[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 24th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 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
082/19:41:00
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
3
086/11:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
4
087/13:50:30
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
3
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
3
092/20:30:37
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
3
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
2
Coasting Arc #1 (Orbit 2518)
---------------------------------------
Vector Time (GMT): 2018/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3797066
00 A = 6778435
80 meter
Y = 2345111
66 meter E =
0004738
Z = 5100551
34 I = 51
99848
XDOT = -2024
338875 Wp = 143
59777
YDOT = -7178
089221 meter/sec RA = 85
05143 deg
ZDOT = 1788
749837 TA = 289
16060
MA = 289
21188
Ha = 220
592 n
mi
Hp = 215
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12457565
62 X = -3847783
32
Y = 7693935
90 feet Y = 2302367
02 meter
Z = 16734092
31 Z = 5081983
12
XDOT = -6641
531742 XDOT = -1952
609903
YDOT = -23550
161485 feet/sec YDOT = -7200
325590 meter/sec
ZDOT = 5868
601826 ZDOT = 1779
090972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12560348
25 X = -3828394
15
Y = 7707360
87 feet Y = 2349203
59 meter
Z = 16650876
15 Z = 5075187
05
XDOT = -6140
831712 XDOT = -1871
725506
YDOT = -22627
333661 feet/sec YDOT = -6896
811300 meter/sec
ZDOT = 5826
459205 ZDOT = 1775
904766
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 18082
55131063
00016717 00000-0 10270-3 0 9000
2 25544 51
6377 85
6329 0001771 244
5890 115
5079 15
54114497 25198
Satellite: ISS
Catalog Number: 25544
Epoch time: 18082
55131063 = yrday
fracday
Element set: 900
Inclination: 51
6377 deg
RA of node: 85
6329 deg
Eccentricity:
0001771
Arg of perigee: 244
5890 deg
Mean anomaly: 115
5079 deg
Mean motion: 15
54114497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2519
Checksum: 312
Coasting Arc #2 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2018/082/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3433337
50 A = 6779498
50 meter
Y = 3270772
07 meter E =
0006179
Z = 4842906
47 I = 52
00509
XDOT = -2767
253668 Wp = 132
18105
YDOT = -6684
372321 meter/sec RA = 83
47052 deg
ZDOT = 2546
519027 TA = 292
86852
MA = 292
93374
Ha = 220
512 n
mi
Hp = 215
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11264230
64 X = -3493181
31
Y = 10730879
50 feet Y = 3232043
83 meter
Z = 15888800
76 Z = 4826082
93
XDOT = -9078
916232 XDOT = -2704
671195
YDOT = -21930
355383 feet/sec YDOT = -6714
967575 meter/sec
ZDOT = 8354
721216 ZDOT = 2533
229071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14592946
17 X = 4447929
99
Y = 5610338
62 feet Y = 1710031
21 meter
Z = 15813243
79 Z = 4819876
71
XDOT = -15414
750149 XDOT = -4698
415846
YDOT = 16654
366533 feet/sec YDOT = 5076
250919 meter/sec
ZDOT = 8296
304758 ZDOT = 2528
713690
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 18082
87282200
00016717 00000-0 10270-3 0 9016
2 25544 51
6416 84
0319 0001818 251
3399 108
7556 15
54118379 25249
Satellite: ISS
Catalog Number: 25544
Epoch time: 18082
87282200 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 84
0319 deg
Eccentricity:
0001818
Arg of perigee: 251
3399 deg
Mean anomaly: 108
7556 deg
Mean motion: 15
54118379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 309
Coasting Arc #3 (Orbit 2538)
---------------------------------------
Vector Time (GMT): 2018/083/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3919779
84 A = 6777422
52 meter
Y = -1563670
10 meter E =
0012778
Z = -5314236
30 I = 51
99372
XDOT = 2029
373564 Wp = 85
65803
YDOT = 7355
182887 meter/sec RA = 78
49695 deg
ZDOT = -667
774660 TA = 177
99173
MA = 177
98660
Ha = 220
285 n
mi
Hp = 215
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12860170
09 X = 3962787
59
Y = -5130151
24 feet Y = -1519596
25 meter
Z = -17435158
47 Z = -5295090
88
XDOT = 6658
049750 XDOT = 1950
218771
YDOT = 24131
177451 feet/sec YDOT = 7377
434118 meter/sec
ZDOT = -2190
861744 ZDOT = -658
109364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10399083
88 X = -3169640
77
Y = -9302815
86 feet Y = -2835498
27 meter
Z = -17349462
50 Z = -5288116
17
XDOT = 17908
971016 XDOT = 5458
654366
YDOT = -16014
785793 feet/sec YDOT = -4881
306710 meter/sec
ZDOT = -2148
733569 ZDOT = -654
933992
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 18083
83735074
00016717 00000-0 10270-3 0 9026
2 25544 51
6416 79
2236 0001887 259
4333 100
6607 15
54154273 25393
Satellite: ISS
Catalog Number: 25544
Epoch time: 18083
83735074 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 79
2236 deg
Eccentricity:
0001887
Arg of perigee: 259
4333 deg
Mean anomaly: 100
6607 deg
Mean motion: 15
54154273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2539
Checksum: 313
Coasting Arc #4 (Orbit 2554)
---------------------------------------
Vector Time (GMT): 2018/084/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4318234
79 A = 6777787
79 meter
Y = -217422
40 meter E =
0002634
Z = 5218654
74 I = 51
98687
XDOT = -1169
550577 Wp = 35
63162
YDOT = -7471
580958 meter/sec RA = 73
52115 deg
ZDOT = -1276
635371 TA = 66
57913
MA = 66
55144
Ha = 220
393 n
mi
Hp = 215
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14167436
96 X = -4340831
87
Y = -713328
09 feet Y = -265837
89 meter
Z = 17121570
68 Z = 5197623
53
XDOT = -3837
108191 XDOT = -1079
713224
YDOT = -24513
060887 feet/sec YDOT = -7484
157446 meter/sec
ZDOT = -4188
436255 ZDOT = -1282
097937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5983176
84 X = 1823672
30
Y = 12985850
05 feet Y = 3958087
09 meter
Z = 17027700
47 Z = 5190043
10
XDOT = -19014
087466 XDOT = -5795
493860
YDOT = 14293
763877 feet/sec YDOT = 4356
739230 meter/sec
ZDOT = -4211
771923 ZDOT = -1283
748082
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 18084
86617979
00016717 00000-0 10270-3 0 9034
2 25544 51
6410 74
0950 0001945 262
7785 97
3147 15
54164674 25551
Satellite: ISS
Catalog Number: 25544
Epoch time: 18084
86617979 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 74
0950 deg
Eccentricity:
0001945
Arg of perigee: 262
7785 deg
Mean anomaly: 97
3147 deg
Mean motion: 15
54164674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2555
Checksum: 339
Coasting Arc #5 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2018/085/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4611716
65 A = 6780443
82 meter
Y = 1913064
41 meter E =
0008171
Z = -4595816
08 I = 51
98474
XDOT = 164
412510 Wp = 115
52067
YDOT = 7010
852570 meter/sec RA = 68
54847 deg
ZDOT = 3084
173277 TA = 185
20472
MA = 185
21322
Ha = 220
254 n
mi
Hp = 215
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15130303
97 X = 4612305
34
Y = 6276458
05 feet Y = 1964638
73 meter
Z = -15078136
74 Z = -4573412
89
XDOT = 539
411122 XDOT = 71
021883
YDOT = 23001
484811 feet/sec YDOT = 7012
169206 meter/sec
ZDOT = 10118
678730 ZDOT = 3084
744553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1774277
09 X = -540799
66
Y = -16375905
38 feet Y = -4991375
96 meter
Z = -14978380
93 Z = -4565410
51
XDOT = 18779
685152 XDOT = 5724
048034
YDOT = -11288
751211 feet/sec YDOT = -3440
811369 meter/sec
ZDOT = 10120
230623 ZDOT = 3084
646294
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 18085
83070715
00016717 00000-0 10270-3 0 9044
2 25544 51
6406 69
2865 0001976 266
9662 93
1265 15
54149177 25704
Satellite: ISS
Catalog Number: 25544
Epoch time: 18085
83070715 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 69
2865 deg
Eccentricity:
0001976
Arg of perigee: 266
9662 deg
Mean anomaly: 93
1265 deg
Mean motion: 15
54149177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2570
Checksum: 332
Coasting Arc #6 (Orbit 2579)
---------------------------------------
Vector Time (GMT): 2018/086/11:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4734975
11 A = 6781321
86 meter
Y = 2089048
05 meter E =
0007253
Z = -4389547
98 I = 51
97678
XDOT = 174
684452 Wp = 115
83081
YDOT = 6840
632199 meter/sec RA = 65
35230 deg
ZDOT = 3445
325595 TA = 188
97342
MA = 188
98639
Ha = 220
416 n
mi
Hp = 215
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15534695
24 X = 4732584
79
Y = 6853832
17 feet Y = 2141984
03 meter
Z = -14401404
13 Z = -4366553
34
XDOT = 573
111718 XDOT = 81
442251
YDOT = 22443
019025 feet/sec YDOT = 6842
064604 meter/sec
ZDOT = 11303
561662 ZDOT = 3445
947054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14358946
15 X = 4376606
79
Y = 9222824
89 feet Y = 2811117
03 meter
Z = -14299034
20 Z = -4358345
62
XDOT = -2360
835796 XDOT = -719
582751
YDOT = 21196
481368 feet/sec YDOT = 6460
687521 meter/sec
ZDOT = 11305
356544 ZDOT = 3445
872674
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 18086
47372394
00016717 00000-0 10270-3 0 9054
2 25544 51
6381 66
0800 0001689 266
0958 94
0001 15
54115930 25809
Satellite: ISS
Catalog Number: 25544
Epoch time: 18086
47372394 = yrday
fracday
Element set: 905
Inclination: 51
6381 deg
RA of node: 66
0800 deg
Eccentricity:
0001689
Arg of perigee: 266
0958 deg
Mean anomaly: 94
0001 deg
Mean motion: 15
54115930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2580
Checksum: 307
Coasting Arc #7 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2018/087/11:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4852858
51 A = 6785041
42 meter
Y = -3511078
38 meter E =
0011123
Z = 3176781
41 I = 51
97462
XDOT = 1043
374167 Wp = 94
28633
YDOT = -5846
501643 meter/sec RA = 60
38920 deg
ZDOT = -4854
098828 TA = 49
21549
MA = 49
11903
Ha = 220
373 n
mi
Hp = 215
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15921451
81 X = -4828666
99
Y = -11519286
04 feet Y = -3565210
77 meter
Z = 10422511
19 Z = 3153267
28
XDOT = 3423
143593 XDOT = 1132
252228
YDOT = -19181
435835 feet/sec YDOT = -5834
337506 meter/sec
ZDOT = -15925
521089 ZDOT = -4848
814009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14218826
12 X = -4333898
20
Y = -13644725
46 feet Y = -4158912
32 meter
Z = 10318031
25 Z = 3144935
93
XDOT = 5185
492589 XDOT = 1580
538141
YDOT = -17462
467805 feet/sec YDOT = -5322
560187 meter/sec
ZDOT = -15901
081230 ZDOT = -4846
649559
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
50254701
00016717 00000-0 10270-3 0 9061
2 25544 51
6377 60
9505 0001793 274
8198 85
2750 15
54160763 25962
Satellite: ISS
Catalog Number: 25544
Epoch time: 18087
50254701 = yrday
fracday
Element set: 906
Inclination: 51
6377 deg
RA of node: 60
9505 deg
Eccentricity:
0001793
Arg of perigee: 274
8198 deg
Mean anomaly: 85
2750 deg
Mean motion: 15
54160763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 327
Coasting Arc #8 (Orbit 2597)
---------------------------------------
Vector Time (GMT): 2018/087/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1021282
49 A = 6781078
20 meter
Y = 5070136
89 meter E =
0007714
Z = 4381317
12 I = 51
96148
XDOT = -5493
999039 Wp = 113
01291
YDOT = -4093
222156 meter/sec RA = 59
87760 deg
ZDOT = 3448
352318 TA = 302
14129
MA = 302
21612
Ha = 220
280 n
mi
Hp = 215
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3350664
33 X = -1099184
17
Y = 16634307
38 feet Y = 5058281
13 meter
Z = 14374400
00 Z = 4376166
35
XDOT = -18024
931229 XDOT = -5464
569317
YDOT = -13429
206548 feet/sec YDOT = -4154
494891 meter/sec
ZDOT = 11313
491858 ZDOT = 3421
736568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6083251
21 X = 1854174
97
Y = 15861993
13 feet Y = 4834735
51 meter
Z = 14350670
28 Z = 4374084
30
XDOT = -21328
145656 XDOT = -6500
818796
YDOT = -1972
025255 feet/sec YDOT = -601
073298 meter/sec
ZDOT = 11195
248563 ZDOT = 3412
311762
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
63114981
00016717 00000-0 10270-3 0 9071
2 25544 51
6393 60
3097 0001890 272
1877 87
9059 15
54173703 25984
Satellite: ISS
Catalog Number: 25544
Epoch time: 18087
63114981 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 60
3097 deg
Eccentricity:
0001890
Arg of perigee: 272
1877 deg
Mean anomaly: 87
9059 deg
Mean motion: 15
54173703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2598
Checksum: 339
Coasting Arc #9 (Orbit 2612)
---------------------------------------
Vector Time (GMT): 2018/088/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2200640
67 A = 6778185
53 meter
Y = -3857533
24 meter E =
0011811
Z = -5131179
77 I = 51
93407
XDOT = 5306
095690 Wp = 74
00141
YDOT = 5262
082353 meter/sec RA = 54
90369 deg
ZDOT = -1680
323369 TA = 179
81942
MA = 179
81899
Ha = 220
312 n
mi
Hp = 215
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7219949
72 X = 2268537
52
Y = -12655948
94 feet Y = -3832545
19 meter
Z = -16834579
31 Z = -5120324
48
XDOT = 17408
450428 XDOT = 5255
021370
YDOT = 17264
049715 feet/sec YDOT = 5321
132975 meter/sec
ZDOT = -5512
871944 ZDOT = -1654
673096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -916028
84 X = -279205
59
Y = -14598283
69 feet Y = -4449556
87 meter
Z = -16785552
79 Z = -5116236
49
XDOT = 23024
624381 XDOT = 7017
905511
YDOT = 4763
155485 feet/sec YDOT = 1451
809792 meter/sec
ZDOT = -5399
119187 ZDOT = -1645
651528
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
59567158
00016717 00000-0 10270-3 0 9086
2 25544 51
6393 55
5010 0001808 279
7170 80
3778 15
54151675 26130
Satellite: ISS
Catalog Number: 25544
Epoch time: 18088
59567158 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 55
5010 deg
Eccentricity:
0001808
Arg of perigee: 279
7170 deg
Mean anomaly: 80
3778 deg
Mean motion: 15
54151675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2613
Checksum: 330
Coasting Arc #10 (Orbit 2628)
---------------------------------------
Vector Time (GMT): 2018/089/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3381250
99 A = 6777235
97 meter
Y = 2468774
77 meter E =
0001137
Z = 5329095
52 I = 51
91222
XDOT = -4779
791352 Wp = 24
71686
YDOT = -5992
322597 meter/sec RA = 49
92427 deg
ZDOT = -255
674109 TA = 67
71671
MA = 67
70465
Ha = 220
336 n
mi
Hp = 215
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11093343
16 X = -3434492
09
Y = 8099654
75 feet Y = 2430666
35 meter
Z = 17483909
17 Z = 5312540
95
XDOT = -15681
730156 XDOT = -4711
186399
YDOT = -19659
851040 feet/sec YDOT = -6045
389956 meter/sec
ZDOT = -838
825818 ZDOT = -278
725157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4613514
78 X = -1406199
31
Y = 13037393
68 feet Y = 3973797
60 meter
Z = 17409640
91 Z = 5306458
55
XDOT = -23123
430242 XDOT = -7048
021538
YDOT = -6921
744674 feet/sec YDOT = -2109
747777 meter/sec
ZDOT = -940
853602 ZDOT = -286
772178
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
62449013
00016717 00000-0 10270-3 0 9091
2 25544 51
6402 50
3730 0002031 283
0969 76
9957 15
54175952 26297
Satellite: ISS
Catalog Number: 25544
Epoch time: 18089
62449013 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 50
3730 deg
Eccentricity:
0002031
Arg of perigee: 283
0969 deg
Mean anomaly: 76
9957 deg
Mean motion: 15
54175952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2629
Checksum: 322
Coasting Arc #11 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2018/090/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4484955
67 A = 6778854
06 meter
Y = -1045953
08 meter E =
0010521
Z = -4983996
61 I = 51
89605
XDOT = 3861
597839 Wp = 105
00460
YDOT = 6251
585249 meter/sec RA = 44
94267 deg
ZDOT = 2164
122831 TA = 186
02966
MA = 186
04233
Ha = 220
338 n
mi
Hp = 215
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14714421
48 X = 4520528
16
Y = -3431604
59 feet Y = -995601
02 meter
Z = -16351694
93 Z = -4962123
66
XDOT = 12669
284249 XDOT = 3780
891715
YDOT = 20510
450291 feet/sec YDOT = 6294
317343 meter/sec
ZDOT = 7100
140521 ZDOT = 2182
684276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10045364
91 X = 3061827
23
Y = -11426700
75 feet Y = -3482858
39 meter
Z = -16253897
70 Z = -4954188
02
XDOT = 21376
375746 XDOT = 6515
519327
YDOT = 8581
544131 feet/sec YDOT = 2615
654651 meter/sec
ZDOT = 7182
071598 ZDOT = 2189
095423
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
58900606
00016717 00000-0 10270-3 0 9100
2 25544 51
6408 45
5639 0001871 289
9525 70
1426 15
54158198 26448
Satellite: ISS
Catalog Number: 25544
Epoch time: 18090
58900606 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 45
5639 deg
Eccentricity:
0001871
Arg of perigee: 289
9525 deg
Mean anomaly: 70
1426 deg
Mean motion: 15
54158198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2644
Checksum: 322
Coasting Arc #12 (Orbit 2644)
---------------------------------------
Vector Time (GMT): 2018/090/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3417790
21 A = 6787652
29 meter
Y = -5530088
46 meter E =
0005370
Z = -1943532
66 I = 51
92572
XDOT = 5079
077865 Wp = 151
21911
YDOT = -1167
128681 meter/sec RA = 44
73819 deg
ZDOT = -5621
888129 TA = 50
11812
MA = 50
07091
Ha = 220
311 n
mi
Hp = 215
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11213222
47 X = -3346256
55
Y = -18143334
85 feet Y = -5567908
85 meter
Z = -6376419
48 Z = -1959960
62
XDOT = 16663
641289 XDOT = 5119
059773
YDOT = -3829
162340 feet/sec YDOT = -1110
108173 meter/sec
ZDOT = -18444
514858 ZDOT = -5597
118395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21215302
61 X = -6466424
24
Y = -1974305
11 feet Y = -601768
20 meter
Z = -6448933
05 Z = -1965634
79
XDOT = 6880
924997 XDOT = 2097
305939
YDOT = -14171
204950 feet/sec YDOT = -4319
383269 meter/sec
ZDOT = -18333
768411 ZDOT = -5588
132612
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
65330714
00016717 00000-0 10270-3 0 9116
2 25544 51
6422 45
2441 0001900 286
6793 73
4151 15
54140807 26456
Satellite: ISS
Catalog Number: 25544
Epoch time: 18090
65330714 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 45
2441 deg
Eccentricity:
0001900
Arg of perigee: 286
6793 deg
Mean anomaly: 73
4151 deg
Mean motion: 15
54140807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2645
Checksum: 286
Coasting Arc #13 (Orbit 2660)
---------------------------------------
Vector Time (GMT): 2018/091/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2283539
77 A = 6784268
92 meter
Y = 5390363
23 meter E =
0010714
Z = 3418684
23 I = 51
89005
XDOT = -6105
424221 Wp = 86
02631
YDOT = -357
440297 meter/sec RA = 39
77866 deg
ZDOT = 4630
012895 TA = 313
83360
MA = 313
92211
Ha = 220
359 n
mi
Hp = 215
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7491928
39 X = 2206487
27
Y = 17684918
74 feet Y = 5415468
96 meter
Z = 11216155
60 Z = 3429589
09
XDOT = -20030
919360 XDOT = -6123
463771
YDOT = -1172
704388 feet/sec YDOT = -425
815616 meter/sec
ZDOT = 15190
331019 ZDOT = 4600
310902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18671866
47 X = 5691184
90
Y = 4378436
21 feet Y = 1334547
36 meter
Z = 11264021
78 Z = 3433273
84
XDOT = -12447
756397 XDOT = -3794
076150
YDOT = 14246
899471 feet/sec YDOT = 4342
454959 meter/sec
ZDOT = 15057
803436 ZDOT = 4589
618487
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
68212134
00016717 00000-0 10270-3 0 9126
2 25544 51
6418 40
1154 0001843 294
7012 65
3948 15
54149388 26611
Satellite: ISS
Catalog Number: 25544
Epoch time: 18091
68212134 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 40
1154 deg
Eccentricity:
0001843
Arg of perigee: 294
7012 deg
Mean anomaly: 65
3948 deg
Mean motion: 15
54149388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2661
Checksum: 301
Coasting Arc #14 (Orbit 2675)
---------------------------------------
Vector Time (GMT): 2018/092/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -859027
11 A = 6780367
84 meter
Y = -4955562
56 meter E =
0008643
Z = -4556023
89 I = 51
85227
XDOT = 6776
357366 Wp = 59
54390
YDOT = 1709
721265 meter/sec RA = 34
80788 deg
ZDOT = -3137
479980 TA = 179
07194
MA = 179
07033
Ha = 220
280 n
mi
Hp = 215
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2818330
40 X = -781417
84
Y = -16258407
34 feet Y = -4964735
36 meter
Z = -14947584
94 Z = -4560007
73
XDOT = 22232
143589 XDOT = 6771
975530
YDOT = 5609
321736 feet/sec YDOT = 1785
474305 meter/sec
ZDOT = -10293
569487 ZDOT = -3104
573322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14883214
88 X = -4536403
89
Y = -7089384
47 feet Y = -2160844
39 meter
Z = -14964612
72 Z = -4561213
96
XDOT = 16858
727225 XDOT = 5138
540058
YDOT = -13975
073544 feet/sec YDOT = -4259
602416 meter/sec
ZDOT = -10146
953606 ZDOT = -3092
791459
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
64663095
00016717 00000-0 10270-3 0 9130
2 25544 51
6427 35
3082 0002039 296
2005 63
8938 15
54181359 26766
Satellite: ISS
Catalog Number: 25544
Epoch time: 18092
64663095 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 35
3082 deg
Eccentricity:
0002039
Arg of perigee: 296
2005 deg
Mean anomaly: 63
8938 deg
Mean motion: 15
54181359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2676
Checksum: 320
Coasting Arc #15 (Orbit 2679)
---------------------------------------
Vector Time (GMT): 2018/092/20:30:37
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1720409
54 A = 6777477
68 meter
Y = 3858343
92 meter E =
0001081
Z = 5298985
51 I = 51
83128
XDOT = -6623
440484 Wp = 117
00285
YDOT = -3815
715402 meter/sec RA = 33
64466 deg
ZDOT = 627
337919 TA = 327
02196
MA = 327
02870
Ha = 220
489 n
mi
Hp = 215
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5644388
27 X = -1789166
66
Y = 12658608
65 feet Y = 3838721
23 meter
Z = 17385123
07 Z = 5290460
87
XDOT = -21730
447781 XDOT = -6583
327154
YDOT = -12518
751318 feet/sec YDOT = -3889
558917 meter/sec
ZDOT = 2058
195271 ZDOT = 595
261076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12759211
07 X = 3889007
53
Y = -5535697
25 feet Y = -1687280
52 meter
Z = 17346486
24 Z = 5287209
01
XDOT = 7343
009803 XDOT = 2238
149388
YDOT = 22933
511914 feet/sec YDOT = 6990
134431 meter/sec
ZDOT = 1915
607306 ZDOT = 583
877107
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
90383445
00016717 00000-0 10270-3 0 9148
2 25544 51
6383 34
0213 0001797 291
7795 68
3167 15
54122458 26809
Satellite: ISS
Catalog Number: 25544
Epoch time: 18092
90383445 = yrday
fracday
Element set: 914
Inclination: 51
6383 deg
RA of node: 34
0213 deg
Eccentricity:
0001797
Arg of perigee: 291
7795 deg
Mean anomaly: 68
3167 deg
Mean motion: 15
54122458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2680
Checksum: 321
Coasting Arc #16 (Orbit 2694)
---------------------------------------
Vector Time (GMT): 2018/093/20:30:37
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3272327
63 A = 6777835
59 meter
Y = -2876439
14 meter E =
0012321
Z = -5202877
52 I = 51
80596
XDOT = 6056
915732 Wp = 98
13631
YDOT = 4497
298451 meter/sec RA = 28
65688 deg
ZDOT = 1324
096242 TA = 184
56495
MA = 184
57620
Ha = 220
400 n
mi
Hp = 215
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10735983
05 X = 3329522
65
Y = -9437136
28 feet Y = -2839526
37 meter
Z = -17069808
12 Z = -5186842
36
XDOT = 19871
770775 XDOT = 5999
743727
YDOT = 14754
916178 feet/sec YDOT = 4564
711496 meter/sec
ZDOT = 4344
147775 ZDOT = 1353
379687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14379628
57 X = -4382910
79
Y = -18875
40 feet Y = -5753
22 meter
Z = -16997798
35 Z = -5180928
94
XDOT = -5254
617191 XDOT = -1601
607320
YDOT = -23114
448573 feet/sec YDOT = -7045
283925 meter/sec
ZDOT = 4474
148122 ZDOT = 1363
720348
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
86833995
00016717 00000-0 10270-3 0 9155
2 25544 51
6393 29
2129 0001644 294
3728 65
7253 15
54175124 26959
Satellite: ISS
Catalog Number: 25544
Epoch time: 18093
86833995 = yrday
fracday
Element set: 915
Inclination: 51
6393 deg
RA of node: 29
2129 deg
Eccentricity:
0001644
Arg of perigee: 294
3728 deg
Mean anomaly: 65
7253 deg
Mean motion: 15
54175124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2695
Checksum: 338
Coasting Arc #17 (Orbit 2699)
---------------------------------------
Vector Time (GMT): 2018/094/03:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1292489
38 A = 6777271
29 meter
Y = 4023724
22 meter E =
0000877
Z = 5297488
03 I = 51
79864
XDOT = -7004
667146 Wp = 111
71456
YDOT = -3062
337813 meter/sec RA = 27
25343 deg
ZDOT = 616
600500 TA = 332
41125
MA = 332
41590
Ha = 220
328 n
mi
Hp = 215
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4240450
72 X = -1363120
36
Y = 13201194
96 feet Y = 4008876
22 meter
Z = 17380210
08 Z = 5291037
63
XDOT = -22981
191423 XDOT = -6972
897799
YDOT = -10047
040069 feet/sec YDOT = -3140
491139 meter/sec
ZDOT = 2022
967519 ZDOT = 582
651324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9639400
38 X = -2938089
24
Y = -10017803
91 feet Y = -3053426
63 meter
Z = 17350799
36 Z = 5288523
64
XDOT = 18893
613686 XDOT = 5758
773452
YDOT = -14935
505777 feet/sec YDOT = -4552
342161 meter/sec
ZDOT = 1871
926107 ZDOT = 570
563077
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
18983946
00016717 00000-0 10270-3 0 9164
2 25544 51
6419 27
6130 0001976 294
1472 65
9474 15
54191198 27007
Satellite: ISS
Catalog Number: 25544
Epoch time: 18094
18983946 = yrday
fracday
Element set: 916
Inclination: 51
6419 deg
RA of node: 27
6130 deg
Eccentricity:
0001976
Arg of perigee: 294
1472 deg
Mean anomaly: 65
9474 deg
Mean motion: 15
54191198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2700
Checksum: 335
Coasting Arc #18 (Orbit 2704)
---------------------------------------
Vector Time (GMT): 2018/094/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926561
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1170585
48 A = 6779536
67 meter
Y = 4701708
07 meter E =
0005650
Z = 4738616
40 I = 51
79567
XDOT = -7089
470657 Wp = 115
79668
YDOT = -1009
966038 meter/sec RA = 25
69006 deg
ZDOT = 2748
474193 TA = 307
04873
MA = 307
10038
Ha = 220
286 n
mi
Hp = 215
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3840503
55 X = 1094904
77
Y = 15425551
40 feet Y = 4714375
55 meter
Z = 15546641
72 Z = 4744118
59
XDOT = -23259
418166 XDOT = -7091
000807
YDOT = -3313
536869 feet/sec YDOT = -1089
253731 meter/sec
ZDOT = 9017
303782 ZDOT = 2714
032027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2882097
63 X = 878463
36
Y = 15609267
08 feet Y = 4757704
60 meter
Z = 15570467
79 Z = 4745878
58
XDOT = -21962
271978 XDOT = -6694
100499
YDOT = -4802
756279 feet/sec YDOT = -1463
880114 meter/sec
ZDOT = 8863
747661 ZDOT = 2701
670287
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
51134125
00016717 00000-0 10270-3 0 9179
2 25544 51
6404 26
0113 0002033 302
3000 57
7956 15
54207576 27056
Satellite: ISS
Catalog Number: 25544
Epoch time: 18094
51134125 = yrday
fracday
Element set: 917
Inclination: 51
6404 deg
RA of node: 26
0113 deg
Eccentricity:
0002033
Arg of perigee: 302
3000 deg
Mean anomaly: 57
7956 deg
Mean motion: 15
54207576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2705
Checksum: 269
Coasting Arc #19 (Orbit 2719)
---------------------------------------
Vector Time (GMT): 2018/095/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926561
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 541406
35 A = 6777446
69 meter
Y = -4237780
45 meter E =
0013174
Z = -5272815
77 I = 51
75807
XDOT = 7332
291291 Wp = 76
94120
YDOT = 2030
912688 meter/sec RA = 20
70181 deg
ZDOT = -878
325159 TA = 184
65662
MA = 184
66889
Ha = 220
417 n
mi
Hp = 215
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1776267
55 X = 614366
90
Y = -13903479
16 feet Y = -4231318
43 meter
Z = -17299264
33 Z = -5270008
32
XDOT = 24056
073788 XDOT = 7313
302597
YDOT = 6663
099370 feet/sec YDOT = 2112
801191 meter/sec
ZDOT = -2881
644222 ZDOT = -842
753378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2416308
09 X = 736490
71
Y = -13823153
63 feet Y = -4213297
23 meter
Z = -17286071
98 Z = -5268794
74
XDOT = 22796
658693 XDOT = 6948
421570
YDOT = 7394
649300 feet/sec YDOT = 2253
889107 meter/sec
ZDOT = -2723
215982 ZDOT = -830
036231
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
47584506
00016717 00000-0 10270-3 0 9188
2 25544 51
6403 21
2029 0002010 308
6597 51
4376 15
54176024 27200
Satellite: ISS
Catalog Number: 25544
Epoch time: 18095
47584506 = yrday
fracday
Element set: 918
Inclination: 51
6403 deg
RA of node: 21
2029 deg
Eccentricity:
0002010
Arg of perigee: 308
6597 deg
Mean anomaly: 51
4376 deg
Mean motion: 15
54176024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2720
Checksum: 292
Coasting Arc #20 (Orbit 2735)
---------------------------------------
Vector Time (GMT): 2018/096/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926561
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2294481
07 A = 6777589
42 meter
Y = 3643616
23 meter E =
0003942
Z = 5233200
48 I = 51
72809
XDOT = -7031
067838 Wp = 24
34890
YDOT = -2865
745773 meter/sec RA = 15
70947 deg
ZDOT = -1083
675894 TA = 76
04134
MA = 75
99750
Ha = 220
499 n
mi
Hp = 215
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7527825
02 X = -2360474
73
Y = 11954121
48 feet Y = 3617589
03 meter
Z = 17169292
92 Z = 5221894
15
XDOT = -23067
807867 XDOT = -6993
235767
YDOT = -9402
053062 feet/sec YDOT = -2944
160534 meter/sec
ZDOT = -3555
367107 ZDOT = -1117
738558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7887129
01 X = -2403996
92
Y = 11794575
57 feet Y = 3594986
63 meter
Z = 17118264
30 Z = 5217646
96
XDOT = -21983
993952 XDOT = -6700
721356
YDOT = -9302
629464 feet/sec YDOT = -2835
441461 meter/sec
ZDOT = -3706
919787 ZDOT = -1129
869151
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
50464319
00016717 00000-0 10270-3 0 9193
2 25544 51
6409 16
0748 0002135 312
4251 47
6721 15
54190828 27360
Satellite: ISS
Catalog Number: 25544
Epoch time: 18096
50464319 = yrday
fracday
Element set: 919
Inclination: 51
6409 deg
RA of node: 16
0748 deg
Eccentricity:
0002135
Arg of perigee: 312
4251 deg
Mean anomaly: 47
6721 deg
Mean motion: 15
54190828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2736
Checksum: 307
Coasting Arc #21 (Orbit 2750)
---------------------------------------
Vector Time (GMT): 2018/097/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926561
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3924640
51 A = 6780074
09 meter
Y = -2997280
21 meter E =
0008563
Z = -4653865
05 I = 51
70430
XDOT = 6147
857547 Wp = 102
68099
YDOT = 3513
670289 meter/sec RA = 10
71725 deg
ZDOT = 2924
291941 TA = 196
40647
MA = 196
43420
Ha = 220
524 n
mi
Hp = 215
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12876117
15 X = 3980471
34
Y = -9833596
49 feet Y = -2953080
24 meter
Z = -15268586
12 Z = -4634664
69
XDOT = 20170
136309 XDOT = 6093
905084
YDOT = 11527
789661 feet/sec YDOT = 3582
118337 meter/sec
ZDOT = 9594
133665 ZDOT = 2954
025005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13011211
26 X = 3965817
19
Y = -9789065
32 feet Y = -2983707
11 meter
Z = -15182434
47 Z = -4627606
03
XDOT = 19351
809123 XDOT = 5898
431421
YDOT = 10650
424208 feet/sec YDOT = 3246
249299 meter/sec
ZDOT = 9726
254960 ZDOT = 2964
562512
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
46913782
00016717 00000-0 10270-3 0 9204
2 25544 51
6408 11
2659 0002077 318
7062 41
3934 15
54192657 27517
Satellite: ISS
Catalog Number: 25544
Epoch time: 18097
46913782 = yrday
fracday
Element set: 920
Inclination: 51
6408 deg
RA of node: 11
2659 deg
Eccentricity:
0002077
Arg of perigee: 318
7062 deg
Mean anomaly: 41
3934 deg
Mean motion: 15
54192657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2751
Checksum: 315
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