[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 31st 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) : 74 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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
090/15:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
2
092/20:30:41
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
2
094/03:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
2
094/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 2598)
---------------------------------------
Vector Time (GMT): 2018/087/16:39:03
372
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4021984
84 A = 6788902
97 meter
Y = 5388660
00 meter E =
0009260
Z = -899525
47 I = 51
98755
XDOT = -3344
173028 Wp = 29
63370
YDOT = 3484
566526 meter/sec RA = 59
26513 deg
ZDOT = 5955
844006 TA = 320
67770
MA = 320
74490
Ha = 220
327 n
mi
Hp = 215
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13195488
31 X = 3965797
83
Y = 17679330
70 feet Y = 5433322
33 meter
Z = -2951199
06 Z = -880125
33
XDOT = -10971
696285 XDOT = -3411
819949
YDOT = 11432
304875 feet/sec YDOT = 3446
792133 meter/sec
ZDOT = 19540
170624 ZDOT = 5939
434617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20505711
51 X = 6250140
87
Y = -8166683
93 feet Y = -2489205
26 meter
Z = -2865360
43 Z = -873361
86
XDOT = 7560
958704 XDOT = 2304
580213
YDOT = 12195
023776 feet/sec YDOT = 3717
043247 meter/sec
ZDOT = 19466
401938 ZDOT = 5933
359311
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 18087
69548005
00016717 00000-0 10270-3 0 9008
2 25544 51
6413 59
9899 0001781 276
9125 83
1825 15
54162944 25993
Satellite: ISS
Catalog Number: 25544
Epoch time: 18087
69548005 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 59
9899 deg
Eccentricity:
0001781
Arg of perigee: 276
9125 deg
Mean anomaly: 83
1825 deg
Mean motion: 15
54162944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2599
Checksum: 345
Coasting Arc #2 (Orbit 2614)
---------------------------------------
Vector Time (GMT): 2018/088/16:39:03
372
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3369281
26 A = 6788987
40 meter
Y = -5827410
55 meter E =
0008922
Z = -846659
09 I = 51
97001
XDOT = 4494
963619 Wp = 148
83414
YDOT = -1737
533409 meter/sec RA = 54
31882 deg
ZDOT = -5963
985314 TA = 40
28180
MA = 40
21574
Ha = 220
315 n
mi
Hp = 215
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11054072
39 X = -3299754
56
Y = -19118801
03 feet Y = -5864699
54 meter
Z = -2777752
93 Z = -862856
16
XDOT = 14747
255969 XDOT = 4543
028848
YDOT = -5700
568928 feet/sec YDOT = -1686
999668 meter/sec
ZDOT = -19566
880952 ZDOT = -5942
033501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21228877
10 X = -6470561
74
Y = 6054231
59 feet Y = 1845329
79 meter
Z = -2849217
00 Z = -868441
34
XDOT = -1471
377364 XDOT = -448
475821
YDOT = -14268
243013 feet/sec YDOT = -4348
960470 meter/sec
ZDOT = -19468
621473 ZDOT = -5934
035825
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 18088
72429219
00016717 00000-0 10270-3 0 9019
2 25544 51
6414 54
8616 0001819 275
3452 84
7493 15
54135462 26155
Satellite: ISS
Catalog Number: 25544
Epoch time: 18088
72429219 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 54
8616 deg
Eccentricity:
0001819
Arg of perigee: 275
3452 deg
Mean anomaly: 84
7493 deg
Mean motion: 15
54135462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2615
Checksum: 318
Coasting Arc #3 (Orbit 2630)
---------------------------------------
Vector Time (GMT): 2018/089/16:39:03
372
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2439482
53 A = 6786605
28 meter
Y = 5821233
36 meter E =
0012132
Z = 2477497
77 I = 51
94302
XDOT = -5498
931893 Wp = 70
32780
YDOT = 21
040621 meter/sec RA = 49
36638 deg
ZDOT = 5347
866975 TA = 317
32022
MA = 317
41440
Ha = 220
293 n
mi
Hp = 215
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8003551
60 X = 2362172
24
Y = 19098534
65 feet Y = 5848081
42 meter
Z = 8128273
54 Z = 2489159
32
XDOT = -18041
115133 XDOT = -5524
735564
YDOT = 69
030910 feet/sec YDOT = -40
595746 meter/sec
ZDOT = 17545
495325 ZDOT = 5321
092442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20403363
48 X = 6218945
19
Y = -3417395
08 feet Y = -1041622
02 meter
Z = 8179478
25 Z = 2493104
97
XDOT = -4292
894075 XDOT = -1308
474114
YDOT = 16212
880790 feet/sec YDOT = 4941
686065 meter/sec
ZDOT = 17425
961847 ZDOT = 5311
433171
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 18089
75309951
00016717 00000-0 10270-3 0 9024
2 25544 51
6421 49
7321 0001889 286
7046 73
3900 15
54159720 26319
Satellite: ISS
Catalog Number: 25544
Epoch time: 18089
75309951 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 49
7321 deg
Eccentricity:
0001889
Arg of perigee: 286
7046 deg
Mean anomaly: 73
3900 deg
Mean motion: 15
54159720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2631
Checksum: 317
Coasting Arc #4 (Orbit 2644)
---------------------------------------
Vector Time (GMT): 2018/090/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3415825
11 A = 6787591
15 meter
Y = -5530502
61 meter E =
0005383
Z = -1945710
35 I = 51
92579
XDOT = 5080
739827 Wp = 150
45395
YDOT = -1164
436509 meter/sec RA = 44
73797 deg
ZDOT = -5620
940474 TA = 50
90843
MA = 50
86057
Ha = 220
307 n
mi
Hp = 215
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11206775
28 X = -3344276
39
Y = -18144693
61 feet Y = -5568300
94 meter
Z = -6383564
14 Z = -1962128
73
XDOT = 16669
093920 XDOT = 5120
686904
YDOT = -3820
329754 feet/sec YDOT = -1107
397610 meter/sec
ZDOT = -18441
405753 ZDOT = -5596
162752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21212486
52 X = -6465565
89
Y = -1980312
81 feet Y = -603599
34 meter
Z = -6456034
87 Z = -1967799
43
XDOT = 6890
811242 XDOT = 2100
319267
YDOT = -14170
444169 feet/sec YDOT = -4319
151383 meter/sec
ZDOT = -18330
624046 ZDOT = -5587
174209
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 18090
65330256
00016717 00000-0 10270-3 0 9038
2 25544 51
6422 45
2440 0001837 287
8142 72
2810 15
54160577 26450
Satellite: ISS
Catalog Number: 25544
Epoch time: 18090
65330256 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 45
2440 deg
Eccentricity:
0001837
Arg of perigee: 287
8142 deg
Mean anomaly: 72
2810 deg
Mean motion: 15
54160577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2645
Checksum: 292
Coasting Arc #5 (Orbit 2660)
---------------------------------------
Vector Time (GMT): 2018/091/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2274172
79 A = 6784183
98 meter
Y = 5389711
95 meter E =
0010769
Z = 3425731
06 I = 51
89006
XDOT = -6109
964408 Wp = 86
14479
YDOT = -368
016226 meter/sec RA = 39
77829 deg
ZDOT = 4623
315537 TA = 313
81457
MA = 313
90357
Ha = 220
351 n
mi
Hp = 215
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7461196
82 X = 2197094
04
Y = 17682782
00 feet Y = 5414712
79 meter
Z = 11239275
12 Z = 3436590
36
XDOT = -20045
814986 XDOT = -6127
852825
YDOT = -1207
402317 feet/sec YDOT = -436
441472 meter/sec
ZDOT = 15168
358062 ZDOT = 4593
591858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18652006
64 X = 5685131
62
Y = 4402183
65 feet Y = 1341785
58 meter
Z = 11286938
01 Z = 3440258
71
XDOT = -12482
774470 XDOT = -3804
749658
YDOT = 14239
916327 feet/sec YDOT = 4340
326496 meter/sec
ZDOT = 15035
735267 ZDOT = 4582
892109
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 18091
68210282
00016717 00000-0 10270-3 0 9049
2 25544 51
6418 40
1153 0001781 295
8940 64
2029 15
54171538 26613
Satellite: ISS
Catalog Number: 25544
Epoch time: 18091
68210282 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 40
1153 deg
Eccentricity:
0001781
Arg of perigee: 295
8940 deg
Mean anomaly: 64
2029 deg
Mean motion: 15
54171538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2661
Checksum: 296
Coasting Arc #6 (Orbit 2675)
---------------------------------------
Vector Time (GMT): 2018/092/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -839772
96 A = 6780262
27 meter
Y = -4950639
02 meter E =
0008756
Z = -4564913
51 I = 51
85223
XDOT = 6779
434641 Wp = 59
87902
YDOT = 1727
601278 meter/sec RA = 34
80725 deg
ZDOT = -3120
929691 TA = 178
92102
MA = 178
91913
Ha = 220
267 n
mi
Hp = 215
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2755160
64 X = -762177
01
Y = -16242254
02 feet Y = -4959596
59 meter
Z = -14976750
35 Z = -4568803
85
XDOT = 22242
239637 XDOT = 6774
772244
YDOT = 5667
983196 feet/sec YDOT = 1803
387164 meter/sec
ZDOT = -10239
270639 ZDOT = -3088
008768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14833668
07 X = -4521302
03
Y = -7132052
82 feet Y = -2173849
70 meter
Z = -14993361
56 Z = -4569976
60
XDOT = 16909
272452 XDOT = 5153
946243
YDOT = -13953
045999 feet/sec YDOT = -4252
888421 meter/sec
ZDOT = -10092
593809 ZDOT = -3076
222593
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 18092
64659789
00016717 00000-0 10270-3 0 9056
2 25544 51
6427 35
3080 0001975 297
1274 62
9678 15
54206001 26763
Satellite: ISS
Catalog Number: 25544
Epoch time: 18092
64659789 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 35
3080 deg
Eccentricity:
0001975
Arg of perigee: 297
1274 deg
Mean anomaly: 62
9678 deg
Mean motion: 15
54206001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2676
Checksum: 333
Coasting Arc #7 (Orbit 2679)
---------------------------------------
Vector Time (GMT): 2018/092/20:30:41
000
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1767678
73 A = 6777386
64 meter
Y = 3830856
03 meter E =
0001075
Z = 5303211
54 I = 51
83129
XDOT = -6607
614216 Wp = 111
89411
YDOT = -3850
846546 meter/sec RA = 33
64343 deg
ZDOT = 578
767597 TA = 332
59515
MA = 332
60082
Ha = 220
476 n
mi
Hp = 215
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5799470
89 X = -1836145
48
Y = 12568425
30 feet Y = 3810706
38 meter
Z = 17398988
01 Z = 5294457
99
XDOT = -21678
524331 XDOT = -6566
873285
YDOT = -12634
010978 feet/sec YDOT = -3924
509578 meter/sec
ZDOT = 1898
843822 ZDOT = 546
769162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12812363
04 X = 3905208
25
Y = -5368505
30 feet Y = -1636320
42 meter
Z = 17359333
66 Z = 5291124
90
XDOT = 7245
602488 XDOT = 2208
459638
YDOT = 22977
453457 feet/sec YDOT = 7003
527814 meter/sec
ZDOT = 1756
611178 ZDOT = 535
415087
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 18092
90379727
00016717 00000-0 10270-3 0 9067
2 25544 51
6383 34
0210 0001729 292
5230 67
5739 15
54147523 26800
Satellite: ISS
Catalog Number: 25544
Epoch time: 18092
90379727 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 34
0210 deg
Eccentricity:
0001729
Arg of perigee: 292
5230 deg
Mean anomaly: 67
5739 deg
Mean motion: 15
54147523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2680
Checksum: 311
Coasting Arc #8 (Orbit 2694)
---------------------------------------
Vector Time (GMT): 2018/093/20:30:41
000
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3324314
64 A = 6777808
32 meter
Y = -2837565
10 meter E =
0012305
Z = -5191203
09 I = 51
80621
XDOT = 6020
802057 Wp = 98
58877
YDOT = 4528
549983 meter/sec RA = 28
65541 deg
ZDOT = 1381
221048 TA = 184
67026
MA = 184
68175
Ha = 220
381 n
mi
Hp = 215
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10906544
11 X = 3381014
38
Y = -9309596
79 feet Y = -2800073
74 meter
Z = -17031506
19 Z = -5174916
60
XDOT = 19753
287588 XDOT = 5963
005787
YDOT = 14857
447450 feet/sec YDOT = 4595
555694 meter/sec
ZDOT = 4531
565119 ZDOT = 1410
327546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14424188
50 X = -4396492
65
Y = -222732
82 feet Y = -67888
96 meter
Z = -16958380
70 Z = -5168914
44
XDOT = -5118
903640 XDOT = -1560
241829
YDOT = -23108
288613 feet/sec YDOT = -7043
406369 meter/sec
ZDOT = 4660
770907 ZDOT = 1420
602972
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 18093
86828641
00016717 00000-0 10270-3 0 9078
2 25544 51
6394 29
2126 0001577 295
0624 65
0365 15
54202488 26956
Satellite: ISS
Catalog Number: 25544
Epoch time: 18093
86828641 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 29
2126 deg
Eccentricity:
0001577
Arg of perigee: 295
0624 deg
Mean anomaly: 65
0365 deg
Mean motion: 15
54202488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2695
Checksum: 328
Coasting Arc #9 (Orbit 2699)
---------------------------------------
Vector Time (GMT): 2018/094/03:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1327820
98 A = 6777176
17 meter
Y = 4008104
80 meter E =
0000899
Z = 5300424
86 I = 51
79867
XDOT = -6996
322827 Wp = 107
46029
YDOT = -3088
251700 meter/sec RA = 27
25231 deg
ZDOT = 582
282822 TA = 336
99375
MA = 336
99778
Ha = 220
308 n
mi
Hp = 215
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4356368
06 X = -1398288
95
Y = 13149950
13 feet Y = 3992862
60 meter
Z = 17389845
34 Z = 5293803
23
XDOT = -22953
815048 XDOT = -6964
097625
YDOT = -10132
059384 feet/sec YDOT = -3166
309168 meter/sec
ZDOT = 1910
376711 ZDOT = 548
375290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9539916
08 X = -2907766
42
Y = -10096415
84 feet Y = -3077387
55 meter
Z = 17359672
82 Z = 5291228
27
XDOT = 18949
928452 XDOT = 5775
938192
YDOT = -14878
180036 feet/sec YDOT = -4534
869275 meter/sec
ZDOT = 1759
525167 ZDOT = 536
303271
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 18094
18978014
00016717 00000-0 10270-3 0 9085
2 25544 51
6419 27
6126 0001910 294
6552 65
4402 15
54219530 27001
Satellite: ISS
Catalog Number: 25544
Epoch time: 18094
18978014 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 27
6126 deg
Eccentricity:
0001910
Arg of perigee: 294
6552 deg
Mean anomaly: 65
4402 deg
Mean motion: 15
54219530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2700
Checksum: 300
Coasting Arc #10 (Orbit 2704)
---------------------------------------
Vector Time (GMT): 2018/094/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1131190
19 A = 6779390
97 meter
Y = 4695900
88 meter E =
0005627
Z = 4753717
67 I = 51
79554
XDOT = -7097
741636 Wp = 116
07709
YDOT = -1043
302983 meter/sec RA = 25
68897 deg
ZDOT = 2714
681616 TA = 307
12904
MA = 307
18043
Ha = 220
263 n
mi
Hp = 215
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3711253
91 X = 1055503
99
Y = 15406498
96 feet Y = 4708127
79 meter
Z = 15596186
57 Z = 4759028
47
XDOT = -23286
553923 XDOT = -7098
734240
YDOT = -3422
910048 feet/sec YDOT = -1122
680164 meter/sec
ZDOT = 8906
435749 ZDOT = 2680
200581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2753769
93 X = 839349
08
Y = 15583108
23 feet Y = 4749731
39 meter
Z = 15619159
40 Z = 4760719
79
XDOT = -21984
515744 XDOT = -6700
880399
YDOT = -4904
068859 feet/sec YDOT = -1494
760188 meter/sec
ZDOT = 8752
711333 ZDOT = 2667
826414
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 18094
51127597
00016717 00000-0 10270-3 0 9095
2 25544 51
6404 26
0109 0001970 302
9919 57
1044 15
54236915 27056
Satellite: ISS
Catalog Number: 25544
Epoch time: 18094
51127597 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 26
0109 deg
Eccentricity:
0001970
Arg of perigee: 302
9919 deg
Mean anomaly: 57
1044 deg
Mean motion: 15
54236915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2705
Checksum: 305
Coasting Arc #11 (Orbit 2719)
---------------------------------------
Vector Time (GMT): 2018/095/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 594638
71 A = 6777328
62 meter
Y = -4222840
98 meter E =
0013262
Z = -5278989
03 I = 51
75805
XDOT = 7327
073442 Wp = 77
52225
YDOT = 2069
923060 meter/sec RA = 20
70028 deg
ZDOT = -829
424672 TA = 184
54622
MA = 184
55827
Ha = 220
387 n
mi
Hp = 215
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1950914
40 X = 667458
23
Y = -13854465
15 feet Y = -4215784
47 meter
Z = -17319517
82 Z = -5275923
34
XDOT = 24038
954861 XDOT = 7307
411376
YDOT = 6791
086156 feet/sec YDOT = 2151
749451 meter/sec
ZDOT = -2721
209554 ZDOT = -793
879876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2589101
01 X = 789157
99
Y = -13767549
93 feet Y = -4196349
22 meter
Z = -17305175
35 Z = -5274617
45
XDOT = 22777
695358 XDOT = 6942
641545
YDOT = 7509
267089 feet/sec YDOT = 2288
824609 meter/sec
ZDOT = -2562
907851 ZDOT = -781
174313
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 18095
47576075
00016717 00000-0 10270-3 0 9102
2 25544 51
6403 21
2024 0001947 309
2877 50
8103 15
54207623 27202
Satellite: ISS
Catalog Number: 25544
Epoch time: 18095
47576075 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 21
2024 deg
Eccentricity:
0001947
Arg of perigee: 309
2877 deg
Mean anomaly: 50
8103 deg
Mean motion: 15
54207623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2720
Checksum: 288
Coasting Arc #12 (Orbit 2735)
---------------------------------------
Vector Time (GMT): 2018/096/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2358401
39 A = 6777537
80 meter
Y = 3617227
14 meter E =
0004070
Z = 5222927
00 I = 51
72831
XDOT = -7004
100370 Wp = 25
93582
YDOT = -2907
990648 meter/sec RA = 15
70761 deg
ZDOT = -1144
794706 TA = 75
04665
MA = 75
00158
Ha = 220
467 n
mi
Hp = 215
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7737537
36 X = -2424045
31
Y = 11867543
10 feet Y = 3590487
10 meter
Z = 17135587
27 Z = 5211311
01
XDOT = -22979
331921 XDOT = -6965
501024
YDOT = -9540
651731 feet/sec YDOT = -2986
099553 meter/sec
ZDOT = -3755
888142 ZDOT = -1178
724505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8094775
30 X = -2467287
51
Y = 11703672
73 feet Y = 3567279
45 meter
Z = 17083180
98 Z = 5206953
56
XDOT = -21897
971559 XDOT = -6674
501731
YDOT = -9424
211636 feet/sec YDOT = -2872
499707 meter/sec
ZDOT = -3906
841249 ZDOT = -1190
805213
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 18096
50453668
00016717 00000-0 10270-3 0 9110
2 25544 51
6409 16
0741 0002065 313
0031 47
0948 15
54224668 27363
Satellite: ISS
Catalog Number: 25544
Epoch time: 18096
50453668 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 16
0741 deg
Eccentricity:
0002065
Arg of perigee: 313
0031 deg
Mean anomaly: 47
0948 deg
Mean motion: 15
54224668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2736
Checksum: 297
Coasting Arc #13 (Orbit 2750)
---------------------------------------
Vector Time (GMT): 2018/097/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3992781
35 A = 6780095
00 meter
Y = -2957905
93 meter E =
0008422
Z = -4620854
17 I = 51
70479
XDOT = 6091
729136 Wp = 102
92818
YDOT = 3555
838072 meter/sec RA = 10
71530 deg
ZDOT = 2990
319757 TA = 196
88109
MA = 196
90913
Ha = 220
479 n
mi
Hp = 215
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13099676
36 X = 4048006
47
Y = -9704415
77 feet Y = -2912947
34 meter
Z = -15160282
73 Z = -4601324
28
XDOT = 19985
987980 XDOT = 6036
988583
YDOT = 11666
135406 feet/sec YDOT = 3623
654050 meter/sec
ZDOT = 9810
760356 ZDOT = 3019
778250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13233594
32 X = 4033599
55
Y = -9659092
83 feet Y = -2944091
49 meter
Z = -15072666
84 Z = -4594148
85
XDOT = 19175
226018 XDOT = 5844
608890
YDOT = 10771
916580 feet/sec YDOT = 3283
280173 meter/sec
ZDOT = 9941
649767 ZDOT = 3030
214849
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 18097
46900864
00016717 00000-0 10270-3 0 9122
2 25544 51
6408 11
2651 0002012 319
1609 40
9392 15
54230198 27516
Satellite: ISS
Catalog Number: 25544
Epoch time: 18097
46900864 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 11
2651 deg
Eccentricity:
0002012
Arg of perigee: 319
1609 deg
Mean anomaly: 40
9392 deg
Mean motion: 15
54230198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2751
Checksum: 292
Coasting Arc #14 (Orbit 2766)
---------------------------------------
Vector Time (GMT): 2018/098/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5358253
57 A = 6783937
99 meter
Y = 2240360
23 meter E =
0011178
Z = 3498306
32 I = 51
68515
XDOT = -4666
560270 Wp = 80
21705
YDOT = -4065
648867 meter/sec RA = 5
73146 deg
ZDOT = -4529
756969 TA = 58
66470
MA = 58
55534
Ha = 220
553 n
mi
Hp = 214
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17579572
08 X = -5399900
61
Y = 7350263
23 feet Y = 2180207
87 meter
Z = 11477382
95 Z = 3472176
47
XDOT = -15310
237105 XDOT = -4598
747035
YDOT = -13338
743003 feet/sec YDOT = -4117
454619 meter/sec
ZDOT = -14861
407379 ZDOT = -4552
260629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17552761
43 X = -5350081
68
Y = 7592043
57 feet Y = 2314054
88 meter
Z = 11360435
03 Z = 3462660
60
XDOT = -14839
226107 XDOT = -4522
996118
YDOT = -11850
544481 feet/sec YDOT = -3612
045958 meter/sec
ZDOT = -14961
175724 ZDOT = -4560
166361
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 18098
49777408
00016717 00000-0 10270-3 0 9133
2 25544 51
6409 6
1368 0002052 321
7087 38
3919 15
54233911 27677
Satellite: ISS
Catalog Number: 25544
Epoch time: 18098
49777408 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 6
1368 deg
Eccentricity:
0002052
Arg of perigee: 321
7087 deg
Mean anomaly: 38
3919 deg
Mean motion: 15
54233911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2767
Checksum: 324
Coasting Arc #15 (Orbit 2781)
---------------------------------------
Vector Time (GMT): 2018/099/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6296300
63 A = 6787335
89 meter
Y = -1514752
32 meter E =
0007585
Z = -2020277
85 I = 51
66427
XDOT = 2849
001759 Wp = 23
72201
YDOT = 4438
633961 meter/sec RA =
75481 deg
ZDOT = 5565
136525 TA = 313
96461
MA = 314
02715
Ha = 220
539 n
mi
Hp = 214
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20657154
29 X = 6322584
50
Y = -4969659
83 feet Y = -1444195
90 meter
Z = -6628208
19 Z = -1989628
67
XDOT = 9347
118632 XDOT = 2772
123490
YDOT = 14562
447377 feet/sec YDOT = 4470
063927 meter/sec
ZDOT = 18258
321933 ZDOT = 5578
789013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20537131
23 X = 6259717
60
Y = -5607051
11 feet Y = -1709029
18 meter
Z = -6491217
50 Z = -1978523
09
XDOT = 9262
779245 XDOT = 2823
295114
YDOT = 12774
419266 feet/sec YDOT = 3893
642992 meter/sec
ZDOT = 18318
533945 ZDOT = 5583
489146
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18099
46223655
00016717 00000-0 10270-3 0 9142
2 25544 51
6413 1
3280 0002109 323
4801 36
6208 15
54241865 27824
Satellite: ISS
Catalog Number: 25544
Epoch time: 18099
46223655 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 1
3280 deg
Eccentricity:
0002109
Arg of perigee: 323
4801 deg
Mean anomaly: 36
6208 deg
Mean motion: 15
54241865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2782
Checksum: 290
Coasting Arc #16 (Orbit 2797)
---------------------------------------
Vector Time (GMT): 2018/100/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6738767
85 A = 6788987
46 meter
Y = 727761
97 meter E =
0010596
Z = 291052
14 I = 51
63783
XDOT = -773
764518 Wp = 128
56122
YDOT = -4707
408472 meter/sec RA = 355
78393 deg
ZDOT = -6003
109304 TA = 48
30233
MA = 48
21171
Ha = 220
549 n
mi
Hp = 214
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22108818
41 X = -6747818
82
Y = 2387670
51 feet Y = 652353
84 meter
Z = 954895
48 Z = 258295
52
XDOT = -2538
597501 XDOT = -691
907552
YDOT = -15444
253517 feet/sec YDOT = -4715
603959 meter/sec
ZDOT = -19695
240498 ZDOT = -6006
668844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21974301
45 X = -6697767
08
Y = 3448018
47 feet Y = 1050956
03 meter
Z = 808635
89 Z = 246472
22
XDOT = -2896
690989 XDOT = -882
911413
YDOT = -13709
768622 feet/sec YDOT = -4178
737476 meter/sec
ZDOT = -19710
378260 ZDOT = -6007
723294
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18100
49099052
00016717 00000-0 10270-3 0 9151
2 25544 51
6423 356
1989 0002057 328
4081 31
6948 15
54236976 27989
Satellite: ISS
Catalog Number: 25544
Epoch time: 18100
49099052 = yrday
fracday
Element set: 915
Inclination: 51
6423 deg
RA of node: 356
1989 deg
Eccentricity:
0002057
Arg of perigee: 328
4081 deg
Mean anomaly: 31
6948 deg
Mean motion: 15
54236976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2798
Checksum: 334
Coasting Arc #17 (Orbit 2813)
---------------------------------------
Vector Time (GMT): 2018/101/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6625001
53 A = 6788057
06 meter
Y = 84871
70 meter E =
0014153
Z = 1440495
44 I = 51
60182
XDOT = -1326
907197 Wp = 52
23532
YDOT = 4859
777448 meter/sec RA = 350
81181 deg
ZDOT = 5785
896052 TA = 323
49347
MA = 323
58987
Ha = 220
588 n
mi
Hp = 214
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21735569
32 X = 6616562
92
Y = 278450
47 feet Y = 158909
96 meter
Z = 4726034
90 Z = 1472656
90
XDOT = -4353
370068 XDOT = -1409
256775
YDOT = 15944
151733 feet/sec YDOT = 4844
479084 meter/sec
ZDOT = 18982
598596 ZDOT = 5779
249989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21675821
91 X = 6606790
52
Y = -1137814
20 feet Y = -346805
77 meter
Z = 4869500
74 Z = 1484223
82
XDOT = -3511
749446 XDOT = -1070
381231
YDOT = 14623
231943 feet/sec YDOT = 4457
161096 meter/sec
ZDOT = 18952
185167 ZDOT = 5776
626039
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18101
51973968
00016717 00000-0 10270-3 0 9163
2 25544 51
6419 351
0699 0002191 334
5421 25
5624 15
54246313 28149
Satellite: ISS
Catalog Number: 25544
Epoch time: 18101
51973968 = yrday
fracday
Element set: 916
Inclination: 51
6419 deg
RA of node: 351
0699 deg
Eccentricity:
0002191
Arg of perigee: 334
5421 deg
Mean anomaly: 25
5624 deg
Mean motion: 15
54246313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2814
Checksum: 306
Coasting Arc #18 (Orbit 2828)
---------------------------------------
Vector Time (GMT): 2018/102/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5986353
60 A = 6784931
09 meter
Y = -980033
66 meter E =
0003325
Z = -3043145
09 I = 51
55996
XDOT = 3295
894926 Wp = 78
06182
YDOT = -4861
210349 meter/sec RA = 345
83248 deg
ZDOT = -4921
904357 TA = 136
86208
MA = 136
83603
Ha = 220
547 n
mi
Hp = 214
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19640267
70 X = -5960167
65
Y = -3215333
53 feet Y = -1046831
05 meter
Z = -9984071
81 Z = -3072161
08
XDOT = 10813
303562 XDOT = 3373
917414
YDOT = -15948
852851 feet/sec YDOT = -4823
917589 meter/sec
ZDOT = -16147
980174 ZDOT = -4905
704057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19772323
36 X = -6026604
16
Y = -1592311
86 feet Y = -485336
66 meter
Z = -10113354
88 Z = -3082550
57
XDOT = 9452
226112 XDOT = 2881
038519
YDOT = -15353
818102 feet/sec YDOT = -4679
843758 meter/sec
ZDOT = -16074
952829 ZDOT = -4899
645622
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18102
48418724
00016717 00000-0 10270-3 0 9175
2 25544 51
6426 346
2622 0002211 331
1182 28
9848 15
54255584 28290
Satellite: ISS
Catalog Number: 25544
Epoch time: 18102
48418724 = yrday
fracday
Element set: 917
Inclination: 51
6426 deg
RA of node: 346
2622 deg
Eccentricity:
0002211
Arg of perigee: 331
1182 deg
Mean anomaly: 28
9848 deg
Mean motion: 15
54255584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2829
Checksum: 309
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