[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 31st 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16520 4497 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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
213/11:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
2
000/00:00:00
000 0
0 0
0 220
3
218/16:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
4
000/00:00:00
000 0
0 0
0 221
2
220/06:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
2
000/00:00:00
000 0
0 0
0 221
4
227/05:42:50
809 0
3 2
0 2
0
N/A 2
0 0
0 223
7
000/00:09:41
618 0
5 -0
0 223
0
227/08:46:28
979 0
4 1
5 1
5
N/A 1
4 -0
0 224
2
000/00:06:57
959 0
2 -0
0 223
9
Coasting Arc #1 (Orbit 2215)
---------------------------------------
Vector Time (GMT): 2019/212/17:27:09
770
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5814117
17 A = 6795247
29 meter
Y = -2133037
49 meter E =
0008304
Z = -2786167
47 I = 51
89878
XDOT = -384
071444 Wp = 171
53169
YDOT = 5664
348192 meter/sec RA = 139
19639 deg
ZDOT = -5147
933405 TA = 39
89260
MA = 39
83160
Ha = 226
364 n
mi
Hp = 220
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19075187
58 X = 5851070
62
Y = -6998154
48 feet Y = -2067813
02 meter
Z = -9140969
40 Z = -2757835
84
XDOT = -1260
076917 XDOT = -422
378081
YDOT = 18583
819526 feet/sec YDOT = 5659
839602 meter/sec
ZDOT = -16889
545293 ZDOT = -5149
891464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13087302
59 X = -3989009
83
Y = 15617358
18 feet Y = 4760170
77 meter
Z = -9011931
17 Z = -2746836
62
XDOT = -7144
603536 XDOT = -2177
675158
YDOT = -15719
478272 feet/sec YDOT = -4791
296977 meter/sec
ZDOT = -16898
853838 ZDOT = -5150
770650
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 19212
75388456
00016717 00000-0 10270-3 0 9008
2 25544 51
6408 140
1651 0006299 206
3851 153
6980 15
51000352 22160
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
75388456 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 140
1651 deg
Eccentricity:
0006299
Arg of perigee: 206
3851 deg
Mean anomaly: 153
6980 deg
Mean motion: 15
51000352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2216
Checksum: 292
Coasting Arc #2 (Orbit 2227)
---------------------------------------
Vector Time (GMT): 2019/213/11:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -515196
65 A = 6788707
63 meter
Y = -4772888
74 meter E =
0004108
Z = 4796126
10 I = 51
89713
XDOT = 6363
624967 Wp = 118
22705
YDOT = -3351
740195 meter/sec RA = 135
41658 deg
ZDOT = -2652
091376 TA = 357
85400
MA = 357
85576
Ha = 226
230 n
mi
Hp = 220
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1690277
72 X = -485082
84
Y = -15659083
79 feet Y = -4778482
07 meter
Z = 15735321
84 Z = 4793696
25
XDOT = 20878
034667 XDOT = 6413
514178
YDOT = -10996
522948 feet/sec YDOT = -3280
298491 meter/sec
ZDOT = -8701
087191 ZDOT = -2621
059217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12170753
50 X = -3709645
67
Y = 10013682
26 feet Y = 3052170
35 meter
Z = 15724605
69 Z = 4792859
82
XDOT = -19875
643320 XDOT = -6058
096084
YDOT = -10716
623054 feet/sec YDOT = -3266
426707 meter/sec
ZDOT = -8559
661839 ZDOT = -2608
984928
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 19213
52706378
00016717 00000-0 10270-3 0 9012
2 25544 51
6420 136
3298 0006198 207
8530 152
2290 15
51004787 22284
Satellite: ISS
Catalog Number: 25544
Epoch time: 19213
52706378 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 136
3298 deg
Eccentricity:
0006198
Arg of perigee: 207
8530 deg
Mean anomaly: 152
2290 deg
Mean motion: 15
51004787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2228
Checksum: 300
Coasting Arc #3 (Orbit 2242)
---------------------------------------
Vector Time (GMT): 2019/214/11:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 229296
53 A = 6789975
83 meter
Y = 5119379
06 meter E =
0010121
Z = -4464143
08 I = 51
92510
XDOT = -6124
800188 Wp = 147
22615
YDOT = 3172
737715 meter/sec RA = 130
47015 deg
ZDOT = 3319
069462 TA = 156
21932
MA = 156
17252
Ha = 225
998 n
mi
Hp = 220
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 752285
20 X = 193716
86
Y = 16795863
04 feet Y = 5121744
52 meter
Z = -14646138
71 Z = -4463115
40
XDOT = -20094
488806 XDOT = -6175
945209
YDOT = 10409
244473 feet/sec YDOT = 3103
959738 meter/sec
ZDOT = 10889
335505 ZDOT = 3289
194244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13467511
47 X = 4104897
50
Y = -10070717
24 feet Y = -3069554
61 meter
Z = -14641827
63 Z = -4462829
06
XDOT = 19151
979705 XDOT = 5837
523414
YDOT = 9955
071198 feet/sec YDOT = 3034
305701 meter/sec
ZDOT = 10753
169857 ZDOT = 3277
566172
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 19214
49353179
00016717 00000-0 10270-3 0 9027
2 25544 51
6426 131
5340 0006116 211
3716 148
7071 15
51023252 22433
Satellite: ISS
Catalog Number: 25544
Epoch time: 19214
49353179 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 131
5340 deg
Eccentricity:
0006116
Arg of perigee: 211
3716 deg
Mean anomaly: 148
7071 deg
Mean motion: 15
51023252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2243
Checksum: 274
Coasting Arc #4 (Orbit 2258)
---------------------------------------
Vector Time (GMT): 2019/215/11:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4066
62 A = 6791469
97 meter
Y = -5446944
22 meter E =
0007515
Z = 4048373
52 I = 51
95043
XDOT = 5885
164797 Wp = 111
72711
YDOT = -2935
168249 meter/sec RA = 125
52861 deg
ZDOT = -3940
107369 TA = 19
02790
MA = 18
99984
Ha = 225
924 n
mi
Hp = 220
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13341
95 X = 37178
71
Y = -17870551
91 feet Y = -5446759
20 meter
Z = 13282065
34 Z = 4048453
78
XDOT = 19308
283456 XDOT = 5936
687682
YDOT = -9629
817090 feet/sec YDOT = -2869
068001 meter/sec
ZDOT = -12926
861448 ZDOT = -3911
395096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14601798
42 X = -4450628
16
Y = 10301659
21 feet Y = 3139945
73 meter
Z = 13282822
13 Z = 4048604
18
XDOT = -18239
305693 XDOT = -5559
340375
YDOT = -9340
502638 feet/sec YDOT = -2846
985204 meter/sec
ZDOT = -12795
990998 ZDOT = -3900
218056
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 19215
52442911
00016717 00000-0 10270-3 0 9036
2 25544 51
6422 126
4204 0006076 215
1327 144
9424 15
51012512 22590
Satellite: ISS
Catalog Number: 25544
Epoch time: 19215
52442911 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 126
4204 deg
Eccentricity:
0006076
Arg of perigee: 215
1327 deg
Mean anomaly: 144
9424 deg
Mean motion: 15
51012512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2259
Checksum: 270
Coasting Arc #5 (Orbit 2273)
---------------------------------------
Vector Time (GMT): 2019/216/11:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -166722
75 A = 6792942
65 meter
Y = 5777143
70 meter E =
0005523
Z = -3575744
79 I = 51
97432
XDOT = -5624
045524 Wp = 165
96397
YDOT = 2617
661774 meter/sec RA = 120
58822 deg
ZDOT = 4487
686777 TA = 152
13022
MA = 152
10062
Ha = 225
703 n
mi
Hp = 220
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -546990
64 X = -213943
41
Y = 18953883
54 feet Y = 5775015
31 meter
Z = -11731446
15 Z = -3576669
26
XDOT = -18451
592926 XDOT = -5674
697233
YDOT = 8588
129181 feet/sec YDOT = 2554
486477 meter/sec
ZDOT = 14723
381813 ZDOT = 4460
244833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15634859
70 X = 4765505
24
Y = -10723406
44 feet Y = -3268494
28 meter
Z = -11736074
52 Z = -3577155
51
XDOT = 17045
822088 XDOT = 5195
566573
YDOT = 8862
628600 feet/sec YDOT = 2701
329197 meter/sec
ZDOT = 14598
303705 ZDOT = 4449
562969
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 19216
49089291
00016717 00000-0 10270-3 0 9042
2 25544 51
6425 121
6247 0006131 219
1637 140
9071 15
51033460 22743
Satellite: ISS
Catalog Number: 25544
Epoch time: 19216
49089291 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 121
6247 deg
Eccentricity:
0006131
Arg of perigee: 219
1637 deg
Mean anomaly: 140
9071 deg
Mean motion: 15
51033460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2274
Checksum: 289
Coasting Arc #6 (Orbit 2289)
---------------------------------------
Vector Time (GMT): 2019/217/11:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 284725
07 A = 6794502
30 meter
Y = -6066177
46 meter E =
0010638
Z = 3032175
64 I = 51
99544
XDOT = 5387
258562 Wp = 124
34803
YDOT = -2237
324435 meter/sec RA = 115
65173 deg
ZDOT = -4975
295453 TA = 21
11615
MA = 21
07227
Ha = 225
636 n
mi
Hp = 220
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 934137
38 X = 337809
25
Y = -19902157
03 feet Y = -6062696
68 meter
Z = 9948082
81 Z = 3033687
59
XDOT = 17674
732814 XDOT = 5436
043428
YDOT = -7340
303263 feet/sec YDOT = -2176
807509 meter/sec
ZDOT = -16323
147813 ZDOT = -4949
008102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16446393
33 X = -5012860
69
Y = 11240047
47 feet Y = 3425966
47 meter
Z = 9955415
52 Z = 3034410
65
XDOT = -15719
687675 XDOT = -4791
360803
YDOT = -8630
452591 feet/sec YDOT = -2630
561950 meter/sec
ZDOT = -16203
341659 ZDOT = -4938
778538
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 19217
52178507
00016717 00000-0 10270-3 0 9057
2 25544 51
6426 116
5104 0006152 223
0012 137
0659 15
51015389 22900
Satellite: ISS
Catalog Number: 25544
Epoch time: 19217
52178507 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 116
5104 deg
Eccentricity:
0006152
Arg of perigee: 223
0012 deg
Mean anomaly: 137
0659 deg
Mean motion: 15
51015389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2290
Checksum: 281
Coasting Arc #7 (Orbit 2304)
---------------------------------------
Vector Time (GMT): 2019/218/11:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -350293
55 A = 6795756
06 meter
Y = 6330034
38 meter E =
0000644
Z = -2447911
80 I = 52
01432
XDOT = -5159
517585 Wp = 223
01201
YDOT = 1791
132043 meter/sec RA = 110
71616 deg
ZDOT = 5368
707126 TA = 109
79325
MA = 109
78632
Ha = 225
350 n
mi
Hp = 221
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1149257
07 X = -409161
32
Y = 20767829
32 feet Y = 6325788
03 meter
Z = -8031206
68 Z = -2449756
26
XDOT = -16927
551131 XDOT = -5205
240977
YDOT = 5876
417464 feet/sec YDOT = 1733
178956 meter/sec
ZDOT = 17613
868523 ZDOT = 5343
533380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17074293
66 X = 5204244
71
Y = -11872208
19 feet Y = -3618649
06 meter
Z = -8040085
58 Z = -2450618
08
XDOT = 14231
147006 XDOT = 4337
653607
YDOT = 8613
238652 feet/sec YDOT = 2625
315141 meter/sec
ZDOT = 17499
154101 ZDOT = 5333
742170
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 19218
48824176
00016717 00000-0 10270-3 0 9064
2 25544 51
6435 111
7142 0006088 227
4325 132
6312 15
51049504 23052
Satellite: ISS
Catalog Number: 25544
Epoch time: 19218
48824176 = yrday
fracday
Element set: 906
Inclination: 51
6435 deg
RA of node: 111
7142 deg
Eccentricity:
0006088
Arg of perigee: 227
4325 deg
Mean anomaly: 132
6312 deg
Mean motion: 15
51049504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2305
Checksum: 290
Coasting Arc #8 (Orbit 2307)
---------------------------------------
Vector Time (GMT): 2019/218/16:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -447364
93 A = 6796229
87 meter
Y = 6403118
66 meter E =
0000525
Z = -2232736
73 I = 52
01398
XDOT = -5111
590529 Wp = 292
60261
YDOT = 1556
355533 meter/sec RA = 109
75794 deg
ZDOT = 5486
727922 TA = 42
76203
MA = 42
75794
Ha = 225
386 n
mi
Hp = 221
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1467732
71 X = -508087
92
Y = 21007607
14 feet Y = 6397776
42 meter
Z = -7325251
73 Z = -2235057
21
XDOT = -16770
310133 XDOT = -5155
265433
YDOT = 5106
153323 feet/sec YDOT = 1498
949839 meter/sec
ZDOT = 18001
075860 ZDOT = 5461
791946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5061158
11 X = -1542640
99
Y = -20437622
34 feet Y = -6229387
29 meter
Z = -7336305
73 Z = -2236105
99
XDOT = 13035
868353 XDOT = 3973
332674
YDOT = -9650
068113 feet/sec YDOT = -2941
340761 meter/sec
ZDOT = 17887
459725 ZDOT = 5452
097724
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 19218
68153179
00016717 00000-0 10270-3 0 9075
2 25544 51
6394 110
7522 0006241 227
8541 132
2080 15
51032379 23085
Satellite: ISS
Catalog Number: 25544
Epoch time: 19218
68153179 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 110
7522 deg
Eccentricity:
0006241
Arg of perigee: 227
8541 deg
Mean anomaly: 132
2080 deg
Mean motion: 15
51032379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2308
Checksum: 294
Coasting Arc #9 (Orbit 2323)
---------------------------------------
Vector Time (GMT): 2019/219/16:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 465162
96 A = 6797132
29 meter
Y = -6585632
77 meter E =
0012390
Z = 1582950
55 I = 52
02775
XDOT = 4936
626990 Wp = 144
00680
YDOT = -1042
014153 meter/sec RA = 104
82616 deg
ZDOT = -5772
707234 TA = 18
78945
MA = 18
74375
Ha = 225
093 n
mi
Hp = 221
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1526125
18 X = 531081
80
Y = -21606406
74 feet Y = -6580062
47 meter
Z = 5193407
32 Z = 1585370
02
XDOT = 16196
282777 XDOT = 4975
952558
YDOT = -3418
681605 feet/sec YDOT = -986
589255 meter/sec
ZDOT = -18939
328195 ZDOT = -5748
631674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5535679
78 X = 1687275
20
Y = 20938055
67 feet Y = 6381919
37 meter
Z = 5204942
27 Z = 1586466
40
XDOT = -12829
940902 XDOT = -3910
565987
YDOT = 8083
514068 feet/sec YDOT = 2463
855088 meter/sec
ZDOT = -18829
659105 ZDOT = -5739
280095
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 19219
71241594
00016717 00000-0 10270-3 0 9080
2 25544 51
6395 105
6372 0006251 234
0872 125
9700 15
51084207 23243
Satellite: ISS
Catalog Number: 25544
Epoch time: 19219
71241594 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 105
6372 deg
Eccentricity:
0006251
Arg of perigee: 234
0872 deg
Mean anomaly: 125
9700 deg
Mean motion: 15
51084207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2324
Checksum: 297
Coasting Arc #10 (Orbit 2332)
---------------------------------------
Vector Time (GMT): 2019/220/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4101782
01 A = 6790795
54 meter
Y = -3352814
04 meter E =
0002742
Z = -4250100
44 I = 52
01135
XDOT = 1546
784515 Wp = 107
76084
YDOT = 6542
730241 meter/sec RA = 101
94275 deg
ZDOT = -3671
372058 TA = 124
79847
MA = 124
77266
Ha = 225
203 n
mi
Hp = 221
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13457290
05 X = 4159613
74
Y = -11000046
05 feet Y = -3306621
49 meter
Z = -13943899
07 Z = -4230035
36
XDOT = 5074
752346 XDOT = 1491
340202
YDOT = 21465
650397 feet/sec YDOT = 6559
717615 meter/sec
ZDOT = -12045
183917 ZDOT = -3663
992815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -506115
89 X = -154264
12
Y = -17446770
54 feet Y = -5317775
66 meter
Z = -13852293
48 Z = -4222179
05
XDOT = 18909
838985 XDOT = 5763
718923
YDOT = 8981
534704 feet/sec YDOT = 2737
571778 meter/sec
ZDOT = -12012
122446 ZDOT = -3661
294922
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 19220
29229088
00016717 00000-0 10270-3 0 9090
2 25544 51
6400 102
7619 0006056 234
1758 125
8831 15
51039242 23332
Satellite: ISS
Catalog Number: 25544
Epoch time: 19220
29229088 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 102
7619 deg
Eccentricity:
0006056
Arg of perigee: 234
1758 deg
Mean anomaly: 125
8831 deg
Mean motion: 15
51039242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2333
Checksum: 296
Coasting Arc #11 (Orbit 2348)
---------------------------------------
Vector Time (GMT): 2019/221/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4002878
29 A = 6789262
52 meter
Y = 2943581
59 meter E =
0007161
Z = 4628008
74 I = 52
01376
XDOT = -1539
014252 Wp = 160
44512
YDOT = -6866
902459 meter/sec RA = 97
00508 deg
ZDOT = 3028
554342 TA = 259
41143
MA = 259
49210
Ha = 224
908 n
mi
Hp = 221
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13132802
79 X = -4057976
85
Y = 9657419
92 feet Y = 2898510
26 meter
Z = 15183755
72 Z = 4608430
78
XDOT = -5049
259357 XDOT = -1476
823089
YDOT = -22529
207544 feet/sec YDOT = -6883
765235 meter/sec
ZDOT = 9936
201910 ZDOT = 3021
229123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -86432
68 X = -26344
68
Y = 16383976
99 feet Y = 4993836
19 meter
Z = 15094387
49 Z = 4600769
31
XDOT = -19970
550554 XDOT = -6087
023809
YDOT = -9253
339981 feet/sec YDOT = -2820
418026 meter/sec
ZDOT = 9903
427576 ZDOT = 3018
564725
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 19221
32317073
00016717 00000-0 10270-3 0 9109
2 25544 51
6413 97
6476 0006271 238
6643 121
3895 15
51081604 23497
Satellite: ISS
Catalog Number: 25544
Epoch time: 19221
32317073 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 97
6476 deg
Eccentricity:
0006271
Arg of perigee: 238
6643 deg
Mean anomaly: 121
3895 deg
Mean motion: 15
51081604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2349
Checksum: 300
Coasting Arc #12 (Orbit 2363)
---------------------------------------
Vector Time (GMT): 2019/222/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3950437
99 A = 6788104
38 meter
Y = -2472118
61 meter E =
0006247
Z = -4941296
89 I = 52
01264
XDOT = 1558
151070 Wp = 83
26346
YDOT = 7129
267634 meter/sec RA = 92
06466 deg
ZDOT = -2322
855122 TA = 164
11248
MA = 164
09287
Ha = 224
786 n
mi
Hp = 221
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12960754
58 X = 4001790
12
Y = -8110625
38 feet Y = -2427654
58 meter
Z = -16211603
95 Z = -4921982
80
XDOT = 5112
044192 XDOT = 1489
596749
YDOT = 23389
985677 feet/sec YDOT = 7146
308817 meter/sec
ZDOT = -7620
915756 ZDOT = -2315
452329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 969045
60 X = 295365
10
Y = -15351688
57 feet Y = -4679194
68 meter
Z = -16123464
72 Z = -4914432
05
XDOT = 20930
776707 XDOT = 6379
700740
YDOT = 9284
261788 feet/sec YDOT = 2829
842993 meter/sec
ZDOT = -7587
824793 ZDOT = -2312
768997
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 19222
28962091
00016717 00000-0 10270-3 0 9112
2 25544 51
6414 92
8517 0006024 242
9299 117
1238 15
51048364 23649
Satellite: ISS
Catalog Number: 25544
Epoch time: 19222
28962091 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 92
8517 deg
Eccentricity:
0006024
Arg of perigee: 242
9299 deg
Mean anomaly: 117
1238 deg
Mean motion: 15
51048364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2364
Checksum: 305
Coasting Arc #13 (Orbit 2379)
---------------------------------------
Vector Time (GMT): 2019/223/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3936559
08 A = 6787068
21 meter
Y = 1988196
98 meter E =
0005456
Z = 5161626
72 I = 52
00956
XDOT = -1609
200779 Wp = 197
94149
YDOT = -7320
102483 meter/sec RA = 87
12527 deg
ZDOT = 1587
743805 TA = 236
78644
MA = 236
83876
Ha = 224
515 n
mi
Hp = 221
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12915220
08 X = -3983571
03
Y = 6522955
98 feet Y = 1943912
39 meter
Z = 16934470
88 Z = 5142390
64
XDOT = -5279
530115 XDOT = -1534
937948
YDOT = -24016
084263 feet/sec YDOT = -7337
682579 meter/sec
ZDOT = 5209
133217 ZDOT = 1580
106885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1990983
90 X = -606851
89
Y = 14434411
07 feet Y = 4399608
49 meter
Z = 16846718
63 Z = 5134879
84
XDOT = -21757
291831 XDOT = -6631
622550
YDOT = -9058
626780 feet/sec YDOT = -2761
069443 meter/sec
ZDOT = 5175
006141 ZDOT = 1577
341872
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 19223
32049709
00016717 00000-0 10270-3 0 9121
2 25544 51
6414 87
7380 0006165 247
4237 112
6262 15
51080022 23800
Satellite: ISS
Catalog Number: 25544
Epoch time: 19223
32049709 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 87
7380 deg
Eccentricity:
0006165
Arg of perigee: 247
4237 deg
Mean anomaly: 112
6262 deg
Mean motion: 15
51080022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2380
Checksum: 285
Coasting Arc #14 (Orbit 2394)
---------------------------------------
Vector Time (GMT): 2019/224/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3979579
98 A = 6786540
30 meter
Y = -1472964
10 meter E =
0008674
Z = -5303679
77 I = 52
00504
XDOT = 1663
794085 Wp = 92
81043
YDOT = 7429
602569 meter/sec RA = 82
18294 deg
ZDOT = -816
532081 TA = 169
42203
MA = 169
40378
Ha = 224
380 n
mi
Hp = 221
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13056364
75 X = 4021517
16
Y = -4832559
37 feet Y = -1428226
80 meter
Z = -17400524
18 Z = -5284247
06
XDOT = 5458
642010 XDOT = 1584
556660
YDOT = 24375
336513 feet/sec YDOT = 7447
765294 meter/sec
ZDOT = -2678
911026 ZDOT = -808
642104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3232084
54 X = 985139
37
Y = -13654734
46 feet Y = -4161963
06 meter
Z = -17311914
65 Z = -5276671
58
XDOT = 22358
291967 XDOT = 6814
807392
YDOT = 8637
397725 feet/sec YDOT = 2632
678827 meter/sec
ZDOT = -2643
653213 ZDOT = -805
785499
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 19224
28694399
00016717 00000-0 10270-3 0 9139
2 25544 51
6417 82
9423 0006106 250
8773 109
1717 15
51051883 23951
Satellite: ISS
Catalog Number: 25544
Epoch time: 19224
28694399 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 82
9423 deg
Eccentricity:
0006106
Arg of perigee: 250
8773 deg
Mean anomaly: 109
1717 deg
Mean motion: 15
51051883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2395
Checksum: 324
Coasting Arc #15 (Orbit 2410)
---------------------------------------
Vector Time (GMT): 2019/225/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4067107
40 A = 6786236
88 meter
Y = 963728
85 meter E =
0003916
Z = 5349392
08 I = 51
99922
XDOT = -1719
479090 Wp = 246
29245
YDOT = -7465
687296 meter/sec RA = 77
24133 deg
ZDOT = 36
174994 TA = 203
35532
MA = 203
37312
Ha = 224
118 n
mi
Hp = 221
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13343528
22 X = -4103565
64
Y = 3161840
05 feet Y = 918043
45 meter
Z = 17550498
96 Z = 5329547
53
XDOT = -5641
335597 XDOT = -1636
043546
YDOT = -24493
724725 feet/sec YDOT = -7484
449205 meter/sec
ZDOT = 118
684364 ZDOT = 28
024832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4560845
45 X = -1390145
69
Y = 13054200
94 feet Y = 3978920
45 meter
Z = 17460054
93 Z = 5321824
74
XDOT = -22740
114465 XDOT = -6931
186889
YDOT = -8061
564205 feet/sec YDOT = -2457
164770 meter/sec
ZDOT = 82
255309 ZDOT = 25
071418
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 19225
31781539
00016717 00000-0 10270-3 0 9148
2 25544 51
6423 77
8281 0006190 256
0019 104
0444 15
51081398 24111
Satellite: ISS
Catalog Number: 25544
Epoch time: 19225
31781539 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 77
8281 deg
Eccentricity:
0006190
Arg of perigee: 256
0019 deg
Mean anomaly: 104
0444 deg
Mean motion: 15
51081398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2411
Checksum: 293
Coasting Arc #16 (Orbit 2425)
---------------------------------------
Vector Time (GMT): 2019/226/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4210692
77 A = 6786503
55 meter
Y = -456760
49 meter E =
0008920
Z = -5310287
38 I = 51
99098
XDOT = 1751
974592 Wp = 106
58091
YDOT = 7416
153354 meter/sec RA = 72
29748 deg
ZDOT = 749
867337 TA = 170
56732
MA = 170
55056
Ha = 223
897 n
mi
Hp = 221
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13814608
81 X = 4241281
27
Y = -1498558
04 feet Y = -409502
34 meter
Z = -17422202
71 Z = -5289759
62
XDOT = 5747
948136 XDOT = 1665
272467
YDOT = 24331
211792 feet/sec YDOT = 7435
260357 meter/sec
ZDOT = 2460
194675 ZDOT = 758
167267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5999536
17 X = 1828658
62
Y = -12662711
24 feet Y = -3859594
39 meter
Z = -17328691
52 Z = -5281785
17
XDOT = 22817
739056 XDOT = 6954
846864
YDOT = 7386
962806 feet/sec YDOT = 2251
546263 meter/sec
ZDOT = 2497
301204 ZDOT = 761
177407
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 19226
28425696
00016717 00000-0 10270-3 0 9155
2 25544 51
6419 73
0321 0006028 259
7755 100
2716 15
51056989 24260
Satellite: ISS
Catalog Number: 25544
Epoch time: 19226
28425696 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 73
0321 deg
Eccentricity:
0006028
Arg of perigee: 259
7755 deg
Mean anomaly: 100
2716 deg
Mean motion: 15
51056989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2426
Checksum: 319
Coasting Arc #17 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2019/227/05:47:41
618
Vector Time (MET): N/A
Weight (LBS) : 937094
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4645247
84 A = 6792058
60 meter
Y = 2623515
71 meter E =
0002774
Z = -4205293
05 I = 51
99405
XDOT = -389
272846 Wp = 186
13118
YDOT = 6677
153160 meter/sec RA = 67
48043 deg
ZDOT = 3732
704615 TA = 122
08717
MA = 122
06024
Ha = 223
679 n
mi
Hp = 223
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15240314
42 X = 4635992
18
Y = 8607335
00 feet Y = 2675410
46 meter
Z = -13796893
20 Z = -4182751
14
XDOT = -1277
141882 XDOT = -482
040741
YDOT = 21906
670473 feet/sec YDOT = 6672
281275 meter/sec
ZDOT = 12246
406217 ZDOT = 3730
588524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16514345
44 X = 5033572
49
Y = -6036950
14 feet Y = -1840062
40 meter
Z = -13694498
50 Z = -4174083
14
XDOT = 15304
996841 XDOT = 4664
963037
YDOT = 14088
648571 feet/sec YDOT = 4294
220084 meter/sec
ZDOT = 12236
146264 ZDOT = 3729
577381
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 19227
25069669
00016717 00000-0 10270-3 0 9168
2 25544 51
6411 68
2370 0007605 268
7464 91
2816 15
50666356 24412
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
25069669 = yrday
fracday
Element set: 916
Inclination: 51
6411 deg
RA of node: 68
2370 deg
Eccentricity:
0007605
Arg of perigee: 268
7464 deg
Mean anomaly: 91
2816 deg
Mean motion: 15
50666356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 324
Coasting Arc #18 (Orbit 2442)
---------------------------------------
Vector Time (GMT): 2019/227/08:49:57
959
Vector Time (MET): N/A
Weight (LBS) : 936945
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4618371
05 A = 6790425
60 meter
Y = 1182856
82 meter E =
0003940
Z = -4838511
23 I = 51
98666
XDOT = 868
835671 Wp = 150
16061
YDOT = 7159
978948 meter/sec RA = 66
86200 deg
ZDOT = 2577
262686 TA = 145
13570
MA = 145
10988
Ha = 224
214 n
mi
Hp = 223
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15152135
97 X = 4628303
00
Y = 3880763
84 feet Y = 1234558
30 meter
Z = -15874380
67 Z = -4816053
30
XDOT = 2850
510732 XDOT = 776
187536
YDOT = 23490
744580 feet/sec YDOT = 7169
176813 meter/sec
ZDOT = 8455
586240 ZDOT = 2581
258152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2513697
48 X = 766174
99
Y = -15542248
18 feet Y = -4737277
25 meter
Z = -15772233
85 Z = -4807376
88
XDOT = 22018
377141 XDOT = 6711
201353
YDOT = -5045
503269 feet/sec YDOT = -1537
869397 meter/sec
ZDOT = 8473
107912 ZDOT = 2582
603291
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 19227
37958702
00016717 00000-0 10270-3 0 9177
2 25544 51
6433 67
5991 0008867 270
9427 89
0708 15
50404284 24439
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
37958702 = yrday
fracday
Element set: 917
Inclination: 51
6433 deg
RA of node: 67
5991 deg
Eccentricity:
0008867
Arg of perigee: 270
9427 deg
Mean anomaly: 89
0708 deg
Mean motion: 15
50404284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2443
Checksum: 340
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