[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 11th 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) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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
193/18:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 216
0
196/12:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 215
8
196/17:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 215
8
197/12:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
7
199/15:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
4
201/19:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 215
3
203/18:49:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 215
1
206/03:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
8
Coasting Arc #1 (Orbit 230)
---------------------------------------
Vector Time (GMT): 2018/192/14:06:06
722
Vector Time (MET): N/A
Weight (LBS) : 959643
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4081634
28 A = 6777834
85 meter
Y = -1164290
50 meter E =
0001758
Z = 5284926
32 I = 51
24954
XDOT = 1941
298372 Wp = 334
14618
YDOT = 7417
117213 meter/sec RA = 256
15038 deg
ZDOT = 136
297480 TA = 114
55703
MA = 114
53870
Ha = 220
167 n
mi
Hp = 216
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13391188
58 X = 4068679
16
Y = -3819850
74 feet Y = -1118720
17 meter
Z = 17338997
11 Z = 5304721
68
XDOT = 6369
089147 XDOT = 1857
551791
YDOT = 24334
374060 feet/sec YDOT = 7438
357872 meter/sec
ZDOT = 447
170210 ZDOT = 145
525397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12632901
16 X = -3850508
27
Y = -5589310
67 feet Y = -1703621
89 meter
Z = 17427720
07 Z = 5311969
08
XDOT = 10323
130756 XDOT = 3146
490254
YDOT = -21828
327770 feet/sec YDOT = -6653
274304 meter/sec
ZDOT = 487
457071 ZDOT = 148
576915
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 18192
63607842
00016717 00000-0 10270-3 0 9004
2 25544 51
6397 256
8542 0003704 300
6707 59
4080 15
53963757 2315
Satellite: ISS
Catalog Number: 25544
Epoch time: 18192
63607842 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 256
8542 deg
Eccentricity:
0003704
Arg of perigee: 300
6707 deg
Mean anomaly: 59
4080 deg
Mean motion: 15
53963757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 231
Checksum: 313
Coasting Arc #2 (Orbit 245)
---------------------------------------
Vector Time (GMT): 2018/193/14:06:06
722
Vector Time (MET): N/A
Weight (LBS) : 959643
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4478309
30 A = 6778857
53 meter
Y = -524528
49 meter E =
0009884
Z = -5070646
93 I = 51
26215
XDOT = -1072
877577 Wp = 94
78198
YDOT = -7389
053118 meter/sec RA = 251
12643 deg
ZDOT = 1713
988246 TA = 191
87496
MA = 191
89828
Ha = 220
385 n
mi
Hp = 215
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14692615
83 X = -4447480
86
Y = -1720894
00 feet Y = -574434
82 meter
Z = -16635980
75 Z = -5092325
92
XDOT = -3519
939556 XDOT = -998
496951
YDOT = -24242
300256 feet/sec YDOT = -7400
635170 meter/sec
ZDOT = 5623
321018 ZDOT = 1708
956084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10261799
00 X = 3127796
34
Y = 10502156
67 feet Y = 3201057
35 meter
Z = -16732916
01 Z = -5100192
80
XDOT = -11698
920771 XDOT = -3565
831051
YDOT = 20345
556401 feet/sec YDOT = 6201
325591 meter/sec
ZDOT = 5601
782667 ZDOT = 1707
423357
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 18193
60071450
00016717 00000-0 10270-3 0 9013
2 25544 51
6401 252
0472 0003848 304
4303 55
6485 15
53943096 2461
Satellite: ISS
Catalog Number: 25544
Epoch time: 18193
60071450 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 252
0472 deg
Eccentricity:
0003848
Arg of perigee: 304
4303 deg
Mean anomaly: 55
6485 deg
Mean motion: 15
53943096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 246
Checksum: 288
Coasting Arc #3 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2018/193/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 959643
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3313884
58 A = 6778596
83 meter
Y = 2953586
55 meter E =
0011448
Z = -5132923
80 I = 51
26045
XDOT = -3615
090995 Wp = 64
06680
YDOT = -6593
712046 meter/sec RA = 250
21362 deg
ZDOT = -1457
829104 TA = 191
79668
MA = 191
82353
Ha = 220
452 n
mi
Hp = 215
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10872324
74 X = -3321733
44
Y = 9690244
60 feet Y = 2916485
36 meter
Z = -16840301
18 Z = -5149039
85
XDOT = -11860
534760 XDOT = -3534
008356
YDOT = -21632
913537 feet/sec YDOT = -6633
684888 meter/sec
ZDOT = -4782
903884 ZDOT = -1475
193849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4778617
80 X = 1456522
70
Y = -13668425
54 feet Y = -4166136
10 meter
Z = -16912805
35 Z = -5155023
07
XDOT = 19774
270900 XDOT = 6027
197770
YDOT = 12936
130992 feet/sec YDOT = 3942
932726 meter/sec
ZDOT = -4859
735716 ZDOT = -1481
247446
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 18193
79364218
00016717 00000-0 10270-3 0 9021
2 25544 51
6373 251
0854 0003959 306
5435 53
5353 15
53952632 2494
Satellite: ISS
Catalog Number: 25544
Epoch time: 18193
79364218 = yrday
fracday
Element set: 902
Inclination: 51
6373 deg
RA of node: 251
0854 deg
Eccentricity:
0003959
Arg of perigee: 306
5435 deg
Mean anomaly: 53
5353 deg
Mean motion: 15
53952632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 319
Coasting Arc #4 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2018/194/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 959643
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4035512
79 A = 6777886
11 meter
Y = -1353235
49 meter E =
0003418
Z = 5275441
34 I = 51
27049
XDOT = 2912
781173 Wp = 350
75378
YDOT = 7081
581383 meter/sec RA = 245
19051 deg
ZDOT = -408
348342 TA = 103
17954
MA = 103
14140
Ha = 220
397 n
mi
Hp = 216
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13239871
34 X = 4024720
32
Y = -4439748
98 feet Y = -1308168
71 meter
Z = 17307878
41 Z = 5295017
66
XDOT = 9556
368679 XDOT = 2835
360001
YDOT = 23233
534722 feet/sec YDOT = 7113
721283 meter/sec
ZDOT = -1339
725532 ZDOT = -394
386353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9198877
98 X = -2803818
01
Y = 10360493
11 feet Y = 3157878
30 meter
Z = 17395661
69 Z = 5302197
68
XDOT = -19068
226294 XDOT = -5811
995374
YDOT = -14766
253845 feet/sec YDOT = -4500
754172 meter/sec
ZDOT = -1278
157342 ZDOT = -389
582358
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 18194
82258516
00016717 00000-0 10270-3 0 9030
2 25544 51
6374 245
9581 0004017 310
3359 49
7443 15
53961444 2654
Satellite: ISS
Catalog Number: 25544
Epoch time: 18194
82258516 = yrday
fracday
Element set: 903
Inclination: 51
6374 deg
RA of node: 245
9581 deg
Eccentricity:
0004017
Arg of perigee: 310
3359 deg
Mean anomaly: 49
7443 deg
Mean motion: 15
53961444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 318
Coasting Arc #5 (Orbit 279)
---------------------------------------
Vector Time (GMT): 2018/195/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 959643
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4674019
52 A = 6779459
15 meter
Y = -235917
71 meter E =
0008902
Z = -4912937
77 I = 51
29078
XDOT = -1985
334176 Wp = 94
24919
YDOT = -7055
441311 meter/sec RA = 240
16820 deg
ZDOT = 2230
443560 TA = 197
64146
MA = 197
67240
Ha = 220
572 n
mi
Hp = 215
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15334709
72 X = -4647170
13
Y = -774008
23 feet Y = -288035
12 meter
Z = -16118562
22 Z = -4935576
83
XDOT = -6513
563570 XDOT = -1917
124807
YDOT = -23147
773331 feet/sec YDOT = -7077
261570 meter/sec
ZDOT = 7317
728215 ZDOT = 2220
964545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13489119
74 X = 4111483
70
Y = -7107763
06 feet Y = -2166446
18 meter
Z = -16219858
57 Z = -4943812
89
XDOT = 16941
799839 XDOT = 5163
860591
YDOT = 15569
205764 feet/sec YDOT = 4745
493917 meter/sec
ZDOT = 7276
193217 ZDOT = 2217
783693
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 18195
78721528
00016717 00000-0 10270-3 0 9045
2 25544 51
6375 241
1499 0004078 313
6826 46
3989 15
53963975 2809
Satellite: ISS
Catalog Number: 25544
Epoch time: 18195
78721528 = yrday
fracday
Element set: 904
Inclination: 51
6375 deg
RA of node: 241
1499 deg
Eccentricity:
0004078
Arg of perigee: 313
6826 deg
Mean anomaly: 46
3989 deg
Mean motion: 15
53963975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 280
Checksum: 348
Coasting Arc #6 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2018/196/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5065069
97 A = 6786152
25 meter
Y = 3484376
08 meter E =
0010515
Z = 2865376
04 I = 51
32685
XDOT = -1057
631216 Wp = 85
33310
YDOT = 5688
804337 meter/sec RA = 236
42828 deg
ZDOT = -5031
359019 TA = 61
90845
MA = 61
80219
Ha = 220
640 n
mi
Hp = 215
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16617683
64 X = 5011812
11
Y = 11431680
06 feet Y = 3540719
13 meter
Z = 9400840
02 Z = 2889850
81
XDOT = -3469
918689 XDOT = -1096
727265
YDOT = 18664
056224 feet/sec YDOT = 5676
759061 meter/sec
ZDOT = -16507
083397 ZDOT = -5036
590913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1645819
58 X = 501645
81
Y = -20051395
98 feet Y = -6111665
50 meter
Z = 9509958
39 Z = 2898635
32
XDOT = 16387
625228 XDOT = 4994
948170
YDOT = -6521
195495 feet/sec YDOT = -1987
660387 meter/sec
ZDOT = -16531
206868 ZDOT = -5038
711853
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 18196
55891637
00016717 00000-0 10270-3 0 9051
2 25544 51
6382 237
3036 0003921 317
4146 42
6702 15
53996777 2925
Satellite: ISS
Catalog Number: 25544
Epoch time: 18196
55891637 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 237
3036 deg
Eccentricity:
0003921
Arg of perigee: 317
4146 deg
Mean anomaly: 42
6702 deg
Mean motion: 15
53996777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 292
Checksum: 330
Coasting Arc #7 (Orbit 294)
---------------------------------------
Vector Time (GMT): 2018/196/17:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4851004
56 A = 6780187
81 meter
Y = 382037
61 meter E =
0007754
Z = 4720890
40 I = 51
30813
XDOT = 2095
050014 Wp = 31
59536
YDOT = 6864
299151 meter/sec RA = 235
49244 deg
ZDOT = -2699
775784 TA = 85
26287
MA = 85
17432
Ha = 220
628 n
mi
Hp = 215
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15915369
29 X = 4823440
91
Y = 1253404
22 feet Y = 436130
34 meter
Z = 15488485
57 Z = 4744387
45
XDOT = 6873
523667 XDOT = 2031
249610
YDOT = 22520
666507 feet/sec YDOT = 6887
370964 meter/sec
ZDOT = -8857
532099 ZDOT = -2689
753318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15839009
84 X = -4827730
20
Y = 853314
66 feet Y = 260090
31 meter
Z = 15593614
34 Z = 4752933
65
XDOT = -9795
050773 XDOT = -2985
531476
YDOT = -20246
815376 feet/sec YDOT = -6171
229326 meter/sec
ZDOT = -8813
517536 ZDOT = -2686
360145
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 18196
75184270
00016717 00000-0 10270-3 0 9062
2 25544 51
6362 236
3420 0004089 318
3966 41
6875 15
53977268 2952
Satellite: ISS
Catalog Number: 25544
Epoch time: 18196
75184270 = yrday
fracday
Element set: 906
Inclination: 51
6362 deg
RA of node: 236
3420 deg
Eccentricity:
0004089
Arg of perigee: 318
3966 deg
Mean anomaly: 41
6875 deg
Mean motion: 15
53977268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 295
Checksum: 338
Coasting Arc #8 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2018/197/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -788782
25 A = 6784204
92 meter
Y = -5662042
92 meter E =
0009862
Z = 3642683
59 I = 51
33833
XDOT = 6010
967057 Wp = 77
34136
YDOT = 1962
232323 meter/sec RA = 231
41914 deg
ZDOT = 4343
787203 TA = 326
14606
MA = 326
20898
Ha = 220
876 n
mi
Hp = 215
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2587868
28 X = -743102
97
Y = -18576256
28 feet Y = -5670608
48 meter
Z = 11951061
65 Z = 3638962
58
XDOT = 19721
020529 XDOT = 5967
478711
YDOT = 6437
770089 feet/sec YDOT = 2029
207637 meter/sec
ZDOT = 14251
270352 ZDOT = 4372
880300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13757389
06 X = -4193252
19
Y = 12762840
07 feet Y = 3890113
65 meter
Z = 11935090
87 Z = 3637815
70
XDOT = -4941
938369 XDOT = -1506
302815
YDOT = -18799
667719 feet/sec YDOT = -5730
138721 meter/sec
ZDOT = 14381
266592 ZDOT = 4383
410057
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 18197
58785254
00016717 00000-0 10270-3 0 9074
2 25544 51
6374 232
1748 0003807 323
8727 36
2167 15
53959778 3080
Satellite: ISS
Catalog Number: 25544
Epoch time: 18197
58785254 = yrday
fracday
Element set: 907
Inclination: 51
6374 deg
RA of node: 232
1748 deg
Eccentricity:
0003807
Arg of perigee: 323
8727 deg
Mean anomaly: 36
2167 deg
Mean motion: 15
53959778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 308
Checksum: 348
Coasting Arc #9 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2018/198/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -474503
50 A = 6780538
63 meter
Y = 4909604
25 meter E =
0010181
Z = -4662382
95 I = 51
34902
XDOT = -6293
521184 Wp = 49
22036
YDOT = -3311
942040 meter/sec RA = 226
41157 deg
ZDOT = -2844
613000 TA = 192
37265
MA = 192
39766
Ha = 220
880 n
mi
Hp = 215
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1556770
03 X = -506721
79
Y = 16107625
50 feet Y = 4904118
15 meter
Z = -15296531
98 Z = -4664765
85
XDOT = -20648
035381 XDOT = -6242
201007
YDOT = -10865
951576 feet/sec YDOT = -3382
033431 meter/sec
ZDOT = -9332
719816 ZDOT = -2875
059748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13933684
58 X = 4246987
06
Y = -8208972
58 feet Y = -2502094
84 meter
Z = -15307783
19 Z = -4665812
32
XDOT = 2576
088303 XDOT = 785
191715
YDOT = 22044
213989 feet/sec YDOT = 6719
076424 meter/sec
ZDOT = -9468
631454 ZDOT = -2886
038867
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 18198
55247525
00016717 00000-0 10270-3 0 9087
2 25544 51
6386 227
3677 0003884 324
3995 35
6898 15
53983986 3237
Satellite: ISS
Catalog Number: 25544
Epoch time: 18198
55247525 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 227
3677 deg
Eccentricity:
0003884
Arg of perigee: 324
3995 deg
Mean anomaly: 35
6898 deg
Mean motion: 15
53983986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 368
Coasting Arc #10 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2018/199/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1844936
56 A = 6778157
81 meter
Y = -3923725
82 meter E =
0001812
Z = 5208699
21 I = 51
36411
XDOT = 6226
795161 Wp = 43
65857
YDOT = 4347
904308 meter/sec RA = 221
39595 deg
ZDOT = 1070
801733 TA = 36
05147
MA = 36
03925
Ha = 220
934 n
mi
Hp = 215
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6052941
48 X = 1863374
86
Y = -12873116
22 feet Y = -3902991
65 meter
Z = 17088908
18 Z = 5217705
73
XDOT = 20429
117981 XDOT = 6172
511594
YDOT = 14264
777914 feet/sec YDOT = 4417
233058 meter/sec
ZDOT = 3513
129046 ZDOT = 1100
917313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13872253
24 X = -4228262
79
Y = 2918951
64 feet Y = 889696
46 meter
Z = 17129691
06 Z = 5221129
84
XDOT = -523
997701 XDOT = -159
714499
YDOT = -23874
719763 feet/sec YDOT = -7277
014584 meter/sec
ZDOT = 3647
454864 ZDOT = 1111
744242
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 18199
58140349
00016717 00000-0 10270-3 0 9098
2 25544 51
6380 222
2387 0003951 330
3930 29
6998 15
53990297 3398
Satellite: ISS
Catalog Number: 25544
Epoch time: 18199
58140349 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 222
2387 deg
Eccentricity:
0003951
Arg of perigee: 330
3930 deg
Mean anomaly: 29
6998 deg
Mean motion: 15
53990297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 340
Coasting Arc #11 (Orbit 339)
---------------------------------------
Vector Time (GMT): 2018/199/15:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5106607
87 A = 6781255
00 meter
Y = 293748
94 meter E =
0006879
Z = -4457999
00 I = 51
37555
XDOT = -3180
287402 Wp = 88
13848
YDOT = -6172
187297 meter/sec RA = 220
84307 deg
ZDOT = 3240
856709 TA = 214
61650
MA = 214
66130
Ha = 221
013 n
mi
Hp = 215
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16753962
84 X = -5087858
81
Y = 963743
23 feet Y = 236748
39 meter
Z = -14625980
97 Z = -4482759
24
XDOT = -10434
013785 XDOT = -3126
774101
YDOT = -20249
958324 feet/sec YDOT = -6207
452426 meter/sec
ZDOT = 10632
731985 ZDOT = 3225
537832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16292829
78 X = 4966054
52
Y = 3593278
58 feet Y = 1095231
31 meter
Z = -14736873
41 Z = -4491799
01
XDOT = 4877
635856 XDOT = 1486
703409
YDOT = 21151
653002 feet/sec YDOT = 6447
023835 meter/sec
ZDOT = 10564
865752 ZDOT = 3220
171081
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 18199
64571233
00016717 00000-0 10270-3 0 9107
2 25544 51
6366 221
9187 0004135 330
3990 29
6928 15
53965908 3403
Satellite: ISS
Catalog Number: 25544
Epoch time: 18199
64571233 = yrday
fracday
Element set: 910
Inclination: 51
6366 deg
RA of node: 221
9187 deg
Eccentricity:
0004135
Arg of perigee: 330
3990 deg
Mean anomaly: 29
6928 deg
Mean motion: 15
53965908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 340
Checksum: 324
Coasting Arc #12 (Orbit 355)
---------------------------------------
Vector Time (GMT): 2018/200/15:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5831881
83 A = 6784896
44 meter
Y = 929543
47 meter E =
0011222
Z = 3335236
24 I = 51
41323
XDOT = 1740
803248 Wp = 71
42169
YDOT = 5839
156598 meter/sec RA = 215
84063 deg
ZDOT = -4654
912137 TA = 69
59309
MA = 69
47260
Ha = 221
086 n
mi
Hp = 215
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19133470
56 X = 5804853
33
Y = 3049683
30 feet Y = 994608
28 meter
Z = 10942376
13 Z = 3363499
63
XDOT = 5711
296744 XDOT = 1697
989690
YDOT = 19157
337919 feet/sec YDOT = 5858
384344 meter/sec
ZDOT = -15272
021447 ZDOT = -4646
559654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17654442
37 X = -5381074
03
Y = -7805617
94 feet Y = -2379152
35 meter
Z = 11068823
45 Z = 3373777
39
XDOT = -1309
803291 XDOT = -399
228043
YDOT = -18717
477964 feet/sec YDOT = -5705
087283 meter/sec
ZDOT = -15235
294934 ZDOT = -4643
717896
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 18200
67463851
00016717 00000-0 10270-3 0 9110
2 25544 51
6362 216
7904 0004233 333
7516 26
3422 15
53994202 3567
Satellite: ISS
Catalog Number: 25544
Epoch time: 18200
67463851 = yrday
fracday
Element set: 911
Inclination: 51
6362 deg
RA of node: 216
7904 deg
Eccentricity:
0004233
Arg of perigee: 333
7516 deg
Mean anomaly: 26
3422 deg
Mean motion: 15
53994202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 356
Checksum: 291
Coasting Arc #13 (Orbit 370)
---------------------------------------
Vector Time (GMT): 2018/201/15:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6213254
58 A = 6788125
99 meter
Y = -1941887
86 meter E =
0009589
Z = -1906291
37 I = 51
45161
XDOT = -74
732268 Wp = 17
35588
YDOT = -5240
525874 meter/sec RA = 210
84991 deg
ZDOT = 5598
207301 TA = 321
58404
MA = 321
65228
Ha = 221
154 n
mi
Hp = 215
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20384693
49 X = -6181818
39
Y = -6371023
16 feet Y = -2011192
86 meter
Z = -6254236
79 Z = -1936396
75
XDOT = -245
184607 XDOT = -43
318633
YDOT = -17193
326357 feet/sec YDOT = -5241
186318 meter/sec
ZDOT = 18366
821853 ZDOT = 5597
920221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18240854
76 X = 5559812
53
Y = 11031554
31 feet Y = 3362417
75 meter
Z = -6388831
67 Z = -1947315
89
XDOT = -2932
177248 XDOT = -893
727625
YDOT = 15454
776365 feet/sec YDOT = 4710
615836 meter/sec
ZDOT = 18366
134994 ZDOT = 5597
997946
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 18201
63925491
00016717 00000-0 10270-3 0 9121
2 25544 51
6364 211
9830 0004175 337
4035 22
6933 15
53988305 3716
Satellite: ISS
Catalog Number: 25544
Epoch time: 18201
63925491 = yrday
fracday
Element set: 912
Inclination: 51
6364 deg
RA of node: 211
9830 deg
Eccentricity:
0004175
Arg of perigee: 337
4035 deg
Mean anomaly: 22
6933 deg
Mean motion: 15
53988305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 371
Checksum: 301
Coasting Arc #14 (Orbit 373)
---------------------------------------
Vector Time (GMT): 2018/201/19:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1684667
77 A = 6777763
24 meter
Y = 3900796
23 meter E =
0013905
Z = -5292128
13 I = 51
42581
XDOT = -6788
306300 Wp = 69
84571
YDOT = -3519
584799 meter/sec RA = 209
97357 deg
ZDOT = -429
538325 TA = 196
01836
MA = 196
06237
Ha = 221
188 n
mi
Hp = 215
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5527125
23 X = -1702456
17
Y = 12797887
90 feet Y = 3881858
02 meter
Z = -17362625
10 Z = -5300354
53
XDOT = -22271
346130 XDOT = -6746
358361
YDOT = -11547
194223 feet/sec YDOT = -3595
261753 meter/sec
ZDOT = -1409
246474 ZDOT = -462
411677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6571906
35 X = -2003117
05
Y = -12241281
43 feet Y = -3731142
58 meter
Z = -17399910
17 Z = -5303492
62
XDOT = 22063
887693 XDOT = 6725
072969
YDOT = -9615
949011 feet/sec YDOT = -2930
941258 meter/sec
ZDOT = -1556
060075 ZDOT = -474
287111
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 18201
83217765
00016717 00000-0 10270-3 0 9132
2 25544 51
6401 211
0228 0004290 336
5982 23
4975 15
54014797 3743
Satellite: ISS
Catalog Number: 25544
Epoch time: 18201
83217765 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 211
0228 deg
Eccentricity:
0004290
Arg of perigee: 336
5982 deg
Mean anomaly: 23
4975 deg
Mean motion: 15
54014797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 299
Coasting Arc #15 (Orbit 389)
---------------------------------------
Vector Time (GMT): 2018/202/19:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3225664
45 A = 6778263
19 meter
Y = -3016560
69 meter E =
0007034
Z = 5141546
13 I = 51
45722
XDOT = 6254
306887 Wp = 18
32497
YDOT = 4191
870484 meter/sec RA = 204
96126 deg
ZDOT = -1457
304887 TA = 85
77643
MA = 85
69604
Ha = 221
138 n
mi
Hp = 215
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10582888
63 X = 3234181
99
Y = -9896852
66 feet Y = -2980441
89 meter
Z = 16868589
66 Z = 5157235
61
XDOT = 20519
379551 XDOT = 6214
046172
YDOT = 13752
855918 feet/sec YDOT = 4261
585473 meter/sec
ZDOT = -4781
184014 ZDOT = -1427
021287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1386269
77 X = 422535
02
Y = 14340022
26 feet Y = 4370838
79 meter
Z = 16939201
85 Z = 5163068
72
XDOT = -22424
777202 XDOT = -6835
072091
YDOT = 7683
337343 feet/sec YDOT = 2341
881222 meter/sec
ZDOT = -4646
024654 ZDOT = -1416
108314
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 18202
86109619
00016717 00000-0 10270-3 0 9145
2 25544 51
6403 205
8943 0004385 339
6319 20
4658 15
54043515 3906
Satellite: ISS
Catalog Number: 25544
Epoch time: 18202
86109619 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 205
8943 deg
Eccentricity:
0004385
Arg of perigee: 339
6319 deg
Mean anomaly: 20
4658 deg
Mean motion: 15
54043515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 390
Checksum: 305
Coasting Arc #16 (Orbit 404)
---------------------------------------
Vector Time (GMT): 2018/203/18:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5014413
78 A = 6781986
20 meter
Y = -1738542
14 meter E =
0011057
Z = 4219567
97 I = 51
49774
XDOT = 4737
188752 Wp = 50
74232
YDOT = 4812
602398 meter/sec RA = 200
11061 deg
ZDOT = -3633
406818 TA = 76
58077
MA = 76
45754
Ha = 221
357 n
mi
Hp = 215
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16451488
77 X = 5012985
69
Y = -5703878
41 feet Y = -1682475
89 meter
Z = 13843726
93 Z = 4243922
41
XDOT = 15541
957848 XDOT = 4700
669855
YDOT = 15789
377947 feet/sec YDOT = 4865
373074 meter/sec
ZDOT = -11920
626043 ZDOT = -3610
483623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8382630
64 X = -2555025
82
Y = 15161771
71 feet Y = 4621308
02 meter
Z = 13953016
47 Z = 4252879
42
XDOT = -21063
806312 XDOT = -6420
248164
YDOT = -729
783714 feet/sec YDOT = -222
438076 meter/sec
ZDOT = -11818
486223 ZDOT = -3602
274601
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 18203
82570840
00016717 00000-0 10270-3 0 9151
2 25544 51
6391 201
0870 0004377 345
8993 14
2037 15
54016265 4058
Satellite: ISS
Catalog Number: 25544
Epoch time: 18203
82570840 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 201
0870 deg
Eccentricity:
0004377
Arg of perigee: 345
8993 deg
Mean anomaly: 14
2037 deg
Mean motion: 15
54016265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 405
Checksum: 293
Coasting Arc #17 (Orbit 419)
---------------------------------------
Vector Time (GMT): 2018/204/18:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6009500
04 A = 6785669
00 meter
Y = 865968
10 meter E =
0006533
Z = -3025998
36 I = 51
54184
XDOT = -3189
711642 Wp = 31
12064
YDOT = -4922
781446 meter/sec RA = 195
11862 deg
ZDOT = 4936
087129 TA = 294
15466
MA = 294
22295
Ha = 221
394 n
mi
Hp = 214
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19716207
47 X = -6004038
35
Y = 2841102
70 feet Y = 798796
58 meter
Z = -9927816
14 Z = -3055176
76
XDOT = -10464
933209 XDOT = -3158
403330
YDOT = -16150
857762 feet/sec YDOT = -4958
276470 meter/sec
ZDOT = 16194
511579 ZDOT = 4920
668301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12479826
07 X = 3803850
99
Y = -15441503
92 feet Y = -4706570
39 meter
Z = -10058634
73 Z = -3065871
87
XDOT = 17606
228976 XDOT = 5366
378592
YDOT = 3746
452199 feet/sec YDOT = 1141
918630 meter/sec
ZDOT = 16125
986090 ZDOT = 4915
200560
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 18204
79031661
00016717 00000-0 10270-3 0 9162
2 25544 51
6395 196
2790 0004397 347
1085 12
9955 15
54015444 4206
Satellite: ISS
Catalog Number: 25544
Epoch time: 18204
79031661 = yrday
fracday
Element set: 916
Inclination: 51
6395 deg
RA of node: 196
2790 deg
Eccentricity:
0004397
Arg of perigee: 347
1085 deg
Mean anomaly: 12
9955 deg
Mean motion: 15
54015444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 420
Checksum: 312
Coasting Arc #18 (Orbit 435)
---------------------------------------
Vector Time (GMT): 2018/205/18:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6617479
12 A = 6788729
25 meter
Y = -23580
22 meter E =
0011922
Z = 1498153
55 I = 51
58410
XDOT = 1330
140495 Wp = 101
11060
YDOT = 4879
728645 meter/sec RA = 190
13871 deg
ZDOT = -5761
840033 TA = 62
52113
MA = 62
39998
Ha = 221
611 n
mi
Hp = 214
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21710889
49 X = 6609973
83
Y = -77362
92 feet Y = 50378
87 meter
Z = 4915201
93 Z = 1530280
31
XDOT = 4363
978003 XDOT = 1303
462766
YDOT = 16009
608416 feet/sec YDOT = 4894
454661 meter/sec
ZDOT = -18903
674650 ZDOT = -5755
443019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15588811
46 X = -4751469
73
Y = 15063923
83 feet Y = 4591483
98 meter
Z = 5059157
39 Z = 1542031
17
XDOT = -13223
940023 XDOT = -4030
656919
YDOT = -7306
143355 feet/sec YDOT = -2226
912495 meter/sec
ZDOT = -18875
555265 ZDOT = -5753
269245
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 18205
81922952
00016717 00000-0 10270-3 0 9179
2 25544 51
6397 191
1509 0004297 352
2296 7
8790 15
53988544 4366
Satellite: ISS
Catalog Number: 25544
Epoch time: 18205
81922952 = yrday
fracday
Element set: 917
Inclination: 51
6397 deg
RA of node: 191
1509 deg
Eccentricity:
0004297
Arg of perigee: 352
2296 deg
Mean anomaly: 7
8790 deg
Mean motion: 15
53988544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 436
Checksum: 339
Coasting Arc #19 (Orbit 440)
---------------------------------------
Vector Time (GMT): 2018/206/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -888353
50 A = 6777649
82 meter
Y = 4130793
57 meter E =
0014799
Z = -5311777
41 I = 51
55759
XDOT = -7540
362342 Wp = 76
75048
YDOT = -1314
371968 meter/sec RA = 188
44501 deg
ZDOT = 242
810346 TA = 195
54686
MA = 195
59237
Ha = 221
495 n
mi
Hp = 214
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2914545
61 X = -908677
72
Y = 13552472
35 feet Y = 4120746
33 meter
Z = -17427091
26 Z = -5316141
58
XDOT = -24738
721594 XDOT = -7526
283688
YDOT = -4312
243988 feet/sec YDOT = -1398
614814 meter/sec
ZDOT = 796
621870 ZDOT = 206
216460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5797029
31 X = -1766934
53
Y = 12564254
79 feet Y = 3829584
86 meter
Z = -17447107
07 Z = -5317878
24
XDOT = -22206
251081 XDOT = -6768
465329
YDOT = -9384
732162 feet/sec YDOT = -2860
466363 meter/sec
ZDOT = 632
790257 ZDOT = 192
874470
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 18206
14076291
00016717 00000-0 10270-3 0 9183
2 25544 51
6388 189
5434 0003926 353
1214 6
9884 15
54032291 4412
Satellite: ISS
Catalog Number: 25544
Epoch time: 18206
14076291 = yrday
fracday
Element set: 918
Inclination: 51
6388 deg
RA of node: 189
5434 deg
Eccentricity:
0003926
Arg of perigee: 353
1214 deg
Mean anomaly: 6
9884 deg
Mean motion: 15
54032291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 441
Checksum: 309
Coasting Arc #20 (Orbit 456)
---------------------------------------
Vector Time (GMT): 2018/207/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944929
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2617378
31 A = 6779113
62 meter
Y = -3790774
87 meter E =
0008771
Z = 4971532
28 I = 51
59497
XDOT = 7067
975486 Wp = 34
63067
YDOT = 2101
014861 meter/sec RA = 183
44249 deg
ZDOT = -2110
187724 TA = 75
97264
MA = 75
87515
Ha = 221
560 n
mi
Hp = 214
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8587199
17 X = 2635424
61
Y = -12436925
42 feet Y = -3761405
15 meter
Z = 16310801
45 Z = 4984289
81
XDOT = 23188
895951 XDOT = 7054
206054
YDOT = 6893
093377 feet/sec YDOT = 2179
977074 meter/sec
ZDOT = -6923
188071 ZDOT = -2075
887774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10899459
59 X = 3322155
28
Y = -10379629
78 feet Y = -3163711
16 meter
Z = 16368396
79 Z = 4989087
34
XDOT = 20513
843115 XDOT = 6252
619382
YDOT = 10819
719214 feet/sec YDOT = 3297
850416 meter/sec
ZDOT = -6769
697232 ZDOT = -2063
403716
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 18207
16967147
00016717 00000-0 10270-3 0 9196
2 25544 51
6385 184
4145 0003935 357
9705 2
1431 15
54008538 4579
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
16967147 = yrday
fracday
Element set: 919
Inclination: 51
6385 deg
RA of node: 184
4145 deg
Eccentricity:
0003935
Arg of perigee: 357
9705 deg
Mean anomaly: 2
1431 deg
Mean motion: 15
54008538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 457
Checksum: 319
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