[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 25th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 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
300/09:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 215
6
303/21:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 1861)
---------------------------------------
Vector Time (GMT): 2018/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 518103
10 A = 6790012
70 meter
Y = -6765293
36 meter E =
0007955
Z = -146349
03 I = 52
03615
XDOT = 4693
350290 Wp = 129
61094
YDOT = 485
302802 meter/sec RA = 93
41499 deg
ZDOT = -6041
401947 TA = 51
95640
MA = 51
88463
Ha = 221
123 n
mi
Hp = 215
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1699813
32 X = 594426
89
Y = -22195844
35 feet Y = -6759072
83 meter
Z = -480147
73 Z = -143646
35
XDOT = 15398
130872 XDOT = 4716
921423
YDOT = 1592
200795 feet/sec YDOT = 537
918490 meter/sec
ZDOT = -19820
872531 ZDOT = -6018
545442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10304718
28 X = 3140878
13
Y = 19732458
01 feet Y = 6014453
20 meter
Z = -467221
25 Z = -142409
04
XDOT = -12578
537257 XDOT = -3833
938156
YDOT = 6119
674548 feet/sec YDOT = 1865
276802 meter/sec
ZDOT = -19718
100671 ZDOT = -6010
077085
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 18297
53191140
00016717 00000-0 10270-3 0 9008
2 25544 51
6357 94
1573 0004004 327
9822 32
1086 15
53889466 18621
Satellite: ISS
Catalog Number: 25544
Epoch time: 18297
53191140 = yrday
fracday
Element set: 900
Inclination: 51
6357 deg
RA of node: 94
1573 deg
Eccentricity:
0004004
Arg of perigee: 327
9822 deg
Mean anomaly: 32
1086 deg
Mean motion: 15
53889466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1862
Checksum: 313
Coasting Arc #2 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2018/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1185410
51 A = 6788786
71 meter
Y = 6445639
43 meter E =
0014112
Z = 1738901
60 I = 52
03489
XDOT = -4526
935811 Wp = 49
20269
YDOT = -2380
885259 meter/sec RA = 88
47192 deg
ZDOT = 5718
061928 TA = 329
78062
MA = 329
86194
Ha = 221
205 n
mi
Hp = 215
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3889142
10 X = -1265846
26
Y = 21147111
00 feet Y = 6431933
69 meter
Z = 5705057
75 Z = 1732947
44
XDOT = -14852
151611 XDOT = -4527
751789
YDOT = -7811
303344 feet/sec YDOT = -2431
512891 meter/sec
ZDOT = 18760
045694 ZDOT = 5696
069124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8206099
97 X = -2501219
27
Y = -19882130
15 feet Y = -6060073
27 meter
Z = 5677520
39 Z = 1730508
21
XDOT = 15365
707387 XDOT = 4683
467611
YDOT = -993
099859 feet/sec YDOT = -302
696837 meter/sec
ZDOT = 18661
379669 ZDOT = 5687
988523
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 18298
56092432
00016717 00000-0 10270-3 0 9017
2 25544 51
6378 89
0294 0003792 329
7231 30
3702 15
53879943 18785
Satellite: ISS
Catalog Number: 25544
Epoch time: 18298
56092432 = yrday
fracday
Element set: 901
Inclination: 51
6378 deg
RA of node: 89
0294 deg
Eccentricity:
0003792
Arg of perigee: 329
7231 deg
Mean anomaly: 30
3702 deg
Mean motion: 15
53879943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1878
Checksum: 336
Coasting Arc #3 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2018/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1863766
53 A = 6785786
53 meter
Y = -5692269
35 meter E =
0003911
Z = -3194807
50 I = 52
02347
XDOT = 4273
804515 Wp = 46
90415
YDOT = 4117
900280 meter/sec RA = 83
52335 deg
ZDOT = -4844
875097 TA = 169
75433
MA = 169
74635
Ha = 221
339 n
mi
Hp = 215
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6114719
58 X = 1942799
71
Y = -18675424
39 feet Y = -5670985
60 meter
Z = -10481651
91 Z = -3185561
59
XDOT = 14021
668355 XDOT = 4250
973927
YDOT = 13510
171522 feet/sec YDOT = 4165
565154 meter/sec
ZDOT = -15895
259504 ZDOT = -4824
169365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5294453
93 X = 1613749
56
Y = 18947678
26 feet Y = 5775252
33 meter
Z = -10439374
72 Z = -3181921
41
XDOT = -17880
512702 XDOT = -5449
980272
YDOT = -3708
249228 feet/sec YDOT = -1130
274365 meter/sec
ZDOT = -15802
596311 ZDOT = -4816
631356
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 18299
52562113
00016717 00000-0 10270-3 0 9023
2 25544 51
6384 84
2222 0003905 335
8980 24
1990 15
53871860 18932
Satellite: ISS
Catalog Number: 25544
Epoch time: 18299
52562113 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 84
2222 deg
Eccentricity:
0003905
Arg of perigee: 335
8980 deg
Mean anomaly: 24
1990 deg
Mean motion: 15
53871860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1893
Checksum: 319
Coasting Arc #4 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2018/300/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3387244
85 A = 6779566
25 meter
Y = -3086664
36 meter E =
0012991
Z = -5007788
40 I = 51
99692
XDOT = 2990
432347 Wp = 56
27114
YDOT = 6724
130890 meter/sec RA = 79
02472 deg
ZDOT = -2118
783298 TA = 193
15615
MA = 193
19006
Ha = 221
498 n
mi
Hp = 215
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11113008
04 X = 3445834
95
Y = -10126851
58 feet Y = -3048458
27 meter
Z = -16429751
97 Z = -4991191
54
XDOT = 9811
129748 XDOT = 2925
311216
YDOT = 22060
796884 feet/sec YDOT = 6757
207855 meter/sec
ZDOT = -6951
388772 ZDOT = -2104
414600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11029846
12 X = -3361897
10
Y = 10337068
44 feet Y = 3150738
46 meter
Z = -16354703
64 Z = -4984913
67
XDOT = -9516
044176 XDOT = -2900
490265
YDOT = -21066
922853 feet/sec YDOT = -6421
198086 meter/sec
ZDOT = -6887
563614 ZDOT = -2099
329390
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 18300
42600226
00016717 00000-0 10270-3 0 9034
2 25544 51
6369 79
7371 0004055 341
3387 18
7616 15
53872541 19076
Satellite: ISS
Catalog Number: 25544
Epoch time: 18300
42600226 = yrday
fracday
Element set: 903
Inclination: 51
6369 deg
RA of node: 79
7371 deg
Eccentricity:
0004055
Arg of perigee: 341
3387 deg
Mean anomaly: 18
7616 deg
Mean motion: 15
53872541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 304
Coasting Arc #5 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2018/301/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3913418
90 A = 6778252
16 meter
Y = 1476592
60 meter E =
0003618
Z = 5332491
82 I = 51
98458
XDOT = -2336
909141 Wp = 22
09047
YDOT = -7298
431069 meter/sec RA = 74
05242 deg
ZDOT = 309
150831 TA = 64
99563
MA = 64
95806
Ha = 221
795 n
mi
Hp = 215
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12839300
85 X = -3955542
81
Y = 4844463
92 feet Y = 1432594
44 meter
Z = 17495051
92 Z = 5313379
01
XDOT = -7667
024740 XDOT = -2256
624096
YDOT = -23944
983821 feet/sec YDOT = -7324
115111 meter/sec
ZDOT = 1014
274380 ZDOT = 297
993553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12772691
45 X = 3893116
35
Y = -5308747
18 feet Y = -1618106
14 meter
Z = 17408873
46 Z = 5306224
63
XDOT = 8143
071700 XDOT = 2482
008254
YDOT = 22721
907007 feet/sec YDOT = 6925
637256 meter/sec
ZDOT = 964
986475 ZDOT = 294
127878
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 18301
45500899
00016717 00000-0 10270-3 0 9044
2 25544 51
6367 74
6090 0004087 344
6237 15
4791 15
53827381 19239
Satellite: ISS
Catalog Number: 25544
Epoch time: 18301
45500899 = yrday
fracday
Element set: 904
Inclination: 51
6367 deg
RA of node: 74
6090 deg
Eccentricity:
0004087
Arg of perigee: 344
6237 deg
Mean anomaly: 15
4791 deg
Mean motion: 15
53827381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 317
Coasting Arc #6 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2018/302/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4389621
32 A = 6778851
43 meter
Y = 153583
14 meter E =
0012634
Z = -5173920
18 I = 51
97879
XDOT = 1533
530949 Wp = 84
35412
YDOT = 7347
680506 meter/sec RA = 69
07920 deg
ZDOT = 1523
574795 TA = 200
24697
MA = 200
29712
Ha = 221
693 n
mi
Hp = 215
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14401644
75 X = 4412710
37
Y = 503881
68 feet Y = 202800
15 meter
Z = -16974803
72 Z = -5152540
38
XDOT = 5031
269519 XDOT = 1443
852283
YDOT = 24106
563340 feet/sec YDOT = 7364
328054 meter/sec
ZDOT = 4998
604970 ZDOT = 1530
806665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14520484
14 X = -4425843
57
Y = 269727
94 feet Y = 82213
08 meter
Z = -16878626
03 Z = -5144605
21
XDOT = -6252
816743 XDOT = -1905
858543
YDOT = -22748
271352 feet/sec YDOT = -6933
673108 meter/sec
ZDOT = 5030
208512 ZDOT = 1533
207554
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 18302
41969758
00016717 00000-0 10270-3 0 9055
2 25544 51
6386 69
8020 0004035 348
6299 11
4761 15
53881192 19383
Satellite: ISS
Catalog Number: 25544
Epoch time: 18302
41969758 = yrday
fracday
Element set: 905
Inclination: 51
6386 deg
RA of node: 69
8020 deg
Eccentricity:
0004035
Arg of perigee: 348
6299 deg
Mean anomaly: 11
4761 deg
Mean motion: 15
53881192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 332
Coasting Arc #7 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2018/303/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4758639
67 A = 6781635
61 meter
Y = -1728043
59 meter E =
0010749
Z = 4509368
31 I = 51
97384
XDOT = -555
974760 Wp = 47
22211
YDOT = -6932
418675 meter/sec RA = 64
10888 deg
ZDOT = -3231
316254 TA = 75
17521
MA = 75
05616
Ha = 221
889 n
mi
Hp = 215
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15612334
88 X = -4760867
03
Y = -5669434
35 feet Y = -1781270
55 meter
Z = 14794515
44 Z = 4486246
66
XDOT = -1824
064172 XDOT = -462
716912
YDOT = -22744
155759 feet/sec YDOT = -6938
114464 meter/sec
ZDOT = -10601
431281 ZDOT = -3233
790670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16070223
33 X = 4898204
07
Y = 4549328
49 feet Y = 1386635
32 meter
Z = 14690701
33 Z = 4477725
77
XDOT = 3680
629206 XDOT = 1121
855782
YDOT = 21393
415678 feet/sec YDOT = 6520
713099 meter/sec
ZDOT = -10611
668245 ZDOT = -3234
436481
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 18303
44869764
00016717 00000-0 10270-3 0 9066
2 25544 51
6375 64
6737 0003999 352
8476 7
2618 15
53850156 19549
Satellite: ISS
Catalog Number: 25544
Epoch time: 18303
44869764 = yrday
fracday
Element set: 906
Inclination: 51
6375 deg
RA of node: 64
6737 deg
Eccentricity:
0003999
Arg of perigee: 352
8476 deg
Mean anomaly: 7
2618 deg
Mean motion: 15
53850156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 349
Coasting Arc #8 (Orbit 1960)
---------------------------------------
Vector Time (GMT): 2018/303/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4836726
63 A = 6785067
93 meter
Y = 3246456
58 meter E =
0006292
Z = -3478558
16 I = 51
97835
XDOT = -795
009043 Wp = 46
09275
YDOT = 6089
255023 meter/sec RA = 61
70382 deg
ZDOT = 4586
936204 TA = 273
30422
MA = 273
37620
Ha = 222
014 n
mi
Hp = 215
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15868525
68 X = 4816961
61
Y = 10651104
27 feet Y = 3300433
76 meter
Z = -11412592
40 Z = -3455110
64
XDOT = -2608
297385 XDOT = -885
322942
YDOT = 19977
870812 feet/sec YDOT = 6079
859628 meter/sec
ZDOT = 15049
003295 ZDOT = 4582
855011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15805562
04 X = 4817535
31
Y = 10854852
35 feet Y = 3308559
00 meter
Z = -11307510
08 Z = -3446529
07
XDOT = -2174
077770 XDOT = -662
658904
YDOT = 18789
852498 feet/sec YDOT = 5727
147041 meter/sec
ZDOT = 15029
846701 ZDOT = 4581
097274
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 18303
89888298
00016717 00000-0 10270-3 0 9079
2 25544 51
6376 62
4350 0004493 355
0043 5
1064 15
53861420 19618
Satellite: ISS
Catalog Number: 25544
Epoch time: 18303
89888298 = yrday
fracday
Element set: 907
Inclination: 51
6376 deg
RA of node: 62
4350 deg
Eccentricity:
0004493
Arg of perigee: 355
0043 deg
Mean anomaly: 5
1064 deg
Mean motion: 15
53861420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1961
Checksum: 311
Coasting Arc #9 (Orbit 1976)
---------------------------------------
Vector Time (GMT): 2018/304/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4781946
04 A = 6788251
73 meter
Y = -4346993
85 meter E =
0012769
Z = 2065864
65 I = 51
97292
XDOT = 2011
581102 Wp = 91
91438
YDOT = -4872
508994 meter/sec RA = 56
74959 deg
ZDOT = -5567
237511 TA = 65
34570
MA = 65
21276
Ha = 221
965 n
mi
Hp = 214
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15688799
35 X = -4743016
34
Y = -14261790
85 feet Y = -4400251
22 meter
Z = 6777771
16 Z = 2042729
90
XDOT = 6599
675533 XDOT = 2092
960372
YDOT = -15985
921896 feet/sec YDOT = -4849
559081 meter/sec
ZDOT = -18265
214932 ZDOT = -5557
268172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15794960
53 X = -4814303
97
Y = -14193271
59 feet Y = -4326109
18 meter
Z = 6674245
18 Z = 2034309
93
XDOT = 5617
051501 XDOT = 1712
077298
YDOT = -14864
324542 feet/sec YDOT = -4530
646121 meter/sec
ZDOT = -18219
715164 ZDOT = -5553
369182
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 18304
92787913
00016717 00000-0 10270-3 0 9087
2 25544 51
6378 57
3066 0004569 357
3018 2
8109 15
53896534 19773
Satellite: ISS
Catalog Number: 25544
Epoch time: 18304
92787913 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 57
3066 deg
Eccentricity:
0004569
Arg of perigee: 357
3018 deg
Mean anomaly: 2
8109 deg
Mean motion: 15
53896534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1977
Checksum: 344
Coasting Arc #10 (Orbit 1991)
---------------------------------------
Vector Time (GMT): 2018/305/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4478225
84 A = 6789878
04 meter
Y = 5069040
59 meter E =
0014820
Z = -491656
62 I = 51
96016
XDOT = -3266
782538 Wp = 30
37259
YDOT = 3460
724903 meter/sec RA = 51
80142 deg
ZDOT = 6016
501330 TA = 324
34581
MA = 324
44471
Ha = 222
047 n
mi
Hp = 214
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14692342
00 X = 4423597
82
Y = 16630710
58 feet Y = 5118813
76 meter
Z = -1613046
65 Z = -470035
50
XDOT = -10717
790480 XDOT = -3334
463854
YDOT = 11354
084327 feet/sec YDOT = 3423
815173 meter/sec
ZDOT = 19739
177591 ZDOT = 6000
467792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15057173
66 X = 4589426
53
Y = 16310405
15 feet Y = 4971411
49 meter
Z = -1516434
26 Z = -462209
16
XDOT = -9412
725175 XDOT = -2868
998633
YDOT = 10488
331558 feet/sec YDOT = 3196
843459 meter/sec
ZDOT = 19666
574030 ZDOT = 5994
371764
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 18305
89255974
00016717 00000-0 10270-3 0 9092
2 25544 51
6385 52
4997 0004460 1
8835 358
2333 15
53908930 19926
Satellite: ISS
Catalog Number: 25544
Epoch time: 18305
89255974 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 52
4997 deg
Eccentricity:
0004460
Arg of perigee: 1
8835 deg
Mean anomaly: 358
2333 deg
Mean motion: 15
53908930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1992
Checksum: 342
Coasting Arc #11 (Orbit 2007)
---------------------------------------
Vector Time (GMT): 2018/306/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3864617
43 A = 6789385
34 meter
Y = -5458071
97 meter E =
0006568
Z = -1165946
37 I = 51
93764
XDOT = 4504
299336 Wp = 112
55317
YDOT = -1937
458714 meter/sec RA = 46
85310 deg
ZDOT = -5888
998915 TA = 80
04663
MA = 79
97250
Ha = 222
141 n
mi
Hp = 214
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12679191
06 X = -3797632
90
Y = -17907060
26 feet Y = -5500914
32 meter
Z = -3825283
36 Z = -1184556
67
XDOT = 14777
884961 XDOT = 4554
235795
YDOT = -6356
491845 feet/sec YDOT = -1886
809534 meter/sec
ZDOT = -19320
862582 ZDOT = -5866
996941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13337161
38 X = -4065166
79
Y = -17404105
95 feet Y = -5304771
49 meter
Z = -3908287
17 Z = -1191245
93
XDOT = 13379
744377 XDOT = 4078
146086
YDOT = -5957
587097 feet/sec YDOT = -1815
872547 meter/sec
ZDOT = -19221
607706 ZDOT = -5858
746029
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 18306
92154922
00016717 00000-0 10270-3 0 9100
2 25544 51
6390 47
3714 0004717 4
8403 355
2795 15
53900405 20088
Satellite: ISS
Catalog Number: 25544
Epoch time: 18306
92154922 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 47
3714 deg
Eccentricity:
0004717
Arg of perigee: 4
8403 deg
Mean anomaly: 355
2795 deg
Mean motion: 15
53900405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2008
Checksum: 292
Coasting Arc #12 (Orbit 2023)
---------------------------------------
Vector Time (GMT): 2018/307/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2959645
20 A = 6786844
87 meter
Y = 5477366
58 meter E =
0015611
Z = 2679204
41 I = 51
90615
XDOT = -5605
596216 Wp = 62
04575
YDOT = 467
922457 meter/sec RA = 41
90019 deg
ZDOT = 5219
739011 TA = 328
10467
MA = 328
19909
Ha = 222
113 n
mi
Hp = 214
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9710122
04 X = 2885161
41
Y = 17970362
79 feet Y = 5510047
06 meter
Z = 8790040
73 Z = 2693400
39
XDOT = -18391
063702 XDOT = -5635
767195
YDOT = 1535
178664 feet/sec YDOT = 405
068352 meter/sec
ZDOT = 17125
127989 ZDOT = 5192
435215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10640762
82 X = 3243304
51
Y = 17403470
26 feet Y = 5304577
74 meter
Z = 8853169
73 Z = 2698446
13
XDOT = -17120
762126 XDOT = -5218
408296
YDOT = 1792
357045 feet/sec YDOT = 546
310427 meter/sec
ZDOT = 17002
221622 ZDOT = 5182
277150
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 18307
95053564
00016717 00000-0 10270-3 0 9115
2 25544 51
6392 42
2443 0004543 7
7536 352
3686 15
53921574 20244
Satellite: ISS
Catalog Number: 25544
Epoch time: 18307
95053564 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 42
2443 deg
Eccentricity:
0004543
Arg of perigee: 7
7536 deg
Mean anomaly: 352
3686 deg
Mean motion: 15
53921574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2024
Checksum: 303
Coasting Arc #13 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2018/308/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1761182
88 A = 6783247
11 meter
Y = -5220861
15 meter E =
0009989
Z = -3968029
38 I = 51
86987
XDOT = 6449
502805 Wp = 47
66103
YDOT = 889
027964 meter/sec RA = 36
93643 deg
ZDOT = -4032
216892 TA = 180
32000
MA = 180
32064
Ha = 222
264 n
mi
Hp = 214
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5778159
06 X = -1683395
86
Y = -17128809
55 feet Y = -5240121
19 meter
Z = -13018469
10 Z = -3976395
57
XDOT = 21159
786107 XDOT = 6458
668895
YDOT = 2916
758413 feet/sec YDOT = 961
201831 meter/sec
ZDOT = -13229
058045 ZDOT = -4000
864577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6927651
07 X = -2111548
05
Y = -16668176
89 feet Y = -5080460
32 meter
Z = -13055393
75 Z = -3979284
02
XDOT = 20188
156165 XDOT = 6153
349999
YDOT = 1860
871433 feet/sec YDOT = 567
193613 meter/sec
ZDOT = -13088
131490 ZDOT = -3989
262478
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 18308
91520812
00016717 00000-0 10270-3 0 9128
2 25544 51
6403 37
4367 0004752 11
2351 348
8907 15
53916551 20396
Satellite: ISS
Catalog Number: 25544
Epoch time: 18308
91520812 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 37
4367 deg
Eccentricity:
0004752
Arg of perigee: 11
2351 deg
Mean anomaly: 348
8907 deg
Mean motion: 15
53916551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 298
Coasting Arc #14 (Orbit 2054)
---------------------------------------
Vector Time (GMT): 2018/309/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 343815
97 A = 6779831
79 meter
Y = 4712847
34 meter E =
0007193
Z = 4855234
43 I = 51
83171
XDOT = -6966
022126 Wp = 81
30014
YDOT = -2048
857887 meter/sec RA = 31
96265 deg
ZDOT = 2479
992315 TA = 344
41425
MA = 344
43639
Ha = 222
276 n
mi
Hp = 214
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1128005
15 X = 267505
29
Y = 15462097
57 feet Y = 4716265
65 meter
Z = 15929246
81 Z = 4856719
06
XDOT = -22854
403300 XDOT = -6954
640286
YDOT = -6721
974696 feet/sec YDOT = -2126
693042 meter/sec
ZDOT = 8136
457727 ZDOT = 2446
180693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2412624
93 X = 735368
08
Y = 15308038
67 feet Y = 4665890
19 meter
Z = 15935273
88 Z = 4857071
48
XDOT = -22304
682266 XDOT = -6798
467155
YDOT = -4803
532801 feet/sec YDOT = -1464
116798 meter/sec
ZDOT = 7984
640200 ZDOT = 2433
718333
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 18309
94418580
00016717 00000-0 10270-3 0 9131
2 25544 51
6404 32
3097 0004706 13
6620 346
4659 15
53947401 20559
Satellite: ISS
Catalog Number: 25544
Epoch time: 18309
94418580 = yrday
fracday
Element set: 913
Inclination: 51
6404 deg
RA of node: 32
3097 deg
Eccentricity:
0004706
Arg of perigee: 13
6620 deg
Mean anomaly: 346
4659 deg
Mean motion: 15
53947401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 304
Coasting Arc #15 (Orbit 2069)
---------------------------------------
Vector Time (GMT): 2018/310/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1202759
68 A = 6778123
03 meter
Y = -4068702
39 meter E =
0017143
Z = -5300477
46 I = 51
79667
XDOT = 7022
474601 Wp = 69
63987
YDOT = 2971
421037 meter/sec RA = 26
97920 deg
ZDOT = -683
365975 TA = 193
81436
MA = 193
86132
Ha = 222
430 n
mi
Hp = 214
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3946061
94 X = 1273915
29
Y = -13348761
13 feet Y = -4054854
58 meter
Z = -17390017
92 Z = -5294461
78
XDOT = 23039
614833 XDOT = 6992
044936
YDOT = 9748
756683 feet/sec YDOT = 3049
781066 meter/sec
ZDOT = -2242
014355 ZDOT = -649
326277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2605527
25 X = 794164
71
Y = -13708837
86 feet Y = -4178453
78 meter
Z = -17362388
78 Z = -5292056
10
XDOT = 22967
447304 XDOT = 7000
477938
YDOT = 7028
108820 feet/sec YDOT = 2142
167568 meter/sec
ZDOT = -2089
314306 ZDOT = -636
823000
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 18310
90885288
00016717 00000-0 10270-3 0 9143
2 25544 51
6403 27
5026 0004822 18
3245 341
8080 15
53912812 20702
Satellite: ISS
Catalog Number: 25544
Epoch time: 18310
90885288 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 27
5026 deg
Eccentricity:
0004822
Arg of perigee: 18
3245 deg
Mean anomaly: 341
8080 deg
Mean motion: 15
53912812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2070
Checksum: 289
Coasting Arc #16 (Orbit 2085)
---------------------------------------
Vector Time (GMT): 2018/311/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2778574
34 A = 6778426
54 meter
Y = 3311349
10 meter E =
0008519
Z = 5218116
63 I = 51
76832
XDOT = -6625
059072 Wp = 36
11863
YDOT = -3681
509507 meter/sec RA = 21
99253 deg
ZDOT = -1183
809224 TA = 65
25553
MA = 65
16690
Ha = 222
553 n
mi
Hp = 214
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9116057
56 X = -2840743
85
Y = 10864006
25 feet Y = 3279929
56 meter
Z = 17119805
23 Z = 5204467
88
XDOT = -21735
758111 XDOT = -6577
648528
YDOT = -12078
443263 feet/sec YDOT = -3755
330435 meter/sec
ZDOT = -3883
888531 ZDOT = -1215
877217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7806392
17 X = -2379388
33
Y = 11929107
80 feet Y = 3635992
06 meter
Z = 17057945
26 Z = 5199261
72
XDOT = -22173
568901 XDOT = -6758
503801
YDOT = -8714
833542 feet/sec YDOT = -2656
281264 meter/sec
ZDOT = -4027
604788 ZDOT = -1227
613939
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 18311
93782564
00016717 00000-0 10270-3 0 9151
2 25544 51
6408 22
3759 0004845 20
6119 339
5228 15
53929748 20865
Satellite: ISS
Catalog Number: 25544
Epoch time: 18311
93782564 = yrday
fracday
Element set: 915
Inclination: 51
6408 deg
RA of node: 22
3759 deg
Eccentricity:
0004845
Arg of perigee: 20
6119 deg
Mean anomaly: 339
5228 deg
Mean motion: 15
53929748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2086
Checksum: 330
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