[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 8th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
013/10:05:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 214
3
017/20:15:11
040 0
9 1
1 1
1
N/A 0
5 -0
1 221
6
000/00:00:22
080 -0
3 -0
0 214
4
018/18:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
3
Coasting Arc #1 (Orbit 1367)
---------------------------------------
Vector Time (GMT): 2018/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2869618
53 A = 6781925
70 meter
Y = -4604161
56 meter E =
0011217
Z = 4065134
05 I = 52
01473
XDOT = 3447
421961 Wp = 60
93880
YDOT = -5619
943533 meter/sec RA = 93
87684 deg
ZDOT = -3918
130541 TA = 69
52597
MA = 69
40559
Ha = 220
928 n
mi
Hp = 214
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9414758
97 X = -2837666
42
Y = -15105516
92 feet Y = -4636073
04 meter
Z = 13337053
98 Z = 4051272
04
XDOT = 11310
439503 XDOT = 3529
041542
YDOT = -18438
134951 feet/sec YDOT = -5580
935645 meter/sec
ZDOT = -12854
758993 ZDOT = -3901
186171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11637872
96 X = 3547223
68
Y = -13527686
88 feet Y = -4123238
96 meter
Z = 13276028
68 Z = 4046533
54
XDOT = 19990
068848 XDOT = 6092
972985
YDOT = 4613
288177 feet/sec YDOT = 1406
130236 meter/sec
ZDOT = -12778
435824 ZDOT = -3894
867239
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 18008
54103844
00016717 00000-0 10270-3 0 9003
2 25544 51
6416 94
5927 0003284 348
0807 12
0268 15
54285888 13689
Satellite: ISS
Catalog Number: 25544
Epoch time: 18008
54103844 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 94
5927 deg
Eccentricity:
0003284
Arg of perigee: 348
0807 deg
Mean anomaly: 12
0268 deg
Mean motion: 15
54285888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1368
Checksum: 316
Coasting Arc #2 (Orbit 1382)
---------------------------------------
Vector Time (GMT): 2018/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2238425
58 A = 6785822
12 meter
Y = 5793690
98 meter E =
0006856
Z = -2727505
22 I = 52
02789
XDOT = -3984
563769 Wp = 30
27489
YDOT = 3982
278963 meter/sec RA = 88
91997 deg
ZDOT = 5200
393469 TA = 299
05811
MA = 299
12676
Ha = 220
994 n
mi
Hp = 214
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7343915
94 X = 2186721
32
Y = 19008172
50 feet Y = 5818433
57 meter
Z = -8948507
94 Z = -2716757
17
XDOT = -13072
715778 XDOT = -4054
059197
YDOT = 13065
219695 feet/sec YDOT = 3937
332108 meter/sec
ZDOT = 17061
658363 ZDOT = 5180
869261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15765746
37 X = -4805399
49
Y = 12943078
35 feet Y = 3945050
28 meter
Z = -8901543
77 Z = -2713190
54
XDOT = -15573
267694 XDOT = -4746
731993
YDOT = -7321
594382 feet/sec YDOT = -2231
621968 meter/sec
ZDOT = 16974
087200 ZDOT = 5173
701778
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 18009
50548029
00016717 00000-0 10270-3 0 9019
2 25544 51
6408 89
7847 0003295 349
5494 10
5589 15
54259663 13835
Satellite: ISS
Catalog Number: 25544
Epoch time: 18009
50548029 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 89
7847 deg
Eccentricity:
0003295
Arg of perigee: 349
5494 deg
Mean anomaly: 10
5589 deg
Mean motion: 15
54259663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1383
Checksum: 338
Coasting Arc #3 (Orbit 1398)
---------------------------------------
Vector Time (GMT): 2018/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1518803
89 A = 6788409
19 meter
Y = -6526826
17 meter E =
0011840
Z = 1057329
11 I = 52
03542
XDOT = 4437
372514 Wp = 110
86275
YDOT = -2000
325644 meter/sec RA = 83
97225 deg
ZDOT = -5924
579585 TA = 57
73559
MA = 57
62091
Ha = 221
033 n
mi
Hp = 214
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4982952
38 X = -1450842
21
Y = -21413471
70 feet Y = -6543430
53 meter
Z = 3468927
52 Z = 1050116
10
XDOT = 14558
308773 XDOT = 4488
189284
YDOT = -6562
748175 feet/sec YDOT = -1950
419521 meter/sec
ZDOT = -19437
597064 ZDOT = -5902
901101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18598210
19 X = 5668734
47
Y = -11734049
34 feet Y = -3576538
24 meter
Z = 3437834
56 Z = 1047851
97
XDOT = 10151
070466 XDOT = 3094
046278
YDOT = 10375
041837 feet/sec YDOT = 3162
312752 meter/sec
ZDOT = -19340
733448 ZDOT = -5895
055555
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 18010
53421523
00016717 00000-0 10270-3 0 9024
2 25544 51
6411 84
6555 0003314 355
6325 4
4798 15
54284979 13991
Satellite: ISS
Catalog Number: 25544
Epoch time: 18010
53421523 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 84
6555 deg
Eccentricity:
0003314
Arg of perigee: 355
6325 deg
Mean anomaly: 4
4798 deg
Mean motion: 15
54284979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1399
Checksum: 309
Coasting Arc #4 (Orbit 1414)
---------------------------------------
Vector Time (GMT): 2018/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 745541
56 A = 6788764
31 meter
Y = 6702764
66 meter E =
0015666
Z = 696861
19 I = 52
03220
XDOT = -4785
527698 Wp = 42
11994
YDOT = -98
022979 meter/sec RA = 79
02801 deg
ZDOT = 5996
293818 TA = 325
37131
MA = 325
47323
Ha = 221
247 n
mi
Hp = 214
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2446002
50 X = 667149
06
Y = 21990697
72 feet Y = 6710663
46 meter
Z = 2286290
01 Z = 700292
73
XDOT = -15700
550191 XDOT = -4813
202637
YDOT = -321
597701 feet/sec YDOT = -151
693096 meter/sec
ZDOT = 19672
879979 ZDOT = 5972
980243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19820098
92 X = -6041166
15
Y = 9832203
19 feet Y = 2996855
53 meter
Z = 2300499
00 Z = 701192
10
XDOT = -4416
566873 XDOT = -1346
169583
YDOT = -13532
392882 feet/sec YDOT = -4124
673351 meter/sec
ZDOT = 19569
063161 ZDOT = 5964
650452
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 18011
56294721
00016717 00000-0 10270-3 0 9037
2 25544 51
6414 79
5260 0003555
6843 359
4314 15
54253034 14153
Satellite: ISS
Catalog Number: 25544
Epoch time: 18011
56294721 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 79
5260 deg
Eccentricity:
0003555
Arg of perigee:
6843 deg
Mean anomaly: 359
4314 deg
Mean motion: 15
54253034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1415
Checksum: 284
Coasting Arc #5 (Orbit 1429)
---------------------------------------
Vector Time (GMT): 2018/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 145984
76 A = 6786400
20 meter
Y = -6344237
36 meter E =
0004401
Z = -2408263
48 I = 52
01672
XDOT = 4995
637418 Wp = 94
76668
YDOT = 2159
230288 meter/sec RA = 74
08159 deg
ZDOT = -5394
182638 TA = 111
98693
MA = 111
94016
Ha = 221
230 n
mi
Hp = 214
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 478952
61 X = 228614
89
Y = -20814427
04 feet Y = -6342142
69 meter
Z = -7901126
89 Z = -2407354
07
XDOT = 16389
886543 XDOT = 4997
323002
YDOT = 7084
088873 feet/sec YDOT = 2215
104709 meter/sec
ZDOT = -17697
449599 ZDOT = -5369
911445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19615251
69 X = 5978728
71
Y = -6985122
76 feet Y = -2129065
42 meter
Z = -7896045
59 Z = -2406714
69
XDOT = -1186
725551 XDOT = -361
713948
YDOT = 16518
339488 feet/sec YDOT = 5034
789876 meter/sec
ZDOT = -17589
699923 ZDOT = -5361
340537
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 18012
52737984
00016717 00000-0 10270-3 0 9048
2 25544 51
6406 74
7180 0003443 5
6042 354
5148 15
54290229 14309
Satellite: ISS
Catalog Number: 25544
Epoch time: 18012
52737984 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 74
7180 deg
Eccentricity:
0003443
Arg of perigee: 5
6042 deg
Mean anomaly: 354
5148 deg
Mean motion: 15
54290229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1430
Checksum: 291
Coasting Arc #6 (Orbit 1443)
---------------------------------------
Vector Time (GMT): 2018/013/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4323815
52 A = 6784027
72 meter
Y = 3971524
92 meter E =
0006151
Z = -3399977
81 I = 52
00074
XDOT = -1703
756065 Wp = 55
82133
YDOT = 5839
298452 meter/sec RA = 69
46873 deg
ZDOT = 4663
572813 TA = 264
68771
MA = 264
75790
Ha = 221
254 n
mi
Hp = 214
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14185746
45 X = 4295598
68
Y = 13029937
40 feet Y = 4019719
27 meter
Z = -11154782
83 Z = -3379042
59
XDOT = -5589
750868 XDOT = -1791
579062
YDOT = 19157
803319 feet/sec YDOT = 5819
754489 meter/sec
ZDOT = 15300
435737 ZDOT = 4655
083744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14593760
47 X = -4448178
19
Y = 12652823
28 feet Y = 3856580
54 meter
Z = -11062190
99 Z = -3371755
81
XDOT = -17447
827494 XDOT = -5318
097820
YDOT = -6808
346577 feet/sec YDOT = -2075
184037 meter/sec
ZDOT = 15261
665397 ZDOT = 4651
755613
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 18013
42751480
00016717 00000-0 10270-3 0 9056
2 25544 51
6417 70
2294 0003302 5
3979 354
7209 15
54292963 14440
Satellite: ISS
Catalog Number: 25544
Epoch time: 18013
42751480 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 70
2294 deg
Eccentricity:
0003302
Arg of perigee: 5
3979 deg
Mean anomaly: 354
7209 deg
Mean motion: 15
54292963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1444
Checksum: 300
Coasting Arc #7 (Orbit 1459)
---------------------------------------
Vector Time (GMT): 2018/014/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4037981
05 A = 6787431
11 meter
Y = -5129765
11 meter E =
0013599
Z = 1840411
49 I = 51
99991
XDOT = 2859
709682 Wp = 99
63069
YDOT = -4297
573466 meter/sec RA = 64
51521 deg
ZDOT = -5670
867777 TA = 60
22855
MA = 60
09335
Ha = 221
332 n
mi
Hp = 214
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13247969
31 X = -3989258
18
Y = -16829938
03 feet Y = -5174648
30 meter
Z = 6038095
42 Z = 1820914
50
XDOT = 9382
249613 XDOT = 2935
099576
YDOT = -14099
650480 feet/sec YDOT = -4265
172257 meter/sec
ZDOT = -18605
209241 ZDOT = -5656
793668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18059821
58 X = 5504633
62
Y = -11559816
89 feet Y = -3523432
19 meter
Z = 5952107
15 Z = 1814202
26
XDOT = 12250
279957 XDOT = 3733
885331
YDOT = 9534
284933 feet/sec YDOT = 2906
050048 meter/sec
ZDOT = -18541
807066 ZDOT = -5651
542794
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 18014
45623824
00016717 00000-0 10270-3 0 9061
2 25544 51
6419 65
1002 0003459 11
2839 348
8391 15
54302148 14607
Satellite: ISS
Catalog Number: 25544
Epoch time: 18014
45623824 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 65
1002 deg
Eccentricity:
0003459
Arg of perigee: 11
2839 deg
Mean anomaly: 348
8391 deg
Mean motion: 15
54302148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1460
Checksum: 292
Coasting Arc #8 (Orbit 1474)
---------------------------------------
Vector Time (GMT): 2018/015/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3510390
08 A = 6788941
12 meter
Y = 5800398
59 meter E =
0015201
Z = -113525
17 I = 51
98909
XDOT = -3993
644156 Wp = 37
48409
YDOT = 2526
707555 meter/sec RA = 59
56762 deg
ZDOT = 6043
124825 TA = 321
29834
MA = 321
40716
Ha = 221
511 n
mi
Hp = 214
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11517027
81 X = 3445819
00
Y = 19030179
09 feet Y = 5839293
14 meter
Z = -372457
92 Z = -96629
52
XDOT = -13102
507072 XDOT = -4050
955590
YDOT = 8289
722949 feet/sec YDOT = 2481
726975 meter/sec
ZDOT = 19826
525018 ZDOT = 6023
586340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19907276
29 X = -6067737
81
Y = 9926722
16 feet Y = 3025664
91 meter
Z = -298175
25 Z = -90883
81
XDOT = -6459
207692 XDOT = -1968
766504
YDOT = -12414
077831 feet/sec YDOT = -3783
810923 meter/sec
ZDOT = 19739
072634 ZDOT = 6016
469339
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 18015
42066382
00016717 00000-0 10270-3 0 9070
2 25544 51
6414 60
2917 0003663 14
1618 345
9637 15
54261312 14751
Satellite: ISS
Catalog Number: 25544
Epoch time: 18015
42066382 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 60
2917 deg
Eccentricity:
0003663
Arg of perigee: 14
1618 deg
Mean anomaly: 345
9637 deg
Mean motion: 15
54261312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1475
Checksum: 295
Coasting Arc #9 (Orbit 1490)
---------------------------------------
Vector Time (GMT): 2018/016/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2672955
80 A = 6787612
84 meter
Y = -6012480
35 meter E =
0006540
Z = -1664351
33 I = 51
96670
XDOT = 5038
016469 Wp = 114
78249
YDOT = -657
094907 meter/sec RA = 54
61976 deg
ZDOT = -5737
618770 TA = 83
35714
MA = 83
28270
Ha = 221
451 n
mi
Hp = 213
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8769540
03 X = -2597439
56
Y = -19725985
40 feet Y = -6041948
82 meter
Z = -5460470
25 Z = -1677152
43
XDOT = 16528
925423 XDOT = 5072
859718
YDOT = -2155
823185 feet/sec YDOT = -600
561130 meter/sec
ZDOT = -18824
208563 ZDOT = -5713
061650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20248719
23 X = 6171809
62
Y = -7442712
38 feet Y = -2268538
73 meter
Z = -5516472
57 Z = -1681420
84
XDOT = 535
983745 XDOT = 163
367845
YDOT = 15280
517321 feet/sec YDOT = 4657
501679 meter/sec
ZDOT = -18714
713829 ZDOT = -5704
244775
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 18016
44938360
00016717 00000-0 10270-3 0 9088
2 25544 51
6404 55
1626 0003521 19
4561 340
6725 15
54304847 14917
Satellite: ISS
Catalog Number: 25544
Epoch time: 18016
44938360 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 55
1626 deg
Eccentricity:
0003521
Arg of perigee: 19
4561 deg
Mean anomaly: 340
6725 deg
Mean motion: 15
54304847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1491
Checksum: 299
Coasting Arc #10 (Orbit 1506)
---------------------------------------
Vector Time (GMT): 2018/017/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1572223
56 A = 6784358
03 meter
Y = 5750026
31 meter E =
0014677
Z = 3222512
35 I = 51
93648
XDOT = -5876
105249 Wp = 73
92562
YDOT = -1098
133120 meter/sec RA = 49
66300 deg
ZDOT = 4812
150081 TA = 323
23175
MA = 323
33234
Ha = 221
514 n
mi
Hp = 213
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5158213
78 X = 1492155
40
Y = 18864915
71 feet Y = 5767160
11 meter
Z = 10572547
07 Z = 3229955
39
XDOT = -19278
560528 XDOT = -5886
763354
YDOT = -3602
798950 feet/sec YDOT = -1163
903630 meter/sec
ZDOT = 15787
893967 ZDOT = 4783
580584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19085502
08 X = -5817261
04
Y = 4189801
99 feet Y = 1277051
65 meter
Z = 10604722
30 Z = 3232319
36
XDOT = 4820
346678 XDOT = 1469
241667
YDOT = -17798
250317 feet/sec YDOT = -5424
906697 meter/sec
ZDOT = 15660
824819 ZDOT = 4773
419405
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 18017
47809888
00016717 00000-0 10270-3 0 9095
2 25544 51
6408 50
0326 0003587 22
8394 337
2917 15
54313397 15079
Satellite: ISS
Catalog Number: 25544
Epoch time: 18017
47809888 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 50
0326 deg
Eccentricity:
0003587
Arg of perigee: 22
8394 deg
Mean anomaly: 337
2917 deg
Mean motion: 15
54313397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1507
Checksum: 328
Coasting Arc #11 (Orbit 1512)
---------------------------------------
Vector Time (GMT): 2018/017/20:15:22
080
Vector Time (MET): N/A
Weight (LBS) : 904547
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1204958
53 A = 6778912
71 meter
Y = -4459833
79 meter E =
0014387
Z = -4974234
57 I = 51
90864
XDOT = 6083
329993 Wp = 61
81678
YDOT = 4097
756207 meter/sec RA = 47
55371 deg
ZDOT = -2198
592345 TA = 186
77659
MA = 186
79606
Ha = 221
600 n
mi
Hp = 214
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3953276
01 X = 1278901
77
Y = -14632000
63 feet Y = -4445945
42 meter
Z = -16319667
22 Z = -4968202
06
XDOT = 19958
431734 XDOT = 6047
735048
YDOT = 13444
082045 feet/sec YDOT = 4165
585262 meter/sec
ZDOT = -7213
229477 ZDOT = -2169
128451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10674894
90 X = -3253707
97
Y = -10801459
20 feet Y = -3292284
76 meter
Z = -16292037
01 Z = -4965812
88
XDOT = 20825
664958 XDOT = 6347
662679
YDOT = -9889
889626 feet/sec YDOT = -3014
438358 meter/sec
ZDOT = -7082
688447 ZDOT = -2158
803439
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 18017
86386876
00016717 00000-0 10270-3 0 9107
2 25544 51
6421 48
1107 0003404 12
7116 347
4122 15
54125244 15137
Satellite: ISS
Catalog Number: 25544
Epoch time: 18017
86386876 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 48
1107 deg
Eccentricity:
0003404
Arg of perigee: 12
7116 deg
Mean anomaly: 347
4122 deg
Mean motion: 15
54125244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1513
Checksum: 278
Coasting Arc #12 (Orbit 1527)
---------------------------------------
Vector Time (GMT): 2018/018/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 904547
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5094201
25 A = 6781063
67 meter
Y = 58714
88 meter E =
0011612
Z = 4470740
93 I = 51
89197
XDOT = -2966
450642 Wp = 55
54436
YDOT = -6264
199135 meter/sec RA = 42
83455 deg
ZDOT = -3285
394405 TA = 67
49773
MA = 67
37484
Ha = 221
828 n
mi
Hp = 214
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16713258
69 X = -5116195
26
Y = 192634
13 feet Y = 1624
89 meter
Z = 14667785
20 Z = 4445942
16
XDOT = -9732
449612 XDOT = -2880
223825
YDOT = -20551
834431 feet/sec YDOT = -6296
889770 meter/sec
ZDOT = -10778
853035 ZDOT = -3299
594907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12702784
31 X = -3871808
66
Y = 11010805
00 feet Y = 3356093
36 meter
Z = 14557317
43 Z = 4437070
35
XDOT = -19851
784038 XDOT = -6050
823775
YDOT = -8514
954551 feet/sec YDOT = -2595
358147 meter/sec
ZDOT = -10841
033394 ZDOT = -3304
346978
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 18018
82841525
00016717 00000-0 10270-3 0 9112
2 25544 51
6402 43
3026 0003417 16
6908 343
4356 15
54097849 15289
Satellite: ISS
Catalog Number: 25544
Epoch time: 18018
82841525 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 43
3026 deg
Eccentricity:
0003417
Arg of perigee: 16
6908 deg
Mean anomaly: 343
4356 deg
Mean motion: 15
54097849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1528
Checksum: 305
Coasting Arc #13 (Orbit 1542)
---------------------------------------
Vector Time (GMT): 2018/019/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 904547
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5788273
44 A = 6784753
19 meter
Y = 1183962
90 meter E =
0006787
Z = -3336684
15 I = 51
88034
XDOT = 1510
891775 Wp = 57
28818
YDOT = 5855
140174 meter/sec RA = 37
86472 deg
ZDOT = 4709
114579 TA = 264
02450
MA = 264
10185
Ha = 221
774 n
mi
Hp = 214
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18990398
43 X = 5790811
37
Y = 3884392
73 feet Y = 1248705
60 meter
Z = -10947126
48 Z = -3308561
12
XDOT = 4956
994014 XDOT = 1422
431807
YDOT = 19209
777474 feet/sec YDOT = 5871
541293 meter/sec
ZDOT = 15449
850980 ZDOT = 4716
239087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16893285
51 X = 5149073
42
Y = -9646918
88 feet Y = -2940380
87 meter
Z = -10822069
04 Z = -3298566
64
XDOT = 15612
279023 XDOT = 4758
622646
YDOT = 10012
382532 feet/sec YDOT = 3051
774196 meter/sec
ZDOT = 15480
580090 ZDOT = 4718
480811
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 18019
79295932
00016717 00000-0 10270-3 0 9125
2 25544 51
6408 38
4940 0003372 18
7439 341
3838 15
54114879 15439
Satellite: ISS
Catalog Number: 25544
Epoch time: 18019
79295932 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 38
4940 deg
Eccentricity:
0003372
Arg of perigee: 18
7439 deg
Mean anomaly: 341
3838 deg
Mean motion: 15
54114879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1543
Checksum: 328
Coasting Arc #14 (Orbit 1558)
---------------------------------------
Vector Time (GMT): 2018/020/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 904547
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6129705
81 A = 6788070
12 meter
Y = -2262191
50 meter E =
0014249
Z = 1822168
39 I = 51
86542
XDOT = 210
362438 Wp = 100
54775
YDOT = -5162
549280 meter/sec RA = 32
90378 deg
ZDOT = -5666
551647 TA = 59
48237
MA = 59
34178
Ha = 221
814 n
mi
Hp = 214
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20110583
35 X = -6112804
76
Y = -7421888
12 feet Y = -2330643
58 meter
Z = 5978242
76 Z = 1792434
03
XDOT = 690
165479 XDOT = 295
600405
YDOT = -16937
497639 feet/sec YDOT = -5159
720239 meter/sec
ZDOT = -18591
048710 ZDOT = -5665
322802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19907865
75 X = -6067917
48
Y = 8047247
67 feet Y = 2452801
09 meter
Z = 5846200
39 Z = 1781921
88
XDOT = -10196
164700 XDOT = -3107
791001
YDOT = -11637
181471 feet/sec YDOT = -3547
012912 meter/sec
ZDOT = -18584
689106 ZDOT = -5664
613239
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 18020
82180410
00016717 00000-0 10270-3 0 9136
2 25544 51
6415 33
3653 0003366 22
9372 337
1931 15
54099423 15599
Satellite: ISS
Catalog Number: 25544
Epoch time: 18020
82180410 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 33
3653 deg
Eccentricity:
0003366
Arg of perigee: 22
9372 deg
Mean anomaly: 337
1931 deg
Mean motion: 15
54099423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1559
Checksum: 289
Coasting Arc #15 (Orbit 1573)
---------------------------------------
Vector Time (GMT): 2018/021/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 904547
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6046529
35 A = 6789375
51 meter
Y = 3066678
45 meter E =
0015239
Z = -158696
58 I = 51
84225
XDOT = -2025
355314 Wp = 39
70373
YDOT = 4288
295552 meter/sec RA = 27
94705 deg
ZDOT = 6029
295312 TA = 318
59087
MA = 318
70627
Ha = 221
877 n
mi
Hp = 214
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19837694
72 X = 6012558
39
Y = 10061281
00 feet Y = 3134104
94 meter
Z = -520658
07 Z = -129407
67
XDOT = -6644
866515 XDOT = -2102
444300
YDOT = 14069
211129 feet/sec YDOT = 4265
215649 meter/sec
ZDOT = 19781
152598 ZDOT = 6019
269747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21349012
48 X = 6507179
01
Y = -6253125
21 feet Y = -1905952
56 meter
Z = -390746
82 Z = -119099
63
XDOT = 4241
234723 XDOT = 1292
728344
YDOT = 13337
050843 feet/sec YDOT = 4065
133097 meter/sec
ZDOT = 19735
765646 ZDOT = 6015
461369
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 18021
78634315
00016717 00000-0 10270-3 0 9141
2 25544 51
6418 28
5571 0003519 25
1053 335
0270 15
54110862 15749
Satellite: ISS
Catalog Number: 25544
Epoch time: 18021
78634315 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 28
5571 deg
Eccentricity:
0003519
Arg of perigee: 25
1053 deg
Mean anomaly: 335
0270 deg
Mean motion: 15
54110862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1574
Checksum: 284
Coasting Arc #16 (Orbit 1589)
---------------------------------------
Vector Time (GMT): 2018/022/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 904547
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5494766
75 A = 6788348
78 meter
Y = -3665803
90 meter E =
0007324
Z = -1561697
00 I = 51
80955
XDOT = 3830
476698 Wp = 117
39652
YDOT = -3297
605774 meter/sec RA = 22
99030 deg
ZDOT = -5760
828529 TA = 79
62586
MA = 79
54331
Ha = 221
845 n
mi
Hp = 214
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18027449
98 X = -5445780
57
Y = -12026915
68 feet Y = -3726976
27 meter
Z = -5123677
81 Z = -1588269
27
XDOT = 12567
180767 XDOT = 3895
049403
YDOT = -10818
916580 feet/sec YDOT = -3254
409780 meter/sec
ZDOT = -18900
356066 ZDOT = -5742
064789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21284591
92 X = -6487543
62
Y = 3921968
21 feet Y = 1195415
91 meter
Z = -5241377
67 Z = -1597571
91
XDOT = 1840
823131 XDOT = 561
082890
YDOT = -15053
278748 feet/sec YDOT = -4588
239362 meter/sec
ZDOT = -18816
228460 ZDOT = -5735
186435
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 18022
81518450
00016717 00000-0 10270-3 0 9158
2 25544 51
6421 23
4293 0003299 28
7880 331
3454 15
54091841 15906
Satellite: ISS
Catalog Number: 25544
Epoch time: 18022
81518450 = yrday
fracday
Element set: 915
Inclination: 51
6421 deg
RA of node: 23
4293 deg
Eccentricity:
0003299
Arg of perigee: 28
7880 deg
Mean anomaly: 331
3454 deg
Mean motion: 15
54091841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1590
Checksum: 298
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