[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 12th 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
261/11:24:45
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 214
6
267/01:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 215
2
Coasting Arc #1 (Orbit 1208)
---------------------------------------
Vector Time (GMT): 2018/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3083478
61 A = 6789841
01 meter
Y = 5982564
97 meter E =
0017816
Z = 821545
82 I = 51
34102
XDOT = -4626
862370 Wp = 132
29311
YDOT = -1562
397798 meter/sec RA = 302
87084 deg
ZDOT = -5917
764597 TA = 38
78053
MA = 38
65280
Ha = 222
673 n
mi
Hp = 214
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10116399
65 X = -3154138
79
Y = 19627837
83 feet Y = 5947688
38 meter
Z = 2695360
31 Z = 806395
02
XDOT = -15179
994653 XDOT = -4580
301873
YDOT = -5125
977027 feet/sec YDOT = -1613
878909 meter/sec
ZDOT = -19415
238179 ZDOT = -5940
127079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13214214
03 X = 4027692
44
Y = -17701519
92 feet Y = -5395423
27 meter
Z = 2626645
54 Z = 800601
56
XDOT = 12715
842198 XDOT = 3875
788702
YDOT = 6561
359256 feet/sec YDOT = 1999
902301 meter/sec
ZDOT = -19515
326097 ZDOT = -5948
271394
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 18255
53375049
00016717 00000-0 10270-3 0 9004
2 25544 51
6399 303
4235 0004769 150
1493 209
9932 15
53860871 12094
Satellite: ISS
Catalog Number: 25544
Epoch time: 18255
53375049 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 303
4235 deg
Eccentricity:
0004769
Arg of perigee: 150
1493 deg
Mean anomaly: 209
9932 deg
Mean motion: 15
53860871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1209
Checksum: 322
Coasting Arc #2 (Orbit 1224)
---------------------------------------
Vector Time (GMT): 2018/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3686566
01 A = 6790003
23 meter
Y = -5644681
20 meter E =
0013516
Z = 773293
78 I = 51
32355
XDOT = 3660
975843 Wp = 73
30590
YDOT = 3213
255716 meter/sec RA = 297
88073 deg
ZDOT = 5919
779177 TA = 295
08723
MA = 295
22744
Ha = 222
729 n
mi
Hp = 214
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12095032
83 X = 3745656
13
Y = -18519295
27 feet Y = -5603124
99 meter
Z = 2537053
07 Z = 791345
99
XDOT = 12011
075602 XDOT = 3596
016920
YDOT = 10542
177545 feet/sec YDOT = 3253
832651 meter/sec
ZDOT = 19421
847693 ZDOT = 5937
404931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14667574
59 X = -4470676
73
Y = 16543738
72 feet Y = 5042531
56 meter
Z = 2618724
81 Z = 798187
32
XDOT = -8997
407726 XDOT = -2742
409875
YDOT = -11105
206381 feet/sec YDOT = -3384
866905 meter/sec
ZDOT = 19500
482530 ZDOT = 5943
747075
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 18256
56277591
00016717 00000-0 10270-3 0 9012
2 25544 51
6394 298
2961 0004659 151
6492 208
4914 15
53804090 12252
Satellite: ISS
Catalog Number: 25544
Epoch time: 18256
56277591 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 298
2961 deg
Eccentricity:
0004659
Arg of perigee: 151
6492 deg
Mean anomaly: 208
4914 deg
Mean motion: 15
53804090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1225
Checksum: 328
Coasting Arc #3 (Orbit 1239)
---------------------------------------
Vector Time (GMT): 2018/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4093942
68 A = 6787747
42 meter
Y = 4877783
78 meter E =
0010276
Z = -2340127
22 I = 51
30253
XDOT = -2647
764951 Wp = 143
99379
YDOT = -4788
831226 meter/sec RA = 292
88675 deg
ZDOT = -5369
947586 TA = 62
23454
MA = 62
13038
Ha = 222
556 n
mi
Hp = 214
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13431570
47 X = -4136815
97
Y = 16003227
61 feet Y = 4831762
57 meter
Z = -7677582
75 Z = -2360118
82
XDOT = -8686
892885 XDOT = -2567
933592
YDOT = -15711
388536 feet/sec YDOT = -4817
994432 meter/sec
ZDOT = -17617
938274 ZDOT = -5382
615307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15345310
65 X = 4677250
69
Y = -14129319
75 feet Y = -4306616
66 meter
Z = -7767845
29 Z = -2367639
24
XDOT = 5425
963298 XDOT = 1653
833613
YDOT = 15573
591075 feet/sec YDOT = 4746
830560 meter/sec
ZDOT = -17674
144706 ZDOT = -5387
079306
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
52748278
00016717 00000-0 10270-3 0 9025
2 25544 51
6399 293
4889 0004808 156
2823 203
8551 15
53853874 12405
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
52748278 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 293
4889 deg
Eccentricity:
0004808
Arg of perigee: 156
2823 deg
Mean anomaly: 203
8551 deg
Mean motion: 15
53853874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1240
Checksum: 344
Coasting Arc #4 (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 = -3747234
17 A = 6778299
64 meter
Y = -2031058
02 meter E =
0017382
Z = -5285246
65 I = 51
26819
XDOT = 3208
661758 Wp = 107
21844
YDOT = -6939
807419 meter/sec RA = 292
48125 deg
ZDOT = 387
959643 TA = 166
52957
MA = 166
48311
Ha = 222
615 n
mi
Hp = 214
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12294075
37 X = -3698570
72
Y = -6663576
18 feet Y = -2072690
51 meter
Z = -17340048
07 Z = -5303331
17
XDOT = 10527
105505 XDOT = 3284
141620
YDOT = -22768
397044 feet/sec YDOT = -6903
503874 meter/sec
ZDOT = 1272
833474 ZDOT = 403
730174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13727709
81 X = 4184205
95
Y = 2070582
17 feet Y = 631113
45 meter
Z = -17420891
96 Z = -5309887
87
XDOT = -1896
686753 XDOT = -578
110122
YDOT = 23995
749473 feet/sec YDOT = 7313
904439 meter/sec
ZDOT = 1344
424825 ZDOT = 409
780687
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
59179597
00016717 00000-0 10270-3 0 9035
2 25544 51
6385 293
1692 0004743 157
4165 202
7197 15
53825219 12416
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
59179597 = yrday
fracday
Element set: 903
Inclination: 51
6385 deg
RA of node: 293
1692 deg
Eccentricity:
0004743
Arg of perigee: 157
4165 deg
Mean anomaly: 202
7197 deg
Mean motion: 15
53825219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1241
Checksum: 335
Coasting Arc #5 (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 = 501862
71 A = 6785752
70 meter
Y = 5934208
58 meter E =
0015307
Z = 3234558
51 I = 51
29079
XDOT = -5224
516084 Wp = 108
67110
YDOT = 3029
874062 meter/sec RA = 290
96863 deg
ZDOT = -4734
461712 TA = 33
62101
MA = 33
52399
Ha = 222
537 n
mi
Hp = 214
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1646531
19 X = 419755
57
Y = 19469188
24 feet Y = 5939361
90 meter
Z = 10612068
59 Z = 3236796
53
XDOT = -17140
800801 XDOT = -5235
011023
YDOT = 9940
531700 feet/sec YDOT = 2971
390871 meter/sec
ZDOT = -15533
010867 ZDOT = -4759
866462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14437933
48 X = -4400682
12
Y = 13157091
78 feet Y = 4010281
57 meter
Z = 10621363
78 Z = 3237391
68
XDOT = -17325
471439 XDOT = -5280
803695
YDOT = -6344
437327 feet/sec YDOT = -1933
784497 meter/sec
ZDOT = -15647
314257 ZDOT = -4769
301385
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
91336716
00016717 00000-0 10270-3 0 9040
2 25544 51
6400 291
5682 0004631 157
8969 202
2384 15
53829246 12469
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
91336716 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 291
5682 deg
Eccentricity:
0004631
Arg of perigee: 157
8969 deg
Mean anomaly: 202
2384 deg
Mean motion: 15
53829246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1246
Checksum: 323
Coasting Arc #6 (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 = 338385
90 A = 6788665
12 meter
Y = -6527741
10 meter E =
0006019
Z = -1834871
57 I = 51
29138
XDOT = 5051
354977 Wp = 76
69428
YDOT = -1310
336605 meter/sec RA = 285
96807 deg
ZDOT = 5610
162600 TA = 263
04185
MA = 263
11032
Ha = 222
388 n
mi
Hp = 214
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1110189
95 X = 420268
64
Y = -21416473
41 feet Y = -6523499
31 meter
Z = -6019919
85 Z = -1833028
52
XDOT = 16572
686932 XDOT = 5038
380753
YDOT = -4299
004608 feet/sec YDOT = -1253
921050 meter/sec
ZDOT = 18406
045274 ZDOT = 5634
669014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17433444
36 X = 5313713
84
Y = -12493277
56 feet Y = -3807951
00 meter
Z = -6010850
50 Z = -1832107
23
XDOT = 12728
314287 XDOT = 3879
590195
YDOT = 8879
607117 feet/sec YDOT = 2706
504249 meter/sec
ZDOT = 18516
103786 ZDOT = 5643
708434
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
87807140
00016717 00000-0 10270-3 0 9051
2 25544 51
6413 286
7604 0004492 162
9650 197
1654 15
53865544 12612
Satellite: ISS
Catalog Number: 25544
Epoch time: 18258
87807140 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 286
7604 deg
Eccentricity:
0004492
Arg of perigee: 162
9650 deg
Mean anomaly: 197
1654 deg
Mean motion: 15
53865544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1261
Checksum: 327
Coasting Arc #7 (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 = -1111404
00 A = 6790220
41 meter
Y = 6685635
11 meter E =
0016544
Z = 226668
23 I = 51
28777
XDOT = -4769
832695 Wp = 141
12865
YDOT = -582
526494 meter/sec RA = 280
97446 deg
ZDOT = -5980
648420 TA = 36
41618
MA = 36
30374
Ha = 222
407 n
mi
Hp = 214
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3646338
58 X = -1187183
06
Y = 21934498
40 feet Y = 6672782
93 meter
Z = 743662
16 Z = 221084
98
XDOT = -15649
057397 XDOT = -4733
913300
YDOT = -1911
176160 feet/sec YDOT = -635
665558 meter/sec
ZDOT = -19621
549935 ZDOT = -6003
731401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19211422
43 X = -5855641
56
Y = 11197188
57 feet Y = 3412903
08 meter
Z = 717812
76 Z = 218789
33
XDOT = -7621
313658 XDOT = -2322
976403
YDOT = -11762
609436 feet/sec YDOT = -3585
243356 meter/sec
ZDOT = -19724
995099 ZDOT = -6012
178506
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
90708893
00016717 00000-0 10270-3 0 9062
2 25544 51
6410 281
6333 0004603 165
9834 194
1447 15
53816475 12776
Satellite: ISS
Catalog Number: 25544
Epoch time: 18259
90708893 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 281
6333 deg
Eccentricity:
0004603
Arg of perigee: 165
9834 deg
Mean anomaly: 194
1447 deg
Mean motion: 15
53816475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1277
Checksum: 332
Coasting Arc #8 (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 = 1771045
66 A = 6789326
35 meter
Y = -6406502
04 meter E =
0012997
Z = 1364441
01 I = 51
27930
XDOT = 4400
258985 Wp = 78
53693
YDOT = 2456
396889 meter/sec RA = 275
98033 deg
ZDOT = 5777
696836 TA = 296
39870
MA = 296
53205
Ha = 222
223 n
mi
Hp = 214
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5810517
26 X = 1835925
58
Y = -21018707
49 feet Y = -6386334
15 meter
Z = 4476512
49 Z = 1373202
05
XDOT = 14436
545225 XDOT = 4344
398821
YDOT = 8059
044913 feet/sec YDOT = 2505
291608 meter/sec
ZDOT = 18955
698282 ZDOT = 5798
935970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19708898
61 X = 6007272
30
Y = -9313822
09 feet Y = -2838852
97 meter
Z = 4516566
52 Z = 1376649
48
XDOT = 2533
655286 XDOT = 772
258131
YDOT = 14669
659709 feet/sec YDOT = 4471
312279 meter/sec
ZDOT = 19050
655551 ZDOT = 5806
639812
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
93610307
00016717 00000-0 10270-3 0 9070
2 25544 51
6404 276
5057 0004346 170
5189 189
6046 15
53853935 12938
Satellite: ISS
Catalog Number: 25544
Epoch time: 18260
93610307 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 276
5057 deg
Eccentricity:
0004346
Arg of perigee: 170
5189 deg
Mean anomaly: 189
6046 deg
Mean motion: 15
53853935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1293
Checksum: 322
Coasting Arc #9 (Orbit 1301)
---------------------------------------
Vector Time (GMT): 2018/261/11:24:45
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2481348
23 A = 6785031
46 meter
Y = 5294418
48 meter E =
0013889
Z = 3426277
92 I = 51
26159
XDOT = -3904
154046 Wp = 108
35425
YDOT = 4784
768061 meter/sec RA = 272
93007 deg
ZDOT = -4555
258498 TA = 31
24229
MA = 31
15982
Ha = 222
189 n
mi
Hp = 214
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8140906
26 X = 2405317
12
Y = 17370139
36 feet Y = 5321741
70 meter
Z = 11241069
28 Z = 3438146
48
XDOT = -12808
904349 XDOT = -3935
241464
YDOT = 15698
057943 feet/sec YDOT = 4740
935035 meter/sec
ZDOT = -14945
073813 ZDOT = -4574
299270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4161803
11 X = -1268517
59
Y = -18694653
66 feet Y = -5698130
43 meter
Z = 11293673
20 Z = 3442311
59
XDOT = 14410
732646 XDOT = 4392
391311
YDOT = -12310
093528 feet/sec YDOT = -3752
116507 meter/sec
ZDOT = -15031
030696 ZDOT = -4581
458156
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
51492274
00016717 00000-0 10270-3 0 9087
2 25544 51
6386 273
6202 0004584 169
6414 190
4834 15
53876958 13027
Satellite: ISS
Catalog Number: 25544
Epoch time: 18261
51492274 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 273
6202 deg
Eccentricity:
0004584
Arg of perigee: 169
6414 deg
Mean anomaly: 190
4834 deg
Mean motion: 15
53876958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1302
Checksum: 328
Coasting Arc #10 (Orbit 1316)
---------------------------------------
Vector Time (GMT): 2018/262/11:24:45
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1876882
12 A = 6788164
55 meter
Y = -6190997
77 meter E =
0004854
Z = -2059768
33 I = 51
27317
XDOT = 4306
242496 Wp = 86
19715
YDOT = -3134
082699 meter/sec RA = 267
92757 deg
ZDOT = 5507
734075 TA = 250
91744
MA = 250
97002
Ha = 222
177 n
mi
Hp = 214
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6157749
75 X = -1797507
94
Y = -20311672
47 feet Y = -6211542
68 meter
Z = -6757770
10 Z = -2068692
38
XDOT = 14128
092179 XDOT = 4314
215041
YDOT = -10282
423554 feet/sec YDOT = -3085
882398 meter/sec
ZDOT = 18069
993683 ZDOT = 5528
671798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1987892
83 X = 605909
73
Y = 21118649
60 feet Y = 6436964
40 meter
Z = -6797080
14 Z = -2071750
03
XDOT = -14219
755014 XDOT = -4334
181328
YDOT = 7172
540855 feet/sec YDOT = 2186
190452 meter/sec
ZDOT = 18164
259529 ZDOT = 5536
466304
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
47962088
00016717 00000-0 10270-3 0 9099
2 25544 51
6400 268
8132 0004645 172
9353 187
1865 15
53901639 13177
Satellite: ISS
Catalog Number: 25544
Epoch time: 18262
47962088 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 268
8132 deg
Eccentricity:
0004645
Arg of perigee: 172
9353 deg
Mean anomaly: 187
1865 deg
Mean motion: 15
53901639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1317
Checksum: 330
Coasting Arc #11 (Orbit 1332)
---------------------------------------
Vector Time (GMT): 2018/263/11:24:45
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1202447
70 A = 6790015
73 meter
Y = 6656946
27 meter E =
0016361
Z = 466714
31 I = 51
27913
XDOT = -4659
677938 Wp = 141
36044
YDOT = 1266
743614 meter/sec RA = 262
93197 deg
ZDOT = -5962
134492 TA = 33
57836
MA = 33
47478
Ha = 222
104 n
mi
Hp = 214
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3945038
38 X = 1125651
47
Y = 21840374
90 feet Y = 6669963
51 meter
Z = 1531214
92 Z = 472368
35
XDOT = -15287
657278 XDOT = -4644
535913
YDOT = 4155
982987 feet/sec YDOT = 1214
720099 meter/sec
ZDOT = -19560
808702 ZDOT = -5984
732810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 66881
35 X = 20385
43
Y = -22191999
91 feet Y = -6764121
57 meter
Z = 1555824
33 Z = 474215
26
XDOT = 14039
638825 XDOT = 4279
281914
YDOT = -1358
964357 feet/sec YDOT = -414
212336 meter/sec
ZDOT = -19662
307976 ZDOT = -5993
071471
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
50863035
00016717 00000-0 10270-3 0 9108
2 25544 51
6380 263
6855 0004500 176
1010 184
0178 15
53861231 13339
Satellite: ISS
Catalog Number: 25544
Epoch time: 18263
50863035 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 263
6855 deg
Eccentricity:
0004500
Arg of perigee: 176
1010 deg
Mean anomaly: 184
0178 deg
Mean motion: 15
53861231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1333
Checksum: 281
Coasting Arc #12 (Orbit 1348)
---------------------------------------
Vector Time (GMT): 2018/264/11:24:45
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -494246
53 A = 6789468
09 meter
Y = -6671889
28 meter E =
0011671
Z = 1136172
63 I = 51
28187
XDOT = 4924
318371 Wp = 76
18776
YDOT = 637
994445 meter/sec RA = 257
93847 deg
ZDOT = 5840
667316 TA = 296
20369
MA = 296
32365
Ha = 221
968 n
mi
Hp = 214
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1621543
73 X = -425121
78
Y = -21889400
53 feet Y = -6677029
69 meter
Z = 3727600
49 Z = 1133940
24
XDOT = 16155
900167 XDOT = 4888
447392
YDOT = 2093
157627 feet/sec YDOT = 692
861531 meter/sec
ZDOT = 19162
294345 ZDOT = 5864
500663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1950838
30 X = -594615
52
Y = 21864093
56 feet Y = 6664175
72 meter
Z = 3718320
51 Z = 1133344
09
XDOT = -13876
487394 XDOT = -4229
553358
YDOT = -4541
951449 feet/sec YDOT = -1384
386802 meter/sec
ZDOT = 19269
124803 ZDOT = 5873
229240
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
53763659
00016717 00000-0 10270-3 0 9114
2 25544 51
6371 258
5583 0004566 182
4687 177
6444 15
53893813 13494
Satellite: ISS
Catalog Number: 25544
Epoch time: 18264
53763659 = yrday
fracday
Element set: 911
Inclination: 51
6371 deg
RA of node: 258
5583 deg
Eccentricity:
0004566
Arg of perigee: 182
4687 deg
Mean anomaly: 177
6444 deg
Mean motion: 15
53893813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1349
Checksum: 352
Coasting Arc #13 (Orbit 1363)
---------------------------------------
Vector Time (GMT): 2018/265/11:24:45
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -326510
90 A = 6787083
46 meter
Y = 6228615
97 meter E =
0008133
Z = -2668674
80 I = 51
28138
XDOT = -5093
511798 Wp = 152
88349
YDOT = -2475
554996 meter/sec RA = 252
94015 deg
ZDOT = -5168
037986 TA = 57
39317
MA = 57
31469
Ha = 221
908 n
mi
Hp = 215
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1071230
00 X = -383173
77
Y = 20435091
77 feet Y = 6224647
60 meter
Z = -8755494
74 Z = -2670399
14
XDOT = -16710
996713 XDOT = -5040
347367
YDOT = -8121
899592 feet/sec YDOT = -2532
217454 meter/sec
ZDOT = -16955
505205 ZDOT = -5192
651037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3992259
26 X = 1216840
62
Y = -20066269
72 feet Y = -6116199
01 meter
Z = -8763896
58 Z = -2671235
68
XDOT = 13767
333295 XDOT = 4196
283188
YDOT = 10173
335567 feet/sec YDOT = 3100
832681 meter/sec
ZDOT = -17065
642465 ZDOT = -5201
607823
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
50233051
00016717 00000-0 10270-3 0 9121
2 25544 51
6369 253
7501 0004405 184
2424 175
8692 15
53859376 13647
Satellite: ISS
Catalog Number: 25544
Epoch time: 18265
50233051 = yrday
fracday
Element set: 912
Inclination: 51
6369 deg
RA of node: 253
7501 deg
Eccentricity:
0004405
Arg of perigee: 184
2424 deg
Mean anomaly: 175
8692 deg
Mean motion: 15
53859376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1364
Checksum: 312
Coasting Arc #14 (Orbit 1379)
---------------------------------------
Vector Time (GMT): 2018/266/11:24:45
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1198004
34 A = 6783496
22 meter
Y = -5404292
99 meter E =
0011861
Z = 3917029
05 I = 51
27988
XDOT = 5119
248440 Wp = 121
26638
YDOT = 4057
047260 meter/sec RA = 247
93546 deg
ZDOT = 4016
685191 TA = 286
49500
MA = 286
62529
Ha = 221
712 n
mi
Hp = 215
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3930460
43 X = 1239320
75
Y = -17730620
06 feet Y = -5390664
60 meter
Z = 12851145
16 Z = 3922949
52
XDOT = 16795
434515 XDOT = 5053
990009
YDOT = 13310
522506 feet/sec YDOT = 4113
929840 meter/sec
ZDOT = 13178
101020 ZDOT = 4041
393726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6104966
32 X = -1860793
73
Y = 17083762
80 feet Y = 5207130
90 meter
Z = 12878267
50 Z = 3925295
93
XDOT = -13600
388225 XDOT = -4145
398331
YDOT = -14914
704015 feet/sec YDOT = -4546
001784 meter/sec
ZDOT = 13288
512295 ZDOT = 4050
338548
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
53133184
00016717 00000-0 10270-3 0 9132
2 25544 51
6364 248
6226 0004344 190
8020 169
3040 15
53888700 13802
Satellite: ISS
Catalog Number: 25544
Epoch time: 18266
53133184 = yrday
fracday
Element set: 913
Inclination: 51
6364 deg
RA of node: 248
6226 deg
Eccentricity:
0004344
Arg of perigee: 190
8020 deg
Mean anomaly: 169
3040 deg
Mean motion: 15
53888700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1380
Checksum: 298
Coasting Arc #15 (Orbit 1388)
---------------------------------------
Vector Time (GMT): 2018/267/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4011669
30 A = 6778180
27 meter
Y = -1410878
59 meter E =
0004198
Z = 5276607
42 I = 51
27065
XDOT = 2968
926894 Wp = 157
29574
YDOT = 7062
219974 meter/sec RA = 244
96296 deg
ZDOT = -372
584620 TA = 296
25279
MA = 296
29592
Ha = 221
717 n
mi
Hp = 215
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13161644
69 X = 4001516
97
Y = -4628866
77 feet Y = -1366073
43 meter
Z = 17311704
14 Z = 5296070
26
XDOT = 9740
573799 XDOT = 2891
544354
YDOT = 23170
013037 feet/sec YDOT = 7094
987856 meter/sec
ZDOT = -1222
390485 ZDOT = -358
351410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9958867
94 X = 3035462
95
Y = -9614609
06 feet Y = -2930532
84 meter
Z = 17399156
33 Z = 5303262
85
XDOT = 17766
852651 XDOT = 5415
336688
YDOT = 16327
028857 feet/sec YDOT = 4976
478396 meter/sec
ZDOT = -1159
270810 ZDOT = -353
345743
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
11014762
00016717 00000-0 10270-3 0 9148
2 25544 51
6376 245
7337 0004650 190
7664 169
3389 15
53856166 13895
Satellite: ISS
Catalog Number: 25544
Epoch time: 18267
11014762 = yrday
fracday
Element set: 914
Inclination: 51
6376 deg
RA of node: 245
7337 deg
Eccentricity:
0004650
Arg of perigee: 190
7664 deg
Mean anomaly: 169
3389 deg
Mean motion: 15
53856166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1389
Checksum: 337
Coasting Arc #16 (Orbit 1403)
---------------------------------------
Vector Time (GMT): 2018/268/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4659171
14 A = 6779607
66 meter
Y = -155990
60 meter E =
0013366
Z = -4934503
54 I = 51
29145
XDOT = -2067
508109 Wp = 126
84808
YDOT = -7046
589672 meter/sec RA = 239
94254 deg
ZDOT = 2171
131557 TA = 164
47704
MA = 164
43601
Ha = 221
688 n
mi
Hp = 215
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15285994
54 X = -4633111
18
Y = -511780
19 feet Y = -207947
61 meter
Z = -16189316
08 Z = -4957072
98
XDOT = -6783
163088 XDOT = -1999
103795
YDOT = -23118
732519 feet/sec YDOT = -7069
327231 meter/sec
ZDOT = 7123
135029 ZDOT = 2161
255317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13925799
60 X = -4244583
72
Y = 6058686
93 feet Y = 1846687
77 meter
Z = -16290547
00 Z = -4965358
73
XDOT = -15659
555577 XDOT = -4773
032540
YDOT = -16924
759624 feet/sec YDOT = -5158
666733 meter/sec
ZDOT = 7079
540917 ZDOT = 2157
844071
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
07483378
00016717 00000-0 10270-3 0 9158
2 25544 51
6383 240
9271 0004738 195
2412 164
8598 15
53886754 14041
Satellite: ISS
Catalog Number: 25544
Epoch time: 18268
07483378 = yrday
fracday
Element set: 915
Inclination: 51
6383 deg
RA of node: 240
9271 deg
Eccentricity:
0004738
Arg of perigee: 195
2412 deg
Mean anomaly: 164
8598 deg
Mean motion: 15
53886754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1404
Checksum: 343
Coasting Arc #17 (Orbit 1419)
---------------------------------------
Vector Time (GMT): 2018/269/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5145416
94 A = 6782826
19 meter
Y = 1603531
79 meter E =
0008835
Z = 4109387
71 I = 51
32070
XDOT = 954
463550 Wp = 103
01664
YDOT = 6612
929831 meter/sec RA = 234
92846 deg
ZDOT = -3770
638860 TA = 26
02423
MA = 25
97984
Ha = 221
513 n
mi
Hp = 215
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16881289
17 X = 5107141
95
Y = 5260931
08 feet Y = 1660857
93 meter
Z = 13482243
15 Z = 4134289
44
XDOT = 3131
442093 XDOT = 898
760949
YDOT = 21695
964012 feet/sec YDOT = 6623
291376 meter/sec
ZDOT = -12370
862400 ZDOT = -3766
138490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17378161
03 X = 5296863
48
Y = -2763032
63 feet Y = -842172
35 meter
Z = 13593798
97 Z = 4143389
93
XDOT = 12333
940048 XDOT = 3759
384927
YDOT = 16729
066449 feet/sec YDOT = 5099
019454 meter/sec
ZDOT = -12351
327547 ZDOT = -3764
684636
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
10383116
00016717 00000-0 10270-3 0 9163
2 25544 51
6395 235
7986 0004712 198
1389 161
9596 15
53858312 14209
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
10383116 = yrday
fracday
Element set: 916
Inclination: 51
6395 deg
RA of node: 235
7986 deg
Eccentricity:
0004712
Arg of perigee: 198
1389 deg
Mean anomaly: 161
9596 deg
Mean motion: 15
53858312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1420
Checksum: 336
Coasting Arc #18 (Orbit 1434)
---------------------------------------
Vector Time (GMT): 2018/270/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5433822
95 A = 6786417
92 meter
Y = -2845234
07 meter E =
0003354
Z = -2909284
07 I = 51
35310
XDOT = 354
933636 Wp = 134
97514
YDOT = -5791
787719 meter/sec RA = 229
92612 deg
ZDOT = 5002
570231 TA = 191
74598
MA = 191
75381
Ha = 221
473 n
mi
Hp = 215
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17827503
11 X = -5387470
93
Y = -9334757
46 feet Y = -2905740
02 meter
Z = -9544895
25 Z = -2935567
14
XDOT = 1164
480434 XDOT = 395
372452
YDOT = -19001
928212 feet/sec YDOT = -5787
591913 meter/sec
ZDOT = 16412
631992 ZDOT = 5004
393296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20067053
10 X = -6116437
78
Y = -106602
32 feet Y = -32492
39 meter
Z = -9662536
16 Z = -2945141
02
XDOT = -7820
784970 XDOT = -2383
775259
YDOT = -15888
892953 feet/sec YDOT = -4842
934572 meter/sec
ZDOT = 16421
376127 ZDOT = 5005
235444
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
06851218
00016717 00000-0 10270-3 0 9174
2 25544 51
6399 230
9920 0004538 203
4208 156
6738 15
53865481 14354
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
06851218 = yrday
fracday
Element set: 917
Inclination: 51
6399 deg
RA of node: 230
9920 deg
Eccentricity:
0004538
Arg of perigee: 203
4208 deg
Mean anomaly: 156
6738 deg
Mean motion: 15
53865481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1435
Checksum: 322
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