[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 9th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 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
101/03:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 214
7
105/08:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 214
6
108/10:36:00
987 0
3 0
8 0
8
N/A -0
7 -0
0 220
9
000/00:02:01
974 -0
4 -0
0 214
8
Coasting Arc #1 (Orbit 2782)
---------------------------------------
Vector Time (GMT): 2018/099/12:03:23
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4867084
31 A = 6783191
69 meter
Y = -2964863
85 meter E =
0005258
Z = -3685123
17 I = 51
65080
XDOT = 5338
668199 Wp = 55
64099
YDOT = -3376
524123 meter/sec RA =
57961 deg
ZDOT = -4335
925158 TA = 168
17766
MA = 168
16531
Ha = 220
511 n
mi
Hp = 214
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15968124
39 X = -4815668
27
Y = -9727243
60 feet Y = -3019003
66 meter
Z = -12090299
13 Z = -3708640
74
XDOT = 17515
315612 XDOT = 5397
090279
YDOT = -11077
835049 feet/sec YDOT = -3316
497055 meter/sec
ZDOT = -14225
476240 ZDOT = -4309
849658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18090300
71 X = -5513923
66
Y = -4450217
35 feet Y = -1356426
25 meter
Z = -12194760
48 Z = -3716962
99
XDOT = 13093
867624 XDOT = 3991
010852
YDOT = -14579
367606 feet/sec YDOT = -4443
791246 meter/sec
ZDOT = -14108
597956 ZDOT = -4300
300657
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 18099
52661025
00016717 00000-0 10270-3 0 9001
2 25544 51
6430 1
0083 0002203 324
9441 35
1566 15
54226406 27838
Satellite: ISS
Catalog Number: 25544
Epoch time: 18099
52661025 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 1
0083 deg
Eccentricity:
0002203
Arg of perigee: 324
9441 deg
Mean anomaly: 35
1566 deg
Mean motion: 15
54226406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2783
Checksum: 273
Coasting Arc #2 (Orbit 2798)
---------------------------------------
Vector Time (GMT): 2018/100/12:03:23
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3388321
38 A = 6779508
00 meter
Y = 3488995
99 meter E =
0006069
Z = 4718786
83 I = 51
60573
XDOT = -6628
867395 Wp = 105
44335
YDOT = 2702
651261 meter/sec RA = 355
58833 deg
ZDOT = 2757
018754 TA = 317
23886
MA = 317
28606
Ha = 220
551 n
mi
Hp = 214
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11116539
96 X = 3326133
27
Y = 11446837
24 feet Y = 3526539
14 meter
Z = 15481584
09 Z = 4735094
83
XDOT = -21748
252607 XDOT = -6671
988649
YDOT = 8866
966080 feet/sec YDOT = 2628
281788 meter/sec
ZDOT = 9045
337120 ZDOT = 2724
713105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14095896
69 X = 4296429
31
Y = 7326134
32 feet Y = 2233005
74 meter
Z = 15553791
88 Z = 4740795
77
XDOT = -17293
910245 XDOT = -5271
183843
YDOT = 14346
155977 feet/sec YDOT = 4372
708342 meter/sec
ZDOT = 8900
778230 ZDOT = 2712
957205
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 18100
55537957
00016717 00000-0 10270-3 0 9014
2 25544 51
6433 355
8788 0002151 332
9599 27
1441 15
54223534 27997
Satellite: ISS
Catalog Number: 25544
Epoch time: 18100
55537957 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 355
8788 deg
Eccentricity:
0002151
Arg of perigee: 332
9599 deg
Mean anomaly: 27
1441 deg
Mean motion: 15
54223534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2799
Checksum: 325
Coasting Arc #3 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2018/101/03:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1133689
08 A = 6777810
29 meter
Y = 4267695
02 meter E =
0005585
Z = 5140304
76 I = 51
57638
XDOT = -7519
905683 Wp = 34
40186
YDOT = -184
977385 meter/sec RA = 352
30987 deg
ZDOT = -1499
623099 TA = 70
07956
MA = 70
01940
Ha = 220
713 n
mi
Hp = 214
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3719452
37 X = -1206296
24
Y = 14001624
10 feet Y = 4254611
76 meter
Z = 16864516
93 Z = 5134621
01
XDOT = -24671
606571 XDOT = -7509
993943
YDOT = -606
881183 feet/sec YDOT = -269
014842 meter/sec
ZDOT = -4920
023292 ZDOT = -1536
128100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12330231
70 X = -3758254
62
Y = -7663056
45 feet Y = -2335699
61 meter
Z = 16838488
25 Z = 5132371
22
XDOT = 7045
874112 XDOT = 2147
582429
YDOT = -22544
342942 feet/sec YDOT = -6871
515729 meter/sec
ZDOT = -5082
854461 ZDOT = -1549
254040
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 18101
19835660
00016717 00000-0 10270-3 0 9028
2 25544 51
6409 352
6722 0001958 337
7050 22
4018 15
54243106 28099
Satellite: ISS
Catalog Number: 25544
Epoch time: 18101
19835660 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 352
6722 deg
Eccentricity:
0001958
Arg of perigee: 337
7050 deg
Mean anomaly: 22
4018 deg
Mean motion: 15
54243106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2809
Checksum: 291
Coasting Arc #4 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2018/102/03:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2863921
24 A = 6780792
97 meter
Y = -4257989
88 meter E =
0007838
Z = -4439842
26 I = 51
55355
XDOT = 6818
483753 Wp = 98
77725
YDOT = 1149
703184 meter/sec RA = 347
30992 deg
ZDOT = 3299
470024 TA = 204
56200
MA = 204
59935
Ha = 220
731 n
mi
Hp = 214
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9396067
07 X = 2932888
84
Y = -13969783
06 feet Y = -4225578
31 meter
Z = -14566411
60 Z = -4425762
41
XDOT = 22370
353519 XDOT = 6789
093587
YDOT = 3771
992074 feet/sec YDOT = 1225
788129 meter/sec
ZDOT = 10825
032888 ZDOT = 3332
520408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10909344
88 X = 3325168
32
Y = 12894662
90 feet Y = 3930293
25 meter
Z = -14502935
06 Z = -4420494
60
XDOT = -8680
993751 XDOT = -2645
966895
YDOT = 19671
076831 feet/sec YDOT = 5995
744218 meter/sec
ZDOT = 10972
289593 ZDOT = 3344
353868
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 18102
16282206
00016717 00000-0 10270-3 0 9039
2 25544 51
6409 347
8647 0002094 337
7882 22
3179 15
54217660 28246
Satellite: ISS
Catalog Number: 25544
Epoch time: 18102
16282206 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 347
8647 deg
Eccentricity:
0002094
Arg of perigee: 337
7882 deg
Mean anomaly: 22
3179 deg
Mean motion: 15
54217660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 309
Coasting Arc #5 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2018/103/03:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4343883
65 A = 6784560
74 meter
Y = 4080693
19 meter E =
0012234
Z = 3232809
45 I = 51
53406
XDOT = -5604
507494 Wp = 83
33064
YDOT = -2181
972832 meter/sec RA = 342
31620 deg
ZDOT = -4759
569356 TA = 59
15574
MA = 59
03543
Ha = 220
762 n
mi
Hp = 214
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14251586
76 X = -4404895
57
Y = 13388101
01 feet Y = 4031776
07 meter
Z = 10606330
21 Z = 3211559
70
XDOT = -18387
491779 XDOT = -5556
571967
YDOT = -7158
703517 feet/sec YDOT = -2244
378736 meter/sec
ZDOT = -15615
385027 ZDOT = -4786
677576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9349893
28 X = -2849847
47
Y = -17232049
18 feet Y = -5252328
59 meter
Z = 10510908
18 Z = 3203724
81
XDOT = 10277
930043 XDOT = 3132
713077
YDOT = -15209
124405 feet/sec YDOT = -4635
741119 meter/sec
ZDOT = -15735
963926 ZDOT = -4796
321805
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 18103
19158036
00016717 00000-0 10270-3 0 9047
2 25544 51
6402 342
7351 0002210 343
5631 16
5450 15
54271875 28405
Satellite: ISS
Catalog Number: 25544
Epoch time: 18103
19158036 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 342
7351 deg
Eccentricity:
0002210
Arg of perigee: 343
5631 deg
Mean anomaly: 16
5450 deg
Mean motion: 15
54271875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 276
Coasting Arc #6 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2018/104/03:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5408234
01 A = 6787729
05 meter
Y = -3724492
76 meter E =
0009300
Z = -1701135
83 I = 51
51303
XDOT = 4004
940738 Wp = 28
23029
YDOT = 3227
421532 meter/sec RA = 337
33207 deg
ZDOT = 5687
057475 TA = 313
08370
MA = 313
16149
Ha = 220
839 n
mi
Hp = 214
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17743549
90 X = 5457743
64
Y = -12219464
44 feet Y = -3663737
51 meter
Z = -5581154
29 Z = -1674743
68
XDOT = 13139
569349 XDOT = 3940
928229
YDOT = 10588
653320 feet/sec YDOT = 3271
850186 meter/sec
ZDOT = 18658
325048 ZDOT = 5706
356441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7695204
57 X = 2345498
35
Y = 20155374
27 feet Y = 6143358
08 meter
Z = -5462862
99 Z = -1665080
64
XDOT = -11884
644672 XDOT = -3622
439696
YDOT = 9598
932776 feet/sec YDOT = 2925
754710 meter/sec
ZDOT = 18743
902266 ZDOT = 5713
141411
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 18104
15603885
00016717 00000-0 10270-3 0 9052
2 25544 51
6396 337
9276 0002050 351
0126 9
0990 15
54273252 28557
Satellite: ISS
Catalog Number: 25544
Epoch time: 18104
15603885 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 337
9276 deg
Eccentricity:
0002050
Arg of perigee: 351
0126 deg
Mean anomaly: 9
0990 deg
Mean motion: 15
54273252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 303
Coasting Arc #7 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2018/105/03:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6027925
14 A = 6788950
90 meter
Y = 3113752
47 meter E =
0010186
Z = -49150
37 I = 51
48577
XDOT = -2158
170132 Wp = 127
18973
YDOT = -4259
060150 meter/sec RA = 332
35084 deg
ZDOT = -5998
948591 TA = 53
34073
MA = 53
24714
Ha = 220
843 n
mi
Hp = 214
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19776657
28 X = -6062057
21
Y = 10215723
32 feet Y = 3046153
21 meter
Z = -161254
48 Z = -78515
48
XDOT = -7080
610669 XDOT = -2081
243676
YDOT = -13973
294456 feet/sec YDOT = -4282
764730 meter/sec
ZDOT = -19681
589867 ZDOT = -6009
245120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5649151
69 X = -1721861
43
Y = -21529156
80 feet Y = -6562086
99 meter
Z = -292697
66 Z = -89214
25
XDOT = 13585
687291 XDOT = 4140
917486
YDOT = -3317
865632 feet/sec YDOT = -1011
285444 meter/sec
ZDOT = -19726
853587 ZDOT = -6012
744973
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 18105
18479134
00016717 00000-0 10270-3 0 9065
2 25544 51
6383 332
7976 0002280 351
5628 8
5486 15
54256841 28717
Satellite: ISS
Catalog Number: 25544
Epoch time: 18105
18479134 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 332
7976 deg
Eccentricity:
0002280
Arg of perigee: 351
5628 deg
Mean anomaly: 8
5486 deg
Mean motion: 15
54256841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 326
Coasting Arc #8 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2018/105/08:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 781172
47 A = 6779339
05 meter
Y = -4763046
85 meter E =
0010215
Z = -4769822
55 I = 51
45030
XDOT = 7043
055500 Wp = 96
63963
YDOT = -1473
252438 meter/sec RA = 331
26334 deg
ZDOT = 2628
322806 TA = 199
36254
MA = 199
40138
Ha = 220
826 n
mi
Hp = 214
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2562901
81 X = 857545
69
Y = -15626794
12 feet Y = -4753884
64 meter
Z = -15649024
12 Z = -4765841
91
XDOT = 23107
137466 XDOT = 7046
239181
YDOT = -4833
505373 feet/sec YDOT = -1394
474102 meter/sec
ZDOT = 8623
106318 ZDOT = 2662
543834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9141851
35 X = 2786436
29
Y = -12952604
51 feet Y = -3947953
85 meter
Z = -15630537
63 Z = -4764187
87
XDOT = 21937
208067 XDOT = 6686
461019
YDOT = 4907
395907 feet/sec YDOT = 1495
774273 meter/sec
ZDOT = 8775
950067 ZDOT = 2674
909580
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 18105
37768308
00016717 00000-0 10270-3 0 9071
2 25544 51
6412 331
8367 0002365 349
3320 10
7782 15
54259234 28748
Satellite: ISS
Catalog Number: 25544
Epoch time: 18105
37768308 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 331
8367 deg
Eccentricity:
0002365
Arg of perigee: 349
3320 deg
Mean anomaly: 10
7782 deg
Mean motion: 15
54259234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2874
Checksum: 313
Coasting Arc #9 (Orbit 2889)
---------------------------------------
Vector Time (GMT): 2018/106/08:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2348018
86 A = 6783113
85 meter
Y = 5148373
97 meter E =
0011861
Z = 3733821
35 I = 51
43425
XDOT = -6380
551144 Wp = 72
58896
YDOT = 184
633411 meter/sec RA = 326
25942 deg
ZDOT = -4252
339741 TA = 62
63061
MA = 62
50996
Ha = 220
926 n
mi
Hp = 214
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7703473
96 X = -2423552
12
Y = 16890990
72 feet Y = 5121694
76 meter
Z = 12250070
06 Z = 3722231
45
XDOT = -20933
566744 XDOT = -6361
485576
YDOT = 605
752660 feet/sec YDOT = 113
387974 meter/sec
ZDOT = -13951
245868 ZDOT = -4283
288467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14098232
44 X = -4297141
25
Y = 12131438
49 feet Y = 3697662
45 meter
Z = 12197595
56 Z = 3717827
13
XDOT = -18323
946392 XDOT = -5585
138860
YDOT = -7080
003148 feet/sec YDOT = -2157
984959 meter/sec
ZDOT = -14089
286876 ZDOT = -4294
414640
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 18106
40643124
00016717 00000-0 10270-3 0 9085
2 25544 51
6411 326
7079 0002345 352
8270 7
2849 15
54249799 28909
Satellite: ISS
Catalog Number: 25544
Epoch time: 18106
40643124 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 326
7079 deg
Eccentricity:
0002345
Arg of perigee: 352
8270 deg
Mean anomaly: 7
2849 deg
Mean motion: 15
54249799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2890
Checksum: 318
Coasting Arc #10 (Orbit 2904)
---------------------------------------
Vector Time (GMT): 2018/107/08:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3605260
09 A = 6786666
83 meter
Y = -5259540
59 meter E =
0007709
Z = -2314878
87 I = 51
42032
XDOT = 5299
659365 Wp = 30
33820
YDOT = 1264
972871 meter/sec RA = 321
26298 deg
ZDOT = 5394
142861 TA = 303
78034
MA = 303
85375
Ha = 220
931 n
mi
Hp = 214
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11828281
14 X = 3675050
43
Y = -17255710
61 feet Y = -5218834
00 meter
Z = -7594746
95 Z = -2297195
63
XDOT = 17387
333874 XDOT = 5258
917808
YDOT = 4150
173461 feet/sec YDOT = 1324
009813 meter/sec
ZDOT = 17697
319097 ZDOT = 5419
788230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17785778
54 X = 5421105
30
Y = -11069664
48 feet Y = -3374033
73 meter
Z = -7515089
80 Z = -2290599
37
XDOT = 13363
593441 XDOT = 4073
223281
YDOT = 9411
812805 feet/sec YDOT = 2868
720543 meter/sec
ZDOT = 17811
481490 ZDOT = 5428
939558
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 18107
37087805
00016717 00000-0 10270-3 0 9091
2 25544 51
6417 321
8984 0002431 356
0098 4
1035 15
54277490 29055
Satellite: ISS
Catalog Number: 25544
Epoch time: 18107
37087805 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 321
8984 deg
Eccentricity:
0002431
Arg of perigee: 356
0098 deg
Mean anomaly: 4
1035 deg
Mean motion: 15
54277490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2905
Checksum: 310
Coasting Arc #11 (Orbit 2920)
---------------------------------------
Vector Time (GMT): 2018/108/08:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4534724
49 A = 6788859
43 meter
Y = 5009083
12 meter E =
0011732
Z = 608203
78 I = 51
40178
XDOT = -3925
087827 Wp = 119
69961
YDOT = -2820
814987 meter/sec RA = 316
27492 deg
ZDOT = -5952
505009 TA = 53
71346
MA = 53
60515
Ha = 220
989 n
mi
Hp = 214
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14877705
03 X = -4593354
78
Y = 16433999
75 feet Y = 4958044
91 meter
Z = 1995419
24 Z = 586032
67
XDOT = -12877
584733 XDOT = -3864
338294
YDOT = -9254
642347 feet/sec YDOT = -2864
368546 meter/sec
ZDOT = -19529
215910 ZDOT = -5971
424445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20058650
34 X = -6113876
62
Y = 9458364
65 feet Y = 2882909
54 meter
Z = 1895794
67 Z = 577838
22
XDOT = -7528
258243 XDOT = -2294
613113
YDOT = -11978
292397 feet/sec YDOT = -3650
983523 meter/sec
ZDOT = -19613
146423 ZDOT = -5978
087030
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 18108
39962065
00016717 00000-0 10270-3 0 9106
2 25544 51
6412 316
7696 0002312 359
4382
6768 15
54241367 29210
Satellite: ISS
Catalog Number: 25544
Epoch time: 18108
39962065 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 316
7696 deg
Eccentricity:
0002312
Arg of perigee: 359
4382 deg
Mean anomaly:
6768 deg
Mean motion: 15
54241367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2921
Checksum: 310
Coasting Arc #12 (Orbit 2921)
---------------------------------------
Vector Time (GMT): 2018/108/10:37:01
974
Vector Time (MET): N/A
Weight (LBS) : 928428
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5027600
71 A = 6780431
92 meter
Y = -199327
30 meter E =
0010405
Z = -4555589
45 I = 51
37005
XDOT = 3025
674096 Wp = 56
80335
YDOT = -6335
419697 meter/sec RA = 315
92202 deg
ZDOT = -3061
463966 TA = 182
41968
MA = 182
42472
Ha = 220
921 n
mi
Hp = 214
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16494752
99 X = -5002869
04
Y = -653960
97 feet Y = -255411
26 meter
Z = -14946159
61 Z = -4579952
18
XDOT = 9926
752283 XDOT = 3111
164874
YDOT = -20785
497695 feet/sec YDOT = -6301
106614 meter/sec
ZDOT = -10044
173117 ZDOT = -3046
558165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16391909
31 X = -4996253
96
Y = 742759
68 feet Y = 226393
15 meter
Z = -15054761
57 Z = -4588691
33
XDOT = 8241
564729 XDOT = 2512
028929
YDOT = -20366
079244 feet/sec YDOT = -6207
580953 meter/sec
ZDOT = -9976
742271 ZDOT = -3040
911044
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 18108
46391582
00016717 00000-0 10270-3 0 9115
2 25544 51
6404 316
4487 0002296 341
6735 18
4334 15
54124266 29227
Satellite: ISS
Catalog Number: 25544
Epoch time: 18108
46391582 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 316
4487 deg
Eccentricity:
0002296
Arg of perigee: 341
6735 deg
Mean anomaly: 18
4334 deg
Mean motion: 15
54124266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2922
Checksum: 306
Coasting Arc #13 (Orbit 2937)
---------------------------------------
Vector Time (GMT): 2018/109/10:37:01
974
Vector Time (MET): N/A
Weight (LBS) : 928428
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4064318
32 A = 6777892
68 meter
Y = 1627552
55 meter E =
0002861
Z = 5171718
14 I = 51
33931
XDOT = -4144
949705 Wp = 91
33505
YDOT = 6329
389669 meter/sec RA = 310
90600 deg
ZDOT = 1264
860751 TA = 346
47033
MA = 346
47799
Ha = 220
875 n
mi
Hp = 214
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13334377
69 X = 4020694
61
Y = 5339739
32 feet Y = 1672758
68 meter
Z = 16967579
21 Z = 5191355
56
XDOT = -13598
916356 XDOT = -4221
562734
YDOT = 20765
714137 feet/sec YDOT = 6282
609630 meter/sec
ZDOT = 4149
805613 ZDOT = 1244
539543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13698770
02 X = 4175385
10
Y = 3961250
81 feet Y = 1207389
25 meter
Z = 17054893
16 Z = 5198331
43
XDOT = -11142
619256 XDOT = -3396
270349
YDOT = 21051
428955 feet/sec YDOT = 6416
475545 meter/sec
ZDOT = 4058
234609 ZDOT = 1236
949909
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 18109
49275164
00016717 00000-0 10270-3 0 9127
2 25544 51
6412 311
3196 0002295 346
7724 13
3368 15
54114373 29386
Satellite: ISS
Catalog Number: 25544
Epoch time: 18109
49275164 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 311
3196 deg
Eccentricity:
0002295
Arg of perigee: 346
7724 deg
Mean anomaly: 13
3368 deg
Mean motion: 15
54114373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2938
Checksum: 307
Coasting Arc #14 (Orbit 2952)
---------------------------------------
Vector Time (GMT): 2018/110/10:37:01
974
Vector Time (MET): N/A
Weight (LBS) : 928428
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2972828
26 A = 6777460
59 meter
Y = -3082845
58 meter E =
0014146
Z = -5264996
19 I = 51
31641
XDOT = 4893
323825 Wp = 85
88629
YDOT = -5853
205712 meter/sec RA = 305
88274 deg
ZDOT = 666
845586 TA = 190
50345
MA = 190
53303
Ha = 220
988 n
mi
Hp = 214
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9753373
57 X = -2912559
19
Y = -10114322
77 feet Y = -3115752
77 meter
Z = -17273609
56 Z = -5279290
99
XDOT = 16054
212023 XDOT = 4955
173057
YDOT = -19203
430814 feet/sec YDOT = -5798
139383 meter/sec
ZDOT = 2187
813604 ZDOT = 690
766144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10777323
12 X = -3284928
09
Y = -8893096
71 feet Y = -2710615
88 meter
Z = -17336883
96 Z = -5284282
23
XDOT = 12984
615875 XDOT = 3957
710919
YDOT = -20194
230142 feet/sec YDOT = -6155
201347 meter/sec
ZDOT = 2295
355295 ZDOT = 699
624294
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 18110
45728008
00016717 00000-0 10270-3 0 9136
2 25544 51
6403 306
5098 0002363 349
2220 10
8882 15
54148241 29539
Satellite: ISS
Catalog Number: 25544
Epoch time: 18110
45728008 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 306
5098 deg
Eccentricity:
0002363
Arg of perigee: 349
2220 deg
Mean anomaly: 10
8882 deg
Mean motion: 15
54148241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2953
Checksum: 289
Coasting Arc #15 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2018/111/10:37:01
974
Vector Time (MET): N/A
Weight (LBS) : 928428
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1816212
61 A = 6779452
80 meter
Y = 4438690
96 meter E =
0008472
Z = 4788895
01 I = 51
30454
XDOT = -5308
664564 Wp = 45
26552
YDOT = 4919
917449 meter/sec RA = 300
86270 deg
ZDOT = -2538
162228 TA = 69
86700
MA = 69
77587
Ha = 220
962 n
mi
Hp = 214
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5958702
78 X = 1743180
85
Y = 14562634
38 feet Y = 4458592
69 meter
Z = 15711597
80 Z = 4797540
29
XDOT = -17416
878490 XDOT = -5350
956715
YDOT = 16141
461448 feet/sec YDOT = 4860
315872 meter/sec
ZDOT = -8327
303899 ZDOT = -2564
052753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7786522
14 X = 2373331
95
Y = 13629180
93 feet Y = 4154174
35 meter
Z = 15749484
58 Z = 4800442
90
XDOT = -14003
775892 XDOT = -4268
350892
YDOT = 17790
222604 feet/sec YDOT = 5422
459850 meter/sec
ZDOT = -8443
482789 ZDOT = -2573
573554
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 18111
48610845
00016717 00000-0 10270-3 0 9140
2 25544 51
6401 301
3817 0002396 350
9958 9
1152 15
54160972 29695
Satellite: ISS
Catalog Number: 25544
Epoch time: 18111
48610845 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 301
3817 deg
Eccentricity:
0002396
Arg of perigee: 350
9958 deg
Mean anomaly: 9
1152 deg
Mean motion: 15
54160972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 309
Coasting Arc #16 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2018/112/10:37:01
974
Vector Time (MET): N/A
Weight (LBS) : 928428
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -722045
42 A = 6783032
00 meter
Y = -5552613
83 meter E =
0005798
Z = -3832765
32 I = 51
29953
XDOT = 5393
879500 Wp = 82
45802
YDOT = -3547
059297 meter/sec RA = 295
84813 deg
ZDOT = 4128
695537 TA = 231
17553
MA = 231
22731
Ha = 221
039 n
mi
Hp = 214
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2368915
43 X = -641283
29
Y = -18217236
99 feet Y = -5560236
65 meter
Z = -12574689
37 Z = -3836076
65
XDOT = 17696
455054 XDOT = 5413
087690
YDOT = -11637
333652 feet/sec YDOT = -3486
633847 meter/sec
ZDOT = 13545
589032 ZDOT = 4154
943879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5053724
21 X = -1540375
14
Y = -17651866
10 feet Y = -5380288
79 meter
Z = -12588637
40 Z = -3837016
68
XDOT = 14325
697897 XDOT = 4366
472719
YDOT = -13831
155050 feet/sec YDOT = -4215
736059 meter/sec
ZDOT = 13663
153537 ZDOT = 4164
529198
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 18112
45063402
00016717 00000-0 10270-3 0 9150
2 25544 51
6392 296
5729 0002307 353
4424 6
6698 15
54148038 29842
Satellite: ISS
Catalog Number: 25544
Epoch time: 18112
45063402 = yrday
fracday
Element set: 915
Inclination: 51
6392 deg
RA of node: 296
5729 deg
Eccentricity:
0002307
Arg of perigee: 353
4424 deg
Mean anomaly: 6
6698 deg
Mean motion: 15
54148038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 316
Coasting Arc #17 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2018/113/10:37:01
974
Vector Time (MET): N/A
Weight (LBS) : 928428
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -309774
36 A = 6786618
53 meter
Y = 6318327
07 meter E =
0013140
Z = 2444684
96 I = 51
29892
XDOT = -5235
480616 Wp = 94
63377
YDOT = 1805
207092 meter/sec RA = 290
84325 deg
ZDOT = -5305
338227 TA = 57
85658
MA = 57
72916
Ha = 221
070 n
mi
Hp = 214
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1016320
09 X = -392279
61
Y = 20729419
51 feet Y = 6314401
67 meter
Z = 8020619
93 Z = 2442979
71
XDOT = -17176
773673 XDOT = -5229
507238
YDOT = 5922
595446 feet/sec YDOT = 1746
693682 meter/sec
ZDOT = -17405
965313 ZDOT = -5330
755937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2478606
48 X = 755479
26
Y = 20609095
94 feet Y = 6281652
44 meter
Z = 8012100
74 Z = 2442088
31
XDOT = -14300
083677 XDOT = -4358
665505
YDOT = 8561
037769 feet/sec YDOT = 2609
404312 meter/sec
ZDOT = -17519
566934 ZDOT = -5339
964002
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 18113
47945538
00016717 00000-0 10270-3 0 9163
2 25544 51
6396 291
4436 0002574 356
7094 3
4042 15
54191947 30005
Satellite: ISS
Catalog Number: 25544
Epoch time: 18113
47945538 = yrday
fracday
Element set: 916
Inclination: 51
6396 deg
RA of node: 291
4436 deg
Eccentricity:
0002574
Arg of perigee: 356
7094 deg
Mean anomaly: 3
4042 deg
Mean motion: 15
54191947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 312
Coasting Arc #18 (Orbit 3014)
---------------------------------------
Vector Time (GMT): 2018/114/10:37:01
974
Vector Time (MET): N/A
Weight (LBS) : 928428
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1188687
76 A = 6788989
57 meter
Y = -6625994
89 meter E =
0012155
Z = -830744
21 I = 51
29342
XDOT = 4884
062998 Wp = 32
84234
YDOT = 141
396522 meter/sec RA = 285
84582 deg
ZDOT = 5911
446551 TA = 318
12775
MA = 318
22066
Ha = 221
177 n
mi
Hp = 214
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3899894
22 X = 1266728
42
Y = -21738828
38 feet Y = -6612265
84 meter
Z = -2725538
74 Z = -824780
21
XDOT = 16023
828733 XDOT = 4853
404128
YDOT = 463
899350 feet/sec YDOT = 195
842237 meter/sec
ZDOT = 19394
509682 ZDOT = 5935
097207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -223649
24 X = -68168
29
Y = -22088122
74 feet Y = -6732459
81 meter
Z = -2698001
15 Z = -822350
75
XDOT = 14090
433773 XDOT = 4294
764214
YDOT = -2503
984908 feet/sec YDOT = -763
214600 meter/sec
ZDOT = 19499
950912 ZDOT = 5943
585038
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 18114
44397532
00016717 00000-0 10270-3 0 9177
2 25544 51
6374 286
6349 0002309 2
8088 357
3077 15
54146144 30152
Satellite: ISS
Catalog Number: 25544
Epoch time: 18114
44397532 = yrday
fracday
Element set: 917
Inclination: 51
6374 deg
RA of node: 286
6349 deg
Eccentricity:
0002309
Arg of perigee: 2
8088 deg
Mean anomaly: 357
3077 deg
Mean motion: 15
54146144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3015
Checksum: 313
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