[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 19th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13923 1181 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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
266/16:30:44
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
2
268/13:57:43
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
3
268/17:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
271/11:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
272/00:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
4
275/04:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 218
3
276/07:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
4
Coasting Arc #1 (Orbit 2972)
---------------------------------------
Vector Time (GMT): 2019/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4261267
54 A = 6792788
59 meter
Y = 2935655
77 meter E =
0016531
Z = 4391575
72 I = 51
25344
XDOT = -1230
665702 Wp = 65
30630
YDOT = 6794
796902 meter/sec RA = 257
48960 deg
ZDOT = -3331
288431 TA = 58
63072
MA = 58
46908
Ha = 229
759 n
mi
Hp = 218
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13980536
54 X = 4206791
41
Y = 9631416
57 feet Y = 2983004
03 meter
Z = 14408056
84 Z = 4412143
03
XDOT = -4037
617131 XDOT = -1290
373895
YDOT = 22292
640753 feet/sec YDOT = 6780
700609 meter/sec
ZDOT = -10929
423986 ZDOT = -3337
412183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13219436
32 X = -4029284
19
Y = -10524646
73 feet Y = -3207912
32 meter
Z = 14501379
37 Z = 4420020
43
XDOT = 4654
166424 XDOT = 1418
589926
YDOT = -21018
987563 feet/sec YDOT = -6406
587409 meter/sec
ZDOT = -10957
720938 ZDOT = -3339
913342
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 19261
54235144
00016717 00000-0 10270-3 0 9004
2 25544 51
6389 258
2602 0007298 59
2031 300
9837 15
50107278 29732
Satellite: ISS
Catalog Number: 25544
Epoch time: 19261
54235144 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 258
2602 deg
Eccentricity:
0007298
Arg of perigee: 59
2031 deg
Mean anomaly: 300
9837 deg
Mean motion: 15
50107278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2973
Checksum: 310
Coasting Arc #2 (Orbit 2987)
---------------------------------------
Vector Time (GMT): 2019/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4460907
82 A = 6793635
79 meter
Y = -2957963
73 meter E =
0014159
Z = -4195680
37 I = 51
26506
XDOT = 980
216443 Wp = 87
32298
YDOT = -6649
235387 meter/sec RA = 252
50840 deg
ZDOT = 3656
941313 TA = 220
40918
MA = 220
51445
Ha = 229
975 n
mi
Hp = 218
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14635524
36 X = -4407118
94
Y = -9704605
42 feet Y = -3007548
26 meter
Z = -13765355
54 Z = -4217219
21
XDOT = 3215
933211 XDOT = 1036
733662
YDOT = -21815
076728 feet/sec YDOT = -6637
957677 meter/sec
ZDOT = 11997
838953 ZDOT = 3661
840584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14053485
96 X = 4283502
52
Y = 10400809
55 feet Y = 3170166
75 meter
Z = -13863103
77 Z = -4225474
03
XDOT = -3433
154577 XDOT = -1046
425515
YDOT = 20611
397809 feet/sec YDOT = 6282
354052 meter/sec
ZDOT = 12020
548362 ZDOT = 3663
863141
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 19262
50939772
00016717 00000-0 10270-3 0 9010
2 25544 51
6397 253
4693 0007463 62
8474 297
3437 15
50069382 29887
Satellite: ISS
Catalog Number: 25544
Epoch time: 19262
50939772 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 253
4693 deg
Eccentricity:
0007463
Arg of perigee: 62
8474 deg
Mean anomaly: 297
3437 deg
Mean motion: 15
50069382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2988
Checksum: 351
Coasting Arc #3 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2019/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4650884
30 A = 6794411
14 meter
Y = 2999382
78 meter E =
0018241
Z = 3930324
58 I = 51
27846
XDOT = -787
166141 Wp = 74
13538
YDOT = 6491
754044 meter/sec RA = 247
52729 deg
ZDOT = -4002
177409 TA = 57
94926
MA = 57
77223
Ha = 229
851 n
mi
Hp = 218
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15258806
76 X = 4597907
12
Y = 9840494
67 feet Y = 3051096
21 meter
Z = 12894765
67 Z = 3952788
27
XDOT = -2582
566078 XDOT = -840
259735
YDOT = 21298
405657 feet/sec YDOT = 6482
654353 meter/sec
ZDOT = -13130
503309 ZDOT = -4006
130456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14854869
14 X = -4527764
11
Y = -10313069
75 feet Y = -3143423
66 meter
Z = 12996728
66 Z = 3961402
90
XDOT = 2409
853051 XDOT = 734
523210
YDOT = -20125
513015 feet/sec YDOT = -6134
256367 meter/sec
ZDOT = -13148
890368 ZDOT = -4007
781784
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 19263
54091038
00016717 00000-0 10270-3 0 9020
2 25544 51
6390 248
3578 0007393 65
4334 294
7586 15
50109136 30049
Satellite: ISS
Catalog Number: 25544
Epoch time: 19263
54091038 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 248
3578 deg
Eccentricity:
0007393
Arg of perigee: 65
4334 deg
Mean anomaly: 294
7586 deg
Mean motion: 15
50109136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 313
Coasting Arc #4 (Orbit 3018)
---------------------------------------
Vector Time (GMT): 2019/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4877811
73 A = 6795285
90 meter
Y = -2965937
42 meter E =
0012723
Z = -3695601
43 I = 51
29445
XDOT = 596
564560 Wp = 83
31986
YDOT = -6309
146469 meter/sec RA = 242
54892 deg
ZDOT = 4290
291626 TA = 232
54347
MA = 232
65927
Ha = 230
019 n
mi
Hp = 218
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16003319
32 X = -4826331
89
Y = -9730765
83 feet Y = -3020196
82 meter
Z = -12124676
62 Z = -3719171
09
XDOT = 1957
232809 XDOT = 646
230886
YDOT = -20699
299438 feet/sec YDOT = -6302
197431 meter/sec
ZDOT = 14075
759929 ZDOT = 4293
310361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15781237
53 X = 4810121
20
Y = 9956918
29 feet Y = 3034868
70 meter
Z = -12231685
73 Z = -3728217
81
XDOT = -1430
386799 XDOT = -435
981896
YDOT = 19519
091449 feet/sec YDOT = 5949
419074 meter/sec
ZDOT = 14089
877044 ZDOT = 4294
594523
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 19264
50795444
00016717 00000-0 10270-3 0 9030
2 25544 51
6386 243
5672 0007482 69
1410 291
0541 15
50072768 30198
Satellite: ISS
Catalog Number: 25544
Epoch time: 19264
50795444 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 243
5672 deg
Eccentricity:
0007482
Arg of perigee: 69
1410 deg
Mean anomaly: 291
0541 deg
Mean motion: 15
50072768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3019
Checksum: 312
Coasting Arc #5 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2019/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5089311
25 A = 6796102
99 meter
Y = 2949531
06 meter E =
0019520
Z = 3389241
23 I = 51
31381
XDOT = -470
489256 Wp = 83
55905
YDOT = 6119
624850 meter/sec RA = 237
57083 deg
ZDOT = -4594
170958 TA = 56
68080
MA = 56
49404
Ha = 229
902 n
mi
Hp = 218
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16697215
37 X = 5039487
35
Y = 9676939
19 feet Y = 3006164
83 meter
Z = 11119557
84 Z = 3413842
24
XDOT = -1543
599922 XDOT = -516
569654
YDOT = 20077
509349 feet/sec YDOT = 6114
105749 meter/sec
ZDOT = -15072
739365 ZDOT = -4596
568493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16650662
40 X = -5075121
90
Y = -9628011
43 feet Y = -2934617
88 meter
Z = 11231275
86 Z = 3423292
88
XDOT = 680
009719 XDOT = 207
266962
YDOT = -18866
627043 feet/sec YDOT = -5750
547923 meter/sec
ZDOT = -15084
009257 ZDOT = -4597
606021
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 19265
53946606
00016717 00000-0 10270-3 0 9043
2 25544 51
6385 238
4557 0007364 72
3823 287
8132 15
50105733 30351
Satellite: ISS
Catalog Number: 25544
Epoch time: 19265
53946606 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 238
4557 deg
Eccentricity:
0007364
Arg of perigee: 72
3823 deg
Mean anomaly: 287
8132 deg
Mean motion: 15
50105733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 318
Coasting Arc #6 (Orbit 3049)
---------------------------------------
Vector Time (GMT): 2019/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5325275
27 A = 6796914
33 meter
Y = -2854558
29 meter E =
0011985
Z = -3119804
81 I = 51
33589
XDOT = 348
457528 Wp = 76
47283
YDOT = -5919
698438 meter/sec RA = 232
59522 deg
ZDOT = 4840
100307 TA = 247
54186
MA = 247
66882
Ha = 230
026 n
mi
Hp = 218
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17471375
56 X = -5277804
69
Y = -9365348
73 feet Y = -2913843
93 meter
Z = -10235580
10 Z = -3145557
67
XDOT = 1143
233361 XDOT = 391
116857
YDOT = -19421
582802 feet/sec YDOT = -5915
563094 meter/sec
ZDOT = 15879
594183 ZDOT = 4841
896747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17587462
32 X = 5360658
52
Y = 9012848
55 feet Y = 2747116
24 meter
Z = -10352562
53 Z = -3155461
06
XDOT = 13
233498 XDOT = 4
033570
YDOT = 18155
087130 feet/sec YDOT = 5533
670557 meter/sec
ZDOT = 15888
106515 ZDOT = 4842
694866
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 19266
50650626
00016717 00000-0 10270-3 0 9056
2 25544 51
6392 233
6646 0007455 75
6390 284
5588 15
50082442 30508
Satellite: ISS
Catalog Number: 25544
Epoch time: 19266
50650626 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 233
6646 deg
Eccentricity:
0007455
Arg of perigee: 75
6390 deg
Mean anomaly: 284
5588 deg
Mean motion: 15
50082442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3050
Checksum: 318
Coasting Arc #7 (Orbit 3052)
---------------------------------------
Vector Time (GMT): 2019/266/16:30:44
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4759943
39 A = 6791016
87 meter
Y = 244866
04 meter E =
0018469
Z = -4854143
45 I = 51
32358
XDOT = -2811
302714 Wp = 95
61066
YDOT = -6685
984129 meter/sec RA = 231
66613 deg
ZDOT = 2425
708887 TA = 198
32711
MA = 198
39375
Ha = 229
971 n
mi
Hp = 218
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15616612
17 X = -4738749
03
Y = 803366
28 feet Y = 191755
38 meter
Z = -15925667
48 Z = -4877214
01
XDOT = -9223
434101 XDOT = -2748
111920
YDOT = -21935
643467 feet/sec YDOT = -6717
068710 meter/sec
ZDOT = 7958
362490 ZDOT = 2412
206281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4802318
42 X = 1463746
65
Y = -14768463
91 feet Y = -4501427
80 meter
Z = -16030629
10 Z = -4886135
75
XDOT = 22725
493163 XDOT = 6926
730316
YDOT = -1160
457498 feet/sec YDOT = -353
707445 meter/sec
ZDOT = 7897
321192 ZDOT = 2407
103499
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 19266
69991418
00016717 00000-0 10270-3 0 9064
2 25544 51
6426 232
7072 0007319 75
6954 284
5009 15
50104186 30535
Satellite: ISS
Catalog Number: 25544
Epoch time: 19266
69991418 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 232
7072 deg
Eccentricity:
0007319
Arg of perigee: 75
6954 deg
Mean anomaly: 284
5009 deg
Mean motion: 15
50104186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3053
Checksum: 323
Coasting Arc #8 (Orbit 3068)
---------------------------------------
Vector Time (GMT): 2019/267/16:30:44
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4917824
99 A = 6791598
15 meter
Y = -226622
00 meter E =
0015148
Z = 4668445
40 I = 51
34690
XDOT = 2992
971330 Wp = 71
05168
YDOT = 6470
320124 meter/sec RA = 226
68891 deg
ZDOT = -2826
390236 TA = 47
17191
MA = 47
04470
Ha = 229
814 n
mi
Hp = 218
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16134596
44 X = 4897316
98
Y = -743510
49 feet Y = -171741
88 meter
Z = 15316421
90 Z = 4692284
49
XDOT = 9819
459745 XDOT = 2934
124897
YDOT = 21228
084397 feet/sec YDOT = 6503
460491 meter/sec
ZDOT = -9272
933845 ZDOT = -2811
994735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4782252
08 X = -1457630
43
Y = 15319059
84 feet Y = 4669249
44 meter
Z = 15424890
94 Z = 4701506
76
XDOT = -22209
652191 XDOT = -6769
501988
YDOT = 2378
646552 feet/sec YDOT = 725
011469 meter/sec
ZDOT = -9207
795050 ZDOT = -2806
535931
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 19267
73142069
00016717 00000-0 10270-3 0 9071
2 25544 51
6420 227
5964 0007345 78
7279 281
4696 15
50140119 30695
Satellite: ISS
Catalog Number: 25544
Epoch time: 19267
73142069 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 227
5964 deg
Eccentricity:
0007345
Arg of perigee: 78
7279 deg
Mean anomaly: 281
4696 deg
Mean motion: 15
50140119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3069
Checksum: 330
Coasting Arc #9 (Orbit 3082)
---------------------------------------
Vector Time (GMT): 2019/268/13:57:43
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 838645
91 A = 6790613
18 meter
Y = -4573506
07 meter E =
0012873
Z = 4938887
03 I = 51
36287
XDOT = 6455
391907 Wp = 101
78712
YDOT = 3530
372066 meter/sec RA = 222
28184 deg
ZDOT = 2165
656934 TA = 326
98129
MA = 327
06161
Ha = 229
898 n
mi
Hp = 218
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2751462
96 X = 865735
57
Y = -15004941
17 feet Y = -4563975
96 meter
Z = 16203697
61 Z = 4943026
92
XDOT = 21179
107308 XDOT = 6404
914971
YDOT = 11582
585517 feet/sec YDOT = 3602
278711 meter/sec
ZDOT = 7105
173669 ZDOT = 2196
891865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5866991
49 X = 1788259
01
Y = 14059823
53 feet Y = 4285434
21 meter
Z = 16222774
03 Z = 4944701
52
XDOT = -23015
895198 XDOT = -7015
244856
YDOT = 1214
345274 feet/sec YDOT = 370
132439 meter/sec
ZDOT = 7247
107148 ZDOT = 2208
918259
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 19268
63398912
00016717 00000-0 10270-3 0 9082
2 25544 51
6404 223
1238 0007241 83
2900 276
9075 15
50135411 30835
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
63398912 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 223
1238 deg
Eccentricity:
0007241
Arg of perigee: 83
2900 deg
Mean anomaly: 276
9075 deg
Mean motion: 15
50135411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3083
Checksum: 301
Coasting Arc #10 (Orbit 3084)
---------------------------------------
Vector Time (GMT): 2019/268/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1025748
90 A = 6790396
77 meter
Y = -4450957
23 meter E =
0012392
Z = 5014739
63 I = 51
36658
XDOT = 6451
789118 Wp = 101
41214
YDOT = 3670
216138 meter/sec RA = 221
63751 deg
ZDOT = 1931
428815 TA = 329
74583
MA = 329
81732
Ha = 229
996 n
mi
Hp = 218
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3365317
92 X = 1051085
83
Y = -14602878
06 feet Y = -4439344
59 meter
Z = 16452557
85 Z = 5019784
14
XDOT = 21167
287134 XDOT = 6400
886419
YDOT = 12041
391528 feet/sec YDOT = 3742
080105 meter/sec
ZDOT = 6336
708712 ZDOT = 1962
645188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13747474
88 X = 4190230
34
Y = 5900246
44 feet Y = 1798395
12 meter
Z = 16475742
73 Z = 5021806
38
XDOT = -15312
631703 XDOT = -4667
290143
YDOT = 17528
383459 feet/sec YDOT = 5342
651278 meter/sec
ZDOT = 6478
553621 ZDOT = 1974
663144
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 19268
76292815
00016717 00000-0 10270-3 0 9092
2 25544 51
6420 222
4855 0007361 83
4280 276
7709 15
50097844 30857
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
76292815 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 222
4855 deg
Eccentricity:
0007361
Arg of perigee: 83
4280 deg
Mean anomaly: 276
7709 deg
Mean motion: 15
50097844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3085
Checksum: 333
Coasting Arc #11 (Orbit 3099)
---------------------------------------
Vector Time (GMT): 2019/269/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 932083
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1072576
85 A = 6789843
18 meter
Y = 4322280
88 meter E =
0020726
Z = -5143900
99 I = 51
39108
XDOT = -6654
826894 Wp = 81
24915
YDOT = -3448
310875 meter/sec RA = 216
66221 deg
ZDOT = -1512
053536 TA = 174
10395
MA = 174
07951
Ha = 229
933 n
mi
Hp = 218
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3518952
91 X = -1095843
99
Y = 14180711
54 feet Y = 4310156
00 meter
Z = -16876315
59 Z = -5149168
06
XDOT = -21833
421567 XDOT = -6608
427589
YDOT = -11313
355888 feet/sec YDOT = -3522
470547 meter/sec
ZDOT = -4960
805564 ZDOT = -1544
267078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13405406
80 X = -4085967
99
Y = -5740545
42 feet Y = -1749718
25 meter
Z = -16900498
33 Z = -5151271
89
XDOT = 14398
986358 XDOT = 4388
811042
YDOT = -18609
578209 feet/sec YDOT = -5672
199438 meter/sec
ZDOT = -5107
222598 ZDOT = -1556
681448
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 19269
72996312
00016717 00000-0 10270-3 0 9104
2 25544 51
6424 217
6936 0007188 85
9506 274
2466 15
50126090 31009
Satellite: ISS
Catalog Number: 25544
Epoch time: 19269
72996312 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 217
6936 deg
Eccentricity:
0007188
Arg of perigee: 85
9506 deg
Mean anomaly: 274
2466 deg
Mean motion: 15
50126090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3100
Checksum: 317
Coasting Arc #12 (Orbit 3115)
---------------------------------------
Vector Time (GMT): 2019/270/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 932083
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1121660
02 A = 6789514
51 meter
Y = -4193704
91 meter E =
0010719
Z = 5211605
76 I = 51
41797
XDOT = 6876
751616 Wp = 101
71409
YDOT = 3212
849326 meter/sec RA = 211
68882 deg
ZDOT = 1101
235751 TA = 337
67869
MA = 337
72531
Ha = 229
950 n
mi
Hp = 218
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3679986
94 X = 1143156
77
Y = -13758874
37 feet Y = -4181040
93 meter
Z = 17098444
11 Z = 5217107
05
XDOT = 22561
521051 XDOT = 6834
964315
YDOT = 10540
844247 feet/sec YDOT = 3289
516492 meter/sec
ZDOT = 3612
978186 ZDOT = 1134
538595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13061055
97 X = 3981009
86
Y = 5603046
04 feet Y = 1707808
43 meter
Z = 17123679
82 Z = 5219297
61
XDOT = -13417
595652 XDOT = -4089
683155
YDOT = 19732
144382 feet/sec YDOT = 6014
357608 meter/sec
ZDOT = 3764
384260 ZDOT = 1147
384323
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 19270
76146579
00016717 00000-0 10270-3 0 9113
2 25544 51
6430 212
5823 0007252 89
6706 270
5275 15
50106096 31168
Satellite: ISS
Catalog Number: 25544
Epoch time: 19270
76146579 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 212
5823 deg
Eccentricity:
0007252
Arg of perigee: 89
6706 deg
Mean anomaly: 270
5275 deg
Mean motion: 15
50106096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3116
Checksum: 305
Coasting Arc #13 (Orbit 3126)
---------------------------------------
Vector Time (GMT): 2019/271/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6259895
64 A = 6800630
03 meter
Y = -2482811
87 meter E =
0015407
Z = -923942
12 I = 51
47434
XDOT = 1033
136215 Wp = 61
98337
YDOT = -4770
715278 meter/sec RA = 207
90552 deg
ZDOT = 5902
655129 TA = 288
01096
MA = 288
17880
Ha = 229
996 n
mi
Hp = 218
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20537715
37 X = -6227178
85
Y = -8145708
23 feet Y = -2552631
62 meter
Z = -3031306
18 Z = -954270
73
XDOT = 3389
554512 XDOT = 1057
734989
YDOT = -15651
953013 feet/sec YDOT = -4759
023769 meter/sec
ZDOT = 19365
666433 ZDOT = 5907
734061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19694733
99 X = 6002954
92
Y = 9970587
17 feet Y = 3039034
97 meter
Z = -3169223
37 Z = -965979
28
XDOT = -3935
917030 XDOT = -1199
667511
YDOT = 13855
171247 feet/sec YDOT = 4223
056196 meter/sec
ZDOT = 19389
003037 ZDOT = 5909
768126
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 19271
47062368
00016717 00000-0 10270-3 0 9126
2 25544 51
6403 209
0677 0007388 92
3780 267
8216 15
50112175 31270
Satellite: ISS
Catalog Number: 25544
Epoch time: 19271
47062368 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 209
0677 deg
Eccentricity:
0007388
Arg of perigee: 92
3780 deg
Mean anomaly: 267
8216 deg
Mean motion: 15
50112175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3127
Checksum: 310
Coasting Arc #14 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2019/272/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 269411
02 A = 6790394
41 meter
Y = 4561545
22 meter E =
0019693
Z = -5040472
66 I = 51
45931
XDOT = -7206
137393 Wp = 84
17953
YDOT = -1691
192495 meter/sec RA = 205
13386 deg
ZDOT = -1920
205961 TA = 167
11976
MA = 167
06938
Ha = 229
984 n
mi
Hp = 218
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 883894
41 X = 242866
49
Y = 14965699
55 feet Y = 4564408
94 meter
Z = -16536983
78 Z = -5039228
97
XDOT = -23642
183049 XDOT = -7177
363042
YDOT = -5548
531808 feet/sec YDOT = -1771
615954 meter/sec
ZDOT = -6299
888324 ZDOT = -1955
140863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5536505
52 X = 1687526
88
Y = 13938465
67 feet Y = 4248444
34 meter
Z = -16531531
88 Z = -5038810
92
XDOT = -23147
361463 XDOT = -7055
315774
YDOT = 1551
654455 feet/sec YDOT = 472
944278 meter/sec
ZDOT = -6458
815229 ZDOT = -1968
646882
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 19272
05084261
00016717 00000-0 10270-3 0 9138
2 25544 51
6430 206
1904 0007246 98
7334 261
4638 15
50100899 31367
Satellite: ISS
Catalog Number: 25544
Epoch time: 19272
05084261 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 206
1904 deg
Eccentricity:
0007246
Arg of perigee: 98
7334 deg
Mean anomaly: 261
4638 deg
Mean motion: 15
50100899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 299
Coasting Arc #15 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2019/273/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -209176
89 A = 6789779
60 meter
Y = -4428781
54 meter E =
0011888
Z = 5133733
61 I = 51
48893
XDOT = 7381
372469 Wp = 111
86242
YDOT = 1422
020527 meter/sec RA = 200
16597 deg
ZDOT = 1520
338193 TA = 323
42168
MA = 323
50280
Ha = 229
914 n
mi
Hp = 218
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -686275
89 X = -184574
59
Y = -14530123
15 feet Y = -4430982
57 meter
Z = 16842958
04 Z = 5132777
74
XDOT = 24217
101276 XDOT = 7357
537364
YDOT = 4665
421675 feet/sec YDOT = 1504
431140 meter/sec
ZDOT = 4987
986199 ZDOT = 1556
136566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5449684
47 X = -1661063
83
Y = -13492079
83 feet Y = -4112385
93 meter
Z = 16838806
66 Z = 5132468
27
XDOT = 23409
906054 XDOT = 7135
339365
YDOT = -2997
740440 feet/sec YDOT = -913
711286 meter/sec
ZDOT = 5150
871318 ZDOT = 1569
985578
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 19273
08234100
00016717 00000-0 10270-3 0 9142
2 25544 51
6434 201
0797 0007252 102
4961 257
7002 15
50146575 31523
Satellite: ISS
Catalog Number: 25544
Epoch time: 19273
08234100 = yrday
fracday
Element set: 914
Inclination: 51
6434 deg
RA of node: 201
0797 deg
Eccentricity:
0007252
Arg of perigee: 102
4961 deg
Mean anomaly: 257
7002 deg
Mean motion: 15
50146575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 279
Coasting Arc #16 (Orbit 3166)
---------------------------------------
Vector Time (GMT): 2019/274/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 100734
88 A = 6789525
15 meter
Y = 4341384
74 meter E =
0020919
Z = -5237355
48 I = 51
51935
XDOT = -7482
677395 Wp = 89
72469
YDOT = -1135
872011 meter/sec RA = 195
20011 deg
ZDOT = -1089
158800 TA = 169
81263
MA = 169
77016
Ha = 229
922 n
mi
Hp = 218
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 330495
02 X = 77621
37
Y = 14243388
24 feet Y = 4342381
52 meter
Z = -17182924
79 Z = -5236922
66
XDOT = -24549
466520 XDOT = -7464
128997
YDOT = -3726
614210 feet/sec YDOT = -1219
444976 meter/sec
ZDOT = -3573
355644 ZDOT = -1125
462299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5251165
53 X = 1600555
25
Y = 13246493
82 feet Y = 4037531
32 meter
Z = -17181149
61 Z = -5236814
40
XDOT = -23368
937414 XDOT = -7122
852124
YDOT = 4430
517935 feet/sec YDOT = 1350
421867 meter/sec
ZDOT = -3738
570666 ZDOT = -1139
516339
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 19274
04936976
00016717 00000-0 10270-3 0 9150
2 25544 51
6434 196
2888 0007167 105
2740 254
9203 15
50107020 31670
Satellite: ISS
Catalog Number: 25544
Epoch time: 19274
04936976 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 196
2888 deg
Eccentricity:
0007167
Arg of perigee: 105
2740 deg
Mean anomaly: 254
9203 deg
Mean motion: 15
50107020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3167
Checksum: 314
Coasting Arc #17 (Orbit 3182)
---------------------------------------
Vector Time (GMT): 2019/275/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1790
54 A = 6789109
44 meter
Y = -4259405
40 meter E =
0010279
Z = 5278797
86 I = 51
55091
XDOT = 7594
692351 Wp = 111
43479
YDOT = 831
721864 meter/sec RA = 190
23618 deg
ZDOT = 668
954413 TA = 332
14312
MA = 332
19813
Ha = 229
860 n
mi
Hp = 218
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5874
46 X = 20197
58
Y = -13974427
18 feet Y = -4259302
14 meter
Z = 17318890
61 Z = 5278842
84
XDOT = 24916
969657 XDOT = 7581
577875
YDOT = 2728
746272 feet/sec YDOT = 916
577788 meter/sec
ZDOT = 2194
732325 ZDOT = 705
815321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5080099
28 X = -1548414
26
Y = -13017814
03 feet Y = -3967829
72 meter
Z = 17319287
81 Z = 5278918
93
XDOT = 23296
790335 XDOT = 7100
861694
YDOT = -5927
580802 feet/sec YDOT = -1806
726628 meter/sec
ZDOT = 2362
519336 ZDOT = 720
095894
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 19275
08086281
00016717 00000-0 10270-3 0 9161
2 25544 51
6433 191
1781 0007215 108
4404 251
7531 15
50154314 31836
Satellite: ISS
Catalog Number: 25544
Epoch time: 19275
08086281 = yrday
fracday
Element set: 916
Inclination: 51
6433 deg
RA of node: 191
1781 deg
Eccentricity:
0007215
Arg of perigee: 108
4404 deg
Mean anomaly: 251
7531 deg
Mean motion: 15
50154314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3183
Checksum: 291
Coasting Arc #18 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2019/275/04:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3939885
49 A = 6791846
06 meter
Y = -3045322
04 meter E =
0014648
Z = 4606721
03 I = 51
56285
XDOT = 6167
673436 Wp = 84
82644
YDOT = 3442
445231 meter/sec RA = 189
53866 deg
ZDOT = -2989
727094 TA = 35
06550
MA = 34
96916
Ha = 229
823 n
mi
Hp = 218
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12926133
48 X = 3951269
05
Y = -9991214
04 feet Y = -3001199
52 meter
Z = 15113914
13 Z = 4625887
69
XDOT = 20235
149068 XDOT = 6143
243310
YDOT = 11294
111649 feet/sec YDOT = 3511
279723 meter/sec
ZDOT = -9808
815926 ZDOT = -2959
825877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4920293
57 X = -1499705
48
Y = -15493558
00 feet Y = -4722436
48 meter
Z = 15201317
59 Z = 4633361
60
XDOT = 16505
771509 XDOT = 5030
959156
YDOT = -14762
507822 feet/sec YDOT = -4499
612384 meter/sec
ZDOT = -9672
831281 ZDOT = -2948
278974
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 19275
20980016
00016717 00000-0 10270-3 0 9175
2 25544 51
6416 190
5411 0007350 106
3949 253
8010 15
50146099 31859
Satellite: ISS
Catalog Number: 25544
Epoch time: 19275
20980016 = yrday
fracday
Element set: 917
Inclination: 51
6416 deg
RA of node: 190
5411 deg
Eccentricity:
0007350
Arg of perigee: 106
3949 deg
Mean anomaly: 253
8010 deg
Mean motion: 15
50146099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 298
Coasting Arc #19 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2019/276/04:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4061980
66 A = 6792667
79 meter
Y = 3193988
47 meter E =
0016607
Z = -4425868
46 I = 51
59874
XDOT = -6114
920937 Wp = 110
55911
YDOT = -3148
911686 meter/sec RA = 184
57874 deg
ZDOT = 3344
217025 TA = 193
33425
MA = 193
37819
Ha = 229
958 n
mi
Hp = 218
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13326708
19 X = -4075896
11
Y = 10478964
80 feet Y = 3148486
54 meter
Z = -14520565
82 Z = -4445634
29
XDOT = -20062
076564 XDOT = -6095
499026
YDOT = -10331
075085 feet/sec YDOT = -3217
184306 meter/sec
ZDOT = 10971
840634 ZDOT = 3314
559871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5512580
68 X = 1680234
59
Y = 15949766
69 feet Y = 4861488
89 meter
Z = -14610718
09 Z = -4453346
87
XDOT = -15246
242826 XDOT = -4647
054813
YDOT = 15183
086624 feet/sec YDOT = 4627
804803 meter/sec
ZDOT = 10836
935651 ZDOT = 3303
097987
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 19276
17682550
00016717 00000-0 10270-3 0 9185
2 25544 51
6419 185
7496 0007399 109
5428 250
6522 15
50119952 32000
Satellite: ISS
Catalog Number: 25544
Epoch time: 19276
17682550 = yrday
fracday
Element set: 918
Inclination: 51
6419 deg
RA of node: 185
7496 deg
Eccentricity:
0007399
Arg of perigee: 109
5428 deg
Mean anomaly: 250
6522 deg
Mean motion: 15
50119952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 329
Coasting Arc #20 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2019/276/07:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 950247
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3779806
15 A = 6793236
50 meter
Y = -3661248
05 meter E =
0017153
Z = 4285514
25 I = 51
60260
XDOT = 6361
172438 Wp = 108
76271
YDOT = -2389
163062 meter/sec RA = 183
89067 deg
ZDOT = 3552
330830 TA = 304
91852
MA = 305
07957
Ha = 229
919 n
mi
Hp = 218
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12400938
81 X = -3759401
06
Y = -12011968
66 feet Y = -3703402
24 meter
Z = 14060086
14 Z = 4267202
80
XDOT = 20869
988314 XDOT = 6370
160456
YDOT = -7838
461489 feet/sec YDOT = -2317
977543 meter/sec
ZDOT = 11654
628707 ZDOT = 3583
253426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2871760
93 X = -875312
73
Y = 17092596
81 feet Y = 5209823
51 meter
Z = 13976867
32 Z = 4260149
16
XDOT = -16951
367468 XDOT = -5166
776804
YDOT = -12539
472286 feet/sec YDOT = -3822
031153 meter/sec
ZDOT = 11795
551527 ZDOT = 3595
284105
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 19276
37022920
00016717 00000-0 10270-3 0 9197
2 25544 51
6389 184
7920 0007207 110
9829 249
2093 15
50154660 32031
Satellite: ISS
Catalog Number: 25544
Epoch time: 19276
37022920 = yrday
fracday
Element set: 919
Inclination: 51
6389 deg
RA of node: 184
7920 deg
Eccentricity:
0007207
Arg of perigee: 110
9829 deg
Mean anomaly: 249
2093 deg
Mean motion: 15
50154660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 312
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