[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 16th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
257/13:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 214
1
257/20:59:14
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 214
3
261/11:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 214
6
270/15:15:09
148 -0
4 0
9 0
9
N/A -0
7 -0
1 221
3
000/00:00:18
297 0
3 -0
0 216
0
271/01:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 216
1
Coasting Arc #1 (Orbit 1240)
---------------------------------------
Vector Time (GMT): 2018/257/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4329473
71 A = 6778548
64 meter
Y = 441692
30 meter E =
0008280
Z = 5193550
72 I = 51
27000
XDOT = -2084
114790 Wp = 140
80137
YDOT = 7299
012988 meter/sec RA = 292
66687 deg
ZDOT = 1109
334565 TA = 298
47427
MA = 298
55764
Ha = 222
496 n
mi
Hp = 214
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14204310
09 X = 4298985
13
Y = 1449121
72 feet Y = 489937
41 meter
Z = 17039208
40 Z = 5214507
84
XDOT = -6837
646950 XDOT = -2170
968078
YDOT = 23946
893005 feet/sec YDOT = 7275
221432 meter/sec
ZDOT = 3639
549097 ZDOT = 1098
999069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14158947
25 X = -4315647
12
Y = 420658
33 feet Y = 128216
66 meter
Z = 17133133
43 Z = 5222179
07
XDOT = 3674
159634 XDOT = 1119
883857
YDOT = -23610
441737 feet/sec YDOT = -7196
462642 meter/sec
ZDOT = 3592
285229 ZDOT = 1094
928538
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 18257
59179460
00016717 00000-0 10270-3 0 9001
2 25544 51
6387 293
1683 0004796 155
2233 204
9150 15
53852726 12414
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
59179460 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 293
1683 deg
Eccentricity:
0004796
Arg of perigee: 155
2233 deg
Mean anomaly: 204
9150 deg
Mean motion: 15
53852726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1241
Checksum: 319
Coasting Arc #2 (Orbit 1240)
---------------------------------------
Vector Time (GMT): 2018/257/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3746807
63 A = 6778292
29 meter
Y = -2031967
06 meter E =
0017375
Z = -5285190
16 I = 51
26822
XDOT = 3209
269289 Wp = 107
12980
YDOT = -6939
479050 meter/sec RA = 292
48081 deg
ZDOT = 388
889370 TA = 166
62697
MA = 166
58086
Ha = 222
606 n
mi
Hp = 214
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12292675
96 X = -3698134
32
Y = -6666558
60 feet Y = -2073594
73 meter
Z = -17339862
73 Z = -5303272
58
XDOT = 10529
098718 XDOT = 3284
740919
YDOT = -22767
319719 feet/sec YDOT = -6903
168757 meter/sec
ZDOT = 1275
883760 ZDOT = 404
662832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13727422
48 X = 4184118
37
Y = 2073863
48 feet Y = 632113
59 meter
Z = -17420697
10 Z = -5309828
48
XDOT = -1898
670595 XDOT = -578
714797
YDOT = 23995
437006 feet/sec YDOT = 7313
809199 meter/sec
ZDOT = 1347
488213 ZDOT = 410
714407
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 18257
59179432
00016717 00000-0 10270-3 0 9011
2 25544 51
6386 293
1689 0004716 157
2593 202
8770 15
53827821 12415
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
59179432 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 293
1689 deg
Eccentricity:
0004716
Arg of perigee: 157
2593 deg
Mean anomaly: 202
8770 deg
Mean motion: 15
53827821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1241
Checksum: 330
Coasting Arc #3 (Orbit 1245)
---------------------------------------
Vector Time (GMT): 2018/257/20:59:14
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 500926
43 A = 6785747
58 meter
Y = 5934778
49 meter E =
0015302
Z = 3233675
86 I = 51
29082
XDOT = -5224
601944 Wp = 108
57431
YDOT = 3028
497841 meter/sec RA = 290
96820 deg
ZDOT = -4735
227041 TA = 33
72998
MA = 33
63270
Ha = 222
528 n
mi
Hp = 214
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1643459
41 X = 418817
27
Y = 19471058
02 feet Y = 5939921
33 meter
Z = 10609172
76 Z = 3235909
33
XDOT = -17141
082495 XDOT = -5235
077770
YDOT = 9936
016539 feet/sec YDOT = 2970
013796 meter/sec
ZDOT = -15535
521788 ZDOT = -4760
632161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14441279
71 X = -4401702
06
Y = 13155820
76 feet Y = 4009894
17 meter
Z = 10618447
46 Z = 3236502
78
XDOT = -17322
154302 XDOT = -5279
792631
YDOT = -6347
165129 feet/sec YDOT = -1934
615931 meter/sec
ZDOT = -15649
826666 ZDOT = -4770
067168
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 18257
91336497
00016717 00000-0 10270-3 0 9024
2 25544 51
6400 291
5678 0004604 157
7321 202
4032 15
53831849 12469
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
91336497 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 291
5678 deg
Eccentricity:
0004604
Arg of perigee: 157
7321 deg
Mean anomaly: 202
4032 deg
Mean motion: 15
53831849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1246
Checksum: 307
Coasting Arc #4 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2018/258/20:59:14
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 339985
33 A = 6788660
44 meter
Y = -6528146
41 meter E =
0006034
Z = -1833033
81 I = 51
29142
XDOT = 5051
216589 Wp = 76
38724
YDOT = -1307
652282 meter/sec RA = 285
96763 deg
ZDOT = 5610
951180 TA = 263
37000
MA = 263
43868
Ha = 222
379 n
mi
Hp = 214
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1115437
44 X = 421863
56
Y = -21417803
18 feet Y = -6523886
76 meter
Z = -6013890
46 Z = -1831183
00
XDOT = 16572
232903 XDOT = 5038
208528
YDOT = -4290
197776 feet/sec YDOT = -1251
238464 meter/sec
ZDOT = 18408
632480 ZDOT = 5635
456840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17437737
66 X = 5315022
44
Y = -12490044
81 feet Y = -3806965
66 meter
Z = -6004786
26 Z = -1830258
85
XDOT = 12721
382176 XDOT = 3877
477287
YDOT = 8884
432878 feet/sec YDOT = 2707
975141 meter/sec
ZDOT = 18518
687277 ZDOT = 5644
495882
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 18258
87806760
00016717 00000-0 10270-3 0 9036
2 25544 51
6413 286
7600 0004466 162
8037 197
3268 15
53868139 12613
Satellite: ISS
Catalog Number: 25544
Epoch time: 18258
87806760 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 286
7600 deg
Eccentricity:
0004466
Arg of perigee: 162
8037 deg
Mean anomaly: 197
3268 deg
Mean motion: 15
53868139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1261
Checksum: 333
Coasting Arc #5 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2018/259/20:59:14
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1113621
46 A = 6790213
30 meter
Y = 6685377
55 meter E =
0016522
Z = 223826
22 I = 51
28780
XDOT = -4769
147110 Wp = 141
07271
YDOT = -586
549910 meter/sec RA = 280
97402 deg
ZDOT = -5980
774374 TA = 36
50293
MA = 36
39042
Ha = 222
398 n
mi
Hp = 214
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3653613
73 X = -1189383
68
Y = 21933653
38 feet Y = 6672500
66 meter
Z = 734338
00 Z = 218232
24
XDOT = -15646
808104 XDOT = -4733
182164
YDOT = -1924
376344 feet/sec YDOT = -639
681052 meter/sec
ZDOT = -19621
963168 ZDOT = -6003
853914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19215377
70 X = -5856847
12
Y = 11191097
71 feet Y = 3411046
58 meter
Z = 708440
51 Z = 215932
67
XDOT = -7610
161447 XDOT = -2319
577209
YDOT = -11769
017389 feet/sec YDOT = -3587
196500 meter/sec
ZDOT = -19725
392412 ZDOT = -6012
299607
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 18259
90708340
00016717 00000-0 10270-3 0 9047
2 25544 51
6411 281
6329 0004577 165
8229 194
3053 15
53819089 12778
Satellite: ISS
Catalog Number: 25544
Epoch time: 18259
90708340 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 281
6329 deg
Eccentricity:
0004577
Arg of perigee: 165
8229 deg
Mean anomaly: 194
3053 deg
Mean motion: 15
53819089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1277
Checksum: 329
Coasting Arc #6 (Orbit 1292)
---------------------------------------
Vector Time (GMT): 2018/260/20:59:14
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1773710
83 A = 6789314
74 meter
Y = -6404967
83 meter E =
0013015
Z = 1368011
98 I = 51
27932
XDOT = 4398
889294 Wp = 78
46156
YDOT = 2461
435787 meter/sec RA = 275
97987 deg
ZDOT = 5776
636294 TA = 296
51415
MA = 296
64755
Ha = 222
215 n
mi
Hp = 214
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5819261
26 X = 1838556
05
Y = -21013674
00 feet Y = -6384770
33 meter
Z = 4488228
28 Z = 1376785
89
XDOT = 14432
051490 XDOT = 4342
978038
YDOT = 8075
576729 feet/sec YDOT = 2510
314903 meter/sec
ZDOT = 18952
218813 ZDOT = 5797
868650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19710728
07 X = 6007829
92
Y = -9303968
35 feet Y = -2835849
55 meter
Z = 4528339
81 Z = 1380237
98
XDOT = 2518
921829 XDOT = 767
767373
YDOT = 14676
909631 feet/sec YDOT = 4473
522056 meter/sec
ZDOT = 19047
145085 ZDOT = 5805
569822
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 18260
93609583
00016717 00000-0 10270-3 0 9052
2 25544 51
6404 276
5053 0004319 170
3496 189
7740 15
53856495 12939
Satellite: ISS
Catalog Number: 25544
Epoch time: 18260
93609583 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 276
5053 deg
Eccentricity:
0004319
Arg of perigee: 170
3496 deg
Mean anomaly: 189
7740 deg
Mean motion: 15
53856495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1293
Checksum: 335
Coasting Arc #7 (Orbit 1301)
---------------------------------------
Vector Time (GMT): 2018/261/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1118212
66 A = 6788717
17 meter
Y = 6438833
98 meter E =
0017045
Z = 1801688
87 I = 51
27394
XDOT = -4639
521604 Wp = 126
99198
YDOT = 2387
619298 meter/sec RA = 272
92005 deg
ZDOT = -5626
483561 TA = 33
09016
MA = 32
98364
Ha = 222
269 n
mi
Hp = 214
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3668676
70 X = 1037377
08
Y = 21124783
40 feet Y = 6450886
73 meter
Z = 5911052
71 Z = 1806924
06
XDOT = -15221
527571 XDOT = -4638
545344
YDOT = 7833
396646 feet/sec YDOT = 2335
742103 meter/sec
ZDOT = -18459
591737 ZDOT = -5649
018482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 483456
22 X = 147357
46
Y = -21429251
43 feet Y = -6531635
84 meter
Z = 5933772
82 Z = 1808613
96
XDOT = 14756
266327 XDOT = 4497
709976
YDOT = -4830
905862 feet/sec YDOT = -1472
460107 meter/sec
ZDOT = -18560
936596 ZDOT = -5657
373474
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 18261
51491501
00016717 00000-0 10270-3 0 9067
2 25544 51
6388 273
6197 0004620 169
0366 191
0888 15
53863611 13021
Satellite: ISS
Catalog Number: 25544
Epoch time: 18261
51491501 = yrday
fracday
Element set: 906
Inclination: 51
6388 deg
RA of node: 273
6197 deg
Eccentricity:
0004620
Arg of perigee: 169
0366 deg
Mean anomaly: 191
0888 deg
Mean motion: 15
53863611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1302
Checksum: 312
Coasting Arc #8 (Orbit 1316)
---------------------------------------
Vector Time (GMT): 2018/262/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -427333
56 A = 6789994
84 meter
Y = -6770338
19 meter E =
0009358
Z = -226907
52 I = 51
27884
XDOT = 4775
399917 Wp = 65
50009
YDOT = -494
992055 meter/sec RA = 267
92508 deg
ZDOT = 5974
612436 TA = 292
04417
MA = 292
14354
Ha = 222
156 n
mi
Hp = 214
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1402012
99 X = -350491
80
Y = -22212395
64 feet Y = -6774687
30 meter
Z = -744447
24 Z = -228796
30
XDOT = 15667
322562 XDOT = 4751
558706
YDOT = -1623
989683 feet/sec YDOT = -441
723163 meter/sec
ZDOT = 19601
746838 ZDOT = 5997
751726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2502580
67 X = -762786
59
Y = 22115192
54 feet Y = 6740710
69 meter
Z = -752137
73 Z = -229251
58
XDOT = -13968
659657 XDOT = -4257
647463
YDOT = -932
478444 feet/sec YDOT = -284
219430 meter/sec
ZDOT = 19705
582288 ZDOT = 6006
261481
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 18262
47961105
00016717 00000-0 10270-3 0 9076
2 25544 51
6397 268
8130 0004573 173
9289 186
1920 15
53890048 13171
Satellite: ISS
Catalog Number: 25544
Epoch time: 18262
47961105 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 268
8130 deg
Eccentricity:
0004573
Arg of perigee: 173
9289 deg
Mean anomaly: 186
1920 deg
Mean motion: 15
53890048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1317
Checksum: 331
Coasting Arc #9 (Orbit 1332)
---------------------------------------
Vector Time (GMT): 2018/263/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -314816
95 A = 6789283
54 meter
Y = 6627897
28 meter E =
0012562
Z = -1406921
01 I = 51
27643
XDOT = -4841
157176 Wp = 153
95878
YDOT = -1448
133304 meter/sec RA = 262
93079 deg
ZDOT = -5769
497517 TA = 41
45968
MA = 41
36444
Ha = 222
116 n
mi
Hp = 214
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1032864
01 X = -382074
49
Y = 21745069
82 feet Y = 6624000
62 meter
Z = -4615882
56 Z = -1408614
10
XDOT = -15883
061600 XDOT = -4796
578881
YDOT = -4751
093516 feet/sec YDOT = -1502
021644 meter/sec
ZDOT = -18928
797629 ZDOT = -5792
905703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4417267
45 X = 1346383
12
Y = -21314913
86 feet Y = -6496785
74 meter
Z = -4624222
83 Z = -1409463
12
XDOT = 13256
439316 XDOT = 4040
562704
YDOT = 6854
715243 feet/sec YDOT = 2089
317206 meter/sec
ZDOT = -19033
623528 ZDOT = -5801
448451
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 18263
50861887
00016717 00000-0 10270-3 0 9088
2 25544 51
6378 263
6851 0004513 176
2802 183
8385 15
53854175 13332
Satellite: ISS
Catalog Number: 25544
Epoch time: 18263
50861887 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 263
6851 deg
Eccentricity:
0004513
Arg of perigee: 176
2802 deg
Mean anomaly: 183
8385 deg
Mean motion: 15
53854175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1333
Checksum: 334
Coasting Arc #10 (Orbit 1348)
---------------------------------------
Vector Time (GMT): 2018/264/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1060793
55 A = 6786536
84 meter
Y = -6053098
39 meter E =
0013172
Z = 2871539
30 I = 51
27156
XDOT = 4808
770924 Wp = 100
61734
YDOT = 3234
832314 meter/sec RA = 257
93208 deg
ZDOT = 5020
397679 TA = 292
24711
MA = 292
38676
Ha = 221
944 n
mi
Hp = 214
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3480293
79 X = 1114453
77
Y = -19859246
69 feet Y = -6040935
58 meter
Z = 9421060
68 Z = 2876823
10
XDOT = 15776
807492 XDOT = 4747
854391
YDOT = 10612
966908 feet/sec YDOT = 3288
267159 meter/sec
ZDOT = 16471
120994 ZDOT = 5043
608681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6176162
08 X = -1882494
20
Y = 19180653
53 feet Y = 5846263
20 meter
Z = 9445425
37 Z = 2878965
65
XDOT = -12620
030265 XDOT = -3846
585225
YDOT = -12261
431404 feet/sec YDOT = -3737
284292 meter/sec
ZDOT = 16574
874773 ZDOT = 5052
021831
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 18264
53762390
00016717 00000-0 10270-3 0 9092
2 25544 51
6367 258
5577 0004462 182
8076 177
3052 15
53881888 13494
Satellite: ISS
Catalog Number: 25544
Epoch time: 18264
53762390 = yrday
fracday
Element set: 909
Inclination: 51
6367 deg
RA of node: 258
5577 deg
Eccentricity:
0004462
Arg of perigee: 182
8076 deg
Mean anomaly: 177
3052 deg
Mean motion: 15
53881888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1349
Checksum: 350
Coasting Arc #11 (Orbit 1363)
---------------------------------------
Vector Time (GMT): 2018/265/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1882810
61 A = 6782943
66 meter
Y = 5068846
00 meter E =
0006995
Z = -4099602
83 I = 51
26750
XDOT = -4643
140120 Wp = 106
08350
YDOT = -4779
223911 meter/sec RA = 252
92404 deg
ZDOT = -3784
005362 TA = 124
67506
MA = 124
60913
Ha = 221
878 n
mi
Hp = 214
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6177200
16 X = -1919438
27
Y = 16630072
18 feet Y = 5047585
88 meter
Z = -13450140
53 Z = -4108838
33
XDOT = -15233
399345 XDOT = -4570
971776
YDOT = -15679
868474 feet/sec YDOT = -4830
743600 meter/sec
ZDOT = -12414
715755 ZDOT = -3806
384274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8095846
32 X = 2467613
96
Y = -15749401
05 feet Y = -4800417
44 meter
Z = -13492109
61 Z = -4112395
01
XDOT = 11948
273878 XDOT = 3641
833878
YDOT = 16842
383877 feet/sec YDOT = 5133
558606 meter/sec
ZDOT = -12514
585035 ZDOT = -3814
445519
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 18265
50231549
00016717 00000-0 10270-3 0 9109
2 25544 51
6368 253
7496 0004367 184
4340 175
6775 15
53860339 13646
Satellite: ISS
Catalog Number: 25544
Epoch time: 18265
50231549 = yrday
fracday
Element set: 910
Inclination: 51
6368 deg
RA of node: 253
7496 deg
Eccentricity:
0004367
Arg of perigee: 184
4340 deg
Mean anomaly: 175
6775 deg
Mean motion: 15
53860339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1364
Checksum: 329
Coasting Arc #12 (Orbit 1379)
---------------------------------------
Vector Time (GMT): 2018/266/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2707809
36 A = 6779785
11 meter
Y = -3805868
33 meter E =
0009023
Z = 4912592
93 I = 51
26714
XDOT = 4321
806689 Wp = 147
88028
YDOT = 5937
707201 meter/sec RA = 247
90836 deg
ZDOT = 2208
482500 TA = 280
40440
MA = 280
50608
Ha = 221
708 n
mi
Hp = 215
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8883888
97 X = 2726303
61
Y = -12486444
65 feet Y = -3775483
74 meter
Z = 16117430
87 Z = 4925791
89
XDOT = 14179
155803 XDOT = 4244
360754
YDOT = 19480
666670 feet/sec YDOT = 5985
603876 meter/sec
ZDOT = 7245
677492 ZDOT = 2229
287518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10056102
57 X = -3065100
06
Y = 11479751
33 feet Y = 3499028
20 meter
Z = 16177035
32 Z = 4930760
37
XDOT = -11138
814891 XDOT = -3395
110779
YDOT = -20141
799426 feet/sec YDOT = -6139
220465 meter/sec
ZDOT = 7338
382293 ZDOT = 2236
738923
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 18266
53131633
00016717 00000-0 10270-3 0 9117
2 25544 51
6362 248
6218 0004236 189
5939 170
5133 15
53863579 13809
Satellite: ISS
Catalog Number: 25544
Epoch time: 18266
53131633 = yrday
fracday
Element set: 911
Inclination: 51
6362 deg
RA of node: 248
6218 deg
Eccentricity:
0004236
Arg of perigee: 189
5939 deg
Mean anomaly: 170
5133 deg
Mean motion: 15
53863579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1380
Checksum: 320
Coasting Arc #13 (Orbit 1394)
---------------------------------------
Vector Time (GMT): 2018/267/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3562036
45 A = 6778196
73 meter
Y = 2338497
88 meter E =
0014197
Z = -5283159
02 I = 51
27518
XDOT = -3771
788338 Wp = 103
61787
YDOT = -6652
534243 meter/sec RA = 242
88671 deg
ZDOT = -405
798093 TA = 162
51203
MA = 162
46309
Ha = 221
669 n
mi
Hp = 215
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11686471
30 X = -3562258
57
Y = 7672237
14 feet Y = 2298662
80 meter
Z = -17333198
89 Z = -5300463
04
XDOT = -12374
633656 XDOT = -3695
146366
YDOT = -21825
899747 feet/sec YDOT = -6694
284517 meter/sec
ZDOT = -1331
358572 ZDOT = -423
933190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12210185
22 X = 3721664
45
Y = -6606279
18 feet Y = -2013593
89 meter
Z = -17411061
72 Z = -5306891
61
XDOT = 9883
862660 XDOT = 3012
601339
YDOT = 21953
315841 feet/sec YDOT = 6691
370668 meter/sec
ZDOT = -1412
031348 ZDOT = -430
387155
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 18267
49600302
00016717 00000-0 10270-3 0 9128
2 25544 51
6361 243
8145 0004254 192
8362 167
2683 15
53861264 13959
Satellite: ISS
Catalog Number: 25544
Epoch time: 18267
49600302 = yrday
fracday
Element set: 912
Inclination: 51
6361 deg
RA of node: 243
8145 deg
Eccentricity:
0004254
Arg of perigee: 192
8362 deg
Mean anomaly: 167
2683 deg
Mean motion: 15
53861264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1395
Checksum: 311
Coasting Arc #14 (Orbit 1410)
---------------------------------------
Vector Time (GMT): 2018/268/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4343669
75 A = 6778723
90 meter
Y = -822911
86 meter E =
0002777
Z = 5136364
70 I = 51
29376
XDOT = 2995
075198 Wp = 122
21153
YDOT = 6915
891759 meter/sec RA = 237
86485 deg
ZDOT = -1425
718730 TA = 341
56333
MA = 341
57339
Ha = 221
396 n
mi
Hp = 215
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14250884
99 X = 4327599
01
Y = -2699842
07 feet Y = -774427
13 meter
Z = 16851590
21 Z = 5157425
96
XDOT = 9826
362199 XDOT = 2924
442615
YDOT = 22689
933594 feet/sec YDOT = 6948
989654 meter/sec
ZDOT = -4677
554887 ZDOT = -1411
342035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14296506
59 X = -4357575
21
Y = 1670533
66 feet Y = 509178
66 meter
Z = 16946155
30 Z = 5165188
14
XDOT = -8071
107403 XDOT = -2460
073536
YDOT = -22299
703279 feet/sec YDOT = -6796
949559 meter/sec
ZDOT = -4613
751711 ZDOT = -1406
271522
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 18268
52499979
00016717 00000-0 10270-3 0 9130
2 25544 51
6366 238
6864 0004248 198
2495 161
8506 15
53879985 14116
Satellite: ISS
Catalog Number: 25544
Epoch time: 18268
52499979 = yrday
fracday
Element set: 913
Inclination: 51
6366 deg
RA of node: 238
6864 deg
Eccentricity:
0004248
Arg of perigee: 198
2495 deg
Mean anomaly: 161
8506 deg
Mean motion: 15
53879985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1411
Checksum: 370
Coasting Arc #15 (Orbit 1425)
---------------------------------------
Vector Time (GMT): 2018/269/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5026180
61 A = 6781333
39 meter
Y = -646173
04 meter E =
0010585
Z = -4516832
83 I = 51
32183
XDOT = -1948
215663 Wp = 133
36539
YDOT = -6714
894233 meter/sec RA = 232
84860 deg
ZDOT = 3126
034161 TA = 168
16973
MA = 168
14484
Ha = 221
448 n
mi
Hp = 215
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16490093
85 X = -4996640
72
Y = -2119990
29 feet Y = -702214
67 meter
Z = -14819005
36 Z = -4541176
73
XDOT = -6391
783670 XDOT = -1888
167855
YDOT = -22030
492890 feet/sec YDOT = -6736
344400 meter/sec
ZDOT = 10256
017587 ZDOT = 3116
716971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16249588
09 X = 4952874
45
Y = 3020183
67 feet Y = 920551
98 meter
Z = -14928156
34 Z = -4550102
05
XDOT = 5457
525871 XDOT = 1663
453886
YDOT = 21167
029083 feet/sec YDOT = 6451
710464 meter/sec
ZDOT = 10214
878206 ZDOT = 3113
494877
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 18269
48968136
00016717 00000-0 10270-3 0 9143
2 25544 51
6375 233
8792 0004103 201
5484 158
5496 15
53866619 14266
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
48968136 = yrday
fracday
Element set: 914
Inclination: 51
6375 deg
RA of node: 233
8792 deg
Eccentricity:
0004103
Arg of perigee: 201
5484 deg
Mean anomaly: 158
5496 deg
Mean motion: 15
53866619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1426
Checksum: 343
Coasting Arc #16 (Orbit 1441)
---------------------------------------
Vector Time (GMT): 2018/270/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5495627
34 A = 6784853
32 meter
Y = 1958136
64 meter E =
0010953
Z = 3451349
19 I = 51
35442
XDOT = 667
156556 Wp = 108
06516
YDOT = 6147
270498 meter/sec RA = 227
84245 deg
ZDOT = -4541
446549 TA = 31
24868
MA = 31
18361
Ha = 221
143 n
mi
Hp = 215
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18030273
42 X = 5456557
37
Y = 6424332
80 feet Y = 2019374
49 meter
Z = 11323324
12 Z = 3477950
33
XDOT = 2188
833845 XDOT = 620
426773
YDOT = 20168
210296 feet/sec YDOT = 6154
469319 meter/sec
ZDOT = -14899
759019 ZDOT = -4538
319869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17698417
21 X = -5394477
57
Y = -7100428
98 feet Y = -2164210
75 meter
Z = 11442482
99 Z = 3487668
82
XDOT = -2040
310766 XDOT = -621
886722
YDOT = -18948
720522 feet/sec YDOT = -5775
570015 meter/sec
ZDOT = -14886
327439 ZDOT = -4537
352604
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 18270
51867306
00016717 00000-0 10270-3 0 9157
2 25544 51
6372 228
7515 0004061 206
6457 153
4488 15
53892791 14421
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
51867306 = yrday
fracday
Element set: 915
Inclination: 51
6372 deg
RA of node: 228
7515 deg
Eccentricity:
0004061
Arg of perigee: 206
6457 deg
Mean anomaly: 153
4488 deg
Mean motion: 15
53892791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1442
Checksum: 322
Coasting Arc #17 (Orbit 1443)
---------------------------------------
Vector Time (GMT): 2018/270/15:15:18
297
Vector Time (MET): N/A
Weight (LBS) : 943647
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4773114
00 A = 6780615
80 meter
Y = 505631
01 meter E =
0010966
Z = -4799615
58 I = 51
34528
XDOT = -3238
544059 Wp = 129
22074
YDOT = -6460
257775 meter/sec RA = 227
06596 deg
ZDOT = 2537
187614 TA = 165
89464
MA = 165
86400
Ha = 221
261 n
mi
Hp = 215
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15659822
82 X = -4755098
99
Y = 1658894
38 feet Y = 452354
94 meter
Z = -15746770
27 Z = -4822758
37
XDOT = -10625
144552 XDOT = -3178
387479
YDOT = -21195
071440 feet/sec YDOT = -6496
136790 meter/sec
ZDOT = 8324
106345 ZDOT = 2521
602462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7728173
13 X = 2355547
17
Y = -13600547
43 feet Y = -4145446
86 meter
Z = -15850653
14 Z = -4831279
08
XDOT = 22452
950931 XDOT = 6843
659444
YDOT = 3126
822972 feet/sec YDOT = 953
055642 meter/sec
ZDOT = 8254
806958 ZDOT = 2516
065161
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 18270
64729731
00016717 00000-0 10270-3 0 9161
2 25544 51
6404 228
1111 0004148 216
7943 143
2925 15
53730034 14447
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
64729731 = yrday
fracday
Element set: 916
Inclination: 51
6404 deg
RA of node: 228
1111 deg
Eccentricity:
0004148
Arg of perigee: 216
7943 deg
Mean anomaly: 143
2925 deg
Mean motion: 15
53730034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1444
Checksum: 292
Coasting Arc #18 (Orbit 1450)
---------------------------------------
Vector Time (GMT): 2018/271/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943647
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -55509
72 A = 6781983
08 meter
Y = -5106224
93 meter E =
0009216
Z = 4462001
57 I = 51
35868
XDOT = 6388
241349 Wp = 141
20343
YDOT = 2755
552595 meter/sec RA = 225
06518 deg
ZDOT = 3222
196850 TA = 276
19266
MA = 276
29764
Ha = 221
348 n
mi
Hp = 216
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -182118
49 X = -20080
78
Y = -16752706
46 feet Y = -5106647
13 meter
Z = 14639112
76 Z = 4461818
49
XDOT = 20958
797078 XDOT = 6341
301210
YDOT = 9040
526888 feet/sec YDOT = 2826
728213 meter/sec
ZDOT = 10571
511976 ZDOT = 3253
114932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6402469
20 X = -1951472
61
Y = -15482388
54 feet Y = -4719032
03 meter
Z = 14638783
98 Z = 4461901
36
XDOT = 21619
407110 XDOT = 6589
595287
YDOT = 1219
195804 feet/sec YDOT = 371
610881 meter/sec
ZDOT = 10709
969470 ZDOT = 3264
398694
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 18271
09752655
00016717 00000-0 10270-3 0 9173
2 25544 51
6399 225
8637 0004721 215
1135 144
9707 15
53752954 14519
Satellite: ISS
Catalog Number: 25544
Epoch time: 18271
09752655 = yrday
fracday
Element set: 917
Inclination: 51
6399 deg
RA of node: 225
8637 deg
Eccentricity:
0004721
Arg of perigee: 215
1135 deg
Mean anomaly: 144
9707 deg
Mean motion: 15
53752954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1451
Checksum: 326
Coasting Arc #19 (Orbit 1465)
---------------------------------------
Vector Time (GMT): 2018/272/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943647
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1259375
26 A = 6779377
27 meter
Y = 4279324
22 meter E =
0010291
Z = -5113743
14 I = 51
37486
XDOT = -6467
972618 Wp = 94
46671
YDOT = -3788
049834 meter/sec RA = 220
05580 deg
ZDOT = -1580
601971 TA = 160
23932
MA = 160
19942
Ha = 221
203 n
mi
Hp = 216
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4131808
59 X = -1282293
93
Y = 14039777
63 feet Y = 4265112
44 meter
Z = -16777372
51 Z = -5119916
88
XDOT = -21220
382604 XDOT = -6417
455006
YDOT = -12427
985019 feet/sec YDOT = -3860
096860 meter/sec
ZDOT = -5185
702004 ZDOT = -1611
898690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1657312
22 X = 505148
76
Y = 14508495
02 feet Y = 4422189
28 meter
Z = -16805484
66 Z = -5122311
73
XDOT = -23270
746032 XDOT = -7092
923391
YDOT = -3497
293863 feet/sec YDOT = -1065
975169 meter/sec
ZDOT = -5325
774969 ZDOT = -1623
296210
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 18272
06230445
00016717 00000-0 10270-3 0 9180
2 25544 51
6408 221
0580 0004647 219
2362 140
8454 15
53732422 14667
Satellite: ISS
Catalog Number: 25544
Epoch time: 18272
06230445 = yrday
fracday
Element set: 918
Inclination: 51
6408 deg
RA of node: 221
0580 deg
Eccentricity:
0004647
Arg of perigee: 219
2362 deg
Mean anomaly: 140
8454 deg
Mean motion: 15
53732422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1466
Checksum: 291
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