[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 9th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19998 2692 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 626 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
227/05:42:47
391 0
3 1
8 1
8
N/A 1
7 0
0 223
7
000/00:09:34
783 0
4 -0
0 222
9
227/08:44:47
334 0
6 1
8 1
8
N/A 1
7 -0
0 224
0
000/00:09:34
669 0
1 -0
0 223
6
234/03:28:32
000 0
0 0
0 0
0
N/A 0
0 0
0 226
4
000/00:00:00
000 0
0 0
0 223
3
Coasting Arc #1 (Orbit 2321)
---------------------------------------
Vector Time (GMT): 2019/219/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2182047
90 A = 6790367
44 meter
Y = -4759567
40 meter E =
0004521
Z = 4319407
09 I = 52
00730
XDOT = 4334
362232 Wp = 98
70446
YDOT = -5222
219636 meter/sec RA = 105
48823 deg
ZDOT = -3562
267491 TA = 27
44545
MA = 27
42158
Ha = 225
153 n
mi
Hp = 221
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7158949
80 X = -2149643
97
Y = -15615378
61 feet Y = -4783787
54 meter
Z = 14171283
09 Z = 4308886
17
XDOT = 14220
348530 XDOT = 4409
739822
YDOT = -17133
266521 feet/sec YDOT = -5173
328183 meter/sec
ZDOT = -11687
229300 ZDOT = -3541
030044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1562725
13 X = -476318
62
Y = 17146220
40 feet Y = 5226167
98 meter
Z = 14123770
46 Z = 4304925
24
XDOT = -19716
608944 XDOT = -6009
622406
YDOT = 7756
906144 feet/sec YDOT = 2364
304993 meter/sec
ZDOT = -11590
149809 ZDOT = -3532
677662
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
58355382
00016717 00000-0 10270-3 0 9008
2 25544 51
6427 106
2802 0006061 233
6334 126
4258 15
51080936 23228
Satellite: ISS
Catalog Number: 25544
Epoch time: 19219
58355382 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 106
2802 deg
Eccentricity:
0006061
Arg of perigee: 233
6334 deg
Mean anomaly: 126
4258 deg
Mean motion: 15
51080936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2322
Checksum: 290
Coasting Arc #2 (Orbit 2336)
---------------------------------------
Vector Time (GMT): 2019/220/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2121833
82 A = 6791987
01 meter
Y = 5157640
87 meter E =
0005098
Z = -3881442
63 I = 52
02011
XDOT = -4207
557985 Wp = 169
77462
YDOT = 4862
961288 meter/sec RA = 100
55031 deg
ZDOT = 4157
729411 TA = 143
78033
MA = 143
74580
Ha = 224
971 n
mi
Hp = 221
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6961397
06 X = 2082855
64
Y = 16921393
94 feet Y = 5181150
95 meter
Z = -12734391
84 Z = -3871230
08
XDOT = -13804
324097 XDOT = -4281
820075
YDOT = 15954
597401 feet/sec YDOT = 4815
494003 meter/sec
ZDOT = 13640
844525 ZDOT = 4137
110694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2084560
30 X = 635373
98
Y = -18210447
31 feet Y = -5550544
34 meter
Z = -12688324
33 Z = -3867401
26
XDOT = 18578
665523 XDOT = 5662
777252
YDOT = -7321
291270 feet/sec YDOT = -2231
529579 meter/sec
ZDOT = 13546
591788 ZDOT = 4129
001177
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
55000817
00016717 00000-0 10270-3 0 9018
2 25544 51
6426 101
4845 0006188 236
8902 123
1656 15
51048261 23374
Satellite: ISS
Catalog Number: 25544
Epoch time: 19220
55000817 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 101
4845 deg
Eccentricity:
0006188
Arg of perigee: 236
8902 deg
Mean anomaly: 123
1656 deg
Mean motion: 15
51048261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2337
Checksum: 286
Coasting Arc #3 (Orbit 2352)
---------------------------------------
Vector Time (GMT): 2019/221/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2101416
90 A = 6793436
70 meter
Y = -5505830
39 meter E =
0007720
Z = 3370080
75 I = 52
03131
XDOT = 4117
298374 Wp = 113
50252
YDOT = -4447
342871 meter/sec RA = 95
61487 deg
ZDOT = -4692
954564 TA = 27
46978
MA = 27
42899
Ha = 224
762 n
mi
Hp = 221
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6894412
42 X = -2056062
76
Y = -18063748
00 feet Y = -5529076
52 meter
Z = 11056695
38 Z = 3359982
79
XDOT = 13508
196766 XDOT = 4189
519378
YDOT = -14591
019918 feet/sec YDOT = -4400
896256 meter/sec
ZDOT = -15396
832560 ZDOT = -4672
779321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2379099
64 X = -725149
57
Y = 19213954
31 feet Y = 5856413
27 meter
Z = 11011188
49 Z = 3356210
25
XDOT = -17485
203446 XDOT = -5329
490010
YDOT = 6616
144823 feet/sec YDOT = 2016
600942 meter/sec
ZDOT = -15304
615465 ZDOT = -4664
846794
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
58088794
00016717 00000-0 10270-3 0 9023
2 25544 51
6436 96
3694 0006133 242
4522 117
6006 15
51082793 23533
Satellite: ISS
Catalog Number: 25544
Epoch time: 19221
58088794 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 96
3694 deg
Eccentricity:
0006133
Arg of perigee: 242
4522 deg
Mean anomaly: 117
6006 deg
Mean motion: 15
51082793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2353
Checksum: 310
Coasting Arc #4 (Orbit 2367)
---------------------------------------
Vector Time (GMT): 2019/222/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2122799
41 A = 6794995
70 meter
Y = 5811192
39 meter E =
0001525
Z = -2808930
59 I = 52
03685
XDOT = -4059
156114 Wp = 261
98216
YDOT = 3969
307591 meter/sec RA = 90
68052 deg
ZDOT = 5141
588064 TA = 66
39279
MA = 66
37678
Ha = 224
582 n
mi
Hp = 221
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6964564
98 X = 2071303
26
Y = 19065591
84 feet Y = 5834643
29 meter
Z = -9215651
55 Z = -2798743
64
XDOT = -13317
441320 XDOT = -4128
215030
YDOT = 13022
662701 feet/sec YDOT = 3923
528772 meter/sec
ZDOT = 16868
727243 ZDOT = 5121
702995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2454373
57 X = 748093
07
Y = -20169815
50 feet Y = -6147759
76 meter
Z = -9169775
58 Z = -2794947
60
XDOT = 16424
896071 XDOT = 5006
308322
YDOT = -5632
903288 feet/sec YDOT = -1716
908922 meter/sec
ZDOT = 16777
856287 ZDOT = 5113
890596
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
54733699
00016717 00000-0 10270-3 0 9032
2 25544 51
6421 91
5733 0006168 245
1351 114
9159 15
51049039 23687
Satellite: ISS
Catalog Number: 25544
Epoch time: 19222
54733699 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 91
5733 deg
Eccentricity:
0006168
Arg of perigee: 245
1351 deg
Mean anomaly: 114
9159 deg
Mean motion: 15
51049039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2368
Checksum: 313
Coasting Arc #5 (Orbit 2383)
---------------------------------------
Vector Time (GMT): 2019/223/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2164024
24 A = 6796192
94 meter
Y = -6051367
92 meter E =
0009930
Z = 2191349
11 I = 52
04043
XDOT = 4056
570042 Wp = 132
45844
YDOT = -3450
528309 meter/sec RA = 85
74968 deg
ZDOT = -5513
229702 TA = 23
37898
MA = 23
33386
Ha = 224
388 n
mi
Hp = 221
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7099817
07 X = -2106839
46
Y = -19853569
29 feet Y = -6075247
97 meter
Z = 7189465
57 Z = 2180975
72
XDOT = 13308
956832 XDOT = 4121
633123
YDOT = -11320
630936 feet/sec YDOT = -3404
800717 meter/sec
ZDOT = -18088
023957 ZDOT = -5493
366941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2345685
32 X = -714964
88
Y = 20969945
43 feet Y = 6391639
37 meter
Z = 7142771
17 Z = 2177116
65
XDOT = -15518
854319 XDOT = -4730
146796
YDOT = 4404
813533 feet/sec YDOT = 1342
587165 meter/sec
ZDOT = -17997
286895 ZDOT = -5485
573046
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
57821341
00016717 00000-0 10270-3 0 9049
2 25544 51
6421 86
4593 0006143 249
8849 110
1641 15
51083785 23848
Satellite: ISS
Catalog Number: 25544
Epoch time: 19223
57821341 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 86
4593 deg
Eccentricity:
0006143
Arg of perigee: 249
8849 deg
Mean anomaly: 110
1641 deg
Mean motion: 15
51083785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2384
Checksum: 311
Coasting Arc #6 (Orbit 2398)
---------------------------------------
Vector Time (GMT): 2019/224/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2228102
37 A = 6797288
44 meter
Y = 6229627
16 meter E =
0004676
Z = -1545109
55 I = 52
03946
XDOT = -4101
950473 Wp = 347
58358
YDOT = 2901
343050 meter/sec RA = 80
81778 deg
ZDOT = 5783
773932 TA = 355
65164
MA = 355
65570
Ha = 224
213 n
mi
Hp = 221
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7310047
15 X = 2165780
43
Y = 20438409
31 feet Y = 6254195
00 meter
Z = -5069257
05 Z = -1534437
45
XDOT = -13457
842758 XDOT = -4162
183073
YDOT = 9518
842029 feet/sec YDOT = 2855
135009 meter/sec
ZDOT = 18975
636260 ZDOT = 5763
702475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2056375
51 X = 626783
26
Y = -21619929
04 feet Y = -6589754
37 meter
Z = -5021226
90 Z = -1530469
96
XDOT = 14769
146574 XDOT = 4501
635876
YDOT = -2980
121885 feet/sec YDOT = -908
341151 meter/sec
ZDOT = 18883
987977 ZDOT = 5755
839535
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
54465923
00016717 00000-0 10270-3 0 9058
2 25544 51
6414 81
6629 0006301 252
3985 107
6478 15
51054118 23996
Satellite: ISS
Catalog Number: 25544
Epoch time: 19224
54465923 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 81
6629 deg
Eccentricity:
0006301
Arg of perigee: 252
3985 deg
Mean anomaly: 107
6478 deg
Mean motion: 15
51054118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2399
Checksum: 318
Coasting Arc #7 (Orbit 2414)
---------------------------------------
Vector Time (GMT): 2019/225/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2286109
97 A = 6797883
42 meter
Y = -6336602
76 meter E =
0010345
Z = 861304
16 I = 52
03542
XDOT = 4211
887954 Wp = 152
06675
YDOT = -2332
926141 meter/sec RA = 75
88739 deg
ZDOT = -5963
933385 TA = 18
67603
MA = 18
63809
Ha = 223
958 n
mi
Hp = 221
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7500360
79 X = -2219265
99
Y = -20789379
12 feet Y = -6361793
94 meter
Z = 2825801
06 Z = 850361
38
XDOT = 13818
530034 XDOT = 4266
631207
YDOT = -7653
957157 feet/sec YDOT = -2285
519465 meter/sec
ZDOT = -19566
710581 ZDOT = -5943
341221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1668387
20 X = -508524
42
Y = 22044184
49 feet Y = 6719067
43 meter
Z = 2776555
78 Z = 846294
20
XDOT = -14254
874983 XDOT = -4344
885895
YDOT = 1382
219948 feet/sec YDOT = 421
300640 meter/sec
ZDOT = -19472
736020 ZDOT = -5935
289939
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
57553073
00016717 00000-0 10270-3 0 9067
2 25544 51
6415 76
5476 0006142 257
7812 102
2651 15
51087098 24157
Satellite: ISS
Catalog Number: 25544
Epoch time: 19225
57553073 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 76
5476 deg
Eccentricity:
0006142
Arg of perigee: 257
7812 deg
Mean anomaly: 102
2651 deg
Mean motion: 15
51087098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2415
Checksum: 308
Coasting Arc #8 (Orbit 2429)
---------------------------------------
Vector Time (GMT): 2019/226/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2342765
47 A = 6798270
13 meter
Y = 6374275
93 meter E =
0007597
Z = -172522
73 I = 52
02522
XDOT = -4374
688951 Wp = 16
14043
YDOT = 1769
336505 meter/sec RA = 70
95612 deg
ZDOT = 6037
300753 TA = 342
01338
MA = 342
04024
Ha = 223
865 n
mi
Hp = 221
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7686238
43 X = 2272150
37
Y = 20912978
77 feet Y = 6400079
55 meter
Z = -566019
45 Z = -161314
03
XDOT = -14352
654039 XDOT = -4423
474212
YDOT = 5804
909793 feet/sec YDOT = 1720
142693 meter/sec
ZDOT = 19807
417168 ZDOT = 6015
932220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1180926
42 X = 359946
37
Y = -22250638
56 feet Y = -6781994
63 meter
Z = -515574
06 Z = -157146
97
XDOT = 13978
893229 XDOT = 4260
766656
YDOT = 291
113072 feet/sec YDOT = 88
731264 meter/sec
ZDOT = 19709
955427 ZDOT = 6007
594414
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
54197222
00016717 00000-0 10270-3 0 9076
2 25544 51
6395 71
7513 0006187 259
3599 100
6855 15
51053399 24304
Satellite: ISS
Catalog Number: 25544
Epoch time: 19226
54197222 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 71
7513 deg
Eccentricity:
0006187
Arg of perigee: 259
3599 deg
Mean anomaly: 100
6855 deg
Mean motion: 15
51053399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2430
Checksum: 324
Coasting Arc #9 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2019/227/05:47:34
783
Vector Time (MET): N/A
Weight (LBS) : 937367
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4647799
05 A = 6791847
01 meter
Y = 2577900
75 meter E =
0002903
Z = -4230618
46 I = 51
99372
XDOT = -349
036138 Wp = 179
58622
YDOT = 6699
568809 meter/sec RA = 67
48047 deg
ZDOT = 3696
079200 TA = 128
19152
MA = 128
16538
Ha = 223
698 n
mi
Hp = 222
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15248684
55 X = 4639176
30
Y = 8457679
62 feet Y = 2629827
57 meter
Z = -13879981
81 Z = -4208062
62
XDOT = -1145
131686 XDOT = -441
879780
YDOT = 21980
212627 feet/sec YDOT = 6695
146455 meter/sec
ZDOT = 12126
244093 ZDOT = 3694
158375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16409607
47 X = 5001648
36
Y = -6132973
29 feet Y = -1869330
26 meter
Z = -13777519
42 Z = -4199387
92
XDOT = 15432
675906 XDOT = 4703
879616
YDOT = 14051
248071 feet/sec YDOT = 4282
820412 meter/sec
ZDOT = 12116
871152 ZDOT = 3693
222327
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
25069648
00016717 00000-0 10270-3 0 9086
2 25544 51
6409 68
2367 0007403 268
1203 91
9100 15
50708244 24412
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
25069648 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 68
2367 deg
Eccentricity:
0007403
Arg of perigee: 268
1203 deg
Mean anomaly: 91
9100 deg
Mean motion: 15
50708244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 302
Coasting Arc #10 (Orbit 2442)
---------------------------------------
Vector Time (GMT): 2019/227/08:49:34
669
Vector Time (MET): N/A
Weight (LBS) : 937180
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4596939
37 A = 6790260
49 meter
Y = 1018068
04 meter E =
0004235
Z = -4896100
18 I = 51
98585
XDOT = 1003
244683 Wp = 147
55503
YDOT = 7192
022834 meter/sec RA = 66
86370 deg
ZDOT = 2434
913647 TA = 146
25672
MA = 146
22976
Ha = 224
004 n
mi
Hp = 223
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15081822
07 X = 4608995
36
Y = 3340118
24 feet Y = 1069541
73 meter
Z = -16063320
82 Z = -4873741
21
XDOT = 3291
485180 XDOT = 910
919671
YDOT = 23595
875440 feet/sec YDOT = 7202
725564 meter/sec
ZDOT = 7988
561833 ZDOT = 2439
562791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2007469
80 X = 611876
79
Y = -15422228
19 feet Y = -4700695
15 meter
Z = -15961609
10 Z = -4865098
45
XDOT = 22101
492694 XDOT = 6736
534973
YDOT = -5420
820631 feet/sec YDOT = -1652
266128 meter/sec
ZDOT = 8009
056901 ZDOT = 2441
160543
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
37958360
00016717 00000-0 10270-3 0 9098
2 25544 51
6431 67
5987 0008950 269
7315 90
2810 15
50380352 24434
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
37958360 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 67
5987 deg
Eccentricity:
0008950
Arg of perigee: 269
7315 deg
Mean anomaly: 90
2810 deg
Mean motion: 15
50380352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2443
Checksum: 326
Coasting Arc #11 (Orbit 2458)
---------------------------------------
Vector Time (GMT): 2019/228/08:49:34
669
Vector Time (MET): N/A
Weight (LBS) : 937180
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4775912
87 A = 6790984
25 meter
Y = -1163027
52 meter E =
0004463
Z = 4689048
08 I = 51
97508
XDOT = -1153
465972 Wp = 338
48629
YDOT = -6991
510599 meter/sec RA = 61
92818 deg
ZDOT = -2905
779834 TA = 140
32277
MA = 140
29011
Ha = 224
865 n
mi
Hp = 224
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15669005
49 X = -4785328
90
Y = -3815707
08 feet Y = -1216487
77 meter
Z = 15384016
03 Z = 4665826
14
XDOT = -3784
337178 XDOT = -1061
084810
YDOT = -22938
026900 feet/sec YDOT = -7003
892942 meter/sec
ZDOT = -9533
398404 ZDOT = -2911
158416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2154381
33 X = -656655
43
Y = 16083366
71 feet Y = 4902210
17 meter
Z = 15278391
90 Z = 4656853
85
XDOT = -21254
774119 XDOT = -6478
455151
YDOT = 6241
714808 feet/sec YDOT = 1902
474673 meter/sec
ZDOT = -9557
225649 ZDOT = -2913
042378
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 19228
41091014
00016717 00000-0 10270-3 0 9100
2 25544 51
6437 62
4868 0009064 274
2159 85
7956 15
50419784 24595
Satellite: ISS
Catalog Number: 25544
Epoch time: 19228
41091014 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 62
4868 deg
Eccentricity:
0009064
Arg of perigee: 274
2159 deg
Mean anomaly: 85
7956 deg
Mean motion: 15
50419784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2459
Checksum: 329
Coasting Arc #12 (Orbit 2473)
---------------------------------------
Vector Time (GMT): 2019/229/08:49:34
669
Vector Time (MET): N/A
Weight (LBS) : 937180
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4975329
42 A = 6792011
35 meter
Y = 1275070
16 meter E =
0001991
Z = -4444973
82 I = 51
96135
XDOT = 1265
782457 Wp = 194
46595
YDOT = 6768
504662 meter/sec RA = 56
99115 deg
ZDOT = 3356
201817 TA = 109
34465
MA = 109
32313
Ha = 225
289 n
mi
Hp = 224
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16323259
27 X = 4982292
24
Y = 4183301
05 feet Y = 1330746
64 meter
Z = -14583247
46 Z = -4420789
13
XDOT = 4152
829583 XDOT = 1173
698771
YDOT = 22206
380125 feet/sec YDOT = 6782
144726 meter/sec
ZDOT = 11011
160816 ZDOT = 3362
126609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2163806
28 X = 659528
16
Y = -16806627
09 feet Y = -5122659
94 meter
Z = -14473255
87 Z = -4411448
39
XDOT = 20324
473213 XDOT = 6194
899435
YDOT = -6894
623613 feet/sec YDOT = -2101
481277 meter/sec
ZDOT = 11037
487893 ZDOT = 3364
226310
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 19229
37777811
00016717 00000-0 10270-3 0 9113
2 25544 51
6436 57
6934 0009037 277
8909 82
1216 15
50387788 24741
Satellite: ISS
Catalog Number: 25544
Epoch time: 19229
37777811 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 57
6934 deg
Eccentricity:
0009037
Arg of perigee: 277
8909 deg
Mean anomaly: 82
1216 deg
Mean motion: 15
50387788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2474
Checksum: 348
Coasting Arc #13 (Orbit 2489)
---------------------------------------
Vector Time (GMT): 2019/230/08:49:34
669
Vector Time (MET): N/A
Weight (LBS) : 937180
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5192890
44 A = 6792930
05 meter
Y = -1356125
44 meter E =
0004597
Z = 4165929
67 I = 51
94514
XDOT = -1333
994899 Wp = 16
30177
YDOT = -6525
151688 meter/sec RA = 52
05468 deg
ZDOT = -3781
657377 TA = 112
55634
MA = 112
50769
Ha = 225
488 n
mi
Hp = 224
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17037042
13 X = -5197575
36
Y = -4449230
46 feet Y = -1414222
07 meter
Z = 13667748
27 Z = 4140693
63
XDOT = -4376
623683 XDOT = -1242
560736
YDOT = -21407
977978 feet/sec YDOT = -6539
558236 meter/sec
ZDOT = -12407
012392 ZDOT = -3787
915040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2040103
08 X = -621823
42
Y = 17578918
33 feet Y = 5358054
31 meter
Z = 13552985
24 Z = 4130949
90
XDOT = -19328
809788 XDOT = -5891
421223
YDOT = 7357
373317 feet/sec YDOT = 2242
527387 meter/sec
ZDOT = -12434
869384 ZDOT = -3790
148188
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 19230
40910085
00016717 00000-0 10270-3 0 9122
2 25544 51
6431 52
5814 0009053 282
5477 77
4661 15
50421172 24903
Satellite: ISS
Catalog Number: 25544
Epoch time: 19230
40910085 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 52
5814 deg
Eccentricity:
0009053
Arg of perigee: 282
5477 deg
Mean anomaly: 77
4661 deg
Mean motion: 15
50421172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2490
Checksum: 289
Coasting Arc #14 (Orbit 2504)
---------------------------------------
Vector Time (GMT): 2019/231/08:49:34
669
Vector Time (MET): N/A
Weight (LBS) : 937180
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5415543
67 A = 6794064
11 meter
Y = 1392928
22 meter E =
0002991
Z = -3855666
12 I = 51
92675
XDOT = 1361
773339 Wp = 287
68358
YDOT = 6276
011606 meter/sec RA = 47
11704 deg
ZDOT = 4178
243576 TA = 26
17199
MA = 26
15688
Ha = 225
801 n
mi
Hp = 223
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17767531
72 X = 5418293
51
Y = 4569974
48 feet Y = 1453503
87 meter
Z = -12649823
24 Z = -3829353
14
XDOT = 4467
760297 XDOT = 1271
196622
YDOT = 20590
589259 feet/sec YDOT = 6290
733626 meter/sec
ZDOT = 13708
148216 ZDOT = 4184
638250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1744515
00 X = 531728
17
Y = -18345009
80 feet Y = -5591558
99 meter
Z = -12530170
04 Z = -3819195
83
XDOT = 18325
704820 XDOT = 5585
674829
YDOT = -7643
871593 feet/sec YDOT = -2329
852062 meter/sec
ZDOT = 13736
643425 ZDOT = 4186
928916
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 19231
37596645
00016717 00000-0 10270-3 0 9132
2 25544 51
6426 47
7884 0009106 285
2936 74
7208 15
50388530 25053
Satellite: ISS
Catalog Number: 25544
Epoch time: 19231
37596645 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 47
7884 deg
Eccentricity:
0009106
Arg of perigee: 285
2936 deg
Mean anomaly: 74
7208 deg
Mean motion: 15
50388530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2505
Checksum: 329
Coasting Arc #15 (Orbit 2520)
---------------------------------------
Vector Time (GMT): 2019/232/08:49:34
669
Vector Time (MET): N/A
Weight (LBS) : 937180
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5645884
07 A = 6795024
55 meter
Y = -1400044
80 meter E =
0004908
Z = 3512568
81 I = 51
90789
XDOT = -1338
603055 Wp = 46
49559
YDOT = -6018
724232 meter/sec RA = 42
17906 deg
ZDOT = -4543
273264 TA = 92
44745
MA = 92
39126
Ha = 225
910 n
mi
Hp = 223
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18523241
69 X = -5646870
72
Y = -4593322
83 feet Y = -1463186
44 meter
Z = 11524175
89 Z = 3485141
11
XDOT = -4391
742307 XDOT = -1249
131946
YDOT = -19746
470577 feet/sec YDOT = -6033
193338 meter/sec
ZDOT = -14905
752177 ZDOT = -4549
558110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1323020
57 X = -403256
67
Y = 19113285
26 feet Y = 5825729
35 meter
Z = 11399459
21 Z = 3474555
17
XDOT = -17320
493555 XDOT = -5279
286436
YDOT = 7722
176107 feet/sec YDOT = 2353
719277 meter/sec
ZDOT = -14933
762406 ZDOT = -4551
810781
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 19232
40728552
00016717 00000-0 10270-3 0 9142
2 25544 51
6437 42
6762 0009241 290
0153 70
0003 15
50425038 25214
Satellite: ISS
Catalog Number: 25544
Epoch time: 19232
40728552 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 42
6762 deg
Eccentricity:
0009241
Arg of perigee: 290
0153 deg
Mean anomaly: 70
0003 deg
Mean motion: 15
50425038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2521
Checksum: 270
Coasting Arc #16 (Orbit 2535)
---------------------------------------
Vector Time (GMT): 2019/233/08:49:34
669
Vector Time (MET): N/A
Weight (LBS) : 937180
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5864815
77 A = 6796141
02 meter
Y = 1359712
24 meter E =
0006306
Z = -3143982
37 I = 51
88464
XDOT = 1275
308170 Wp = 319
12965
YDOT = 5773
450676 meter/sec RA = 37
23909 deg
ZDOT = 4875
001086 TA = 4
82963
MA = 4
82355
Ha = 226
236 n
mi
Hp = 223
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19241521
55 X = 5864446
83
Y = 4460998
17 feet Y = 1425294
59 meter
Z = -10314902
80 Z = -3115494
38
XDOT = 4184
081923 XDOT = 1186
973069
YDOT = 18941
767311 feet/sec YDOT = 5787
218300 meter/sec
ZDOT = 15994
098051 ZDOT = 4880
981306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 729961
49 X = 222492
26
Y = -19805538
11 feet Y = -6036728
02 meter
Z = -10185366
58 Z = -3104499
73
XDOT = 16386
576983 XDOT = 4994
628664
YDOT = -7636
511530 feet/sec YDOT = -2327
608714 meter/sec
ZDOT = 16020
735624 ZDOT = 4883
120218
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 19233
37414638
00016717 00000-0 10270-3 0 9157
2 25544 51
6425 37
8826 0009185 293
1102 66
9080 15
50392240 25366
Satellite: ISS
Catalog Number: 25544
Epoch time: 19233
37414638 = yrday
fracday
Element set: 915
Inclination: 51
6425 deg
RA of node: 37
8826 deg
Eccentricity:
0009185
Arg of perigee: 293
1102 deg
Mean anomaly: 66
9080 deg
Mean motion: 15
50392240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2536
Checksum: 307
Coasting Arc #17 (Orbit 2547)
---------------------------------------
Vector Time (GMT): 2019/234/03:28:32
000
Vector Time (MET): N/A
Weight (LBS) : 937180
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6087954
30 A = 6799368
91 meter
Y = 2618487
07 meter E =
0011116
Z = -1486281
88 I = 51
87353
XDOT = -723
151174 Wp = 344
51430
YDOT = 4968
526622 meter/sec RA = 33
41089 deg
ZDOT = 5791
757056 TA = 359
33378
MA = 359
33526
Ha = 226
368 n
mi
Hp = 223
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19973603
35 X = 6065440
66
Y = 8590836
84 feet Y = 2686440
95 meter
Z = -4876252
89 Z = -1456763
71
XDOT = -2372
543221 XDOT = -806
789971
YDOT = 16300
940360 feet/sec YDOT = 4959
972291 meter/sec
ZDOT = 19001
827611 ZDOT = 5788
041035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21761183
50 X = 6632808
73
Y = 698510
57 feet Y = 212906
02 meter
Z = -4742164
73 Z = -1445411
81
XDOT = 3671
168265 XDOT = 1118
972087
YDOT = 14503
684968 feet/sec YDOT = 4420
723178 meter/sec
ZDOT = 18984
405620 ZDOT = 5786
446833
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 19234
14763550
00016717 00000-0 10270-3 0 9164
2 25544 51
6418 34
0493 0009013 296
7555 63
2673 15
50379003 25481
Satellite: ISS
Catalog Number: 25544
Epoch time: 19234
14763550 = yrday
fracday
Element set: 916
Inclination: 51
6418 deg
RA of node: 34
0493 deg
Eccentricity:
0009013
Arg of perigee: 296
7555 deg
Mean anomaly: 63
2673 deg
Mean motion: 15
50379003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2548
Checksum: 309
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