoch time: 18079
52910183 = yrday
fracday
Element set: 901
Inclination: 51
6388 deg
RA of node: 100
6995 deg
Eccentricity:
0001899
Arg of perigee: 226
5920 deg
Mean anomaly: 133
5075 deg
Mean motion: 15
54104466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2472
Checksum: 317
Coasting Arc #3 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2902605
93 A = 6785293
88 meter
Y = 5275714
63 meter E =
0011567
Z = 3117395
65 I = 52
02174
XDOT = -3427
903061 Wp = 88
93824
YDOT = -4794
956024 meter/sec RA = 94
98003 deg
ZDOT = 4907
557146 TA = 306
74203
MA = 306
84819
Ha = 220
603 n
mi
Hp = 215
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9522985
33 X = -2976527
43
Y = 17308775
05 feet Y = 5242842
71 meter
Z = 10227676
02 Z = 3103115
62
XDOT = -11246
401118 XDOT = -3397
868251
YDOT = -15731
483020 feet/sec YDOT = -4833
120740 meter/sec
ZDOT = 16100
909271 ZDOT = 4890
978947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10163649
47 X = -3097880
36
Y = 16979256
11 feet Y = 5175277
26 meter
Z = 10163237
26 Z = 3097754
72
XDOT = -9582
053131 XDOT = -2920
609794
YDOT = -15359
844890 feet/sec YDOT = -4681
680722 meter/sec
ZDOT = 16027
531640 ZDOT = 4885
191644
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 18080
55794044
00016717 00000-0 10270-3 0 9024
2 25544 51
6388 95
5702 0001689 234
6746 125
4249 15
54117480 24882
Satellite: ISS
Catalog Number: 25544
Epoch time: 18080
55794044 = yrday
fracday
Element set: 902
Inclination: 51
6388 deg
RA of node: 95
5702 deg
Eccentricity:
0001689
Arg of perigee: 234
6746 deg
Mean anomaly: 125
4249 deg
Mean motion: 15
54117480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 330
Coasting Arc #4 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2018/080/17:44:25
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3598952
47 A = 6779455
25 meter
Y = 3086701
57 meter E =
0010469
Z = -4855626
59 I = 52
00342
XDOT = -2427
248047 Wp = 114
72348
YDOT = 6810
217098 meter/sec RA = 93
75075 deg
ZDOT = 2530
180711 TA = 180
05816
MA = 180
05829
Ha = 220
476 n
mi
Hp = 215
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11807586
83 X = 3587754
86
Y = 10126973
64 feet Y = 3126884
43 meter
Z = -15930533
43 Z = -4838171
54
XDOT = -7963
412228 XDOT = -2515
511703
YDOT = 22343
231948 feet/sec YDOT = 6782
580683 meter/sec
ZDOT = 8301
117818 ZDOT = 2518
174852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11235322
46 X = 3424526
29
Y = -10872254
44 feet Y = -3313863
15 meter
Z = -15853018
95 Z = -4832000
18
XDOT = 20666
243980 XDOT = 6299
071165
YDOT = 9331
883118 feet/sec YDOT = 2844
357975 meter/sec
ZDOT = 8246
625017 ZDOT = 2513
571305
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 18080
75084847
00016717 00000-0 10270-3 0 9030
2 25544 51
6392 94
6089 0001720 241
9713 118
1266 15
54126024 24912
Satellite: ISS
Catalog Number: 25544
Epoch time: 18080
75084847 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 94
6089 deg
Eccentricity:
0001720
Arg of perigee: 241
9713 deg
Mean anomaly: 118
1266 deg
Mean motion: 15
54126024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 306
Coasting Arc #5 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2018/081/17:44:25
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3130218
29 A = 6783018
13 meter
Y = -4590373
67 meter E =
0009628
Z = 3883472
25 I = 52
01647
XDOT = 3120
867308 Wp = 84
40268
YDOT = -5646
561794 meter/sec RA = 88
78653 deg
ZDOT = -4149
145009 TA = 48
97470
MA = 48
89150
Ha = 220
538 n
mi
Hp = 215
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10269745
06 X = -3097518
79
Y = -15060281
06 feet Y = -4625194
78 meter
Z = 12741050
68 Z = 3868346
45
XDOT = 10239
065971 XDOT = 3203
931201
YDOT = -18525
465205 feet/sec YDOT = -5611
198002 meter/sec
ZDOT = -13612
680475 ZDOT = -4133
782650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15839611
21 X = -4827913
50
Y = 9115203
97 feet Y = 2778314
17 meter
Z = 12674141
97 Z = 3863078
47
XDOT = -16975
772871 XDOT = -5174
215571
YDOT = -10623
258850 feet/sec YDOT = -3237
969297 meter/sec
ZDOT = -13543
339472 ZDOT = -4128
009871
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 18081
77968451
00016717 00000-0 10270-3 0 9046
2 25544 51
6392 89
4811 0001742 245
9791 114
1180 15
54121204 25075
Satellite: ISS
Catalog Number: 25544
Epoch time: 18081
77968451 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 89
4811 deg
Eccentricity:
0001742
Arg of perigee: 245
9791 deg
Mean anomaly: 114
1180 deg
Mean motion: 15
54121204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 305
Coasting Arc #6 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2018/082/17:44:25
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2604757
41 A = 6786633
95 meter
Y = 5732965
40 meter E =
0003642
Z = -2528635
68 I = 52
02769
XDOT = -3743
412792 Wp = 39
47658
YDOT = 4046
662901 meter/sec RA = 83
83118 deg
ZDOT = 5325
488438 TA = 292
31299
MA = 292
35160
Ha = 220
393 n
mi
Hp = 215
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8545792
04 X = 2552739
04
Y = 18808941
60 feet Y = 5761802
57 meter
Z = -8296048
82 Z = -2516109
36
XDOT = -12281
538030 XDOT = -3814
253916
YDOT = 13276
453086 feet/sec YDOT = 4004
405725 meter/sec
ZDOT = 17472
074929 ZDOT = 5307
131892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19311826
93 X = 5886244
85
Y = -7400811
36 feet Y = -2255767
30 meter
Z = -8240910
35 Z = -2511829
47
XDOT = 11932
436718 XDOT = 3637
006712
YDOT = 11798
693449 feet/sec YDOT = 3596
241763 meter/sec
ZDOT = 17389
568395 ZDOT = 5300
340447
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 18082
74421572
00016717 00000-0 10270-3 0 9053
2 25544 51
6400 84
6727 0001822 250
2875 109
8081 15
54134377 25222
Satellite: ISS
Catalog Number: 25544
Epoch time: 18082
74421572 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 84
6727 deg
Eccentricity:
0001822
Arg of perigee: 250
2875 deg
Mean anomaly: 109
8081 deg
Mean motion: 15
54134377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 299
Coasting Arc #7 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2018/082/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3434006
55 A = 6779486
74 meter
Y = 3269197
97 meter E =
0006194
Z = 4843459
27 I = 52
00486
XDOT = -2766
202410 Wp = 132
05101
YDOT = -6685
377362 meter/sec RA = 83
47100 deg
ZDOT = 2545
089249 TA = 293
01344
MA = 293
07876
Ha = 220
516 n
mi
Hp = 215
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11266425
67 X = -3493835
39
Y = 10725715
13 feet Y = 3230462
33 meter
Z = 15890614
41 Z = 4826632
52
XDOT = -9075
467226 XDOT = -2703
601833
YDOT = -21933
652761 feet/sec YDOT = -6715
960759 meter/sec
ZDOT = 8350
030344 ZDOT = 2531
804444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14589244
03 X = 4446801
58
Y = 5614561
66 feet Y = 1711318
40 meter
Z = 15815043
31 Z = 4820425
20
XDOT = -15418
920450 XDOT = -4699
686953
YDOT = 16652
924744 feet/sec YDOT = 5075
811462 meter/sec
ZDOT = 8291
637018 ZDOT = 2527
290963
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 18082
87281927
00016717 00000-0 10270-3 0 9066
2 25544 51
6414 84
0323 0001795 251
0896 109
0063 15
54121619 25243
Satellite: ISS
Catalog Number: 25544
Epoch time: 18082
87281927 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 84
0323 deg
Eccentricity:
0001795
Arg of perigee: 251
0896 deg
Mean anomaly: 109
0063 deg
Mean motion: 15
54121619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 303
Coasting Arc #8 (Orbit 2538)
---------------------------------------
Vector Time (GMT): 2018/083/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3920720
12 A = 6777408
37 meter
Y = -1560356
80 meter E =
0012805
Z = -5314521
29 I = 51
99350
XDOT = 2027
088964 Wp = 85
70488
YDOT = 7356
074422 meter/sec RA = 78
49736 deg
ZDOT = -664
746294 TA = 177
97381
MA = 177
96862
Ha = 220
287 n
mi
Hp = 215
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12863254
99 X = 3963692
13
Y = -5119280
85 feet Y = -1516272
64 meter
Z = -17436093
47 Z = -5295371
39
XDOT = 6650
554343 XDOT = 1947
909661
YDOT = 24134
102435 feet/sec YDOT = 7378
299969 meter/sec
ZDOT = -2180
926160 ZDOT = -655
092156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10390749
02 X = -3167100
30
Y = -9310447
92 feet Y = -2837824
53 meter
Z = -17350377
95 Z = -5288395
20
XDOT = 17914
416605 XDOT = 5460
314181
YDOT = -16009
943725 feet/sec YDOT = -4879
830847 meter/sec
ZDOT = -2138
847922 ZDOT = -651
920847
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 18083
83734559
00016717 00000-0 10270-3 0 9078
2 25544 51
6414 79
2239 0001863 259
2096 100
8847 15
54158715 25395
Satellite: ISS
Catalog Number: 25544
Epoch time: 18083
83734559 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 79
2239 deg
Eccentricity:
0001863
Arg of perigee: 259
2096 deg
Mean anomaly: 100
8847 deg
Mean motion: 15
54158715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2539
Checksum: 337
Coasting Arc #9 (Orbit 2554)
---------------------------------------
Vector Time (GMT): 2018/084/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4319082
63 A = 6777775
08 meter
Y = -222901
72 meter E =
0002655
Z = 5217679
42 I = 51
98666
XDOT = -1165
469938 Wp = 36
18030
YDOT = -7471
413701 meter/sec RA = 73
52148 deg
ZDOT = -1281
515756 TA = 66
07785
MA = 66
05004
Ha = 220
393 n
mi
Hp = 215
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14170218
60 X = -4341613
65
Y = -731304
86 feet Y = -271326
33 meter
Z = 17118370
79 Z = 5196644
25
XDOT = -3823
720268 XDOT = -1075
611052
YDOT = -24512
512141 feet/sec YDOT = -7483
944435 meter/sec
ZDOT = -4204
448018 ZDOT = -1286
958448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5968522
94 X = 1819205
79
Y = 12996623
02 feet Y = 3961370
70 meter
Z = 17024483
68 Z = 5189062
63
XDOT = -19019
066416 XDOT = -5797
011444
YDOT = 14282
620134 feet/sec YDOT = 4353
342617 meter/sec
ZDOT = -4227
694974 ZDOT = -1288
601428
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 18084
86617123
00016717 00000-0 10270-3 0 9080
2 25544 51
6408 74
0953 0001921 262
5151 97
5784 15
54170479 25559
Satellite: ISS
Catalog Number: 25544
Epoch time: 18084
86617123 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 74
0953 deg
Eccentricity:
0001921
Arg of perigee: 262
5151 deg
Mean anomaly: 97
5784 deg
Mean motion: 15
54170479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2555
Checksum: 323
Coasting Arc #10 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2018/085/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4611893
33 A = 6780436
49 meter
Y = 1920688
89 meter E =
0008178
Z = -4592452
23 I = 51
98457
XDOT = 157
986130 Wp = 115
53452
YDOT = 7008
202173 meter/sec RA = 68
54875 deg
ZDOT = 3090
525908 TA = 185
26109
MA = 185
26968
Ha = 220
252 n
mi
Hp = 215
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15130883
63 X = 4612380
41
Y = 6301472
74 feet Y = 1972264
62 meter
Z = -15067100
48 Z = -4570048
43
XDOT = 518
327199 XDOT = 64
594761
YDOT = 22992
789282 feet/sec YDOT = 7009
446941 meter/sec
ZDOT = 10139
520695 ZDOT = 3091
065966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1752551
61 X = -534177
73
Y = -16388316
59 feet Y = -4995158
90 meter
Z = -14967343
03 Z = -4562046
16
XDOT = 18781
296483 XDOT = 5724
539168
YDOT = -11267
541006 feet/sec YDOT = -3434
346499 meter/sec
ZDOT = 10140
933579 ZDOT = 3090
956555
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 18085
83069460
00016717 00000-0 10270-3 0 9094
2 25544 51
6403 69
2867 0001952 266
6645 93
4285 15
54156147 25705
Satellite: ISS
Catalog Number: 25544
Epoch time: 18085
83069460 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 69
2867 deg
Eccentricity:
0001952
Arg of perigee: 266
6645 deg
Mean anomaly: 93
4285 deg
Mean motion: 15
54156147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2570
Checksum: 333
Coasting Arc #11 (Orbit 2579)
---------------------------------------
Vector Time (GMT): 2018/086/11:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4735205
17 A = 6781316
18 meter
Y = 2098309
21 meter E =
0007254
Z = -4384870
59 I = 51
97663
XDOT = 166
481267 Wp = 115
83260
YDOT = 6837
027342 meter/sec RA = 65
35252 deg
ZDOT = 3452
887119 TA = 189
05911
MA = 189
07221
Ha = 220
412 n
mi
Hp = 215
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15535450
03 X = 4732688
55
Y = 6884216
57 feet Y = 2151247
06 meter
Z = -14386058
38 Z = -4361875
15
XDOT = 546
198382 XDOT = 73
243257
YDOT = 22431
192067 feet/sec YDOT = 6838
368038 meter/sec
ZDOT = 11328
369813 ZDOT = 3453
468741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14354818
30 X = 4375348
62
Y = 9252935
89 feet Y = 2820294
86 meter
Z = -14283686
16 Z = -4353667
54
XDOT = -2383
522926 XDOT = -726
497788
YDOT = 21180
850770 feet/sec YDOT = 6455
923315 meter/sec
ZDOT = 11329
987342 ZDOT = 3453
380142
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 18086
47370829
00016717 00000-0 10270-3 0 9101
2 25544 51
6378 66
0802 0001665 265
6590 94
4372 15
54123793 25809
Satellite: ISS
Catalog Number: 25544
Epoch time: 18086
47370829 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 66
0802 deg
Eccentricity:
0001665
Arg of perigee: 265
6590 deg
Mean anomaly: 94
4372 deg
Mean motion: 15
54123793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2580
Checksum: 324
Coasting Arc #12 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2018/087/11:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4850900
60 A = 6785038
16 meter
Y = -3521765
70 meter E =
0011163
Z = 3167859
79 I = 51
97449
XDOT = 1054
772054 Wp = 94
52142
YDOT = -5838
306251 meter/sec RA = 60
38940 deg
ZDOT = -4861
549012 TA = 49
09908
MA = 49
00245
Ha = 220
367 n
mi
Hp = 215
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15915028
22 X = -4826546
38
Y = -11554349
42 feet Y = -3575875
29 meter
Z = 10393240
78 Z = 3144355
57
XDOT = 3460
538234 XDOT = 1143
593813
YDOT = -19154
548068 feet/sec YDOT = -5826
014972 meter/sec
ZDOT = -15949
963949 ZDOT = -4856
208964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14207362
76 X = -4330404
17
Y = -13678518
54 feet Y = -4169212
45 meter
Z = 10288806
62 Z = 3136028
26
XDOT = 5216
447279 XDOT = 1589
973131
YDOT = -17431
422328 feet/sec YDOT = -5313
097526 meter/sec
ZDOT = -15925
278686 ZDOT = -4854
024943
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 18087
50252567
00016717 00000-0 10270-3 0 9115
2 25544 51
6375 60
9506 0001768 274
4201 85
6749 15
54170032 25966
Satellite: ISS
Catalog Number: 25544
Epoch time: 18087
50252567 = yrday
fracday
Element set: 911
Inclination: 51
6375 deg
RA of node: 60
9506 deg
Eccentricity:
0001768
Arg of perigee: 274
4201 deg
Mean anomaly: 85
6749 deg
Mean motion: 15
54170032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 315
Coasting Arc #13 (Orbit 2597)
---------------------------------------
Vector Time (GMT): 2018/087/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1031654
56 A = 6781026
83 meter
Y = 5062397
70 meter E =
0007716
Z = 4387763
11 I = 51
96118
XDOT = -5491
536576 Wp = 113
23678
YDOT = -4105
455449 meter/sec RA = 59
87771 deg
ZDOT = 3437
762311 TA = 302
03955
MA = 302
11448
Ha = 220
274 n
mi
Hp = 215
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3384693
45 X = -1109500
24
Y = 16608916
33 feet Y = 5050426
26 meter
Z = 14395548
25 Z = 4382562
09
XDOT = -18016
852283 XDOT = -5461
918801
YDOT = -13469
342023 feet/sec YDOT = -4166
699597 meter/sec
ZDOT = 11278
747738 ZDOT = 3411
158980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6040782
86 X = 1841230
62
Y = 15859074
74 feet Y = 4833845
98 meter
Z = 14371595
30 Z = 4380462
25
XDOT = -21343
040575 XDOT = -6505
358767
YDOT = -2007
197648 feet/sec YDOT = -611
793843 meter/sec
ZDOT = 11160
561663 ZDOT = 3401
739195
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 18087
63112769
00016717 00000-0 10270-3 0 9129
2 25544 51
6391 60
3098 0001867 271
7552 88
3387 15
54183182 25983
Satellite: ISS
Catalog Number: 25544
Epoch time: 18087
63112769 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 60
3098 deg
Eccentricity:
0001867
Arg of perigee: 271
7552 deg
Mean anomaly: 88
3387 deg
Mean motion: 15
54183182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2598
Checksum: 336
Coasting Arc #14 (Orbit 2612)
---------------------------------------
Vector Time (GMT): 2018/088/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2213676
64 A = 6778137
05 meter
Y = -3844596
49 meter E =
0011852
Z = -5135253
32 I = 51
93380
XDOT = 5299
202579 Wp = 74
25339
YDOT = 5274
112454 meter/sec RA = 54
90362 deg
ZDOT = -1664
262191 TA = 179
72630
MA = 179
72566
Ha = 220
303 n
mi
Hp = 215
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7262718
63 X = 2281447
64
Y = -12613505
55 feet Y = -3819463
37 meter
Z = -16847943
95 Z = -5124335
01
XDOT = 17385
835234 XDOT = 5247
916231
YDOT = 17303
518551 feet/sec YDOT = 5333
084809 meter/sec
ZDOT = -5460
177792 ZDOT = -1638
645919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -856831
63 X = -261162
28
Y = -14586720
72 feet Y = -4446032
48 meter
Z = -16798637
97 Z = -5120224
85
XDOT = 23028
240794 XDOT = 7019
007794
YDOT = 4804
420598 feet/sec YDOT = 1464
387398 meter/sec
ZDOT = -5346
578587 ZDOT = -1629
637153
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 18088
59564315
00016717 00000-0 10270-3 0 9134
2 25544 51
6391 55
5011 0001784 279
2402 80
8549 15
54162387 26138
Satellite: ISS
Catalog Number: 25544
Epoch time: 18088
59564315 = yrday
fracday
Element set: 913
Inclination: 51
6391 deg
RA of node: 55
5011 deg
Eccentricity:
0001784
Arg of perigee: 279
2402 deg
Mean anomaly: 80
8549 deg
Mean motion: 15
54162387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2613
Checksum: 316
Coasting Arc #15 (Orbit 2628)
---------------------------------------
Vector Time (GMT): 2018/089/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3395991
20 A = 6777205
41 meter
Y = 2450235
94 meter E =
0001169
Z = 5328217
52 I = 51
91201
XDOT = -4766
427603 Wp = 25
65257
YDOT = -6002
069883 meter/sec RA = 49
92404 deg
ZDOT = -276
765850 TA = 66
98152
MA = 66
96920
Ha = 220
325 n
mi
Hp = 215
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11141703
43 X = -3449019
63
Y = 8038831
81 feet Y = 2411963
87 meter
Z = 17481028
62 Z = 5311591
87
XDOT = -15637
885836 XDOT = -4697
612194
YDOT = -19691
830324 feet/sec YDOT = -6054
986626 meter/sec
ZDOT = -908
024442 ZDOT = -299
751469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4687865
18 X = -1428861
31
Y = 13014849
23 feet Y = 3966926
04 meter
Z = 17406445
74 Z = 5305484
66
XDOT = -23106
820856 XDOT = -7042
958997
YDOT = -6967
823945 feet/sec YDOT = -2123
792738 meter/sec
ZDOT = -1009
758695 ZDOT = -307
774450
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 18089
62445403
00016717 00000-0 10270-3 0 9146
2 25544 51
6399 50
3730 0002004 282
6474 77
4455 15
54187888 26298
Satellite: ISS
Catalog Number: 25544
Epoch time: 18089
62445403 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 50
3730 deg
Eccentricity:
0002004
Arg of perigee: 282
6474 deg
Mean anomaly: 77
4455 deg
Mean motion: 15
54187888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2629
Checksum: 328
Coasting Arc #16 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2018/090/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4499661
80 A = 6778849
07 meter
Y = -1022075
17 meter E =
0010491
Z = -4975654
68 I = 51
89594
XDOT = 3839
764663 Wp = 105
28287
YDOT = 6256
618556 meter/sec RA = 44
94234 deg
ZDOT = 2188
377924 TA = 185
99864
MA = 186
01121
Ha = 220
322 n
mi
Hp = 215
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14762669
95 X = 4534925
67
Y = -3353264
99 feet Y = -971560
38 meter
Z = -16324326
36 Z = -4953711
04
XDOT = 12597
653095 XDOT = 3758
886059
YDOT = 20526
963768 feet/sec YDOT = 6299
105536 meter/sec
ZDOT = 7179
717597 ZDOT = 2206
832891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10130077
92 X = 3087647
75
Y = -11391042
10 feet Y = -3471989
63 meter
Z = -16226217
14 Z = -4945750
98
XDOT = 21329
962573 XDOT = 6501
372592
YDOT = 8630
836948 feet/sec YDOT = 2630
679102 meter/sec
ZDOT = 7261
172604 ZDOT = 2213
205410
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 18090
58896183
00016717 00000-0 10270-3 0 9159
2 25544 51
6406 45
5638 0001843 289
4038 70
6915 15
54172007 26441
Satellite: ISS
Catalog Number: 25544
Epoch time: 18090
58896183 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 45
5638 deg
Eccentricity:
0001843
Arg of perigee: 289
4038 deg
Mean anomaly: 70
6915 deg
Mean motion: 15
54172007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2644
Checksum: 324
Coasting Arc #17 (Orbit 2644)
---------------------------------------
Vector Time (GMT): 2018/090/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3398128
41 A = 6787575
50 meter
Y = -5534504
39 meter E =
0005330
Z = -1965182
20 I = 51
92539
XDOT = 5095
896226 Wp = 151
04924
YDOT = -1139
906782 meter/sec RA = 44
73817 deg
ZDOT = -5612
246855 TA = 50
53775
MA = 50
49061
Ha = 220
295 n
mi
Hp = 215
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11148715
25 X = -3326441
67
Y = -18157822
79 feet Y = -5572104
05 meter
Z = -6447448
17 Z = -1981514
28
XDOT = 16718
819639 XDOT = 5135
525649
YDOT = -3739
851646 feet/sec YDOT = -1082
700168 meter/sec
ZDOT = -18412
883382 ZDOT = -5587
396283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21187841
77 X = -6458054
17
Y = -2034949
13 feet Y = -620252
49 meter
Z = -6519533
06 Z = -1987153
68
XDOT = 6980
922984 XDOT = 2127
785325
YDOT = -14163
472559 feet/sec YDOT = -4317
026436 meter/sec
ZDOT = -18301
780116 ZDOT = -5578
382580
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 18090
65326234
00016717 00000-0 10270-3 0 9163
2 25544 51
6420 45
2440 0001875 286
1342 73
9604 15
54154811 26457
Satellite: ISS
Catalog Number: 25544
Epoch time: 18090
65326234 = yrday
fracday
Element set: 916
Inclination: 51
6420 deg
RA of node: 45
2440 deg
Eccentricity:
0001875
Arg of perigee: 286
1342 deg
Mean anomaly: 73
9604 deg
Mean motion: 15
54154811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2645
Checksum: 294
Coasting Arc #18 (Orbit 2660)
---------------------------------------
Vector Time (GMT): 2018/091/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2255022
42 A = 6784161
24 meter
Y = 5388600
24 meter E =
0010678
Z = 3440196
57 I = 51
88962
XDOT = -6118
989923 Wp = 86
61108
YDOT = -389
580995 meter/sec RA = 39
77839 deg
ZDOT = 4609
487032 TA = 313
55127
MA = 313
63991
Ha = 220
339 n
mi
Hp = 215
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7398367
53 X = 2177887
26
Y = 17679134
64 feet Y = 5413386
61 meter
Z = 11286734
14 Z = 3450962
70
XDOT = -20075
426255 XDOT = -6136
569354
YDOT = -1278
152871 feet/sec YDOT = -458
105444 meter/sec
ZDOT = 15122
988950 ZDOT = 4579
720263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18611987
14 X = 5672933
68
Y = 4451158
60 feet Y = 1356713
14 meter
Z = 11333981
34 Z = 3454597
51
XDOT = -12553
688247 XDOT = -3826
364178
YDOT = 14225
023201 feet/sec YDOT = 4335
787072 meter/sec
ZDOT = 14990
177056 ZDOT = 4569
005967
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 18091
68206677
00016717 00000-0 10270-3 0 9176
2 25544 51
6416 40
1153 0001815 294
0622 66
0341 15
54164945 26618
Satellite: ISS
Catalog Number: 25544
Epoch time: 18091
68206677 = yrday
fracday
Element set: 917
Inclination: 51
6416 deg
RA of node: 40
1153 deg
Eccentricity:
0001815
Arg of perigee: 294
0622 deg
Mean anomaly: 66
0341 deg
Mean motion: 15
54164945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2661
Checksum: 298
Coasting Arc #19 (Orbit 2675)
---------------------------------------
Vector Time (GMT): 2018/092/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -821144
51 A = 6780250
56 meter
Y = -4945884
86 meter E =
0008739
Z = -4573413
42 I = 51
85182
XDOT = 6782
369360 Wp = 59
98342
YDOT = 1744
897563 meter/sec RA = 34
80726 deg
ZDOT = -3104
938191 TA = 178
99409
MA = 178
99233
Ha = 220
256 n
mi
Hp = 215
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2694043
65 X = -743561
81
Y = -16226656
35 feet Y = -4954634
18 meter
Z = -15004637
20 Z = -4577213
30
XDOT = 22251
867979 XDOT = 6777
435654
YDOT = 5724
729536 feet/sec YDOT = 1820
714751 meter/sec
ZDOT = -10186
805089 ZDOT = -3072
003673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14785757
77 X = -4506698
97
Y = -7173350
42 feet Y = -2186437
21 meter
Z = -15020845
38 Z = -4578353
67
XDOT = 16958
086992 XDOT = 5168
824915
YDOT = -13931
623366 feet/sec YDOT = -4246
358802 meter/sec
ZDOT = -10040
070210 ZDOT = -3060
213400
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 18092
64656615
00016717 00000-0 10270-3 0 9185
2 25544 51
6425 35
3079 0002011 295
5625 64
5320 15
54198870 26769
Satellite: ISS
Catalog Number: 25544
Epoch time: 18092
64656615 = yrday
fracday
Element set: 918
Inclination: 51
6425 deg
RA of node: 35
3079 deg
Eccentricity:
0002011
Arg of perigee: 295
5625 deg
Mean anomaly: 64
5320 deg
Mean motion: 15
54198870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2676
Checksum: 318
Coasting Arc #20 (Orbit 2679)
---------------------------------------
Vector Time (GMT): 2018/092/20:30:37
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1758762
40 A = 6777411
72 meter
Y = 3836125
30 meter E =
0001049
Z = 5302447
49 I = 51
83101
XDOT = -6610
597678 Wp = 115
42801
YDOT = -3844
214752 meter/sec RA = 33
64384 deg
ZDOT = 587
956564 TA = 328
97320
MA = 328
97939
Ha = 220
465 n
mi
Hp = 215
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5770217
84 X = -1827285
02
Y = 12585712
92 feet Y = 3816075
04 meter
Z = 17396481
26 Z = 5293737
11
XDOT = -21688
312591 XDOT = -6569
975319
YDOT = -12612
253124 feet/sec YDOT = -3917
911809 meter/sec
ZDOT = 1928
991353 ZDOT = 555
943348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12803792
96 X = 3902596
09
Y = -5397214
77 feet Y = -1645071
06 meter
Z = 17357018
82 Z = 5290419
34
XDOT = 7258
530256 XDOT = 2212
400022
YDOT = 22970
849336 feet/sec YDOT = 7001
514878 meter/sec
ZDOT = 1786
691722 ZDOT = 544
583637
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 18092
90376674
00016717 00000-0 10270-3 0 9199
2 25544 51
6380 34
0210 0001771 290
8803 69
2160 15
54140088 26807
Satellite: ISS
Catalog Number: 25544
Epoch time: 18092
90376674 = yrday
fracday
Element set: 919
Inclination: 51
6380 deg
RA of node: 34
0210 deg
Eccentricity:
0001771
Arg of perigee: 290
8803 deg
Mean anomaly: 69
2160 deg
Mean motion: 15
54140088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2680
Checksum: 300
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