[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 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 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
069/22:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
5
072/21:25:54
157 -0
5 0
7 0
7
N/A 0
4 -0
1 220
9
000/00:01:48
313 0
2 0
0 215
1
073/06:47:30
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
1
077/07:56:00
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
2
080/17:44:26
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2018/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3824391
42 A = 6783091
76 meter
Y = -4141778
98 meter E =
0012199
Z = 3760513
88 I = 51
73629
XDOT = 6128
644521 Wp = 97
10633
YDOT = 1782
668268 meter/sec RA = 164
46282 deg
ZDOT = -4258
984320 TA = 37
92138
MA = 37
83552
Ha = 221
343 n
mi
Hp = 214
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12547215
95 X = 3852155
19
Y = -13588513
72 feet Y = -4098856
40 meter
Z = 12337643
95 Z = 3779159
18
XDOT = 20107
101447 XDOT = 6128
942534
YDOT = 5848
649173 feet/sec YDOT = 1851
204227 meter/sec
ZDOT = -13973
045669 ZDOT = -4229
213116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15679698
28 X = 4779172
04
Y = -9703472
33 feet Y = -2957618
37 meter
Z = 12421251
07 Z = 3785997
32
XDOT = 17152
550105 XDOT = 5228
097272
YDOT = 9956
366400 feet/sec YDOT = 3034
700479 meter/sec
ZDOT = -13840
494126 ZDOT = -4218
582610
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 18066
54029919
00016717 00000-0 10270-3 0 9007
2 25544 51
6405 165
4499 0002886 166
2198 193
9034 15
54180609 22707
Satellite: ISS
Catalog Number: 25544
Epoch time: 18066
54029919 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 165
4499 deg
Eccentricity:
0002886
Arg of perigee: 166
2198 deg
Mean anomaly: 193
9034 deg
Mean motion: 15
54180609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 328
Coasting Arc #2 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2018/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5047421
01 A = 6786760
80 meter
Y = 3874344
33 meter E =
0004618
Z = -2362378
37 I = 51
78015
XDOT = -4666
282939 Wp = 74
17316
YDOT = -2793
462744 meter/sec RA = 159
49047 deg
ZDOT = 5398
576272 TA = 259
52996
MA = 259
58201
Ha = 221
257 n
mi
Hp = 214
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16559780
21 X = -5078894
73
Y = 12711103
45 feet Y = 3817724
42 meter
Z = -7750585
20 Z = -2386973
60
XDOT = -15309
327228 XDOT = -4660
922142
YDOT = -9164
904017 feet/sec YDOT = -2845
613888 meter/sec
ZDOT = 17711
864410 ZDOT = 5375
922500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19197382
46 X = -5851362
17
Y = 8095664
19 feet Y = 2467558
44 meter
Z = -7860710
56 Z = -2395944
58
XDOT = -11998
865591 XDOT = -3657
254232
YDOT = -11384
475659 feet/sec YDOT = -3469
988181 meter/sec
ZDOT = 17611
153863 ZDOT = 5367
879697
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 18067
50478685
00016717 00000-0 10270-3 0 9013
2 25544 51
6408 160
6417 0002573 171
6850 188
4345 15
54173477 22850
Satellite: ISS
Catalog Number: 25544
Epoch time: 18067
50478685 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 160
6417 deg
Eccentricity:
0002573
Arg of perigee: 171
6850 deg
Mean anomaly: 188
4345 deg
Mean motion: 15
54173477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 327
Coasting Arc #3 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2018/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5842520
33 A = 6788933
54 meter
Y = -3373847
14 meter E =
0015294
Z = 678167
71 I = 51
81687
XDOT = 2910
362210 Wp = 135
16215
YDOT = 3823
412860 meter/sec RA = 154
52920 deg
ZDOT = -5980
577175 TA = 37
52780
MA = 37
42114
Ha = 221
267 n
mi
Hp = 214
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19168373
80 X = 5876519
23
Y = -11069052
30 feet Y = -3308321
91 meter
Z = 2224959
68 Z = 706631
26
XDOT = 9548
432449 XDOT = 2896
441722
YDOT = 12544
005446 feet/sec YDOT = 3855
880225 meter/sec
ZDOT = -19621
316191 ZDOT = -5966
473874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21234563
03 X = 6472294
81
Y = -6201688
54 feet Y = -1890274
67 meter
Z = 2352298
98 Z = 716980
73
XDOT = 5968
687574 XDOT = 1819
255973
YDOT = 12934
086627 feet/sec YDOT = 3942
309604 meter/sec
ZDOT = -19558
850032 ZDOT = -5961
537490
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 18068
53357286
00016717 00000-0 10270-3 0 9021
2 25544 51
6398 155
5132 0002752 173
1869 186
9322 15
54190992 23019
Satellite: ISS
Catalog Number: 25544
Epoch time: 18068
53357286 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 155
5132 deg
Eccentricity:
0002752
Arg of perigee: 173
1869 deg
Mean anomaly: 186
9322 deg
Mean motion: 15
54190992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 324
Coasting Arc #4 (Orbit 2316)
---------------------------------------
Vector Time (GMT): 2018/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6152223
48 A = 6788708
17 meter
Y = 2660207
38 meter E =
0012402
Z = 1046347
91 I = 51
84585
XDOT = -1048
582093 Wp = 66
60707
YDOT = -4770
118667 meter/sec RA = 149
57182 deg
ZDOT = 5911
411454 TA = 304
70461
MA = 304
82139
Ha = 221
168 n
mi
Hp = 214
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20184460
24 X = -6186595
95
Y = 8727714
49 feet Y = 2591216
88 meter
Z = 3432899
96 Z = 1016379
16
XDOT = -3440
229964 XDOT = -1023
877628
YDOT = -15649
995626 feet/sec YDOT = -4781
706049 meter/sec
ZDOT = 19394
394535 ZDOT = 5906
378226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21635213
08 X = -6594412
95
Y = 4050307
56 feet Y = 1234533
74 meter
Z = 3298909
09 Z = 1005507
49
XDOT = 270
888558 XDOT = 82
566833
YDOT = -14472
444852 feet/sec YDOT = -4411
201191 meter/sec
ZDOT = 19372
492642 ZDOT = 5904
735757
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 18069
56235518
00016717 00000-0 10270-3 0 9039
2 25544 51
6403 150
3841 0002598 177
5577 182
5589 15
54195365 23171
Satellite: ISS
Catalog Number: 25544
Epoch time: 18069
56235518 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 150
3841 deg
Eccentricity:
0002598
Arg of perigee: 177
5577 deg
Mean anomaly: 182
5589 deg
Mean motion: 15
54195365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2317
Checksum: 334
Coasting Arc #5 (Orbit 2322)
---------------------------------------
Vector Time (GMT): 2018/069/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 43054
11 A = 6778619
13 meter
Y = 4616902
91 meter E =
0013398
Z = -4975437
08 I = 51
82431
XDOT = -6936
256078 Wp = 114
92518
YDOT = 2409
267777 meter/sec RA = 147
38009 deg
ZDOT = 2174
717034 TA = 176
25625
MA = 176
24621
Ha = 221
075 n
mi
Hp = 214
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 141253
63 X = 15591
23
Y = 15147319
24 feet Y = 4617230
43 meter
Z = -16323612
48 Z = -4975295
00
XDOT = -22756
745664 XDOT = -6973
245163
YDOT = 7904
421842 feet/sec YDOT = 2331
495143 meter/sec
ZDOT = 7134
898405 ZDOT = 2140
933460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8582434
38 X = 2615926
00
Y = -12482239
20 feet Y = -3804586
51 meter
Z = -16323513
16 Z = -4975406
81
XDOT = 22250
333990 XDOT = 6781
901800
YDOT = 6161
640639 feet/sec YDOT = 1878
068067 meter/sec
ZDOT = 6983
910047 ZDOT = 2128
695782
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 18069
94814856
00016717 00000-0 10270-3 0 9040
2 25544 51
6399 148
4624 0002184 176
4177 183
6992 15
54210956 23238
Satellite: ISS
Catalog Number: 25544
Epoch time: 18069
94814856 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 148
4624 deg
Eccentricity:
0002184
Arg of perigee: 176
4177 deg
Mean anomaly: 183
6992 deg
Mean motion: 15
54210956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2323
Checksum: 342
Coasting Arc #6 (Orbit 2338)
---------------------------------------
Vector Time (GMT): 2018/070/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1504837
53 A = 6782015
92 meter
Y = -5199362
57 meter E =
0010396
Z = 4077437
31 I = 51
86287
XDOT = 6513
238128 Wp = 89
22794
YDOT = -1167
161943 meter/sec RA = 142
40206 deg
ZDOT = -3883
449991 TA = 40
86652
MA = 40
78861
Ha = 221
057 n
mi
Hp = 214
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4937130
99 X = 1543060
58
Y = -17058276
15 feet Y = -5182320
39 meter
Z = 13377419
00 Z = 4084840
45
XDOT = 21368
891495 XDOT = 6544
669083
YDOT = -3829
271465 feet/sec YDOT = -1094
151011 meter/sec
ZDOT = -12740
977662 ZDOT = -3851
734922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13650866
33 X = -4160784
06
Y = 11318694
15 feet Y = 3449937
98 meter
Z = 13411055
07 Z = 4087689
59
XDOT = -19028
792707 XDOT = -5799
976017
YDOT = -7987
550572 feet/sec YDOT = -2434
605414 meter/sec
ZDOT = -12599
342329 ZDOT = -3840
279542
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 18070
97692660
00016717 00000-0 10270-3 0 9053
2 25544 51
6399 143
3341 0002164 177
9380 182
1782 15
54203509 23392
Satellite: ISS
Catalog Number: 25544
Epoch time: 18070
97692660 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 143
3341 deg
Eccentricity:
0002164
Arg of perigee: 177
9380 deg
Mean anomaly: 182
1782 deg
Mean motion: 15
54203509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2339
Checksum: 319
Coasting Arc #7 (Orbit 2353)
---------------------------------------
Vector Time (GMT): 2018/071/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2811524
08 A = 6785761
45 meter
Y = 5524464
89 meter E =
0003978
Z = -2763892
36 I = 51
90148
XDOT = -5656
110339 Wp = 86
36776
YDOT = -299
703229 meter/sec RA = 137
43516 deg
ZDOT = 5161
177253 TA = 242
46876
MA = 242
50918
Ha = 220
955 n
mi
Hp = 214
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9224160
37 X = -2859665
85
Y = 18124884
82 feet Y = 5492755
07 meter
Z = -9067888
32 Z = -2777667
00
XDOT = -18556
792451 XDOT = -5677
408519
YDOT = -983
278310 feet/sec YDOT = -363
072362 meter/sec
ZDOT = 16932
996236 ZDOT = 5133
650533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17642042
04 X = 5377294
41
Y = -10061044
84 feet Y = -3066606
47 meter
Z = -9130000
66 Z = -2782824
20
XDOT = 14294
981389 XDOT = 4357
110327
YDOT = 9831
282748 feet/sec YDOT = 2996
574982 meter/sec
ZDOT = 16810
204875 ZDOT = 5123
750446
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 18071
94140361
00016717 00000-0 10270-3 0 9068
2 25544 51
6404 138
5255 0002149 183
0365 177
0775 15
54225575 23542
Satellite: ISS
Catalog Number: 25544
Epoch time: 18071
94140361 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 138
5255 deg
Eccentricity:
0002149
Arg of perigee: 183
0365 deg
Mean anomaly: 177
0775 deg
Mean motion: 15
54225575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2354
Checksum: 304
Coasting Arc #8 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2018/072/21:26:48
313
Vector Time (MET): N/A
Weight (LBS) : 904719
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1152542
14 A = 6779067
35 meter
Y = 4487276
21 meter E =
0012252
Z = -4960254
92 I = 51
90018
XDOT = -6110
054533 Wp = 115
98076
YDOT = 4040
788025 meter/sec RA = 132
68183 deg
ZDOT = 2234
835821 TA = 175
79003
MA = 175
77971
Ha = 220
888 n
mi
Hp = 215
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3781306
22 X = 1126372
47
Y = 14722034
80 feet Y = 4500017
89 meter
Z = -16273802
23 Z = -4954720
38
XDOT = -20046
110672 XDOT = -6165
641102
YDOT = 13257
178561 feet/sec YDOT = 3972
150621 meter/sec
ZDOT = 7332
138521 ZDOT = 2205
020329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8273402
77 X = 2521733
17
Y = -12781760
49 feet Y = -3895880
60 meter
Z = -16249634
75 Z = -4952888
67
XDOT = 22396
142434 XDOT = 6826
344214
YDOT = 5340
982138 feet/sec YDOT = 1627
931356 meter/sec
ZDOT = 7198
608789 ZDOT = 2194
135959
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 18072
90587913
00016717 00000-0 10270-3 0 9074
2 25544 51
6403 133
7166 0002060 204
1582 155
9475 15
54088844 23691
Satellite: ISS
Catalog Number: 25544
Epoch time: 18072
90587913 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 133
7166 deg
Eccentricity:
0002060
Arg of perigee: 204
1582 deg
Mean anomaly: 155
9475 deg
Mean motion: 15
54088844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2369
Checksum: 319
Coasting Arc #9 (Orbit 2374)
---------------------------------------
Vector Time (GMT): 2018/073/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -569422
49 A = 6782700
03 meter
Y = 5457769
45 meter E =
0007195
Z = -3994952
74 I = 51
92028
XDOT = -6115
021516 Wp = 128
33270
YDOT = 2292
576821 meter/sec RA = 130
73631 deg
ZDOT = 4004
183740 TA = 183
27422
MA = 183
27893
Ha = 220
950 n
mi
Hp = 215
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1868184
03 X = -611005
35
Y = 17906067
76 feet Y = 5451168
84 meter
Z = -13106800
33 Z = -3997820
35
XDOT = -20062
406547 XDOT = -6159
653171
YDOT = 7521
577497 feet/sec YDOT = 2223
945331 meter/sec
ZDOT = 13137
085762 ZDOT = 3974
370896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17971418
86 X = -5477688
47
Y = -890436
95 feet Y = -271405
18 meter
Z = -13120244
48 Z = -3999050
52
XDOT = -8578
626266 XDOT = -2614
765286
YDOT = -18439
852889 feet/sec YDOT = -5620
467161 meter/sec
ZDOT = 13003
769001 ZDOT = 3963
548791
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 18073
29170115
00016717 00000-0 10270-3 0 9080
2 25544 51
6396 131
7891 0002524 201
5186 158
5861 15
54079654 23755
Satellite: ISS
Catalog Number: 25544
Epoch time: 18073
29170115 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 131
7891 deg
Eccentricity:
0002524
Arg of perigee: 201
5186 deg
Mean anomaly: 158
5861 deg
Mean motion: 15
54079654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2375
Checksum: 319
Coasting Arc #10 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2018/074/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1747012
27 A = 6786452
31 meter
Y = -5985742
26 meter E =
0013318
Z = 2660224
16 I = 51
95333
XDOT = 5562
439979 Wp = 113
11633
YDOT = -710
454551 meter/sec RA = 125
77484 deg
ZDOT = -5235
878872 TA = 36
99673
MA = 36
90496
Ha = 220
943 n
mi
Hp = 215
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5731667
57 X = 1800894
85
Y = -19638262
01 feet Y = -5965904
36 meter
Z = 8727769
55 Z = 2668842
03
XDOT = 18249
474998 XDOT = 5595
403841
YDOT = -2330
887634 feet/sec YDOT = -648
067859 meter/sec
ZDOT = -17178
080289 ZDOT = -5208
778711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19972834
02 X = 6087719
81
Y = 4349007
17 feet Y = 1325577
38 meter
Z = 8766946
27 Z = 2672165
22
XDOT = 3871
166500 XDOT = 1179
931549
YDOT = 16709
152776 feet/sec YDOT = 5092
949766 meter/sec
ZDOT = -17057
046610 ZDOT = -5198
987807
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 18074
32055946
00016717 00000-0 10270-3 0 9090
2 25544 51
6395 126
6604 0002533 202
7268 157
3773 15
54076933 23917
Satellite: ISS
Catalog Number: 25544
Epoch time: 18074
32055946 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 126
6604 deg
Eccentricity:
0002533
Arg of perigee: 202
7268 deg
Mean anomaly: 157
3773 deg
Mean motion: 15
54076933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 321
Coasting Arc #11 (Orbit 2405)
---------------------------------------
Vector Time (GMT): 2018/075/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2682793
35 A = 6788932
54 meter
Y = 6139515
23 meter E =
0007110
Z = -1077005
86 I = 51
98015
XDOT = -4761
049779 Wp = 42
28210
YDOT = -1047
534045 meter/sec RA = 120
82385 deg
ZDOT = 5915
879281 TA = 306
09568
MA = 306
16150
Ha = 220
838 n
mi
Hp = 215
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8801815
44 X = -2746016
22
Y = 20142766
50 feet Y = 6109160
74 meter
Z = -3533483
79 Z = -1090192
17
XDOT = -15620
242056 XDOT = -4777
717997
YDOT = -3436
791485 feet/sec YDOT = -1100
867767 meter/sec
ZDOT = 19409
052760 ZDOT = 5892
711697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20808503
63 X = -6342431
91
Y = -7055811
10 feet Y = -2150611
22 meter
Z = -3593078
25 Z = -1095170
25
XDOT = 1586
189163 XDOT = 483
470457
YDOT = -14463
512054 feet/sec YDOT = -4408
478474 meter/sec
ZDOT = 19305
774896 ZDOT = 5884
400188
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 18075
28511207
00016717 00000-0 10270-3 0 9105
2 25544 51
6396 121
8528 0002429 207
2100 152
8925 15
54088442 24063
Satellite: ISS
Catalog Number: 25544
Epoch time: 18075
28511207 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 121
8528 deg
Eccentricity:
0002429
Arg of perigee: 207
2100 deg
Mean anomaly: 152
8925 deg
Mean motion: 15
54088442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2406
Checksum: 292
Coasting Arc #12 (Orbit 2421)
---------------------------------------
Vector Time (GMT): 2018/076/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3393686
24 A = 6789231
07 meter
Y = -5836936
72 meter E =
0011716
Z = -647391
58 I = 51
99722
XDOT = 3814
535136 Wp = 151
15902
YDOT = 2877
148404 meter/sec RA = 115
87774 deg
ZDOT = -5999
483624 TA = 35
79817
MA = 35
71970
Ha = 220
783 n
mi
Hp = 215
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11134141
19 X = 3461848
88
Y = -19150054
85 feet Y = -5798605
16 meter
Z = -2123988
13 Z = -630739
98
XDOT = 12514
879055 XDOT = 3811
220657
YDOT = 9439
463267 feet/sec YDOT = 2919
785764 meter/sec
ZDOT = -19683
345223 ZDOT = -5980
962564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20179182
90 X = 6150614
95
Y = 9154638
09 feet Y = 2790333
69 meter
Z = -2048952
20 Z = -624520
63
XDOT = -7443
604151 XDOT = -2268
810545
YDOT = 12062
482911 feet/sec YDOT = 3676
644791 meter/sec
ZDOT = -19601
026702 ZDOT = -5974
392939
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 18076
31396631
00016717 00000-0 10270-3 0 9113
2 25544 51
6396 116
7241 0002475 211
8903 148
2101 15
54105473 24228
Satellite: ISS
Catalog Number: 25544
Epoch time: 18076
31396631 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 116
7241 deg
Eccentricity:
0002475
Arg of perigee: 211
8903 deg
Mean anomaly: 148
2101 deg
Mean motion: 15
54105473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2422
Checksum: 285
Coasting Arc #13 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/077/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3853342
92 A = 6787218
58 meter
Y = 5095756
02 meter E =
0012095
Z = 2277084
15 I = 52
00471
XDOT = -2817
925550 Wp = 78
78152
YDOT = -4582
972886 meter/sec RA = 110
92997 deg
ZDOT = 5465
192062 TA = 306
43433
MA = 306
54577
Ha = 220
729 n
mi
Hp = 215
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12642201
19 X = -3921099
49
Y = 16718359
65 feet Y = 5052286
77 meter
Z = 7470748
52 Z = 2258200
73
XDOT = -9245
162565 XDOT = -2793
014974
YDOT = -15036
000282 feet/sec YDOT = -4614
344792 meter/sec
ZDOT = 17930
420152 ZDOT = 5451
564789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18101855
69 X = -5517445
61
Y = -10626063
44 feet Y = -3238824
14 meter
Z = 7385829
69 Z = 2251200
89
XDOT = 13047
587601 XDOT = 3976
904701
YDOT = -9754
807632 feet/sec YDOT = -2973
265366 meter/sec
ZDOT = 17870
158574 ZDOT = 5446
824333
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 18077
34281744
00016717 00000-0 10270-3 0 9126
2 25544 51
6403 111
5953 0002345 214
1368 145
9634 15
54116482 24381
Satellite: ISS
Catalog Number: 25544
Epoch time: 18077
34281744 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 111
5953 deg
Eccentricity:
0002345
Arg of perigee: 214
1368 deg
Mean anomaly: 145
9634 deg
Mean motion: 15
54116482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 301
Coasting Arc #14 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/077/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904719
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2754010
29 A = 6778956
88 meter
Y = 3711313
97 meter E =
0011751
Z = -4970257
90 I = 51
97796
XDOT = -4138
395576 Wp = 116
75508
YDOT = 6049
349365 meter/sec RA = 110
65855 deg
ZDOT = 2222
899011 TA = 174
86893
MA = 174
85688
Ha = 220
639 n
mi
Hp = 215
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9035466
83 X = 2736447
48
Y = 12176226
92 feet Y = 3742012
28 meter
Z = -16306620
42 Z = -4956923
13
XDOT = -13577
413307 XDOT = -4216
531098
YDOT = 19846
946737 feet/sec YDOT = 6002
634418 meter/sec
ZDOT = 7292
975759 ZDOT = 2202
605557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7412858
05 X = -2259439
13
Y = 13299340
35 feet Y = 4053638
94 meter
Z = -16247557
18 Z = -4952255
43
XDOT = -22700
646598 XDOT = -6919
157083
YDOT = -3850
466776 feet/sec YDOT = -1173
622273 meter/sec
ZDOT = 7201
644491 ZDOT = 2195
061241
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 18077
34281726
00016717 00000-0 10270-3 0 9137
2 25544 51
6404 111
5968 0002292 216
9212 143
1783 15
54127115 24387
Satellite: ISS
Catalog Number: 25544
Epoch time: 18077
34281726 = yrday
fracday
Element set: 913
Inclination: 51
6404 deg
RA of node: 111
5968 deg
Eccentricity:
0002292
Arg of perigee: 216
9212 deg
Mean anomaly: 143
1783 deg
Mean motion: 15
54127115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 298
Coasting Arc #15 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2018/078/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904719
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1891111
55 A = 6782344
62 meter
Y = -5067788
61 meter E =
0008930
Z = 4084415
80 I = 51
99934
XDOT = 4514
981321 Wp = 85
96427
YDOT = -4828
169596 meter/sec RA = 105
69039 deg
ZDOT = -3892
230212 TA = 44
15397
MA = 44
08272
Ha = 220
687 n
mi
Hp = 215
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6204434
21 X = -1854141
55
Y = -16626603
05 feet Y = -5088729
04 meter
Z = 13400314
31 Z = 4075319
94
XDOT = 14812
930843 XDOT = 4587
542068
YDOT = -15840
451432 feet/sec YDOT = -4777
274799 meter/sec
ZDOT = -12769
784160 ZDOT = -3870
121093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12420470
55 X = 3785759
42
Y = -12717717
48 feet Y = -3876360
29 meter
Z = 13360349
17 Z = 4072234
43
XDOT = 19719
087851 XDOT = 6010
377977
YDOT = 5920
111203 feet/sec YDOT = 1804
449895 meter/sec
ZDOT = -12670
486698 ZDOT = -3861
964346
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 18078
37166752
00016717 00000-0 10270-3 0 9143
2 25544 51
6400 106
4680 0002229 221
4533 138
6450 15
54109871 24541
Satellite: ISS
Catalog Number: 25544
Epoch time: 18078
37166752 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 106
4680 deg
Eccentricity:
0002229
Arg of perigee: 221
4533 deg
Mean anomaly: 138
6450 deg
Mean motion: 15
54109871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 298
Coasting Arc #16 (Orbit 2468)
---------------------------------------
Vector Time (GMT): 2018/079/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904719
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1068300
10 A = 6786134
68 meter
Y = 6090246
07 meter E =
0002475
Z = -2797107
62 I = 52
01937
XDOT = -4696
305970 Wp = 69
99966
YDOT = 3186
886569 meter/sec RA = 100
73305 deg
ZDOT = 5149
773782 TA = 258
47337
MA = 258
50116
Ha = 220
526 n
mi
Hp = 215
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3504921
57 X = 1013704
83
Y = 19981122
27 feet Y = 6101886
92 meter
Z = -9176862
28 Z = -2792051
55
XDOT = -15407
827984 XDOT = -4756
608539
YDOT = 10455
664598 feet/sec YDOT = 3134
032728 meter/sec
ZDOT = 16895
583275 ZDOT = 5126
813810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16409594
30 X = -5001644
34
Y = 11943801
29 feet Y = 3640470
63 meter
Z = -9155072
33 Z = -2790466
05
XDOT = -15319
586526 XDOT = -4669
409973
YDOT = -8187
152431 feet/sec YDOT = -2495
444061 meter/sec
ZDOT = 16792
683785 ZDOT = 5118
410018
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 18079
33621247
00016717 00000-0 10270-3 0 9156
2 25544 51
6396 101
6601 0002341 228
7909 131
3042 15
54091145 24694
Satellite: ISS
Catalog Number: 25544
Epoch time: 18079
33621247 = yrday
fracday
Element set: 915
Inclination: 51
6396 deg
RA of node: 101
6601 deg
Eccentricity:
0002341
Arg of perigee: 228
7909 deg
Mean anomaly: 131
3042 deg
Mean motion: 15
54091145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2469
Checksum: 294
Coasting Arc #17 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2018/080/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904719
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -262950
78 A = 6788777
53 meter
Y = -6669921
79 meter E =
0013176
Z = 1196830
89 I = 52
03378
XDOT = 4748
666616 Wp = 130
93328
YDOT = -1250
658949 meter/sec RA = 95
78516 deg
ZDOT = -5892
862810 TA = 36
13101
MA = 36
04206
Ha = 220
521 n
mi
Hp = 215
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -862699
42 X = -194159
97
Y = -21882945
51 feet Y = -6672477
53 meter
Z = 3926610
52 Z = 1195721
37
XDOT = 15579
614881 XDOT = 4790
923474
YDOT = -4103
211776 feet/sec YDOT = -1197
320464 meter/sec
ZDOT = -19333
539402 ZDOT = -5869
692539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19109663
22 X = 5824625
35
Y = -10698614
96 feet Y = -3260937
84 meter
Z = 3922529
09 Z = 1195586
87
XDOT = 9990
383895 XDOT = 3045
069011
YDOT = 10753
570106 feet/sec YDOT = 3277
688168 meter/sec
ZDOT = -19229
942752 ZDOT = -5861
286551
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 18080
36505853
00016717 00000-0 10270-3 0 9166
2 25544 51
6399 96
5313 0002171 230
7774 129
3186 15
54110799 24854
Satellite: ISS
Catalog Number: 25544
Epoch time: 18080
36505853 = yrday
fracday
Element set: 916
Inclination: 51
6399 deg
RA of node: 96
5313 deg
Eccentricity:
0002171
Arg of perigee: 230
7774 deg
Mean anomaly: 129
3186 deg
Mean motion: 15
54110799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 324
Coasting Arc #18 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2018/080/17:44:26
000
Vector Time (MET): N/A
Weight (LBS) : 904719
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3602233
88 A = 6779472
39 meter
Y = 3077450
54 meter E =
0010460
Z = -4859078
93 I = 52
00335
XDOT = -2421
024468 Wp = 115
34314
YDOT = 6815
589536 meter/sec RA = 93
75151 deg
ZDOT = 2521
656110 TA = 179
35020
MA = 179
34884
Ha = 220
472 n
mi
Hp = 215
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11818352
62 X = 3591156
24
Y = 10096622
52 feet Y = 3117670
77 meter
Z = -15941860
00 Z = -4841607
64
XDOT = -7942
993663 XDOT = -2509
307254
YDOT = 22360
858058 feet/sec YDOT = 6788
022610 meter/sec
ZDOT = 8273
149968 ZDOT = 2509
680436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11205373
55 X = 3415397
86
Y = -10886809
80 feet Y = -3318299
63 meter
Z = -15864271
84 Z = -4835430
06
XDOT = 20685
463838 XDOT = 6304
929378
YDOT = 9313
707942 feet/sec YDOT = 2838
818181 meter/sec
ZDOT = 8218
791211 ZDOT = 2505
087561
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 18080
75087600
00016717 00000-0 10270-3 0 9175
2 25544 51
6393 94
6091 0001839 240
3695 119
7274 15
54115334 24917
Satellite: ISS
Catalog Number: 25544
Epoch time: 18080
75087600 = yrday
fracday
Element set: 917
Inclination: 51
6393 deg
RA of node: 94
6091 deg
Eccentricity:
0001839
Arg of perigee: 240
3695 deg
Mean anomaly: 119
7274 deg
Mean motion: 15
54115334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 316
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