[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 16th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
235/02:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
5
000/00:00:00
000 0
0 0
0 213
0
238/15:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
0
Coasting Arc #1 (Orbit 776)
---------------------------------------
Vector Time (GMT): 2018/227/17:10:50
574
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2018258
88 A = 6789501
79 meter
Y = -6342352
02 meter E =
0017421
Z = 1310921
94 I = 52
03235
XDOT = 4228
679275 Wp = 105
62042
YDOT = -2569
064276 meter/sec RA = 81
18957 deg
ZDOT = -5859
061625 TA = 60
19020
MA = 60
01709
Ha = 223
392 n
mi
Hp = 213
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6621584
25 X = -1953554
64
Y = -20808241
55 feet Y = -6364559
76 meter
Z = 4300924
99 Z = 1301275
45
XDOT = 13873
619667 XDOT = 4285
552886
YDOT = -8428
688569 feet/sec YDOT = -2521
458485 meter/sec
ZDOT = -19222
643128 ZDOT = -5838
382170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18648745
34 X = 5684137
58
Y = 11376133
99 feet Y = 3467445
64 meter
Z = 4258417
84 Z = 1297965
76
XDOT = -4235
589784 XDOT = -1291
007766
YDOT = 14178
397410 feet/sec YDOT = 4321
575531 meter/sec
ZDOT = -19129
455276 ZDOT = -5830
657968
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 18227
75060283
00016717 00000-0 10270-3 0 9008
2 25544 51
6380 81
8651 0005439 64
8826 295
2890 15
53824645 7778
Satellite: ISS
Catalog Number: 25544
Epoch time: 18227
75060283 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 81
8651 deg
Eccentricity:
0005439
Arg of perigee: 64
8826 deg
Mean anomaly: 295
2890 deg
Mean motion: 15
53824645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 777
Checksum: 330
Coasting Arc #2 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2018/228/17:10:50
574
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1402650
72 A = 6790168
89 meter
Y = 6630249
81 meter E =
0017903
Z = 273967
34 I = 52
03050
XDOT = -4673
463619 Wp = 54
07879
YDOT = 728
244937 meter/sec RA = 76
24705 deg
ZDOT = 6038
481074 TA = 308
85823
MA = 309
01785
Ha = 223
436 n
mi
Hp = 213
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4601872
46 X = 1327074
41
Y = 21752788
10 feet Y = 6645512
66 meter
Z = 898842
97 Z = 280597
12
XDOT = -15332
885888 XDOT = -4710
591222
YDOT = 2389
255044 feet/sec YDOT = 675
775611 meter/sec
ZDOT = 19811
289613 ZDOT = 6015
689007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17942975
90 X = -5469019
05
Y = -13128512
11 feet Y = -4001570
49 meter
Z = 927752
44 Z = 282778
94
XDOT = 8960
772545 XDOT = 2731
243472
YDOT = -10794
688962 feet/sec YDOT = -3290
221196 meter/sec
ZDOT = 19708
849268 ZDOT = 6007
257257
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 18228
77963621
00016717 00000-0 10270-3 0 9010
2 25544 51
6399 76
7376 0005511 68
1870 291
9868 15
53829455 7932
Satellite: ISS
Catalog Number: 25544
Epoch time: 18228
77963621 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 76
7376 deg
Eccentricity:
0005511
Arg of perigee: 68
1870 deg
Mean anomaly: 291
9868 deg
Mean motion: 15
53829455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 793
Checksum: 356
Coasting Arc #3 (Orbit 807)
---------------------------------------
Vector Time (GMT): 2018/229/17:10:50
574
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -637782
35 A = 6788629
04 meter
Y = -6488902
15 meter E =
0010419
Z = -1890255
29 I = 52
01671
XDOT = 5045
922509 Wp = 110
50949
YDOT = 1142
268374 meter/sec RA = 71
30334 deg
ZDOT = -5652
394395 TA = 90
17794
MA = 90
05855
Ha = 223
441 n
mi
Hp = 213
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2092461
78 X = -555992
45
Y = -21289049
05 feet Y = -6495576
99 meter
Z = -6201624
96 Z = -1893154
64
XDOT = 16554
863874 XDOT = 5060
230482
YDOT = 3747
599653 feet/sec YDOT = 1198
775285 meter/sec
ZDOT = -18544
601033 ZDOT = -5627
848495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15985854
61 X = 4872488
48
Y = 14209273
86 feet Y = 4330986
67 meter
Z = -6213786
82 Z = -1893962
22
XDOT = -13736
506205 XDOT = -4186
887091
YDOT = 7433
522140 feet/sec YDOT = 2265
737548 meter/sec
ZDOT = -18434
531221 ZDOT = -5618
845116
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 18229
74435275
00016717 00000-0 10270-3 0 9028
2 25544 51
6400 71
9306 0005585 71
2325 288
9433 15
53844432 8089
Satellite: ISS
Catalog Number: 25544
Epoch time: 18229
74435275 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 71
9306 deg
Eccentricity:
0005585
Arg of perigee: 71
2325 deg
Mean anomaly: 288
9433 deg
Mean motion: 15
53844432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 808
Checksum: 311
Coasting Arc #4 (Orbit 823)
---------------------------------------
Vector Time (GMT): 2018/230/17:10:50
574
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -202444
71 A = 6785540
22 meter
Y = 5927112
83 meter E =
0018096
Z = 3279658
20 I = 51
99532
XDOT = -5305
946755 Wp = 83
93668
YDOT = -2830
472692 meter/sec RA = 66
35336 deg
ZDOT = 4767
175048 TA = 313
95472
MA = 314
10386
Ha = 223
426 n
mi
Hp = 213
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -664188
69 X = -284639
02
Y = 19445908
23 feet Y = 5924389
39 meter
Z = 10760033
48 Z = 3278475
15
XDOT = -17407
961793 XDOT = -5297
057533
YDOT = -9286
327731 feet/sec YDOT = -2889
757742 meter/sec
ZDOT = 15640
338084 ZDOT = 4741
422386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12941496
09 X = -3944568
01
Y = -14533877
46 feet Y = -4429925
85 meter
Z = 10753924
82 Z = 3277796
29
XDOT = 18001
223253 XDOT = 5486
772848
YDOT = -4491
498169 feet/sec YDOT = -1369
008642 meter/sec
ZDOT = 15525
078981 ZDOT = 4732
044073
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 18230
77338177
00016717 00000-0 10270-3 0 9037
2 25544 51
6403 66
8038 0005502 76
0219 284
1545 15
53864631 8244
Satellite: ISS
Catalog Number: 25544
Epoch time: 18230
77338177 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 66
8038 deg
Eccentricity:
0005502
Arg of perigee: 76
0219 deg
Mean anomaly: 284
1545 deg
Mean motion: 15
53864631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 824
Checksum: 305
Coasting Arc #5 (Orbit 838)
---------------------------------------
Vector Time (GMT): 2018/231/17:10:50
574
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1190675
27 A = 6782014
42 meter
Y = -5023911
78 meter E =
0014406
Z = -4411914
66 I = 51
96963
XDOT = 5365
373410 Wp = 72
75339
YDOT = 4263
847017 meter/sec RA = 61
39352 deg
ZDOT = -3412
337363 TA = 162
80912
MA = 162
76028
Ha = 223
459 n
mi
Hp = 213
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3906414
92 X = 1268196
11
Y = -16482650
21 feet Y = -5010163
36 meter
Z = -14474785
62 Z = -4405942
57
XDOT = 17602
931134 XDOT = 5333
870320
YDOT = 13988
999398 feet/sec YDOT = 4323
670210 meter/sec
ZDOT = -11195
332556 ZDOT = -3386
350957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8783842
18 X = 2677315
10
Y = 14511284
34 feet Y = 4423039
47 meter
Z = -14447283
40 Z = -4403531
98
XDOT = -21339
820393 XDOT = -6504
377256
YDOT = 1903
312965 feet/sec YDOT = 580
129792 meter/sec
ZDOT = -11079
225216 ZDOT = -3376
947846
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 18231
73809740
00016717 00000-0 10270-3 0 9044
2 25544 51
6410 61
9974 0005462 78
9013 281
2754 15
53825208 8398
Satellite: ISS
Catalog Number: 25544
Epoch time: 18231
73809740 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 61
9974 deg
Eccentricity:
0005462
Arg of perigee: 78
9013 deg
Mean anomaly: 281
2754 deg
Mean motion: 15
53825208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 839
Checksum: 316
Coasting Arc #6 (Orbit 854)
---------------------------------------
Vector Time (GMT): 2018/232/17:10:50
574
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2226510
59 A = 6779096
91 meter
Y = 3863034
62 meter E =
0010029
Z = 5098566
95 I = 51
94403
XDOT = -5212
873291 Wp = 102
22158
YDOT = -5347
349471 meter/sec RA = 56
42350 deg
ZDOT = 1770
105861 TA = 330
71802
MA = 330
77419
Ha = 223
520 n
mi
Hp = 213
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7304824
78 X = -2294308
51
Y = 12673998
11 feet Y = 3837757
10 meter
Z = 16727581
86 Z = 5087586
83
XDOT = -17102
602660 XDOT = -5161
288467
YDOT = -17543
797478 feet/sec YDOT = -5405
355018 meter/sec
ZDOT = 5807
433928 ZDOT = 1744
909042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3922102
94 X = -1195456
98
Y = -14151773
01 feet Y = -4313460
41 meter
Z = 16677743
16 Z = 5083376
12
XDOT = 23495
007989 XDOT = 7161
278435
YDOT = 219
380036 feet/sec YDOT = 66
867035 meter/sec
ZDOT = 5695
029696 ZDOT = 1735
845051
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 18232
76712235
00016717 00000-0 10270-3 0 9051
2 25544 51
6415 56
8698 0005540 81
5176 278
6604 15
53869010 8557
Satellite: ISS
Catalog Number: 25544
Epoch time: 18232
76712235 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 56
8698 deg
Eccentricity:
0005540
Arg of perigee: 81
5176 deg
Mean anomaly: 278
6604 deg
Mean motion: 15
53869010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 855
Checksum: 322
Coasting Arc #7 (Orbit 869)
---------------------------------------
Vector Time (GMT): 2018/233/17:10:50
574
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3310967
79 A = 6778189
20 meter
Y = -2566469
47 meter E =
0020415
Z = -5346236
20 I = 51
92110
XDOT = 4738
385204 Wp = 88
51265
YDOT = 6009
330513 meter/sec RA = 51
44833 deg
ZDOT = 50
412918 TA = 181
96283
MA = 181
97085
Ha = 223
478 n
mi
Hp = 213
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10862755
22 X = 3365389
53
Y = -8420175
44 feet Y = -2529139
59 meter
Z = -17540145
01 Z = -5330020
73
XDOT = 15545
883214 XDOT = 4670
590168
YDOT = 19715
651290 feet/sec YDOT = 6061
939350 meter/sec
ZDOT = 165
396712 ZDOT = 73
265437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1375158
95 X = -419148
45
Y = 13768415
56 feet Y = 4196613
06 meter
Z = -17466973
50 Z = -5323933
52
XDOT = -24009
235337 XDOT = -7318
014931
YDOT = -2061
893701 feet/sec YDOT = -628
465200 meter/sec
ZDOT = 267
173169 ZDOT = 81
434382
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 18233
73183374
00016717 00000-0 10270-3 0 9066
2 25544 51
6412 52
0640 0005574 84
0136 276
1652 15
53845128 8707
Satellite: ISS
Catalog Number: 25544
Epoch time: 18233
73183374 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 52
0640 deg
Eccentricity:
0005574
Arg of perigee: 84
0136 deg
Mean anomaly: 276
1652 deg
Mean motion: 15
53845128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 870
Checksum: 297
Coasting Arc #8 (Orbit 885)
---------------------------------------
Vector Time (GMT): 2018/234/17:10:50
574
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4326363
73 A = 6779289
51 meter
Y = 1214900
15 meter E =
0010775
Z = 5068158
39 I = 51
90362
XDOT = -3964
905234 Wp = 71
07962
YDOT = -6299
930719 meter/sec RA = 46
47028 deg
ZDOT = -1867
774706 TA = 36
97166
MA = 36
89745
Ha = 223
590 n
mi
Hp = 213
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14194106
72 X = -4364245
58
Y = 3985892
89 feet Y = 1166307
93 meter
Z = 16627816
24 Z = 5047050
75
XDOT = -13008
219272 XDOT = -3885
090470
YDOT = -20669
064038 feet/sec YDOT = -6343
822754 meter/sec
ZDOT = -6127
869770 ZDOT = -1886
840702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6656658
63 X = 2028949
55
Y = -13273941
43 feet Y = -4045897
35 meter
Z = 16532865
92 Z = 5039217
53
XDOT = 23053
876341 XDOT = 7026
821509
YDOT = 3795
971925 feet/sec YDOT = 1157
012243 meter/sec
ZDOT = -6212
594458 ZDOT = -1893
598791
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 18234
76085679
00016717 00000-0 10270-3 0 9070
2 25544 51
6412 46
9359 0005555 87
4609 272
7180 15
53868576 8864
Satellite: ISS
Catalog Number: 25544
Epoch time: 18234
76085679 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 46
9359 deg
Eccentricity:
0005555
Arg of perigee: 87
4609 deg
Mean anomaly: 272
7180 deg
Mean motion: 15
53868576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 886
Checksum: 358
Coasting Arc #9 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2018/235/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -823133
50 A = 6779840
04 meter
Y = 4595534
28 meter E =
0011600
Z = 4907683
52 I = 51
89467
XDOT = -6326
488918 Wp = 104
73631
YDOT = -3652
926028 meter/sec RA = 44
62718 deg
ZDOT = 2351
977139 TA = 322
30191
MA = 322
38314
Ha = 223
457 n
mi
Hp = 213
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2700569
23 X = -898299
40
Y = 15077212
20 feet Y = 4585909
15 meter
Z = 16101323
90 Z = 4903502
53
XDOT = -20756
197237 XDOT = -6296
595166
YDOT = -11984
665447 feet/sec YDOT = -3723
506060 meter/sec
ZDOT = 7716
460431 ZDOT = 2321
318375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1627947
32 X = -496198
34
Y = 15250910
13 feet Y = 4648477
41 meter
Z = 16081901
65 Z = 4901763
62
XDOT = -20562
762519 XDOT = -6267
530016
YDOT = -10213
251948 feet/sec YDOT = -3112
999194 meter/sec
ZDOT = 7579
310488 ZDOT = 2310
173837
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 18235
14673988
00016717 00000-0 10270-3 0 9080
2 25544 51
6388 45
0160 0005526 85
3216 274
8568 15
53879391 8922
Satellite: ISS
Catalog Number: 25544
Epoch time: 18235
14673988 = yrday
fracday
Element set: 908
Inclination: 51
6388 deg
RA of node: 45
0160 deg
Eccentricity:
0005526
Arg of perigee: 85
3216 deg
Mean anomaly: 274
8568 deg
Mean motion: 15
53879391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 346
Coasting Arc #10 (Orbit 906)
---------------------------------------
Vector Time (GMT): 2018/236/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2176285
36 A = 6778299
52 meter
Y = -3619961
31 meter E =
0020379
Z = -5319060
88 I = 51
86501
XDOT = 6148
477444 Wp = 85
99577
YDOT = 4521
774947 meter/sec RA = 39
64713 deg
ZDOT = -562
188219 TA = 178
64800
MA = 178
64248
Ha = 223
522 n
mi
Hp = 213
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7140043
84 X = 2242439
74
Y = -11876513
50 feet Y = -3595254
76 meter
Z = -17450987
14 Z = -5308328
71
XDOT = 20172
170093 XDOT = 6100
187505
YDOT = 14835
219644 feet/sec YDOT = 4590
261465 meter/sec
ZDOT = -1844
449537 ZDOT = -532
438946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6097103
77 X = 1858397
23
Y = -12512175
99 feet Y = -3813711
24 meter
Z = -17402285
15 Z = -5304216
51
XDOT = 20587
054567 XDOT = 6274
934232
YDOT = 12410
206831 feet/sec YDOT = 3782
631042 meter/sec
ZDOT = -1711
513241 ZDOT = -521
669236
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 18236
11144752
00016717 00000-0 10270-3 0 9091
2 25544 51
6391 40
2078 0005651 87
5117 272
6683 15
53837669 9077
Satellite: ISS
Catalog Number: 25544
Epoch time: 18236
11144752 = yrday
fracday
Element set: 909
Inclination: 51
6391 deg
RA of node: 40
2078 deg
Eccentricity:
0005651
Arg of perigee: 87
5117 deg
Mean anomaly: 272
6683 deg
Mean motion: 15
53837669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 907
Checksum: 322
Coasting Arc #11 (Orbit 922)
---------------------------------------
Vector Time (GMT): 2018/237/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3504931
87 A = 6778741
71 meter
Y = 2548915
18 meter E =
0009535
Z = 5204985
06 I = 51
84022
XDOT = -5600
545481 Wp = 75
05259
YDOT = -5090
367719 meter/sec RA = 34
66577 deg
ZDOT = -1274
164429 TA = 27
16175
MA = 27
11190
Ha = 223
668 n
mi
Hp = 213
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11499120
31 X = -3558456
65
Y = 8362582
61 feet Y = 2509421
49 meter
Z = 17076722
64 Z = 5187829
56
XDOT = -18374
493049 XDOT = -5537
018238
YDOT = -16700
681494 feet/sec YDOT = -5152
641733 meter/sec
ZDOT = -4180
329493 ZDOT = -1301
214974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10603358
18 X = -3231903
57
Y = 9610851
68 feet Y = 2929387
59 meter
Z = 16999333
44 Z = 5181396
83
XDOT = -19399
260351 XDOT = -5912
894555
YDOT = -13769
726897 feet/sec YDOT = -4197
012758 meter/sec
ZDOT = -4301
059979 ZDOT = -1310
963082
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 18237
14046651
00016717 00000-0 10270-3 0 9106
2 25544 51
6390 35
0810 0005718 90
4986 269
6822 15
53843697 9230
Satellite: ISS
Catalog Number: 25544
Epoch time: 18237
14046651 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 35
0810 deg
Eccentricity:
0005718
Arg of perigee: 90
4986 deg
Mean anomaly: 269
6822 deg
Mean motion: 15
53843697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 923
Checksum: 320
Coasting Arc #12 (Orbit 937)
---------------------------------------
Vector Time (GMT): 2018/238/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4725891
47 A = 6781186
43 meter
Y = -1505185
55 meter E =
0015653
Z = -4639352
85 I = 51
82076
XDOT = 4617
773784 Wp = 104
05088
YDOT = 5329
312519 meter/sec RA = 29
68558 deg
ZDOT = 2979
600166 TA = 195
60404
MA = 195
65234
Ha = 223
508 n
mi
Hp = 213
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15504893
27 X = 4764906
76
Y = -4938272
80 feet Y = -1452119
43 meter
Z = -15220973
91 Z = -4616301
69
XDOT = 15150
176457 XDOT = 4543
363670
YDOT = 17484
621124 feet/sec YDOT = 5380
535754 meter/sec
ZDOT = 9775
591097 ZDOT = 3001
850322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14838181
52 X = 4522677
73
Y = -6911069
29 feet Y = -2106493
92 meter
Z = -15117267
97 Z = -4607743
28
XDOT = 16710
315192 XDOT = 5093
304071
YDOT = 14311
500546 feet/sec YDOT = 4362
145366 meter/sec
ZDOT = 9874
727061 ZDOT = 3009
816808
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 18238
10517020
00016717 00000-0 10270-3 0 9117
2 25544 51
6393 30
2738 0005610 94
4167 265
7626 15
53843143 9386
Satellite: ISS
Catalog Number: 25544
Epoch time: 18238
10517020 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 30
2738 deg
Eccentricity:
0005610
Arg of perigee: 94
4167 deg
Mean anomaly: 265
7626 deg
Mean motion: 15
53843143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 938
Checksum: 297
Coasting Arc #13 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2018/238/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1464859
22 A = 6778075
54 meter
Y = 3942601
30 meter E =
0008161
Z = 5308550
37 I = 51
79785
XDOT = -6973
603465 Wp = 102
89502
YDOT = -3175
193225 meter/sec RA = 27
02074 deg
ZDOT = 431
525081 TA = 342
98818
MA = 343
01553
Ha = 223
444 n
mi
Hp = 213
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4805968
56 X = -1534623
31
Y = 12935043
64 feet Y = 3925830
46 meter
Z = 17416503
83 Z = 5301265
04
XDOT = -22879
276460 XDOT = -6939
675372
YDOT = -10417
300606 feet/sec YDOT = -3252
987160 meter/sec
ZDOT = 1415
764703 ZDOT = 397
732897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -420231
28 X = -128086
49
Y = -13834516
79 feet Y = -4216760
72 meter
Z = 17383234
57 Z = 5298409
90
XDOT = 24124
605019 XDOT = 7353
179610
YDOT = 865
719592 feet/sec YDOT = 263
871332 meter/sec
ZDOT = 1264
508201 ZDOT = 385
422100
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 18238
68398929
00016717 00000-0 10270-3 0 9126
2 25544 51
6417 27
3863 0005552 101
6913 258
4863 15
53893106 9470
Satellite: ISS
Catalog Number: 25544
Epoch time: 18238
68398929 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 27
3863 deg
Eccentricity:
0005552
Arg of perigee: 101
6913 deg
Mean anomaly: 258
4863 deg
Mean motion: 15
53893106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 947
Checksum: 340
Coasting Arc #14 (Orbit 961)
---------------------------------------
Vector Time (GMT): 2018/239/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2999685
63 A = 6778786
38 meter
Y = -3195439
79 meter E =
0019445
Z = -5188616
44 I = 51
77011
XDOT = 6485
167779 Wp = 101
20334
YDOT = 3814
996984 meter/sec RA = 22
03477 deg
ZDOT = 1400
541302 TA = 182
26366
MA = 182
27248
Ha = 223
443 n
mi
Hp = 213
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9841488
28 X = 3060398
19
Y = -10483726
35 feet Y = -3161556
14 meter
Z = -17023019
81 Z = -5173897
53
XDOT = 21276
797176 XDOT = 6435
222443
YDOT = 12516
394303 feet/sec YDOT = 3887
239461 meter/sec
ZDOT = 4594
951777 ZDOT = 1431
921967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4934936
64 X = -1504168
69
Y = 13589352
05 feet Y = 4142034
51 meter
Z = -16956489
15 Z = -5168337
89
XDOT = -23486
616710 XDOT = -7158
720773
YDOT = -2623
695295 feet/sec YDOT = -799
702326 meter/sec
ZDOT = 4735
278846 ZDOT = 1443
312992
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 18239
64869017
00016717 00000-0 10270-3 0 9135
2 25544 51
6419 22
5803 0005661 103
3227 256
8557 15
53875873 9621
Satellite: ISS
Catalog Number: 25544
Epoch time: 18239
64869017 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 22
5803 deg
Eccentricity:
0005661
Arg of perigee: 103
3227 deg
Mean anomaly: 256
8557 deg
Mean motion: 15
53875873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 962
Checksum: 330
Coasting Arc #15 (Orbit 977)
---------------------------------------
Vector Time (GMT): 2018/240/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4402676
48 A = 6781370
12 meter
Y = 2404067
67 meter E =
0013669
Z = 4552614
81 I = 51
74757
XDOT = -5563
075994 Wp = 82
04725
YDOT = -4273
530017 meter/sec RA = 17
05010 deg
ZDOT = -3113
329721 TA = 39
10409
MA = 39
00537
Ha = 223
545 n
mi
Hp = 213
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14444476
65 X = -4451346
19
Y = 7887361
12 feet Y = 2354562
13 meter
Z = 14936400
30 Z = 4531109
96
XDOT = -18251
561660 XDOT = -5499
751985
YDOT = -14020
767772 feet/sec YDOT = -4335
386374 meter/sec
ZDOT = -10214
336354 ZDOT = -3140
198777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9953368
48 X = 3033786
71
Y = -13216213
03 feet Y = -4028301
73 meter
Z = 14839528
10 Z = 4523088
17
XDOT = 21400
643323 XDOT = 6522
916085
YDOT = 4477
067371 feet/sec YDOT = 1364
610135 meter/sec
ZDOT = -10334
333435 ZDOT = -3149
904831
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 18240
67770196
00016717 00000-0 10270-3 0 9140
2 25544 51
6418 17
4528 0005640 106
6721 253
5051 15
53875726 9786
Satellite: ISS
Catalog Number: 25544
Epoch time: 18240
67770196 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 17
4528 deg
Eccentricity:
0005640
Arg of perigee: 106
6721 deg
Mean anomaly: 253
5051 deg
Mean motion: 15
53875726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 978
Checksum: 320
Coasting Arc #16 (Orbit 992)
---------------------------------------
Vector Time (GMT): 2018/241/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5561642
00 A = 6784930
85 meter
Y = -1656017
42 meter E =
0010463
Z = -3526821
36 I = 51
72714
XDOT = 4206
415696 Wp = 102
08638
YDOT = 4539
326080 meter/sec RA = 12
07248 deg
ZDOT = 4511
077220 TA = 216
49518
MA = 216
56654
Ha = 223
397 n
mi
Hp = 213
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18246856
95 X = 5596878
02
Y = -5433128
01 feet Y = -1593626
56 meter
Z = -11570936
23 Z = -3499719
29
XDOT = 13800
576431 XDOT = 4133
430773
YDOT = 14892
802100 feet/sec YDOT = 4585
957431 meter/sec
ZDOT = 14800
122114 ZDOT = 4531
332744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14193222
63 X = -4326094
26
Y = 12799403
89 feet Y = 3901258
31 meter
Z = -11449057
84 Z = -3489672
83
XDOT = -17849
208640 XDOT = -5440
438794
YDOT = -6500
735026 feet/sec YDOT = -1981
424036 meter/sec
ZDOT = 14890
385450 ZDOT = 4538
589485
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 18241
64239867
00016717 00000-0 10270-3 0 9154
2 25544 51
6415 12
6468 0005550 111
0564 249
1182 15
53867687 9938
Satellite: ISS
Catalog Number: 25544
Epoch time: 18241
64239867 = yrday
fracday
Element set: 915
Inclination: 51
6415 deg
RA of node: 12
6468 deg
Eccentricity:
0005550
Arg of perigee: 111
0564 deg
Mean anomaly: 249
1182 deg
Mean motion: 15
53867687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 993
Checksum: 326
Coasting Arc #17 (Orbit 1008)
---------------------------------------
Vector Time (GMT): 2018/242/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6373799
92 A = 6788237
21 meter
Y = 898101
98 meter E =
0019529
Z = 2126620
99 I = 51
70593
XDOT = -2514
816909 Wp = 110
71207
YDOT = -4703
059568 meter/sec RA = 7
10111 deg
ZDOT = -5516
955032 TA = 45
72788
MA = 45
56780
Ha = 223
432 n
mi
Hp = 213
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20911417
05 X = -6393699
01
Y = 2946528
80 feet Y = 826714
64 meter
Z = 6977102
97 Z = 2095610
96
XDOT = -8250
711645 XDOT = -2435
240698
YDOT = -15429
985458 feet/sec YDOT = -4730
737494 meter/sec
ZDOT = -18100
246169 ZDOT = -5528
977457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17438072
38 X = 5315124
46
Y = -11991972
46 feet Y = -3655153
21 meter
Z = 6837805
87 Z = 2084163
23
XDOT = 13289
043150 XDOT = 4050
500352
YDOT = 8907
884652 feet/sec YDOT = 2715
123242 meter/sec
ZDOT = -18153
527179 ZDOT = -5533
195084
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 18242
67140574
00016717 00000-0 10270-3 0 9165
2 25544 51
6418 7
5194 0005612 112
9398 247
2347 15
53872406 10090
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
67140574 = yrday
fracday
Element set: 916
Inclination: 51
6418 deg
RA of node: 7
5194 deg
Eccentricity:
0005612
Arg of perigee: 112
9398 deg
Mean anomaly: 247
2347 deg
Mean motion: 15
53872406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1009
Checksum: 309
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