[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 14th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 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
172/07:16:38
985 1
2 1
3 1
3
N/A 0
2 -0
1 220
4
000/00:03:17
970 0
5 -0
0 216
0
Coasting Arc #1 (Orbit 3793)
---------------------------------------
Vector Time (GMT): 2018/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5918194
51 A = 6788483
41 meter
Y = -2988580
17 meter E =
0015385
Z = 1417862
61 I = 51
88766
XDOT = 1066
062922 Wp = 129
85683
YDOT = -4886
602762 meter/sec RA = 36
45050 deg
ZDOT = -5818
124597 TA = 34
72901
MA = 34
62867
Ha = 221
246 n
mi
Hp = 214
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19416648
64 X = -5891222
82
Y = -9805053
05 feet Y = -3054610
94 meter
Z = 4651780
23 Z = 1389178
82
XDOT = 3497
581766 XDOT = 1148
888632
YDOT = -16032
161294 feet/sec YDOT = -4874
217183 meter/sec
ZDOT = -19088
335291 ZDOT = -5812
745676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12764531
79 X = -3890629
29
Y = 17646118
44 feet Y = 5378536
90 meter
Z = 4523892
27 Z = 1378882
36
XDOT = -13969
359468 XDOT = -4257
860766
YDOT = -5189
875981 feet/sec YDOT = -1581
874199 meter/sec
ZDOT = -19063
458318 ZDOT = -5810
542095
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18164
53487101
00016717 00000-0 10270-3 0 9006
2 25544 51
6418 36
9276 0003101 185
1082 175
0039 15
54143578 37941
Satellite: ISS
Catalog Number: 25544
Epoch time: 18164
53487101 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 36
9276 deg
Eccentricity:
0003101
Arg of perigee: 185
1082 deg
Mean anomaly: 175
0039 deg
Mean motion: 15
54143578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3794
Checksum: 301
Coasting Arc #2 (Orbit 3809)
---------------------------------------
Vector Time (GMT): 2018/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5657964
67 A = 6789075
62 meter
Y = 3733616
08 meter E =
0010364
Z = 290002
66 I = 51
86315
XDOT = -2830
551370 Wp = 58
00998
YDOT = 3809
959424 meter/sec RA = 31
49543 deg
ZDOT = 6021
159803 TA = 305
10509
MA = 305
20221
Ha = 220
962 n
mi
Hp = 214
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18562876
22 X = 5614385
16
Y = 12249396
60 feet Y = 3796643
62 meter
Z = 951452
28 Z = 317382
01
XDOT = -9286
585859 XDOT = -2902
192695
YDOT = 12499
866875 feet/sec YDOT = 3777
904562 meter/sec
ZDOT = 19754
461295 ZDOT = 6007
236629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14753156
85 X = 4496762
21
Y = -16635070
80 feet Y = -5070369
58 meter
Z = 1073375
19 Z = 327164
76
XDOT = 9829
273139 XDOT = 2995
962453
YDOT = 10016
409474 feet/sec YDOT = 3053
001608 meter/sec
ZDOT = 19691
514163 ZDOT = 6001
973517
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18165
56367189
00016717 00000-0 10270-3 0 9014
2 25544 51
6418 31
7982 0003038 193
5291 166
5781 15
54200069 38109
Satellite: ISS
Catalog Number: 25544
Epoch time: 18165
56367189 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 31
7982 deg
Eccentricity:
0003038
Arg of perigee: 193
5291 deg
Mean anomaly: 166
5781 deg
Mean motion: 15
54200069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3810
Checksum: 317
Coasting Arc #3 (Orbit 3824)
---------------------------------------
Vector Time (GMT): 2018/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4923317
43 A = 6787500
44 meter
Y = -4216081
33 meter E =
0008609
Z = -2000005
36 I = 51
82834
XDOT = 4532
066772 Wp = 156
65426
YDOT = -2648
289273 meter/sec RA = 26
53731 deg
ZDOT = -5589
610523 TA = 45
37221
MA = 45
30203
Ha = 220
887 n
mi
Hp = 214
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16152616
24 X = -4866091
21
Y = -13832287
83 feet Y = -4270816
92 meter
Z = -6561697
37 Z = -2023782
82
XDOT = 14868
985473 XDOT = 4588
495116
YDOT = -8688
613101 feet/sec YDOT = -2597
292054 meter/sec
ZDOT = -18338
617200 ZDOT = -5567
458814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15731093
02 X = -4794837
15
Y = 14260902
54 feet Y = 4346723
09 meter
Z = -6667416
41 Z = -2032228
52
XDOT = -5715
899663 XDOT = -1742
206217
YDOT = -14808
440722 feet/sec YDOT = -4513
612732 meter/sec
ZDOT = -18239
031506 ZDOT = -5559
256803
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 18166
52817336
00016717 00000-0 10270-3 0 9026
2 25544 51
6413 26
9893 0003030 198
4939 161
6104 15
54154213 38256
Satellite: ISS
Catalog Number: 25544
Epoch time: 18166
52817336 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 26
9893 deg
Eccentricity:
0003030
Arg of perigee: 198
4939 deg
Mean anomaly: 161
6104 deg
Mean motion: 15
54154213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3825
Checksum: 306
Coasting Arc #4 (Orbit 3840)
---------------------------------------
Vector Time (GMT): 2018/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3785649
04 A = 6784046
14 meter
Y = 4430832
31 meter E =
0011581
Z = 3465936
43 I = 51
78577
XDOT = -5968
937458 Wp = 104
38412
YDOT = 1511
166422 meter/sec RA = 21
56970 deg
ZDOT = 4572
088892 TA = 296
20068
MA = 296
31971
Ha = 220
789 n
mi
Hp = 214
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12420108
41 X = 3718985
36
Y = 14536851
40 feet Y = 4472792
73 meter
Z = 11371182
53 Z = 3484164
48
XDOT = -19583
128142 XDOT = -6007
600725
YDOT = 4957
895084 feet/sec YDOT = 1444
200712 meter/sec
ZDOT = 15000
291642 ZDOT = 4543
000441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15779899
82 X = 4809713
46
Y = -10711152
47 feet Y = -3264759
27 meter
Z = 11452026
39 Z = 3490577
64
XDOT = 2034
719176 XDOT = 620
182405
YDOT = 18950
239489 feet/sec YDOT = 5776
032996 meter/sec
ZDOT = 14869
849023 ZDOT = 4532
329982
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 18167
55697253
00016717 00000-0 10270-3 0 9035
2 25544 51
6401 21
8597 0002860 201
7356 158
3675 15
54169049 38416
Satellite: ISS
Catalog Number: 25544
Epoch time: 18167
55697253 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 21
8597 deg
Eccentricity:
0002860
Arg of perigee: 201
7356 deg
Mean anomaly: 158
3675 deg
Mean motion: 15
54169049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3841
Checksum: 325
Coasting Arc #5 (Orbit 3855)
---------------------------------------
Vector Time (GMT): 2018/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2267548
98 A = 6780183
49 meter
Y = -4452678
27 meter E =
0008261
Z = -4590427
63 I = 51
74145
XDOT = 7013
004213 Wp = 83
75737
YDOT = -425
080350 meter/sec RA = 16
58966 deg
ZDOT = -3055
760252 TA = 155
73603
MA = 155
69711
Ha = 220
694 n
mi
Hp = 214
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7439465
17 X = -2195291
74
Y = -14608524
51 feet Y = -4477630
89 meter
Z = -15060458
10 Z = -4601267
62
XDOT = 23008
544005 XDOT = 7032
079475
YDOT = -1394
620572 feet/sec YDOT = -346
549012 meter/sec
ZDOT = -10025
460144 ZDOT = -3021
647589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15212938
26 X = -4636903
58
Y = 5989982
58 feet Y = 1825746
69 meter
Z = -15108231
09 Z = -4604988
84
XDOT = 1131
178581 XDOT = 344
783232
YDOT = -21996
827926 feet/sec YDOT = -6704
633152 meter/sec
ZDOT = -9872
716047 ZDOT = -3009
203851
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 18168
52146935
00016717 00000-0 10270-3 0 9040
2 25544 51
6396 17
0508 0002980 207
1276 152
9721 15
54185023 38560
Satellite: ISS
Catalog Number: 25544
Epoch time: 18168
52146935 = yrday
fracday
Element set: 904
Inclination: 51
6396 deg
RA of node: 17
0508 deg
Eccentricity:
0002980
Arg of perigee: 207
1276 deg
Mean anomaly: 152
9721 deg
Mean motion: 15
54185023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 314
Coasting Arc #6 (Orbit 3871)
---------------------------------------
Vector Time (GMT): 2018/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 535911
78 A = 6777723
03 meter
Y = 4306432
64 meter E =
0005143
Z = 5205410
17 I = 51
70154
XDOT = -7549
434133 Wp = 157
61255
YDOT = -556
058240 meter/sec RA = 11
59822 deg
ZDOT = 1232
214025 TA = 280
54530
MA = 280
60324
Ha = 220
691 n
mi
Hp = 215
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1758240
75 X = 462431
36
Y = 14128716
01 feet Y = 4312014
10 meter
Z = 17078117
34 Z = 5207835
46
XDOT = -24768
484688 XDOT = -7548
640435
YDOT = -1824
338057 feet/sec YDOT = -640
476924 meter/sec
ZDOT = 4042
696933 ZDOT = 1195
543722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14212585
97 X = 4331996
20
Y = -606674
43 feet Y = -184914
37 meter
Z = 17088255
17 Z = 5208500
18
XDOT = -3677
755723 XDOT = -1120
979945
YDOT = 23558
374997 feet/sec YDOT = 7180
592699 meter/sec
ZDOT = 3878
677005 ZDOT = 1182
220751
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 18169
55026518
00016717 00000-0 10270-3 0 9059
2 25544 51
6401 11
9211 0002899 208
9189 151
1804 15
54159142 38726
Satellite: ISS
Catalog Number: 25544
Epoch time: 18169
55026518 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 11
9211 deg
Eccentricity:
0002899
Arg of perigee: 208
9189 deg
Mean anomaly: 151
1804 deg
Mean motion: 15
54159142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3872
Checksum: 309
Coasting Arc #7 (Orbit 3886)
---------------------------------------
Vector Time (GMT): 2018/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1303233
58 A = 6777364
66 meter
Y = -4054820
12 meter E =
0013563
Z = -5283515
23 I = 51
66618
XDOT = 7484
769085 Wp = 106
84932
YDOT = 1448
726745 meter/sec RA = 6
59981 deg
ZDOT = 732
091490 TA = 170
16347
MA = 170
13690
Ha = 220
612 n
mi
Hp = 215
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4275700
71 X = 1374143
15
Y = -13303215
60 feet Y = -4039849
45 meter
Z = -17334367
54 Z = -5277012
80
XDOT = 24556
329018 XDOT = 7464
456658
YDOT = 4753
040503 feet/sec YDOT = 1532
312946 meter/sec
ZDOT = 2401
874967 ZDOT = 768
400428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13037808
18 X = -3973923
93
Y = -5128740
48 feet Y = -1563240
10 meter
Z = -17304595
88 Z = -5274440
83
XDOT = 5746
269638 XDOT = 1751
462986
YDOT = -23284
394619 feet/sec YDOT = -7097
083480 meter/sec
ZDOT = 2564
119314 ZDOT = 781
543567
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 18170
51475767
00016717 00000-0 10270-3 0 9062
2 25544 51
6383 7
1117 0002936 211
4214 148
6763 15
54195720 38870
Satellite: ISS
Catalog Number: 25544
Epoch time: 18170
51475767 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 7
1117 deg
Eccentricity:
0002936
Arg of perigee: 211
4214 deg
Mean anomaly: 148
6763 deg
Mean motion: 15
54195720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3887
Checksum: 316
Coasting Arc #8 (Orbit 3902)
---------------------------------------
Vector Time (GMT): 2018/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3054990
68 A = 6779526
40 meter
Y = 3702245
28 meter E =
0004930
Z = 4784098
01 I = 51
64087
XDOT = -6846
097529 Wp = 75
95496
YDOT = -2263
400865 meter/sec RA = 1
60339 deg
ZDOT = -2616
727702 TA = 39
85123
MA = 39
81504
Ha = 220
573 n
mi
Hp = 215
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10022935
30 X = -3119401
67
Y = 12146474
00 feet Y = 3667721
68 meter
Z = 15695859
61 Z = 4769101
89
XDOT = -22460
949899 XDOT = -6807
568122
YDOT = -7425
855855 feet/sec YDOT = -2339
742977 meter/sec
ZDOT = -8585
064638 ZDOT = -2649
890146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11745371
16 X = 3579989
13
Y = 10590726
53 feet Y = 3228053
45 meter
Z = 15628142
55 Z = 4763457
85
XDOT = -7518
539449 XDOT = -2291
650824
YDOT = 21241
848556 feet/sec YDOT = 6474
515440 meter/sec
ZDOT = -8733
082579 ZDOT = -2661
843570
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 18171
54354918
00016717 00000-0 10270-3 0 9071
2 25544 51
6388 1
9831 0003065 217
9706 142
1231 15
54186117 39039
Satellite: ISS
Catalog Number: 25544
Epoch time: 18171
54354918 = yrday
fracday
Element set: 907
Inclination: 51
6388 deg
RA of node: 1
9831 deg
Eccentricity:
0003065
Arg of perigee: 217
9706 deg
Mean anomaly: 142
1231 deg
Mean motion: 15
54186117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3903
Checksum: 304
Coasting Arc #9 (Orbit 3914)
---------------------------------------
Vector Time (GMT): 2018/172/07:18:17
970
Vector Time (MET): N/A
Weight (LBS) : 922901
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3165577
71 A = 6780785
67 meter
Y = -3810275
17 meter E =
0008608
Z = -4638796
99 I = 51
62005
XDOT = 6771
834597 Wp = 127
08111
YDOT = 2045
707314 meter/sec RA = 357
59398 deg
ZDOT = 2939
557032 TA = 172
23358
MA = 172
22024
Ha = 220
409 n
mi
Hp = 216
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10385753
65 X = 3230482
77
Y = -12500902
77 feet Y = -3774512
16 meter
Z = -15219150
23 Z = -4623262
44
XDOT = 22217
305107 XDOT = 6734
176848
YDOT = 6711
638169 feet/sec YDOT = 2121
223812 meter/sec
ZDOT = 9644
215983 ZDOT = 2972
360926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6072105
18 X = 1850777
66
Y = -15145824
44 feet Y = -4616447
29 meter
Z = -15149010
64 Z = -4617418
44
XDOT = 22037
265069 XDOT = 6716
958393
YDOT = -962
068521 feet/sec YDOT = -293
238485 meter/sec
ZDOT = 9790
656715 ZDOT = 2984
192167
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 18172
31514257
00016717 00000-0 10270-3 0 9082
2 25544 51
6425 358
1388 0003320 238
1950 121
8880 15
53963198 39153
Satellite: ISS
Catalog Number: 25544
Epoch time: 18172
31514257 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 358
1388 deg
Eccentricity:
0003320
Arg of perigee: 238
1950 deg
Mean anomaly: 121
8880 deg
Mean motion: 15
53963198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3915
Checksum: 319
Coasting Arc #10 (Orbit 3930)
---------------------------------------
Vector Time (GMT): 2018/173/07:18:17
970
Vector Time (MET): N/A
Weight (LBS) : 922901
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4577535
10 A = 6784401
34 meter
Y = 3471424
35 meter E =
0009335
Z = 3599980
10 I = 51
59885
XDOT = -5608
132229 Wp = 95
10556
YDOT = -2803
664692 meter/sec RA = 352
60553 deg
ZDOT = -4418
386244 TA = 42
24095
MA = 42
16908
Ha = 220
464 n
mi
Hp = 215
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15018159
78 X = -4633500
14
Y = 11389187
49 feet Y = 3419921
92 meter
Z = 11810958
35 Z = 3577608
40
XDOT = -18399
383955 XDOT = -5554
901855
YDOT = -9198
374975 feet/sec YDOT = -2866
080629 meter/sec
ZDOT = -14496
017860 ZDOT = -4445
499636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10530273
37 X = -3209627
32
Y = 15707956
79 feet Y = 4787785
23 meter
Z = 11710289
85 Z = 3569296
35
XDOT = -19161
481279 XDOT = -5840
419494
YDOT = -1926
217027 feet/sec YDOT = -587
110950 meter/sec
ZDOT = -14616
862313 ZDOT = -4455
219633
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 18173
34408651
00016717 00000-0 10270-3 0 9097
2 25544 51
6422 353
0114 0003145 241
4673 118
6163 15
53964720 39313
Satellite: ISS
Catalog Number: 25544
Epoch time: 18173
34408651 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 353
0114 deg
Eccentricity:
0003145
Arg of perigee: 241
4673 deg
Mean anomaly: 118
6163 deg
Mean motion: 15
53964720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3931
Checksum: 294
Coasting Arc #11 (Orbit 3945)
---------------------------------------
Vector Time (GMT): 2018/174/07:18:17
970
Vector Time (MET): N/A
Weight (LBS) : 922901
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5640600
61 A = 6787730
42 meter
Y = -3045841
91 meter E =
0003438
Z = -2226435
40 I = 51
57726
XDOT = 4060
956983 Wp = 19
36343
YDOT = 3537
981431 meter/sec RA = 347
62358 deg
ZDOT = 5453
807067 TA = 315
87915
MA = 315
90657
Ha = 220
259 n
mi
Hp = 216
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18505907
50 X = 5685055
71
Y = -9992919
66 feet Y = -2982516
01 meter
Z = -7304578
08 Z = -2198927
59
XDOT = 13323
349681 XDOT = 3994
600681
YDOT = 11607
550627 feet/sec YDOT = 3583
022218 meter/sec
ZDOT = 17893
067806 ZDOT = 5473
373086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13985728
57 X = 4262850
07
Y = -15764403
91 feet Y = -4804990
31 meter
Z = -7181008
44 Z = -2188771
37
XDOT = 15241
783240 XDOT = 4645
695532
YDOT = 5340
306195 feet/sec YDOT = 1627
725328 meter/sec
ZDOT = 17980
017083 ZDOT = 5480
309207
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 18174
30871908
00016717 00000-0 10270-3 0 9105
2 25544 51
6419 348
2037 0003281 246
3917 113
6891 15
53978738 39468
Satellite: ISS
Catalog Number: 25544
Epoch time: 18174
30871908 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 348
2037 deg
Eccentricity:
0003281
Arg of perigee: 246
3917 deg
Mean anomaly: 113
6891 deg
Mean motion: 15
53978738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3946
Checksum: 337
Coasting Arc #12 (Orbit 3961)
---------------------------------------
Vector Time (GMT): 2018/175/07:18:17
970
Vector Time (MET): N/A
Weight (LBS) : 922901
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6284944
57 A = 6789759
10 meter
Y = 2475541
34 meter E =
0011806
Z = 615160
54 I = 51
55186
XDOT = -2264
841872 Wp = 142
63971
YDOT = -4254
856818 meter/sec RA = 342
64767 deg
ZDOT = -5965
918081 TA = 30
71037
MA = 30
64133
Ha = 220
269 n
mi
Hp = 216
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20619896
88 X = -6315147
78
Y = 8121854
80 feet Y = 2405089
80 meter
Z = 2018243
24 Z = 584557
30
XDOT = -7430
583568 XDOT = -2188
115180
YDOT = -13959
503996 feet/sec YDOT = -4279
754062 meter/sec
ZDOT = -19573
222050 ZDOT = -5976
734135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16325744
09 X = -4976086
80
Y = 15005004
91 feet Y = 4573525
50 meter
Z = 1880926
97 Z = 573306
54
XDOT = -10742
882698 XDOT = -3274
430646
YDOT = -9206
447223 feet/sec YDOT = -2806
125114 meter/sec
ZDOT = -19620
904483 ZDOT = -5980
451686
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 18175
33766063
00016717 00000-0 10270-3 0 9115
2 25544 51
6421 343
0762 0003325 248
0007 112
0792 15
53933372 39623
Satellite: ISS
Catalog Number: 25544
Epoch time: 18175
33766063 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 343
0762 deg
Eccentricity:
0003325
Arg of perigee: 248
0007 deg
Mean anomaly: 112
0792 deg
Mean motion: 15
53933372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3962
Checksum: 292
Coasting Arc #13 (Orbit 3977)
---------------------------------------
Vector Time (GMT): 2018/176/07:18:17
970
Vector Time (MET): N/A
Weight (LBS) : 922901
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6467245
91 A = 6789248
63 meter
Y = -1766762
36 meter E =
0010508
Z = 1035248
97 I = 51
51947
XDOT = 390
526781 Wp = 50
10190
YDOT = 4898
545087 meter/sec RA = 337
66995 deg
ZDOT = 5887
148438 TA = 321
13974
MA = 321
21525
Ha = 220
058 n
mi
Hp = 216
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21217998
38 X = 6481492
96
Y = -5796464
44 feet Y = -1694361
65 meter
Z = 3396486
11 Z = 1066699
04
XDOT = 1281
255843 XDOT = 307
124147
YDOT = 16071
342149 feet/sec YDOT = 4902
445030 meter/sec
ZDOT = 19314
791463 ZDOT = 5888
843634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17460647
75 X = 5322005
43
Y = -13339815
48 feet Y = -4065975
76 meter
Z = 3537467
49 Z = 1078220
09
XDOT = 6138
970508 XDOT = 1871
158211
YDOT = 13186
739255 feet/sec YDOT = 4019
318125 meter/sec
ZDOT = 19321
565256 ZDOT = 5889
213090
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 18176
36659608
00016717 00000-0 10270-3 0 9126
2 25544 51
6419 337
9471 0003368 256
5711 103
5067 15
53987445 39789
Satellite: ISS
Catalog Number: 25544
Epoch time: 18176
36659608 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 337
9471 deg
Eccentricity:
0003368
Arg of perigee: 256
5711 deg
Mean anomaly: 103
5067 deg
Mean motion: 15
53987445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3978
Checksum: 349
Coasting Arc #14 (Orbit 3992)
---------------------------------------
Vector Time (GMT): 2018/177/07:18:17
970
Vector Time (MET): N/A
Weight (LBS) : 922901
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6204285
84 A = 6786878
07 meter
Y = 870235
45 meter E =
0003626
Z = -2604962
18 I = 51
47997
XDOT = 1431
975961 Wp = 168
91490
YDOT = -5421
840482 meter/sec RA = 332
68759 deg
ZDOT = -5226
526749 TA = 40
47257
MA = 40
44560
Ha = 220
020 n
mi
Hp = 216
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20355268
50 X = -6200902
40
Y = 2855103
18 feet Y = 800874
18 meter
Z = -8546463
84 Z = -2635092
11
XDOT = 4698
083862 XDOT = 1517
885759
YDOT = -17788
190558 feet/sec YDOT = -5405
345953 meter/sec
ZDOT = -17147
397469 ZDOT = -5219
362909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17556266
02 X = -5351149
88
Y = 10580248
09 feet Y = 3224859
62 meter
Z = -8681387
45 Z = -2646086
89
XDOT = -1772
778609 XDOT = -540
342920
YDOT = -16972
086173 feet/sec YDOT = -5173
091866 meter/sec
ZDOT = -17114
458365 ZDOT = -5216
486910
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 18177
33122431
00016717 00000-0 10270-3 0 9134
2 25544 51
6407 333
1397 0003425 259
4612 100
6155 15
53950036 39936
Satellite: ISS
Catalog Number: 25544
Epoch time: 18177
33122431 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 333
1397 deg
Eccentricity:
0003425
Arg of perigee: 259
4612 deg
Mean anomaly: 100
6155 deg
Mean motion: 15
53950036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3993
Checksum: 294
Coasting Arc #15 (Orbit 4008)
---------------------------------------
Vector Time (GMT): 2018/178/07:18:17
970
Vector Time (MET): N/A
Weight (LBS) : 922901
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5545154
17 A = 6783260
16 meter
Y = 170401
60 meter E =
0007878
Z = 3898249
24 I = 51
43931
XDOT = -3038
302700 Wp = 105
28459
YDOT = 5751
864767 meter/sec RA = 327
69434 deg
ZDOT = 4061
571877 TA = 302
04372
MA = 302
12023
Ha = 219
937 n
mi
Hp = 216
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18192763
03 X = 5523900
98
Y = 559060
38 feet Y = 232291
85 meter
Z = 12789531
63 Z = 3925134
02
XDOT = -9968
184711 XDOT = -3122
124738
YDOT = 18870
947398 feet/sec YDOT = 5717
419015 meter/sec
ZDOT = 13325
367050 ZDOT = 4046
610264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16763214
15 X = 5109427
67
Y = -6869781
75 feet Y = -2093909
48 meter
Z = 12909765
46 Z = 3934896
51
XDOT = -1990
969539 XDOT = -606
847516
YDOT = 20109
774465 feet/sec YDOT = 6129
459257 meter/sec
ZDOT = 13257
498048 ZDOT = 4040
885405
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 18178
36015964
00016717 00000-0 10270-3 0 9141
2 25544 51
6409 328
0113 0003343 266
0438 94
0332 15
53957637 40092
Satellite: ISS
Catalog Number: 25544
Epoch time: 18178
36015964 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 328
0113 deg
Eccentricity:
0003343
Arg of perigee: 266
0438 deg
Mean anomaly: 94
0332 deg
Mean motion: 15
53957637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4009
Checksum: 307
Coasting Arc #16 (Orbit 4023)
---------------------------------------
Vector Time (GMT): 2018/179/07:18:17
970
Vector Time (MET): N/A
Weight (LBS) : 922901
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4575693
38 A = 6779770
37 meter
Y = -1354621
98 meter E =
0008481
Z = -4824034
89 I = 51
40018
XDOT = 4339
685266 Wp = 65
10960
YDOT = -5803
162146 meter/sec RA = 322
68845 deg
ZDOT = -2486
654489 TA = 180
35076
MA = 180
35136
Ha = 219
941 n
mi
Hp = 216
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15012117
37 X = -4536773
07
Y = -4444297
82 feet Y = -1405572
11 meter
Z = -15826886
13 Z = -4846167
59
XDOT = 14237
812553 XDOT = 4416
334067
YDOT = -19039
245887 feet/sec YDOT = -5754
203808 meter/sec
ZDOT = -8158
315251 ZDOT = -2465
388730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15387362
88 X = -4690068
20
Y = 2282079
31 feet Y = 695577
77 meter
Z = -15925669
64 Z = -4854144
11
XDOT = 5055
383639 XDOT = 1540
880933
YDOT = -22177
387214 feet/sec YDOT = -6759
667623 meter/sec
ZDOT = -8062
246322 ZDOT = -2457
372679
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 18179
32478216
00016717 00000-0 10270-3 0 9152
2 25544 51
6406 323
2028 0003471 269
5498 90
5257 15
53985367 40242
Satellite: ISS
Catalog Number: 25544
Epoch time: 18179
32478216 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 323
2028 deg
Eccentricity:
0003471
Arg of perigee: 269
5498 deg
Mean anomaly: 90
5257 deg
Mean motion: 15
53985367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4024
Checksum: 328
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