[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 26th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24007 8258 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
331/13:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
9
337/11:31:53
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
0
337/17:35:42
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
1
337/18:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
0
338/16:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
0
341/20:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
1
344/22:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 2374)
---------------------------------------
Vector Time (GMT): 2018/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4523990
55 A = 6782273
82 meter
Y = 2913514
85 meter E =
0012945
Z = -4141616
92 I = 51
27463
XDOT = -865
374321 Wp = 75
45231
YDOT = -6632
590811 meter/sec RA = 289
10694 deg
ZDOT = -3727
201882 TA = 155
97433
MA = 155
91388
Ha = 223
072 n
mi
Hp = 212
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14842488
68 X = -4536116
04
Y = 9558775
75 feet Y = 2862857
11 meter
Z = -13587982
01 Z = -4163622
28
XDOT = -2839
154597 XDOT = -773
037534
YDOT = -21760
468541 feet/sec YDOT = -6641
751325 meter/sec
ZDOT = -12228
352630 ZDOT = -3731
182086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2272034
63 X = -692516
16
Y = -17429832
33 feet Y = -5312612
89 meter
Z = -13687283
25 Z = -4171883
94
XDOT = 19556
146243 XDOT = 5960
713375
YDOT = 7049
880945 feet/sec YDOT = 2148
803712 meter/sec
ZDOT = -12245
366584 ZDOT = -3732
387735
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 18330
52298350
00016717 00000-0 10270-3 0 9006
2 25544 51
6387 289
7477 0005275 83
3270 276
8483 15
54022861 23757
Satellite: ISS
Catalog Number: 25544
Epoch time: 18330
52298350 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 289
7477 deg
Eccentricity:
0005275
Arg of perigee: 83
3270 deg
Mean anomaly: 276
8483 deg
Mean motion: 15
54022861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2375
Checksum: 327
Coasting Arc #2 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2018/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4428639
48 A = 6778988
60 meter
Y = -1331640
11 meter E =
0010626
Z = 4948847
14 I = 51
25470
XDOT = -123
637145 Wp = 107
02331
YDOT = 7383
291469 meter/sec RA = 284
09041 deg
ZDOT = 2090
553965 TA = 322
49755
MA = 322
57164
Ha = 222
798 n
mi
Hp = 212
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14529657
10 X = 4419162
06
Y = -4368898
00 feet Y = -1282169
47 meter
Z = 16236375
13 Z = 4970336
93
XDOT = -405
633678 XDOT = -216
344862
YDOT = 24223
397209 feet/sec YDOT = 7381
390304 meter/sec
ZDOT = 6858
772851 ZDOT = 2089
728937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2013038
60 X = -613574
17
Y = 14932981
29 feet Y = 4551572
70 meter
Z = 16333151
19 Z = 4978344
48
XDOT = -20761
755352 XDOT = -6328
183031
YDOT = -10319
775482 feet/sec YDOT = -3145
467567 meter/sec
ZDOT = 6854
105312 ZDOT = 2089
131299
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 18331
55188484
00016717 00000-0 10270-3 0 9017
2 25544 51
6393 284
6206 0005030 87
7527 272
4201 15
54060966 23916
Satellite: ISS
Catalog Number: 25544
Epoch time: 18331
55188484 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 284
6206 deg
Eccentricity:
0005030
Arg of perigee: 87
7527 deg
Mean anomaly: 272
4201 deg
Mean motion: 15
54060966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 307
Coasting Arc #3 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2018/331/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1691114
80 A = 6789617
31 meter
Y = -6568683
49 meter E =
0016557
Z = 92126
60 I = 51
28957
XDOT = 4622
108486 Wp = 58
14913
YDOT = 1284
888240 meter/sec RA = 283
81363 deg
ZDOT = 5983
170337 TA = 302
84812
MA = 303
00741
Ha = 223
035 n
mi
Hp = 212
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5548276
91 X = 1763994
46
Y = -21550798
87 feet Y = -6549364
79 meter
Z = 302252
62 Z = 100517
87
XDOT = 15164
397919 XDOT = 4578
333705
YDOT = 4215
512600 feet/sec YDOT = 1336
330517 meter/sec
ZDOT = 19629
823941 ZDOT = 6005
516894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20889910
81 X = 6367244
82
Y = 7668580
63 feet Y = 2337383
38 meter
Z = 340826
08 Z = 103883
79
XDOT = -5136
610558 XDOT = -1565
638898
YDOT = 13014
218003 feet/sec YDOT = 3966
733647 meter/sec
ZDOT = 19730
111910 ZDOT = 6013
738110
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 18331
61619256
00016717 00000-0 10270-3 0 9021
2 25544 51
6394 284
3000 0005157 87
5754 272
5989 15
54028524 23925
Satellite: ISS
Catalog Number: 25544
Epoch time: 18331
61619256 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 284
3000 deg
Eccentricity:
0005157
Arg of perigee: 87
5754 deg
Mean anomaly: 272
5989 deg
Mean motion: 15
54028524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 320
Coasting Arc #4 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2018/332/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2384996
67 A = 6788243
68 meter
Y = 6101566
93 meter E =
0011352
Z = -1772908
27 I = 51
27914
XDOT = -4073
812118 Wp = 120
36408
YDOT = -3220
780030 meter/sec RA = 278
81828 deg
ZDOT = -5636
934227 TA = 79
19766
MA = 79
06990
Ha = 223
023 n
mi
Hp = 212
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7824792
23 X = -2444436
95
Y = 20018264
19 feet Y = 6074564
02 meter
Z = -5816628
17 Z = -1784637
69
XDOT = -13365
525322 XDOT = -4010
112317
YDOT = -10566
863616 feet/sec YDOT = -3265
979619 meter/sec
ZDOT = -18493
878699 ZDOT = -5656
569013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19305936
72 X = -5884449
51
Y = -9413489
59 feet Y = -2869231
63 meter
Z = -5870132
81 Z = -1789216
48
XDOT = 10939
970417 XDOT = 3334
502983
YDOT = -10915
539117 feet/sec YDOT = -3327
056323 meter/sec
ZDOT = -18581
737927 ZDOT = -5663
713720
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 18332
58078431
00016717 00000-0 10270-3 0 9033
2 25544 51
6404 279
4919 0005185 89
6953 270
4794 15
54033236 24070
Satellite: ISS
Catalog Number: 25544
Epoch time: 18332
58078431 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 279
4919 deg
Eccentricity:
0005185
Arg of perigee: 89
6953 deg
Mean anomaly: 270
4794 deg
Mean motion: 15
54033236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 327
Coasting Arc #5 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2018/333/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2937430
98 A = 6785144
27 meter
Y = -5188241
33 meter E =
0017946
Z = 3223110
56 I = 51
26386
XDOT = 3481
364300 Wp = 88
88604
YDOT = 4929
267493 meter/sec RA = 273
81696 deg
ZDOT = 4739
267936 TA = 308
67909
MA = 308
83950
Ha = 223
000 n
mi
Hp = 212
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9637240
75 X = 2979572
80
Y = -17021789
13 feet Y = -5155157
49 meter
Z = 10574509
70 Z = 3237481
70
XDOT = 11421
798885 XDOT = 3402
964155
YDOT = 16172
137444 feet/sec YDOT = 4967
759899 meter/sec
ZDOT = 15548
779319 ZDOT = 4755
989121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16357999
32 X = 4985918
19
Y = 10660642
24 feet Y = 3249363
75 meter
Z = 10639761
99 Z = 3242999
45
XDOT = -16102
351258 XDOT = -4907
996663
YDOT = 9041
693724 feet/sec YDOT = 2755
908247 meter/sec
ZDOT = 15623
339973 ZDOT = 4761
994024
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 18333
60967882
00016717 00000-0 10270-3 0 9045
2 25544 51
6395 274
3643 0005224 93
5209 266
6541 15
54034147 24236
Satellite: ISS
Catalog Number: 25544
Epoch time: 18333
60967882 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 274
3643 deg
Eccentricity:
0005224
Arg of perigee: 93
5209 deg
Mean anomaly: 266
6541 deg
Mean motion: 15
54034147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 315
Coasting Arc #6 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/334/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3447097
10 A = 6781276
95 meter
Y = 3861222
66 meter E =
0013901
Z = -4394518
92 I = 51
25079
XDOT = -2808
135536 Wp = 79
24429
YDOT = -6294
775806 meter/sec RA = 268
80499 deg
ZDOT = -3334
625693 TA = 156
84112
MA = 156
77841
Ha = 222
986 n
mi
Hp = 212
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11309373
70 X = -3468671
79
Y = 12668053
35 feet Y = 3822554
37 meter
Z = -14417712
98 Z = -4411316
07
XDOT = -9213
043096 XDOT = -2721
338935
YDOT = -20652
151595 feet/sec YDOT = -6325
692890 meter/sec
ZDOT = -10940
373009 ZDOT = -3348
056155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12110476
78 X = -3691273
32
Y = -11811900
82 feet Y = -3600267
37 meter
Z = -14493698
91 Z = -4417679
43
XDOT = 20209
072302 XDOT = 6159
725238
YDOT = -7248
395054 feet/sec YDOT = -2209
310813 meter/sec
ZDOT = -10999
988717 ZDOT = -3352
796561
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 18334
57426442
00016717 00000-0 10270-3 0 9055
2 25544 51
6402 269
5565 0005194 96
6361 263
5383 15
54059056 24385
Satellite: ISS
Catalog Number: 25544
Epoch time: 18334
57426442 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 269
5565 deg
Eccentricity:
0005194
Arg of perigee: 96
6361 deg
Mean anomaly: 263
5383 deg
Mean motion: 15
54059056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 324
Coasting Arc #7 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2018/335/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3858377
21 A = 6778380
02 meter
Y = -2267818
16 meter E =
0009853
Z = 5083888
84 I = 51
24317
XDOT = 2092
244693 Wp = 113
20415
YDOT = 7203
848689 meter/sec RA = 263
78389 deg
ZDOT = 1619
269351 TA = 321
06178
MA = 321
13270
Ha = 222
781 n
mi
Hp = 212
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12658717
88 X = 3858754
74
Y = -7440348
29 feet Y = -2224669
15 meter
Z = 16679425
33 Z = 5102632
52
XDOT = 6864
319858 XDOT = 2003
668111
YDOT = 23634
674176 feet/sec YDOT = 7226
750311 meter/sec
ZDOT = 5312
563487 ZDOT = 1629
217931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7045000
57 X = 2147316
17
Y = 12772727
55 feet Y = 3893127
36 meter
Z = 16763965
77 Z = 5109656
77
XDOT = -22904
747006 XDOT = -6981
366888
YDOT = 5576
152442 feet/sec YDOT = 1699
611264 meter/sec
ZDOT = 5356
433434 ZDOT = 1632
640911
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 18335
60315057
00016717 00000-0 10270-3 0 9060
2 25544 51
6403 264
4282 0005054 101
5430 258
6290 15
54076416 24543
Satellite: ISS
Catalog Number: 25544
Epoch time: 18335
60315057 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 264
4282 deg
Eccentricity:
0005054
Arg of perigee: 101
5430 deg
Mean anomaly: 258
6290 deg
Mean motion: 15
54076416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 287
Coasting Arc #8 (Orbit 2468)
---------------------------------------
Vector Time (GMT): 2018/336/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4226783
45 A = 6777567
86 meter
Y = 516842
81 meter E =
0019930
Z = -5290153
59 I = 51
24578
XDOT = -1271
516275 Wp = 95
04823
YDOT = -7542
135863 meter/sec RA = 258
75715 deg
ZDOT = 278
258562 TA = 177
62863
MA = 177
61917
Ha = 222
963 n
mi
Hp = 212
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13867399
76 X = -4206551
67
Y = 1695678
53 feet Y = 469689
28 meter
Z = -17356146
96 Z = -5310636
96
XDOT = -4171
641322 XDOT = -1188
435151
YDOT = -24744
540233 feet/sec YDOT = -7555
890316 meter/sec
ZDOT = 912
921790 ZDOT = 272
283435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1502734
87 X = -458033
59
Y = -13773687
66 feet Y = -4198220
00 meter
Z = -17448302
36 Z = -5318242
56
XDOT = 23795
853876 XDOT = 7252
976261
YDOT = -3723
090595 feet/sec YDOT = -1134
798013 meter/sec
ZDOT = 886
940162 ZDOT = 270
339361
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 18336
56772958
00016717 00000-0 10270-3 0 9074
2 25544 51
6411 259
6201 0005166 103
2459 256
9270 15
54065961 24691
Satellite: ISS
Catalog Number: 25544
Epoch time: 18336
56772958 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 259
6201 deg
Eccentricity:
0005166
Arg of perigee: 103
2459 deg
Mean anomaly: 256
9270 deg
Mean motion: 15
54065961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2469
Checksum: 329
Coasting Arc #9 (Orbit 2483)
---------------------------------------
Vector Time (GMT): 2018/337/11:31:53
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3200998
43 A = 6778866
65 meter
Y = -3312598
93 meter E =
0010964
Z = 4966287
04 I = 51
25570
XDOT = 3546
167960 Wp = 116
61259
YDOT = 6493
367377 meter/sec RA = 254
12469 deg
ZDOT = 2037
194670 TA = 313
44251
MA = 313
53368
Ha = 222
741 n
mi
Hp = 212
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10501963
36 X = 3213678
95
Y = -10868106
72 feet Y = -3276732
45 meter
Z = 16293592
67 Z = 4981867
29
XDOT = 11634
409318 XDOT = 3463
397976
YDOT = 21303
698745 feet/sec YDOT = 6532
560208 meter/sec
ZDOT = 6683
709548 ZDOT = 2054
220246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5294163
53 X = 1613661
04
Y = 14074038
14 feet Y = 4289766
83 meter
Z = 16364028
32 Z = 4987755
83
XDOT = -23195
566129 XDOT = -7070
008556
YDOT = 834
387262 feet/sec YDOT = 254
321238 meter/sec
ZDOT = 6759
511146 ZDOT = 2060
298997
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 18337
53230432
00016717 00000-0 10270-3 0 9089
2 25544 51
6395 254
8123 0005004 108
4185 251
7512 15
54089991 24844
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
53230432 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 254
8123 deg
Eccentricity:
0005004
Arg of perigee: 108
4185 deg
Mean anomaly: 251
7512 deg
Mean motion: 15
54089991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2484
Checksum: 307
Coasting Arc #10 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/337/17:35:42
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1411066
74 A = 6783662
52 meter
Y = -5499026
34 meter E =
0016444
Z = 3701572
63 I = 51
27211
XDOT = 4855
726808 Wp = 99
85056
YDOT = 4131
902547 meter/sec RA = 252
86620 deg
ZDOT = 4268
281193 TA = 304
58494
MA = 304
73997
Ha = 222
779 n
mi
Hp = 213
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4629484
05 X = 1454472
93
Y = -18041425
01 feet Y = -5483004
29 meter
Z = 12144267
17 Z = 3708532
39
XDOT = 15930
862231 XDOT = 4788
428430
YDOT = 13556
110719 feet/sec YDOT = 4185
826167 meter/sec
ZDOT = 14003
547221 ZDOT = 4291
705757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11609739
34 X = 3538648
55
Y = -14538315
78 feet Y = -4431278
65 meter
Z = 12176193
61 Z = 3711303
81
XDOT = 7742
602416 XDOT = 2359
945216
YDOT = 18051
143403 feet/sec YDOT = 5501
988509 meter/sec
ZDOT = 14108
396194 ZDOT = 4300
239160
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 18337
78952320
00016717 00000-0 10270-3 0 9094
2 25544 51
6379 253
5284 0004843 110
1376 250
0298 15
54067702 24885
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
78952320 = yrday
fracday
Element set: 909
Inclination: 51
6379 deg
RA of node: 253
5284 deg
Eccentricity:
0004843
Arg of perigee: 110
1376 deg
Mean anomaly: 250
0298 deg
Mean motion: 15
54067702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 323
Coasting Arc #11 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/337/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4169202
18 A = 6784325
44 meter
Y = 4071956
53 meter E =
0016847
Z = 3457328
24 I = 51
27488
XDOT = -1972
526875 Wp = 94
76283
YDOT = 5876
361130 meter/sec RA = 252
72948 deg
ZDOT = -4524
652322 TA = 44
39350
MA = 44
25856
Ha = 222
705 n
mi
Hp = 213
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13678484
85 X = 4106564
41
Y = 13359437
42 feet Y = 4118229
05 meter
Z = 11342940
41 Z = 3477429
17
XDOT = -6471
544864 XDOT = -2016
112650
YDOT = 19279
400034 feet/sec YDOT = 5854
059477 meter/sec
ZDOT = -14844
659848 ZDOT = -4534
339914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8699731
39 X = 2651678
13
Y = 16965917
98 feet Y = 5171211
80 meter
Z = 11432852
41 Z = 3484733
41
XDOT = -10885
351120 XDOT = -3317
855021
YDOT = 15653
799911 feet/sec YDOT = 4771
278213 meter/sec
ZDOT = -14888
894779 ZDOT = -4538
135129
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 18337
78952271
00016717 00000-0 10270-3 0 9101
2 25544 51
6381 253
5273 0004832 110
0769 250
0904 15
54076913 24887
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
78952271 = yrday
fracday
Element set: 910
Inclination: 51
6381 deg
RA of node: 253
5273 deg
Eccentricity:
0004832
Arg of perigee: 110
0769 deg
Mean anomaly: 250
0904 deg
Mean motion: 15
54076913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 312
Coasting Arc #12 (Orbit 2501)
---------------------------------------
Vector Time (GMT): 2018/338/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2866994
06 A = 6778898
91 meter
Y = 3604070
39 meter E =
0016844
Z = -4989431
40 I = 51
26812
XDOT = -4176
157318 Wp = 84
96040
YDOT = -6094
323705 meter/sec RA = 248
16359 deg
ZDOT = -2006
926013 TA = 165
42726
MA = 165
37864
Ha = 222
785 n
mi
Hp = 212
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9406148
50 X = -2882846
25
Y = 11824377
94 feet Y = 3571921
36 meter
Z = -16369525
59 Z = -5003396
78
XDOT = -13701
303537 XDOT = -4097
949745
YDOT = -19994
500343 feet/sec YDOT = -6140
586983 meter/sec
ZDOT = -6584
402931 ZDOT = -2027
023134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14968490
63 X = -4562395
94
Y = 1470541
04 feet Y = 448220
91 meter
Z = -16432732
83 Z = -5008696
97
XDOT = 5090
392383 XDOT = 1551
551598
YDOT = -22604
153690 feet/sec YDOT = -6889
746045 meter/sec
ZDOT = -6674
078301 ZDOT = -2034
259066
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 18338
68979068
00016717 00000-0 10270-3 0 9115
2 25544 51
6397 249
0419 0004825 111
6538 248
5129 15
54069321 25022
Satellite: ISS
Catalog Number: 25544
Epoch time: 18338
68979068 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 249
0419 deg
Eccentricity:
0004825
Arg of perigee: 111
6538 deg
Mean anomaly: 248
5129 deg
Mean motion: 15
54069321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2502
Checksum: 331
Coasting Arc #13 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2018/339/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3708727
44 A = 6777578
69 meter
Y = -2052053
25 meter E =
0007333
Z = 5282706
78 I = 51
27688
XDOT = 3563
300985 Wp = 109
40147
YDOT = 6795
361221 meter/sec RA = 243
13986 deg
ZDOT = 135
472132 TA = 339
28714
MA = 339
31684
Ha = 222
725 n
mi
Hp = 213
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12167740
94 X = 3705737
39
Y = -6732458
18 feet Y = -2010596
85 meter
Z = 17331715
14 Z = 5300715
36
XDOT = 11690
620030 XDOT = 3486
390459
YDOT = 22294
492195 feet/sec YDOT = 6834
778484 meter/sec
ZDOT = 444
462376 ZDOT = 152
595486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13266811
48 X = 4043724
14
Y = 3814421
31 feet Y = 1162635
62 meter
Z = 17412930
99 Z = 5307461
37
XDOT = -7316
380255 XDOT = -2230
032702
YDOT = 23031
828734 feet/sec YDOT = 7020
101398 meter/sec
ZDOT = 520
701204 ZDOT = 158
709727
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 18339
71866529
00016717 00000-0 10270-3 0 9128
2 25544 51
6396 243
9134 0004965 115
0499 245
1169 15
54050112 25189
Satellite: ISS
Catalog Number: 25544
Epoch time: 18339
71866529 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 243
9134 deg
Eccentricity:
0004965
Arg of perigee: 115
0499 deg
Mean anomaly: 245
1169 deg
Mean motion: 15
54050112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2518
Checksum: 321
Coasting Arc #14 (Orbit 2532)
---------------------------------------
Vector Time (GMT): 2018/340/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4501174
14 A = 6778517
74 meter
Y = 447880
25 meter E =
0018100
Z = -5064938
90 I = 51
29436
XDOT = -2669
059506 Wp = 107
76671
YDOT = -6955
661009 meter/sec RA = 238
11587 deg
ZDOT = 1756
686243 TA = 179
33740
MA = 179
33500
Ha = 222
777 n
mi
Hp = 212
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14767631
69 X = -4481244
75
Y = 1469423
39 feet Y = 397656
96 meter
Z = -16617253
60 Z = -5086755
92
XDOT = -8756
756911 XDOT = -2599
614174
YDOT = -22820
410134 feet/sec YDOT = -6985
120178 meter/sec
ZDOT = 5763
406308 ZDOT = 1743
888620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11524741
37 X = -3512741
17
Y = -9173339
60 feet Y = -2796033
91 meter
Z = -16715425
36 Z = -5094861
65
XDOT = 8950
474281 XDOT = 2728
104561
YDOT = -21644
492173 feet/sec YDOT = -6597
241214 meter/sec
ZDOT = 5706
623770 ZDOT = 1739
378925
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 18340
68323254
00016717 00000-0 10270-3 0 9130
2 25544 51
6378 239
1050 0004951 119
5264 240
6383 15
54075743 25339
Satellite: ISS
Catalog Number: 25544
Epoch time: 18340
68323254 = yrday
fracday
Element set: 913
Inclination: 51
6378 deg
RA of node: 239
1050 deg
Eccentricity:
0004951
Arg of perigee: 119
5264 deg
Mean anomaly: 240
6383 deg
Mean motion: 15
54075743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2533
Checksum: 303
Coasting Arc #15 (Orbit 2548)
---------------------------------------
Vector Time (GMT): 2018/341/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5120237
84 A = 6781460
96 meter
Y = 1085736
32 meter E =
0013103
Z = 4300724
90 I = 51
32348
XDOT = 1519
767772 Wp = 88
64017
YDOT = 6667
773255 meter/sec RA = 233
09942 deg
ZDOT = -3483
158807 TA = 36
95013
MA = 36
85994
Ha = 222
507 n
mi
Hp = 213
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16798680
59 X = 5086825
38
Y = 3562127
02 feet Y = 1142807
04 meter
Z = 14109989
84 Z = 4325516
53
XDOT = 4986
114739 XDOT = 1462
013467
YDOT = 21875
896507 feet/sec YDOT = 6684
445848 meter/sec
ZDOT = -11427
686376 ZDOT = -3475
915689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9724612
98 X = 2964062
04
Y = 14041380
51 feet Y = 4279812
78 meter
Z = 14221384
15 Z = 4334677
89
XDOT = -10278
508299 XDOT = -3132
889329
YDOT = 18691
856679 feet/sec YDOT = 5697
277916 meter/sec
ZDOT = -11395
840440 ZDOT = -3473
452166
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 18341
71210198
00016717 00000-0 10270-3 0 9148
2 25544 51
6384 233
9764 0004745 124
1262 236
0341 15
54088503 25499
Satellite: ISS
Catalog Number: 25544
Epoch time: 18341
71210198 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 233
9764 deg
Eccentricity:
0004745
Arg of perigee: 124
1262 deg
Mean anomaly: 236
0341 deg
Mean motion: 15
54088503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 301
Coasting Arc #16 (Orbit 2551)
---------------------------------------
Vector Time (GMT): 2018/341/20:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2966847
47 A = 6788406
20 meter
Y = -5892795
80 meter E =
0016840
Z = 1575580
53 I = 51
35145
XDOT = 5017
276636 Wp = 79
41277
YDOT = -984
720936 meter/sec RA = 232
26645 deg
ZDOT = 5715
588935 TA = 297
88992
MA = 298
06038
Ha = 222
807 n
mi
Hp = 213
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9733751
55 X = -2908385
50
Y = -19333319
56 feet Y = -5925646
46 meter
Z = 5169227
45 Z = 1561309
72
XDOT = 16460
881353 XDOT = 5000
151532
YDOT = -3230
711732 feet/sec YDOT = -928
710711 meter/sec
ZDOT = 18751
932200 ZDOT = 5739
919696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15639668
60 X = -4766970
99
Y = -14985888
31 feet Y = -4567698
76 meter
Z = 5105682
57 Z = 1556212
05
XDOT = 13239
981250 XDOT = 4035
546285
YDOT = -7335
929940 feet/sec YDOT = -2235
991446 meter/sec
ZDOT = 18861
483564 ZDOT = 5748
980190
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 18341
90501628
00016717 00000-0 10270-3 0 9151
2 25544 51
6398 233
0122 0005306 127
8753 232
2881 15
54094278 25529
Satellite: ISS
Catalog Number: 25544
Epoch time: 18341
90501628 = yrday
fracday
Element set: 915
Inclination: 51
6398 deg
RA of node: 233
0122 deg
Eccentricity:
0005306
Arg of perigee: 127
8753 deg
Mean anomaly: 232
2881 deg
Mean motion: 15
54094278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2552
Checksum: 304
Coasting Arc #17 (Orbit 2566)
---------------------------------------
Vector Time (GMT): 2018/342/20:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1894484
29 A = 6785384
76 meter
Y = 5722722
35 meter E =
0009573
Z = -3116643
34 I = 51
36204
XDOT = -5898
609037 Wp = 119
02525
YDOT = -677
495617 meter/sec RA = 227
27150 deg
ZDOT = -4845
393281 TA = 96
98753
MA = 96
87864
Ha = 222
798 n
mi
Hp = 213
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6215499
63 X = 1845489
53
Y = 18775335
80 feet Y = 5743634
24 meter
Z = -10225207
82 Z = -3107558
79
XDOT = -19352
391855 XDOT = -5867
058153
YDOT = -2222
754650 feet/sec YDOT = -743
280929 meter/sec
ZDOT = -15896
959582 ZDOT = -4873
970355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12434612
88 X = 3790070
01
Y = 15406088
40 feet Y = 4695775
75 meter
Z = -10184958
89 Z = -3104375
47
XDOT = -17690
432519 XDOT = -5392
043832
YDOT = 3718
472869 feet/sec YDOT = 1133
390530 meter/sec
ZDOT = -16025
447532 ZDOT = -4884
556408
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 18342
86957972
00016717 00000-0 10270-3 0 9165
2 25544 51
6395 228
2045 0005286 130
2655 229
8960 15
54078976 25675
Satellite: ISS
Catalog Number: 25544
Epoch time: 18342
86957972 = yrday
fracday
Element set: 916
Inclination: 51
6395 deg
RA of node: 228
2045 deg
Eccentricity:
0005286
Arg of perigee: 130
2655 deg
Mean anomaly: 229
8960 deg
Mean motion: 15
54078976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2567
Checksum: 354
Coasting Arc #18 (Orbit 2582)
---------------------------------------
Vector Time (GMT): 2018/343/20:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -627517
60 A = 6781578
65 meter
Y = -5206131
17 meter E =
0014711
Z = 4293046
82 I = 51
37258
XDOT = 6489
466462 Wp = 116
98519
YDOT = 2117
897117 meter/sec RA = 222
26866 deg
ZDOT = 3501
085081 TA = 297
19621
MA = 297
34607
Ha = 222
696 n
mi
Hp = 213
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2058784
78 X = -590107
98
Y = -17080482
83 feet Y = -5212939
88 meter
Z = 14084799
28 Z = 4290088
75
XDOT = 21290
900465 XDOT = 6448
294746
YDOT = 6948
481356 feet/sec YDOT = 2190
236192 meter/sec
ZDOT = 11486
499608 ZDOT = 3532
509049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8233186
80 X = -2509475
34
Y = -15118042
97 feet Y = -4607979
50 meter
Z = 14072045
74 Z = 4289159
54
XDOT = 21184
757194 XDOT = 6457
113993
YDOT = -665
516481 feet/sec YDOT = -202
849423 meter/sec
ZDOT = 11627
662577 ZDOT = 3544
111553
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 18343
89844403
00016717 00000-0 10270-3 0 9174
2 25544 51
6392 223
0764 0005252 134
6255 225
5327 15
54108704 25831
Satellite: ISS
Catalog Number: 25544
Epoch time: 18343
89844403 = yrday
fracday
Element set: 917
Inclination: 51
6392 deg
RA of node: 223
0764 deg
Eccentricity:
0005252
Arg of perigee: 134
6255 deg
Mean anomaly: 225
5327 deg
Mean motion: 15
54108704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2583
Checksum: 309
Coasting Arc #19 (Orbit 2597)
---------------------------------------
Vector Time (GMT): 2018/344/20:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -854491
03 A = 6778598
98 meter
Y = 4435472
90 meter E =
0016282
Z = -5068164
28 I = 51
38805
XDOT = -6677
065495 Wp = 93
07297
YDOT = -3302
491325 meter/sec RA = 217
25772 deg
ZDOT = -1770
258137 TA = 159
74836
MA = 159
68370
Ha = 222
657 n
mi
Hp = 213
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2803448
28 X = -879407
75
Y = 14552076
44 feet Y = 4425778
67 meter
Z = -16627835
56 Z = -5072375
09
XDOT = -21906
382859 XDOT = -6631
040876
YDOT = -10834
945293 feet/sec YDOT = -3376
901362 meter/sec
ZDOT = -5807
933519 ZDOT = -1802
581633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3049086
94 X = 929361
70
Y = 14480306
64 feet Y = 4413597
46 meter
Z = -16647250
66 Z = -5074082
00
XDOT = -23289
583443 XDOT = -7098
665033
YDOT = -1918
055215 feet/sec YDOT = -584
623230 meter/sec
ZDOT = -5953
043956 ZDOT = -1814
487798
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 18344
86300474
00016717 00000-0 10270-3 0 9188
2 25544 51
6396 218
2691 0005186 138
1287 222
0263 15
54075424 25989
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
86300474 = yrday
fracday
Element set: 918
Inclination: 51
6396 deg
RA of node: 218
2691 deg
Eccentricity:
0005186
Arg of perigee: 138
1287 deg
Mean anomaly: 222
0263 deg
Mean motion: 15
54075424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2598
Checksum: 321
Coasting Arc #20 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2018/344/22:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5981528
78 A = 6787812
04 meter
Y = 2548185
18 meter E =
0018658
Z = 1915799
61 I = 51
42158
XDOT = -430
892675 Wp = 119
02480
YDOT = 5239
150671 meter/sec RA = 216
66865 deg
ZDOT = -5590
835542 TA = 39
77954
MA = 39
64288
Ha = 222
547 n
mi
Hp = 213
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19624438
27 X = 5943283
76
Y = 8360187
61 feet Y = 2614860
73 meter
Z = 6285431
79 Z = 1944763
22
XDOT = -1413
689879 XDOT = -462
288965
YDOT = 17188
814539 feet/sec YDOT = 5234
157239 meter/sec
ZDOT = -18342
636292 ZDOT = -5593
004311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16402530
37 X = 4999491
26
Y = -13576312
71 feet Y = -4138060
11 meter
Z = 6415504
46 Z = 1955445
76
XDOT = 13696
237378 XDOT = 4174
613153
YDOT = 7825
548254 feet/sec YDOT = 2385
227108 meter/sec
ZDOT = -18352
945530 ZDOT = -5593
977798
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 18344
99161187
00016717 00000-0 10270-3 0 9199
2 25544 51
6391 217
6300 0005038 136
5845 223
5705 15
54094330 26000
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
99161187 = yrday
fracday
Element set: 919
Inclination: 51
6391 deg
RA of node: 217
6300 deg
Eccentricity:
0005038
Arg of perigee: 136
5845 deg
Mean anomaly: 223
5705 deg
Mean motion: 15
54094330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 303
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