[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 7th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16903 7526 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 995 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
131/09:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
3
134/06:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 217
2
134/18:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 217
1
Coasting Arc #1 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2019/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6334344
94 A = 6792870
53 meter
Y = -1990787
54 meter E =
0008191
Z = -1414836
86 I = 51
47784
XDOT = 292
548381 Wp = 28
79775
YDOT = -5024
338389 meter/sec RA = 207
21339 deg
ZDOT = 5780
886178 TA = 315
75344
MA = 315
81890
Ha = 222
910 n
mi
Hp = 217
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20781971
59 X = -6304739
97
Y = -6531455
19 feet Y = -2061457
00 meter
Z = -4641853
21 Z = -1445535
58
XDOT = 959
804398 XDOT = 320
629313
YDOT = -16484
049832 feet/sec YDOT = -5020
910243 meter/sec
ZDOT = 18966
162002 ZDOT = 5782
375202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19602517
03 X = -5974847
19
Y = 9433145
44 feet Y = 2875222
73 meter
Z = -4780600
89 Z = -1457127
15
XDOT = -9981
940398 XDOT = -3042
495433
YDOT = -11161
430497 feet/sec YDOT = -3402
004016 meter/sec
ZDOT = 18973
283158 ZDOT = 5783
056707
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 19126
50284387
00016717 00000-0 10270-3 0 9003
2 25544 51
6408 208
3705 0001361 293
7323 66
3686 15
52601162 8777
Satellite: ISS
Catalog Number: 25544
Epoch time: 19126
50284387 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 208
3705 deg
Eccentricity:
0001361
Arg of perigee: 293
7323 deg
Mean anomaly: 66
3686 deg
Mean motion: 15
52601162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 877
Checksum: 304
Coasting Arc #2 (Orbit 892)
---------------------------------------
Vector Time (GMT): 2019/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6336317
18 A = 6793635
03 meter
Y = 2427447
21 meter E =
0011354
Z = 190332
50 I = 51
51033
XDOT = -1544
865648 Wp = 134
28002
YDOT = 4519
491985 meter/sec RA = 202
23990 deg
ZDOT = -5996
396161 TA = 43
66703
MA = 43
57726
Ha = 222
964 n
mi
Hp = 217
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20788442
20 X = 6307777
30
Y = 7964065
66 feet Y = 2498144
75 meter
Z = 624450
48 Z = 221043
39
XDOT = -5068
456852 XDOT = -1566
161395
YDOT = 14827
729611 feet/sec YDOT = 4502
097624 meter/sec
ZDOT = -19673
215752 ZDOT = -6003
952037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20459108
73 X = 6235936
34
Y = -8764584
54 feet Y = -2671445
37 meter
Z = 763241
27 Z = 232635
94
XDOT = 6147
586071 XDOT = 1873
784235
YDOT = 12584
010152 feet/sec YDOT = 3835
606294 meter/sec
ZDOT = -19707
752633 ZDOT = -6006
923003
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 19127
53266375
00016717 00000-0 10270-3 0 9015
2 25544 51
6403 203
2486 0001212 297
5046 62
5983 15
52640604 8931
Satellite: ISS
Catalog Number: 25544
Epoch time: 19127
53266375 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 203
2486 deg
Eccentricity:
0001212
Arg of perigee: 297
5046 deg
Mean anomaly: 62
5983 deg
Mean motion: 15
52640604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 893
Checksum: 300
Coasting Arc #3 (Orbit 908)
---------------------------------------
Vector Time (GMT): 2019/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6121480
70 A = 6793306
33 meter
Y = -2747835
70 meter E =
0013232
Z = 1015778
05 I = 51
53978
XDOT = 2795
077236 Wp = 50
64867
YDOT = -4032
500611 meter/sec RA = 197
26831 deg
ZDOT = 5892
518945 TA = 320
37130
MA = 320
46793
Ha = 223
034 n
mi
Hp = 217
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20083598
11 X = -6095232
81
Y = -9015209
00 feet Y = -2816143
72 meter
Z = 3332605
17 Z = 986105
27
XDOT = 9170
200907 XDOT = 2811
339093
YDOT = -13229
988881 feet/sec YDOT = -4001
153732 meter/sec
ZDOT = 19332
411237 ZDOT = 5906
135688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20571795
61 X = -6270283
30
Y = 7893155
25 feet Y = 2405833
72 meter
Z = 3198513
59 Z = 974906
94
XDOT = -2424
979692 XDOT = -739
133810
YDOT = -14239
108072 feet/sec YDOT = -4340
080140 meter/sec
ZDOT = 19394
347085 ZDOT = 5911
396992
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 19128
56248029
00016717 00000-0 10270-3 0 9026
2 25544 51
6398 198
1263 0001283 310
3885 49
7154 15
52624412 9096
Satellite: ISS
Catalog Number: 25544
Epoch time: 19128
56248029 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 198
1263 deg
Eccentricity:
0001283
Arg of perigee: 310
3885 deg
Mean anomaly: 49
7154 deg
Mean motion: 15
52624412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 909
Checksum: 316
Coasting Arc #4 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2019/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5668624
28 A = 6791645
51 meter
Y = 3022310
89 meter E =
0005063
Z = -2199689
15 I = 51
56551
XDOT = -4017
027876 Wp = 139
96502
YDOT = 3563
888768 meter/sec RA = 192
29756 deg
ZDOT = -5466
047985 TA = 64
46388
MA = 64
41153
Ha = 223
041 n
mi
Hp = 217
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18597848
70 X = 5645091
60
Y = 9915718
16 feet Y = 3085570
06 meter
Z = -7216827
93 Z = -2172209
71
XDOT = -13179
225316 XDOT = -4030
030481
YDOT = 11692
548450 feet/sec YDOT = 3518
895391 meter/sec
ZDOT = -17933
228297 ZDOT = -5485
592606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20070316
19 X = 6117432
38
Y = -6569673
33 feet Y = -2002436
43 meter
Z = -7092661
60 Z = -2161843
25
XDOT = -1101
376230 XDOT = -335
699475
YDOT = 16053
001940 feet/sec YDOT = 4892
954991 meter/sec
ZDOT = -18021
971791 ZDOT = -5493
097002
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 19129
52793051
00016717 00000-0 10270-3 0 9034
2 25544 51
6387 193
3247 0001199 311
1588 48
9460 15
52651374 9243
Satellite: ISS
Catalog Number: 25544
Epoch time: 19129
52793051 = yrday
fracday
Element set: 903
Inclination: 51
6387 deg
RA of node: 193
3247 deg
Eccentricity:
0001199
Arg of perigee: 311
1588 deg
Mean anomaly: 48
9460 deg
Mean motion: 15
52651374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 924
Checksum: 321
Coasting Arc #5 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2019/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5006264
27 A = 6789248
34 meter
Y = -3233413
98 meter E =
0012032
Z = 3239981
91 I = 51
59076
XDOT = 5122
607781 Wp = 82
33717
YDOT = -3147
228204 meter/sec RA = 187
32405 deg
ZDOT = 4760
762939 TA = 315
21901
MA = 315
31607
Ha = 223
096 n
mi
Hp = 217
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16424751
55 X = -4985473
35
Y = -10608313
57 feet Y = -3289281
57 meter
Z = 10629861
92 Z = 3215713
45
XDOT = 16806
455975 XDOT = 5134
295013
YDOT = -10325
551852 feet/sec YDOT = -3089
878708 meter/sec
ZDOT = 15619
300981 ZDOT = 4785
674863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18998335
00 X = -5790692
51
Y = 4867324
82 feet Y = 1483560
60 meter
Z = 10520226
30 Z = 3206564
98
XDOT = 4156
339163 XDOT = 1266
852177
YDOT = -17878
049507 feet/sec YDOT = -5449
229490 meter/sec
ZDOT = 15732
326841 ZDOT = 4795
213221
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 19130
55774046
00016717 00000-0 10270-3 0 9043
2 25544 51
6391 188
2019 0001263 316
7554 43
3498 15
52660322 9405
Satellite: ISS
Catalog Number: 25544
Epoch time: 19130
55774046 = yrday
fracday
Element set: 904
Inclination: 51
6391 deg
RA of node: 188
2019 deg
Eccentricity:
0001263
Arg of perigee: 316
7554 deg
Mean anomaly: 43
3498 deg
Mean motion: 15
52660322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 940
Checksum: 302
Coasting Arc #6 (Orbit 952)
---------------------------------------
Vector Time (GMT): 2019/131/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -352866
42 A = 6781628
85 meter
Y = 4205244
58 meter E =
0014013
Z = -5320768
87 I = 51
59614
XDOT = -7639
360171 Wp = 87
29011
YDOT = -487
479935 meter/sec RA = 182
92564 deg
ZDOT = 122
280911 TA = 183
87232
MA = 183
88318
Ha = 223
019 n
mi
Hp = 217
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1157698
23 X = -374019
04
Y = 13796734
18 feet Y = 4201180
72 meter
Z = -17456590
77 Z = -5322534
02
XDOT = -25063
517623 XDOT = -7633
935234
YDOT = -1599
343620 feet/sec YDOT = -572
878285 meter/sec
ZDOT = 401
184091 ZDOT = 85
184817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20471
37 X = -6239
67
Y = 13834728
37 feet Y = 4216825
21 meter
Z = -17464895
43 Z = -5323300
13
XDOT = -24106
492191 XDOT = -7347
658820
YDOT = 254
938395 feet/sec YDOT = 77
705223 meter/sec
ZDOT = 233
241111 ZDOT = 71
091891
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 19131
39445934
00016717 00000-0 10270-3 0 9058
2 25544 51
6406 184
0389 0001268 316
8179 43
2874 15
52663168 9537
Satellite: ISS
Catalog Number: 25544
Epoch time: 19131
39445934 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 184
0389 deg
Eccentricity:
0001268
Arg of perigee: 316
8179 deg
Mean anomaly: 43
2874 deg
Mean motion: 15
52663168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 953
Checksum: 329
Coasting Arc #7 (Orbit 968)
---------------------------------------
Vector Time (GMT): 2019/132/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1550183
10 A = 6782215
39 meter
Y = -4133310
41 meter E =
0004673
Z = 5147147
49 I = 51
63193
XDOT = 7462
309924 Wp = 39
22524
YDOT = 922
026887 meter/sec RA = 177
93979 deg
ZDOT = -1502
746716 TA = 65
27453
MA = 65
22590
Ha = 222
928 n
mi
Hp = 217
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5085902
54 X = 1571285
71
Y = -13560729
70 feet Y = -4115857
47 meter
Z = 16886966
83 Z = 5154728
74
XDOT = 24482
644107 XDOT = 7458
744464
YDOT = 3025
022596 feet/sec YDOT = 1005
455808 meter/sec
ZDOT = -4930
271377 ZDOT = -1466
506160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3719595
43 X = 1133732
69
Y = -13955405
41 feet Y = -4253607
57 meter
Z = 16921604
92 Z = 5157705
18
XDOT = 23670
949507 XDOT = 7214
905410
YDOT = 512
843227 feet/sec YDOT = 156
314616 meter/sec
ZDOT = -4766
209933 ZDOT = -1452
740787
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 19132
42426428
00016717 00000-0 10270-3 0 9061
2 25544 51
6406 178
9164 0001312 320
4328 39
6728 15
52698166 9697
Satellite: ISS
Catalog Number: 25544
Epoch time: 19132
42426428 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 178
9164 deg
Eccentricity:
0001312
Arg of perigee: 320
4328 deg
Mean anomaly: 39
6728 deg
Mean motion: 15
52698166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 969
Checksum: 322
Coasting Arc #8 (Orbit 983)
---------------------------------------
Vector Time (GMT): 2019/133/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2677534
03 A = 6784038
38 meter
Y = 4087199
39 meter E =
0010011
Z = -4715803
11 I = 51
67079
XDOT = -6998
058539 Wp = 105
23159
YDOT = -1362
283112 meter/sec RA = 172
96002 deg
ZDOT = 2795
045057 TA = 192
48456
MA = 192
50938
Ha = 223
041 n
mi
Hp = 217
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8784560
48 X = -2700132
43
Y = 13409446
81 feet Y = 4057131
14 meter
Z = -15471794
97 Z = -4728864
35
XDOT = -22959
509643 XDOT = -6995
881814
YDOT = -4469
432781 feet/sec YDOT = -1440
528231 meter/sec
ZDOT = 9170
095331 ZDOT = 2761
056232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7181692
22 X = -2188979
79
Y = 14267503
50 feet Y = 4348735
07 meter
Z = -15531253
87 Z = -4733926
18
XDOT = -22328
068283 XDOT = -6805
595213
YDOT = -1432
696701 feet/sec YDOT = -436
685954 meter/sec
ZDOT = 9016
243312 ZDOT = 2748
150962
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 19133
38970610
00016717 00000-0 10270-3 0 9075
2 25544 51
6402 174
1154 0001220 326
9058 33
2017 15
52692440 9846
Satellite: ISS
Catalog Number: 25544
Epoch time: 19133
38970610 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 174
1154 deg
Eccentricity:
0001220
Arg of perigee: 326
9058 deg
Mean anomaly: 33
2017 deg
Mean motion: 15
52692440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 984
Checksum: 285
Coasting Arc #9 (Orbit 997)
---------------------------------------
Vector Time (GMT): 2019/134/06:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6170094
89 A = 6790591
03 meter
Y = 916392
25 meter E =
0004011
Z = -2683775
11 I = 51
72146
XDOT = -2967
783006 Wp = 119
63605
YDOT = 4782
722345 meter/sec RA = 168
59991 deg
ZDOT = -5197
722949 TA = 90
59294
MA = 90
54698
Ha = 223
148 n
mi
Hp = 217
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20243093
46 X = 6172425
33
Y = 3006536
27 feet Y = 985403
67 meter
Z = -8805036
47 Z = -2653797
23
XDOT = -9736
820885 XDOT = -2995
796382
YDOT = 15691
346276 feet/sec YDOT = 4749
378015 meter/sec
ZDOT = -17052
896815 ZDOT = -5212
207341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15107084
39 X = 4604639
32
Y = 13891360
94 feet Y = 4234086
82 meter
Z = -8669305
21 Z = -2642404
23
XDOT = -15761
576739 XDOT = -4804
128590
YDOT = 6473
624863 feet/sec YDOT = 1973
160858 meter/sec
ZDOT = -17118
859177 ZDOT = -5217
828277
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 19134
29078268
00016717 00000-0 10270-3 0 9085
2 25544 51
6401 169
6309 0001129 331
9342 28
1749 15
52678311 9987
Satellite: ISS
Catalog Number: 25544
Epoch time: 19134
29078268 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 169
6309 deg
Eccentricity:
0001129
Arg of perigee: 331
9342 deg
Mean anomaly: 28
1749 deg
Mean motion: 15
52678311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 998
Checksum: 326
Coasting Arc #10 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2019/134/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1236677
81 A = 6781534
96 meter
Y = -4019841
25 meter E =
0002168
Z = 5318191
44 I = 51
70654
XDOT = 7400
097043 Wp = 59
73308
YDOT = -1998
432752 meter/sec RA = 166
13438 deg
ZDOT = 211
253890 TA = 28
26119
MA = 28
24943
Ha = 223
167 n
mi
Hp = 217
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4057341
89 X = -1217467
93
Y = -13188455
55 feet Y = -4033563
36 meter
Z = 17448134
65 Z = 5312230
64
XDOT = 24278
533605 XDOT = 7420
867934
YDOT = -6556
537900 feet/sec YDOT = -1915
563551 meter/sec
ZDOT = 693
090191 ZDOT = 247
251503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4418002
35 X = -1346607
12
Y = 13107630
91 feet Y = 3995205
90 meter
Z = 17421425
11 Z = 5310050
37
XDOT = -22505
493553 XDOT = -6859
674435
YDOT = -8719
354329 feet/sec YDOT = -2657
659199 meter/sec
ZDOT = 856
312435 ZDOT = 261
004030
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 19134
80568116
00016717 00000-0 10270-3 0 9099
2 25544 51
6391 167
0739 0001735 340
2904 19
8180 15
52698736 10064
Satellite: ISS
Catalog Number: 25544
Epoch time: 19134
80568116 = yrday
fracday
Element set: 909
Inclination: 51
6391 deg
RA of node: 167
0739 deg
Eccentricity:
0001735
Arg of perigee: 340
2904 deg
Mean anomaly: 19
8180 deg
Mean motion: 15
52698736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 317
Coasting Arc #11 (Orbit 1020)
---------------------------------------
Vector Time (GMT): 2019/135/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 75695
88 A = 6782021
18 meter
Y = 4331987
49 meter E =
0013691
Z = -5229576
21 I = 51
73938
XDOT = -7405
206145 Wp = 92
34107
YDOT = 1547
029607 meter/sec RA = 161
15553 deg
ZDOT = 1176
431267 TA = 188
93215
MA = 188
95653
Ha = 223
263 n
mi
Hp = 217
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 248346
05 X = 52651
44
Y = 14212557
38 feet Y = 4332705
27 meter
Z = -17157402
26 Z = -5229264
35
XDOT = -24295
295751 XDOT = -7427
669624
YDOT = 5075
556452 feet/sec YDOT = 1464
093771 meter/sec
ZDOT = 3859
682636 ZDOT = 1140
404564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7896107
38 X = 2406733
53
Y = -11821482
38 feet Y = -3603187
83 meter
Z = -17156309
56 Z = -5229243
15
XDOT = 21936
351099 XDOT = 6686
199815
YDOT = 9297
930002 feet/sec YDOT = 2834
009065 meter/sec
ZDOT = 3696
342663 ZDOT = 1126
645244
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 19135
77111683
00016717 00000-0 10270-3 0 9101
2 25544 51
6384 162
2714 0001724 348
0620 12
0491 15
52671975 10218
Satellite: ISS
Catalog Number: 25544
Epoch time: 19135
77111683 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 162
2714 deg
Eccentricity:
0001724
Arg of perigee: 348
0620 deg
Mean anomaly: 12
0491 deg
Mean motion: 15
52671975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1021
Checksum: 283
Coasting Arc #12 (Orbit 1036)
---------------------------------------
Vector Time (GMT): 2019/136/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1053191
92 A = 6783602
25 meter
Y = -4631774
67 meter E =
0007819
Z = 4840007
06 I = 51
77602
XDOT = 7174
461797 Wp = 48
46730
YDOT = -1003
113465 meter/sec RA = 156
18210 deg
ZDOT = -2513
443328 TA = 66
23456
MA = 66
15258
Ha = 223
247 n
mi
Hp = 217
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3455354
05 X = 1081397
01
Y = -15196111
14 feet Y = -4619839
65 meter
Z = 15879288
26 Z = 4845191
47
XDOT = 23538
260489 XDOT = 7197
354790
YDOT = -3291
054675 feet/sec YDOT = -922
755499 meter/sec
ZDOT = -8246
205145 ZDOT = -2478
536338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11314312
99 X = -3448602
60
Y = 10681287
05 feet Y = 3255656
29 meter
Z = 15903128
28 Z = 4847273
50
XDOT = -20580
934651 XDOT = -6273
068882
YDOT = -9721
196568 feet/sec YDOT = -2963
020714 meter/sec
ZDOT = -8087
959495 ZDOT = -2465
210054
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 19136
80091208
00016717 00000-0 10270-3 0 9117
2 25544 51
6385 157
1499 0001714 349
7767 10
3350 15
52674706 10378
Satellite: ISS
Catalog Number: 25544
Epoch time: 19136
80091208 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 157
1499 deg
Eccentricity:
0001714
Arg of perigee: 349
7767 deg
Mean anomaly: 10
3350 deg
Mean motion: 15
52674706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1037
Checksum: 309
Coasting Arc #13 (Orbit 1051)
---------------------------------------
Vector Time (GMT): 2019/137/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2062908
74 A = 6785966
09 meter
Y = 4911870
45 meter E =
0007411
Z = -4210282
83 I = 51
81458
XDOT = -6695
740918 Wp = 98
08484
YDOT = 357
015081 meter/sec RA = 151
21291 deg
ZDOT = 3701
770954 TA = 209
83771
MA = 209
87998
Ha = 223
285 n
mi
Hp = 216
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6768073
30 X = -2097229
76
Y = 16115060
52 feet Y = 4888609
93 meter
Z = -13813263
87 Z = -4220386
90
XDOT = -21967
653931 XDOT = -6717
217001
YDOT = 1171
309320 feet/sec YDOT = 282
018297 meter/sec
ZDOT = 12144
917829 ZDOT = 3669
192806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14415026
10 X = 4393699
95
Y = -9819951
36 feet Y = -2993121
17 meter
Z = -13859431
02 Z = -4224354
58
XDOT = 18368
569835 XDOT = 5598
740086
YDOT = 10052
476356 feet/sec YDOT = 3063
994793 meter/sec
ZDOT = 11997
254895 ZDOT = 3656
763292
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 19137
76634100
00016717 00000-0 10270-3 0 9128
2 25544 51
6389 152
3467 0001756 353
7686 6
3444 15
52690985 10528
Satellite: ISS
Catalog Number: 25544
Epoch time: 19137
76634100 = yrday
fracday
Element set: 912
Inclination: 51
6389 deg
RA of node: 152
3467 deg
Eccentricity:
0001756
Arg of perigee: 353
7686 deg
Mean anomaly: 6
3444 deg
Mean motion: 15
52690985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1052
Checksum: 320
Coasting Arc #14 (Orbit 1067)
---------------------------------------
Vector Time (GMT): 2019/138/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2960870
70 A = 6788795
93 meter
Y = -5119008
33 meter E =
0012619
Z = 3324922
23 I = 51
85238
XDOT = 6034
557093 Wp = 83
40128
YDOT = 419
091050 meter/sec RA = 146
25226 deg
ZDOT = -4711
854553 TA = 58
04891
MA = 57
92628
Ha = 223
342 n
mi
Hp = 216
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9714142
71 X = 3001741
92
Y = -16794646
77 feet Y = -5085669
58 meter
Z = 10908537
50 Z = 3339404
11
XDOT = 19798
415659 XDOT = 6052
310191
YDOT = 1374
970638 feet/sec YDOT = 486
673380 meter/sec
ZDOT = -15458
840397 ZDOT = -4682
497231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17114728
03 X = -5216569
10
Y = 9059008
09 feet Y = 2761185
67 meter
Z = 10974578
61 Z = 3345051
56
XDOT = -15437
900039 XDOT = -4705
471932
YDOT = -10533
375347 feet/sec YDOT = -3210
572806 meter/sec
ZDOT = -15325
816631 ZDOT = -4671
308909
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 19138
79612944
00016717 00000-0 10270-3 0 9135
2 25544 51
6387 147
2245 0001798 359
5760
5390 15
52684008 10688
Satellite: ISS
Catalog Number: 25544
Epoch time: 19138
79612944 = yrday
fracday
Element set: 913
Inclination: 51
6387 deg
RA of node: 147
2245 deg
Eccentricity:
0001798
Arg of perigee: 359
5760 deg
Mean anomaly:
5390 deg
Mean motion: 15
52684008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1068
Checksum: 327
Coasting Arc #15 (Orbit 1082)
---------------------------------------
Vector Time (GMT): 2019/139/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3664422
71 A = 6791217
31 meter
Y = 5236554
22 meter E =
0007200
Z = -2288777
80 I = 51
88800
XDOT = -5232
541381 Wp = 35
22617
YDOT = -1285
779185 meter/sec RA = 141
29806 deg
ZDOT = 5449
989371 TA = 299
40197
MA = 299
47383
Ha = 223
336 n
mi
Hp = 216
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12022384
22 X = -3711589
21
Y = 17180296
00 feet Y = 5195312
62 meter
Z = -7509113
51 Z = -2306692
45
XDOT = -17167
130514 XDOT = -5244
247993
YDOT = -4218
435645 feet/sec YDOT = -1344
359201 meter/sec
ZDOT = 17880
542556 ZDOT = 5424
542643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19149136
88 X = 5836656
92
Y = -8472203
33 feet Y = -2582327
57 meter
Z = -7590744
77 Z = -2313659
00
XDOT = 11970
117269 XDOT = 3648
491744
YDOT = 11179
704462 feet/sec YDOT = 3407
573920 meter/sec
ZDOT = 17765
297957 ZDOT = 5414
862817
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 19139
76155404
00016717 00000-0 10270-3 0 9147
2 25544 51
6390 142
4220 0001785
5601 359
5553 15
52699249 10833
Satellite: ISS
Catalog Number: 25544
Epoch time: 19139
76155404 = yrday
fracday
Element set: 914
Inclination: 51
6390 deg
RA of node: 142
4220 deg
Eccentricity:
0001785
Arg of perigee:
5601 deg
Mean anomaly: 359
5553 deg
Mean motion: 15
52699249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1083
Checksum: 304
Coasting Arc #16 (Orbit 1098)
---------------------------------------
Vector Time (GMT): 2019/140/18:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4217047
97 A = 6793017
62 meter
Y = -5205316
39 meter E =
0012886
Z = 1092025
01 I = 51
91986
XDOT = 4333
365238 Wp = 116
49835
YDOT = 2261
547971 meter/sec RA = 136
35051 deg
ZDOT = -5905
865041 TA = 51
70784
MA = 51
59202
Ha = 223
414 n
mi
Hp = 216
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13835459
21 X = 4269637
36
Y = -17077809
68 feet Y = -5157864
51 meter
Z = 3582759
23 Z = 1112637
17
XDOT = 14217
077553 XDOT = 4336
441680
YDOT = 7419
776809 feet/sec YDOT = 2310
024669 meter/sec
ZDOT = -19376
197641 ZDOT = -5884
807132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20537496
76 X = -6259829
01
Y = 7784678
90 feet Y = 2372770
13 meter
Z = 3676639
76 Z = 1120639
80
XDOT = -8081
770335 XDOT = -2463
323598
YDOT = -12142
355039 feet/sec YDOT = -3700
989816 meter/sec
ZDOT = -19280
917400 ZDOT = -5876
823624
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 19140
79133794
00016717 00000-0 10270-3 0 9151
2 25544 51
6398 137
2996 0001712 3
3747 356
7416 15
52678463 10994
Satellite: ISS
Catalog Number: 25544
Epoch time: 19140
79133794 = yrday
fracday
Element set: 915
Inclination: 51
6398 deg
RA of node: 137
2996 deg
Eccentricity:
0001712
Arg of perigee: 3
3747 deg
Mean anomaly: 356
7416 deg
Mean motion: 15
52678463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1099
Checksum: 339
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