[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 16th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
050/05:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 214
5
054/08:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
2
000/00:00:00
000 0
0 0
0 214
1
057/02:24:53
072 -3
0 3
0 3
0
N/A -0
1 -0
3 224
4
000/00:07:46
144 -0
3 -0
2 215
7
057/14:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
3
000/00:00:00
000 0
0 0
0 215
7
060/17:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 224
6
000/00:00:00
000 0
0 0
0 215
6
Coasting Arc #1 (Orbit 3633)
---------------------------------------
Vector Time (GMT): 2019/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3694101
45 A = 6791113
16 meter
Y = -5539495
48 meter E =
0014246
Z = -1303255
95 I = 51
30431
XDOT = 3438
820952 Wp = 33
54134
YDOT = -3648
486094 meter/sec RA = 245
32261 deg
ZDOT = 5802
594689 TA = 312
21070
MA = 312
33153
Ha = 223
769 n
mi
Hp = 214
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12119755
41 X = -3625552
31
Y = -18174197
77 feet Y = -5580422
21 meter
Z = -4275774
12 Z = -1321033
76
XDOT = 11282
220972 XDOT = 3451
178482
YDOT = -11970
098734 feet/sec YDOT = -3609
961754 meter/sec
ZDOT = 19037
384150 ZDOT = 5819
328884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 778477
40 X = 237279
91
Y = -21815043
10 feet Y = -6649225
14 meter
Z = -4355461
82 Z = -1327544
76
XDOT = 14450
791214 XDOT = 4404
601162
YDOT = -3273
291026 feet/sec YDOT = -997
699105 meter/sec
ZDOT = 19113
236262 ZDOT = 5825
714413
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 19046
50258410
00016717 00000-0 10270-3 0 9002
2 25544 51
6368 246
3319 0005511 26
3589 333
7842 15
53257573 36343
Satellite: ISS
Catalog Number: 25544
Epoch time: 19046
50258410 = yrday
fracday
Element set: 900
Inclination: 51
6368 deg
RA of node: 246
3319 deg
Eccentricity:
0005511
Arg of perigee: 26
3589 deg
Mean anomaly: 333
7842 deg
Mean motion: 15
53257573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3634
Checksum: 309
Coasting Arc #2 (Orbit 3649)
---------------------------------------
Vector Time (GMT): 2019/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3262249
00 A = 6791767
52 meter
Y = 5952814
94 meter E =
0011675
Z = -139597
91 I = 51
32180
XDOT = -4255
748079 Wp = 107
81020
YDOT = 2201
766740 meter/sec RA = 240
33317 deg
ZDOT = -5980
656382 TA = 73
69900
MA = 73
57062
Ha = 223
895 n
mi
Hp = 214
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10702916
67 X = 3196118
57
Y = 19530232
75 feet Y = 5988925
93 meter
Z = -457998
39 Z = -123912
04
XDOT = -13962
428080 XDOT = -4251
002500
YDOT = 7223
644161 feet/sec YDOT = 2154
202584 meter/sec
ZDOT = -19621
576058 ZDOT = -6001
317208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2313641
90 X = -705198
05
Y = 22151498
31 feet Y = 6751776
68 meter
Z = -387766
46 Z = -118191
22
XDOT = -13867
417468 XDOT = -4226
788844
YDOT = -1765
192626 feet/sec YDOT = -538
030712 meter/sec
ZDOT = -19715
013360 ZDOT = -6009
136072
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 19047
53199069
00016717 00000-0 10270-3 0 9011
2 25544 51
6370 241
2062 0005675 29
7223 330
4250 15
53286579 36501
Satellite: ISS
Catalog Number: 25544
Epoch time: 19047
53199069 = yrday
fracday
Element set: 901
Inclination: 51
6370 deg
RA of node: 241
2062 deg
Eccentricity:
0005675
Arg of perigee: 29
7223 deg
Mean anomaly: 330
4250 deg
Mean motion: 15
53286579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3650
Checksum: 306
Coasting Arc #3 (Orbit 3665)
---------------------------------------
Vector Time (GMT): 2019/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2686499
44 A = 6790887
20 meter
Y = -6035469
90 meter E =
0019025
Z = 1527484
73 I = 51
33449
XDOT = 5037
972399 Wp = 54
51994
YDOT = -781
211114 meter/sec RA = 235
34362 deg
ZDOT = 5734
279489 TA = 322
24885
MA = 322
38217
Ha = 223
966 n
mi
Hp = 214
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8813974
56 X = -2626228
92
Y = -19801410
42 feet Y = -6065175
21 meter
Z = 5011432
85 Z = 1514581
49
XDOT = 16528
780837 XDOT = 5018
480502
YDOT = -2563
028589 feet/sec YDOT = -724
981953 meter/sec
ZDOT = 18813
252916 ZDOT = 5758
704070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3628593
75 X = 1105995
38
Y = -21382006
68 feet Y = -6517235
63 meter
Z = 4953741
96 Z = 1509900
55
XDOT = 13507
500655 XDOT = 4117
086200
YDOT = 6706
898817 feet/sec YDOT = 2044
262760 meter/sec
ZDOT = 18923
554071 ZDOT = 5767
899281
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 19048
56139548
00016717 00000-0 10270-3 0 9022
2 25544 51
6355 236
0800 0005585 35
0639 325
0880 15
53263123 36663
Satellite: ISS
Catalog Number: 25544
Epoch time: 19048
56139548 = yrday
fracday
Element set: 902
Inclination: 51
6355 deg
RA of node: 236
0800 deg
Eccentricity:
0005585
Arg of perigee: 35
0639 deg
Mean anomaly: 325
0880 deg
Mean motion: 15
53263123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3666
Checksum: 309
Coasting Arc #4 (Orbit 3680)
---------------------------------------
Vector Time (GMT): 2019/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1901219
43 A = 6788366
65 meter
Y = 5865627
37 meter E =
0008010
Z = -2848972
83 I = 51
34553
XDOT = -5730
205577 Wp = 74
38159
YDOT = -588
993405 meter/sec RA = 230
35234 deg
ZDOT = -5046
392602 TA = 138
10474
MA = 138
04341
Ha = 224
049 n
mi
Hp = 214
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6237596
54 X = 1849325
33
Y = 19244184
29 feet Y = 5886597
89 meter
Z = -9347023
71 Z = -2839863
91
XDOT = -18799
887063 XDOT = -5698
681582
YDOT = -1932
393061 feet/sec YDOT = -652
896454 meter/sec
ZDOT = -16556
406174 ZDOT = -5074
150364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5101968
62 X = -1555080
04
Y = 19595243
27 feet Y = 5972630
15 meter
Z = -9306419
79 Z = -2836596
75
XDOT = -13248
900359 XDOT = -4038
264829
YDOT = -11356
948482 feet/sec YDOT = -3461
597897 meter/sec
ZDOT = -16681
643449 ZDOT = -5084
564923
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 19049
52646023
00016717 00000-0 10270-3 0 9031
2 25544 51
6348 231
2749 0005701 39
2063 320
9501 15
53287629 36819
Satellite: ISS
Catalog Number: 25544
Epoch time: 19049
52646023 = yrday
fracday
Element set: 903
Inclination: 51
6348 deg
RA of node: 231
2749 deg
Eccentricity:
0005701
Arg of perigee: 39
2063 deg
Mean anomaly: 320
9501 deg
Mean motion: 15
53287629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3681
Checksum: 304
Coasting Arc #5 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2019/050/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2505857
22 A = 6779922
59 meter
Y = -3467682
36 meter E =
0007008
Z = 5253724
32 I = 51
33763
XDOT = 5646
103198 Wp = 66
23326
YDOT = 5147
114705 meter/sec RA = 226
59489 deg
ZDOT = 706
333007 TA = 17
00778
MA = 16
98431
Ha = 223
907 n
mi
Hp = 214
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8221316
33 X = 2518928
70
Y = -11376910
63 feet Y = -3439586
74 meter
Z = 17236628
35 Z = 5265928
39
XDOT = 18523
960625 XDOT = 5584
696216
YDOT = 16886
859267 feet/sec YDOT = 5209
910063 meter/sec
ZDOT = 2317
365507 ZDOT = 733
609387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5270944
04 X = 1606583
74
Y = 12935570
20 feet Y = 3942761
80 meter
Z = 17292011
65 Z = 5270605
15
XDOT = -23227
217277 XDOT = -7079
655826
YDOT = 6211
595422 feet/sec YDOT = 1893
294285 meter/sec
ZDOT = 2440
054639 ZDOT = 743
728654
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 19050
29851099
00016717 00000-0 10270-3 0 9049
2 25544 51
6386 227
4344 0005643 40
2449 319
9120 15
53305359 36933
Satellite: ISS
Catalog Number: 25544
Epoch time: 19050
29851099 = yrday
fracday
Element set: 904
Inclination: 51
6386 deg
RA of node: 227
4344 deg
Eccentricity:
0005643
Arg of perigee: 40
2449 deg
Mean anomaly: 319
9120 deg
Mean motion: 15
53305359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3693
Checksum: 316
Coasting Arc #6 (Orbit 3707)
---------------------------------------
Vector Time (GMT): 2019/051/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3549567
97 A = 6780048
43 meter
Y = 2455089
48 meter E =
0018523
Z = -5244607
29 I = 51
36297
XDOT = -5178
366180 Wp = 82
58803
YDOT = -5562
867365 meter/sec RA = 221
58355 deg
ZDOT = 905
763093 TA = 196
09648
MA = 196
15541
Ha = 224
114 n
mi
Hp = 214
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11645564
22 X = -3551283
02
Y = 8054755
51 feet Y = 2415385
70 meter
Z = -17206716
84 Z = -5261853
63
XDOT = -16989
390355 XDOT = -5120
175330
YDOT = -18250
877183 feet/sec YDOT = -5620
450031 meter/sec
ZDOT = 2971
663692 ZDOT = 880
751065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -873491
48 X = -266240
20
Y = -14037197
08 feet Y = -4278537
67 meter
Z = -17284775
59 Z = -5268399
60
XDOT = 23413
673547 XDOT = 7136
487697
YDOT = -4957
148274 feet/sec YDOT = -1510
938794 meter/sec
ZDOT = 2859
204945 ZDOT = 871
485667
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 19051
26357232
00016717 00000-0 10270-3 0 9058
2 25544 51
6400 222
6293 0005783 43
5138 316
6469 15
53291304 37087
Satellite: ISS
Catalog Number: 25544
Epoch time: 19051
26357232 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 222
6293 deg
Eccentricity:
0005783
Arg of perigee: 43
5138 deg
Mean anomaly: 316
6469 deg
Mean motion: 15
53291304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3708
Checksum: 299
Coasting Arc #7 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2019/052/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4543672
38 A = 6781676
43 meter
Y = -1423768
90 meter E =
0012757
Z = 4822990
74 I = 51
39435
XDOT = 4437
214675 Wp = 53
87232
YDOT = 5749
365669 meter/sec RA = 216
57635 deg
ZDOT = -2471
032944 TA = 60
53384
MA = 60
40662
Ha = 224
001 n
mi
Hp = 214
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14907061
63 X = 4535828
84
Y = -4671157
81 feet Y = -1373001
73 meter
Z = 15823460
43 Z = 4845042
75
XDOT = 14557
790929 XDOT = 4384
596477
YDOT = 18862
748258 feet/sec YDOT = 5798
691236 meter/sec
ZDOT = -8107
063463 ZDOT = -2449
607553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3458315
64 X = -1054094
61
Y = 15129968
34 feet Y = 4611614
35 meter
Z = 15923134
51 Z = 4853371
40
XDOT = -22558
929572 XDOT = -6875
961734
YDOT = 3315
420106 feet/sec YDOT = 1010
540048 meter/sec
ZDOT = -8010
789925 ZDOT = -2441
688769
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 19052
29296696
00016717 00000-0 10270-3 0 9069
2 25544 51
6399 217
5042 0005833 46
1423 314
0211 15
53322585 37242
Satellite: ISS
Catalog Number: 25544
Epoch time: 19052
29296696 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 217
5042 deg
Eccentricity:
0005833
Arg of perigee: 46
1423 deg
Mean anomaly: 314
0211 deg
Mean motion: 15
53322585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3724
Checksum: 305
Coasting Arc #8 (Orbit 3738)
---------------------------------------
Vector Time (GMT): 2019/053/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5402232
80 A = 6784605
91 meter
Y = 500944
73 meter E =
0011515
Z = -4082844
91 I = 51
43155
XDOT = -3414
756380 Wp = 83
88272
YDOT = -5684
838469 meter/sec RA = 211
57691 deg
ZDOT = 3831
279240 TA = 225
84789
MA = 225
94263
Ha = 224
151 n
mi
Hp = 214
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17723860
88 X = -5387601
19
Y = 1643519
46 feet Y = 440614
54 meter
Z = -13395160
48 Z = -4109050
95
XDOT = -11203
268963 XDOT = -3369
542990
YDOT = -18651
044846 feet/sec YDOT = -5722
771430 meter/sec
ZDOT = 12569
813778 ZDOT = 3814
802403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7225867
92 X = 2202444
54
Y = -16169051
08 feet Y = -4928326
77 meter
Z = -13513524
53 Z = -4118922
28
XDOT = 20610
137999 XDOT = 6281
970062
YDOT = -1204
408132 feet/sec YDOT = -367
103599 meter/sec
ZDOT = 12495
860614 ZDOT = 3808
738315
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 19053
25802486
00016717 00000-0 10270-3 0 9077
2 25544 51
6402 212
6998 0005759 49
3718 310
7934 15
53284529 37398
Satellite: ISS
Catalog Number: 25544
Epoch time: 19053
25802486 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 212
6998 deg
Eccentricity:
0005759
Arg of perigee: 49
3718 deg
Mean anomaly: 310
7934 deg
Mean motion: 15
53284529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3739
Checksum: 339
Coasting Arc #9 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2019/054/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6071356
31 A = 6787849
18 meter
Y = 367276
30 meter E =
0017826
Z = 3000111
01 I = 51
47198
XDOT = 2125
518853 Wp = 83
82669
YDOT = 5465
184800 meter/sec RA = 206
58657 deg
ZDOT = -4943
288109 TA = 61
73947
MA = 61
55966
Ha = 224
202 n
mi
Hp = 214
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19919148
01 X = 6052225
44
Y = 1204974
74 feet Y = 435063
79 meter
Z = 9842883
90 Z = 3029556
44
XDOT = 6973
487051 XDOT = 2088
259034
YDOT = 17930
396325 feet/sec YDOT = 5488
744991 meter/sec
ZDOT = -16218
136839 ZDOT = -4933
054353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10507705
75 X = -3202748
71
Y = 16887212
23 feet Y = 5147222
29 meter
Z = 9975819
16 Z = 3040629
68
XDOT = -17907
695769 XDOT = -5458
265670
YDOT = -1537
142776 feet/sec YDOT = -468
521118 meter/sec
ZDOT = -16172
344508 ZDOT = -4929
330606
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 19054
28741688
00016717 00000-0 10270-3 0 9088
2 25544 51
6409 207
5749 0005854 53
6604 306
5088 15
53291739 37552
Satellite: ISS
Catalog Number: 25544
Epoch time: 19054
28741688 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 207
5749 deg
Eccentricity:
0005854
Arg of perigee: 53
6604 deg
Mean anomaly: 306
5088 deg
Mean motion: 15
53291739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 344
Coasting Arc #10 (Orbit 3755)
---------------------------------------
Vector Time (GMT): 2019/054/08:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2187742
34 A = 6779792
67 meter
Y = 3635524
04 meter E =
0019572
Z = -5304623
08 I = 51
44557
XDOT = -6746
283246 Wp = 81
89743
YDOT = -3598
988005 meter/sec RA = 206
17070 deg
ZDOT = 319
460680 TA = 191
14073
MA = 191
18413
Ha = 224
187 n
mi
Hp = 214
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7177632
36 X = -2202466
66
Y = 11927572
31 feet Y = 3610976
30 meter
Z = -17403619
04 Z = -5315286
30
XDOT = -22133
475215 XDOT = -6707
088690
YDOT = -11807
703430 feet/sec YDOT = -3674
210475 meter/sec
ZDOT = 1048
099343 ZDOT = 286
785810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12284648
49 X = -3744360
86
Y = -6417534
58 feet Y = -1956064
54 meter
Z = -17452048
73 Z = -5319384
45
XDOT = 10146
871313 XDOT = 3092
766376
YDOT = -21840
166635 feet/sec YDOT = -6656
882790 meter/sec
ZDOT = 900
827617 ZDOT = 274
572258
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 19054
35175202
00016717 00000-0 10270-3 0 9090
2 25544 51
6388 207
2523 0005703 52
7714 307
3958 15
53302404 37568
Satellite: ISS
Catalog Number: 25544
Epoch time: 19054
35175202 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 207
2523 deg
Eccentricity:
0005703
Arg of perigee: 52
7714 deg
Mean anomaly: 307
3958 deg
Mean motion: 15
53302404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3756
Checksum: 302
Coasting Arc #11 (Orbit 3771)
---------------------------------------
Vector Time (GMT): 2019/055/08:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3474262
64 A = 6780937
90 meter
Y = -2939992
35 meter E =
0011333
Z = 5020277
26 I = 51
47983
XDOT = 6223
785628 Wp = 56
51348
YDOT = 4052
805989 meter/sec RA = 201
16820 deg
ZDOT = -1924
455232 TA = 52
23684
MA = 52
13422
Ha = 224
127 n
mi
Hp = 214
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11398499
48 X = 3482494
82
Y = -9645644
20 feet Y = -2901094
26 meter
Z = 16470725
93 Z = 5037173
97
XDOT = 20419
244185 XDOT = 6187
351268
YDOT = 13296
607574 feet/sec YDOT = 4122
200824 meter/sec
ZDOT = -6313
829500 ZDOT = -1894
311620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10414120
15 X = 3174223
82
Y = 10582223
86 feet Y = 3225461
83 meter
Z = 16547256
40 Z = 5043603
75
XDOT = -11053
399128 XDOT = -3369
076054
YDOT = 20585
608138 feet/sec YDOT = 6274
493361 meter/sec
ZDOT = -6178
005665 ZDOT = -1883
056127
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 19055
38114000
00016717 00000-0 10270-3 0 9105
2 25544 51
6388 202
1271 0005714 56
5132 303
6566 15
53299900 37728
Satellite: ISS
Catalog Number: 25544
Epoch time: 19055
38114000 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 202
1271 deg
Eccentricity:
0005714
Arg of perigee: 56
5132 deg
Mean anomaly: 303
6566 deg
Mean motion: 15
53299900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3772
Checksum: 287
Coasting Arc #12 (Orbit 3786)
---------------------------------------
Vector Time (GMT): 2019/056/08:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4634606
77 A = 6783438
70 meter
Y = 2297878
25 meter E =
0013559
Z = -4400144
21 I = 51
51784
XDOT = -5338
129656 Wp = 92
32566
YDOT = -4334
992607 meter/sec RA = 196
17210 deg
ZDOT = 3367
175114 TA = 211
81266
MA = 211
89463
Ha = 224
242 n
mi
Hp = 213
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15205402
78 X = -4638584
62
Y = 7538970
64 feet Y = 2246028
30 meter
Z = -14436168
67 Z = -4422666
96
XDOT = -17513
548739 XDOT = -5305
613488
YDOT = -14222
416691 feet/sec YDOT = -4394
505262 meter/sec
ZDOT = 11047
162447 ZDOT = 3341
324047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8830194
75 X = -2691443
36
Y = -14391508
45 feet Y = -4386531
78 meter
Z = -14538069
44 Z = -4431203
57
XDOT = 11579
949507 XDOT = 3529
568610
YDOT = -18119
323533 feet/sec YDOT = -5522
769813 meter/sec
ZDOT = 10930
729747 ZDOT = 3331
686427
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 19056
34619044
00016717 00000-0 10270-3 0 9111
2 25544 51
6370 197
3220 0005708 61
0004 299
1720 15
53299907 37874
Satellite: ISS
Catalog Number: 25544
Epoch time: 19056
34619044 = yrday
fracday
Element set: 911
Inclination: 51
6370 deg
RA of node: 197
3220 deg
Eccentricity:
0005708
Arg of perigee: 61
0004 deg
Mean anomaly: 299
1720 deg
Mean motion: 15
53299907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3787
Checksum: 309
Coasting Arc #13 (Orbit 3798)
---------------------------------------
Vector Time (GMT): 2019/057/02:28:46
144
Vector Time (MET): N/A
Weight (LBS) : 900432
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1721238
25 A = 6781587
21 meter
Y = 3915401
64 meter E =
0017418
Z = -5277785
72 I = 51
53306
XDOT = -7291
081160 Wp = 87
59243
YDOT = -2204
577263 meter/sec RA = 192
36570 deg
ZDOT = 745
181589 TA = 189
53448
MA = 189
56759
Ha = 224
353 n
mi
Hp = 215
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5647107
12 X = -1739257
20
Y = 12845805
89 feet Y = 3896052
50 meter
Z = -17315569
95 Z = -5286190
74
XDOT = -23920
869947 XDOT = -7269
506704
YDOT = -7232
865035 feet/sec YDOT = -2285
990552 meter/sec
ZDOT = 2444
821485 ZDOT = 709
817199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2748166
83 X = 837641
25
Y = -13712243
88 feet Y = -4179491
93 meter
Z = -17353831
20 Z = -5289447
75
XDOT = 23916
172371 XDOT = 7289
649339
YDOT = 1912
863835 feet/sec YDOT = 583
040897 meter/sec
ZDOT = 2285
242858 ZDOT = 696
542023
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 19057
11823249
00016717 00000-0 10270-3 0 9122
2 25544 51
6393 193
4790 0003629 51
8036 308
3442 15
52732656 37999
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
11823249 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 193
4790 deg
Eccentricity:
0003629
Arg of perigee: 51
8036 deg
Mean anomaly: 308
3442 deg
Mean motion: 15
52732656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3799
Checksum: 325
Coasting Arc #14 (Orbit 3806)
---------------------------------------
Vector Time (GMT): 2019/057/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900432
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2331709
82 A = 6782049
72 meter
Y = 3754148
97 meter E =
0016407
Z = -5158883
83 I = 51
55228
XDOT = -7115
574215 Wp = 93
37746
YDOT = -2408
806345 meter/sec RA = 189
78738 deg
ZDOT = 1466
284977 TA = 190
76362
MA = 190
79878
Ha = 224
269 n
mi
Hp = 215
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7649966
61 X = -2348457
81
Y = 12316761
71 feet Y = 3727980
26 meter
Z = -16925471
87 Z = -5170251
12
XDOT = -23345
059760 XDOT = -7095
231728
YDOT = -7902
907957 feet/sec YDOT = -2488
263849 meter/sec
ZDOT = 4810
646249 ZDOT = 1431
770159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3293017
80 X = -1003711
83
Y = 14058098
74 feet Y = 4284908
50 meter
Z = -16977105
17 Z = -5174621
65
XDOT = -23650
618539 XDOT = -7208
708531
YDOT = 69
227468 feet/sec YDOT = 21
100532 meter/sec
ZDOT = 4654
908943 ZDOT = 1418
816246
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 19057
63311043
00016717 00000-0 10270-3 0 9134
2 25544 51
6400 190
9155 0003318 58
0296 302
1178 15
52746926 38070
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
63311043 = yrday
fracday
Element set: 913
Inclination: 51
6400 deg
RA of node: 190
9155 deg
Eccentricity:
0003318
Arg of perigee: 58
0296 deg
Mean anomaly: 302
1178 deg
Mean motion: 15
52746926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 298
Coasting Arc #15 (Orbit 3822)
---------------------------------------
Vector Time (GMT): 2019/058/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900432
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3466165
03 A = 6783837
72 meter
Y = -3446549
05 meter E =
0011196
Z = 4697769
45 I = 51
59188
XDOT = 6576
333849 Wp = 62
32983
YDOT = 2781
182320 meter/sec RA = 184
79979 deg
ZDOT = -2801
590421 TA = 55
50591
MA = 55
40022
Ha = 224
183 n
mi
Hp = 215
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11371932
51 X = 3481628
90
Y = -11307575
61 feet Y = -3407701
30 meter
Z = 15412629
44 Z = 4714644
23
XDOT = 21575
898455 XDOT = 6558
353482
YDOT = 9124
613911 feet/sec YDOT = 2854
622821 meter/sec
ZDOT = -9191
569622 ZDOT = -2769
689340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6906655
24 X = 2105148
52
Y = -14391533
48 feet Y = -4386539
40 meter
Z = 15489129
71 Z = 4721086
73
XDOT = 22386
248252 XDOT = 6823
328467
YDOT = 969
861741 feet/sec YDOT = 295
613859 meter/sec
ZDOT = -9047
645728 ZDOT = -2757
722418
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 19058
66286628
00016717 00000-0 10270-3 0 9149
2 25544 51
6404 185
7923 0003382 59
6160 300
5326 15
52767376 38234
Satellite: ISS
Catalog Number: 25544
Epoch time: 19058
66286628 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 185
7923 deg
Eccentricity:
0003382
Arg of perigee: 59
6160 deg
Mean anomaly: 300
5326 deg
Mean motion: 15
52767376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3823
Checksum: 327
Coasting Arc #16 (Orbit 3837)
---------------------------------------
Vector Time (GMT): 2019/059/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900432
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4466316
42 A = 6786414
17 meter
Y = 3184551
88 meter E =
0009868
Z = -4004905
01 I = 51
63246
XDOT = -5766
128256 Wp = 94
87041
YDOT = -3116
756401 meter/sec RA = 179
82065 deg
ZDOT = 3959
727503 TA = 216
35843
MA = 216
42551
Ha = 224
304 n
mi
Hp = 215
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14653269
08 X = -4482141
78
Y = 10448004
85 feet Y = 3134517
75 meter
Z = -13139452
12 Z = -4026638
88
XDOT = -18917
743623 XDOT = -5750
081066
YDOT = -10225
578743 feet/sec YDOT = -3181
147376 meter/sec
ZDOT = 12991
231966 ZDOT = 3931
757436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10048240
38 X = -3062703
67
Y = 14843017
07 feet Y = 4524151
60 meter
Z = -13237900
57 Z = -4034912
09
XDOT = -20286
309627 XDOT = -6183
267174
YDOT = -2281
404499 feet/sec YDOT = -695
372091 meter/sec
ZDOT = 12865
073864 ZDOT = 3921
274514
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 19059
62826191
00016717 00000-0 10270-3 0 9152
2 25544 51
6391 180
9910 0003431 65
3715 294
7794 15
52764615 38389
Satellite: ISS
Catalog Number: 25544
Epoch time: 19059
62826191 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 180
9910 deg
Eccentricity:
0003431
Arg of perigee: 65
3715 deg
Mean anomaly: 294
7794 deg
Mean motion: 15
52764615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3838
Checksum: 335
Coasting Arc #17 (Orbit 3853)
---------------------------------------
Vector Time (GMT): 2019/060/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900432
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5319066
38 A = 6789259
75 meter
Y = -2900402
33 meter E =
0016079
Z = 3050267
62 I = 51
67570
XDOT = 4736
262365 Wp = 90
01163
YDOT = 3482
160395 meter/sec RA = 174
84816 deg
ZDOT = -4925
587364 TA = 55
01375
MA = 54
86289
Ha = 224
269 n
mi
Hp = 215
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17451005
18 X = 5336287
98
Y = -9515755
69 feet Y = -2840824
37 meter
Z = 10007439
69 Z = 3076147
08
XDOT = 15538
918520 XDOT = 4720
897127
YDOT = 11424
410746 feet/sec YDOT = 3535
038433 meter/sec
ZDOT = -16160
063530 ZDOT = -4902
618349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12756251
00 X = 3888105
30
Y = -15165956
51 feet Y = -4622583
54 meter
Z = 10124616
58 Z = 3085983
13
XDOT = 17616
125432 XDOT = 5369
395032
YDOT = 4049
377242 feet/sec YDOT = 1234
250183 meter/sec
ZDOT = -16056
514573 ZDOT = -4894
025642
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 19060
65801361
00016717 00000-0 10270-3 0 9160
2 25544 51
6396 175
8681 0003428 66
2531 293
8980 15
52766996 38543
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
65801361 = yrday
fracday
Element set: 916
Inclination: 51
6396 deg
RA of node: 175
8681 deg
Eccentricity:
0003428
Arg of perigee: 66
2531 deg
Mean anomaly: 293
8980 deg
Mean motion: 15
52766996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3854
Checksum: 347
Coasting Arc #18 (Orbit 3855)
---------------------------------------
Vector Time (GMT): 2019/060/17:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 900432
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6113669
44 A = 6790727
20 meter
Y = -1431852
94 meter E =
0017522
Z = 2563818
09 I = 51
68250
XDOT = 3276
730168 Wp = 74
14685
YDOT = -4508
871022 meter/sec RA = 174
35716 deg
ZDOT = 5270
279361 TA = 314
65609
MA = 314
79879
Ha = 224
631 n
mi
Hp = 215
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20057970
61 X = -6109657
02
Y = -4697680
25 feet Y = -1500197
70 meter
Z = 8411476
66 Z = 2534130
62
XDOT = 10750
427060 XDOT = 3301
306556
YDOT = -14792
883932 feet/sec YDOT = -4472
090655 meter/sec
ZDOT = 17290
942787 ZDOT = 5286
256070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14066891
75 X = -4287588
60
Y = 15124495
82 feet Y = 4609946
33 meter
Z = 8277409
44 Z = 2522954
40
XDOT = -6453
400057 XDOT = -1966
996337
YDOT = -15551
004572 feet/sec YDOT = -4739
946193 meter/sec
ZDOT = 17363
484924 ZDOT = 5292
390205
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 19060
78673426
00016717 00000-0 10270-3 0 9174
2 25544 51
6387 175
2283 0003887 66
6891 293
4670 15
52722957 38560
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
78673426 = yrday
fracday
Element set: 917
Inclination: 51
6387 deg
RA of node: 175
2283 deg
Eccentricity:
0003887
Arg of perigee: 66
6891 deg
Mean anomaly: 293
4670 deg
Mean motion: 15
52722957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 358
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