[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 15th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14319 0147 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
134/18:07:30
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
136/05:55:00
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
137/07:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 217
1
143/14:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
5
000/00:00:00
000 0
0 0
0 216
7
143/16:02:53
424 -2
1 7
1 7
1
N/A 6
7 -0
7 223
7
000/00:19:46
849 -1
2 -0
1 221
4
143/19:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 221
4
143/21:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
6
000/00:00:00
000 0
0 0
0 221
4
144/08:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
7
000/00:00:00
000 0
0 0
0 221
2
Coasting Arc #1 (Orbit 985)
---------------------------------------
Vector Time (GMT): 2019/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2012994
91 A = 6782275
85 meter
Y = 3878313
31 meter E =
0013645
Z = -5199160
93 I = 51
66795
XDOT = -7268
515399 Wp = 74
59883
YDOT = 2016
030715 meter/sec RA = 172
38847 deg
ZDOT = -1309
675565 TA = 182
80092
MA = 182
80857
Ha = 223
179 n
mi
Hp = 217
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6604314
00 X = 1994731
62
Y = 12724125
03 feet Y = 3900722
08 meter
Z = -17057614
60 Z = -5189426
75
XDOT = -23846
835298 XDOT = -7284
157318
YDOT = 6614
273999 feet/sec YDOT = 1934
661670 meter/sec
ZDOT = -4296
835843 ZDOT = -1345
021347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14068654
21 X = 4288125
80
Y = 3014282
97 feet Y = 918753
45 meter
Z = -17013806
28 Z = -5185808
15
XDOT = -9995
686376 XDOT = -3046
685208
YDOT = 21483
231680 feet/sec YDOT = 6548
089016 meter/sec
ZDOT = -4457
082998 ZDOT = -1358
518898
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
51845042
00016717 00000-0 10270-3 0 9003
2 25544 51
6399 173
4760 0001351 336
0126 24
0963 15
52650651 9867
Satellite: ISS
Catalog Number: 25544
Epoch time: 19133
51845042 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 173
4760 deg
Eccentricity:
0001351
Arg of perigee: 336
0126 deg
Mean anomaly: 24
0963 deg
Mean motion: 15
52650651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 986
Checksum: 294
Coasting Arc #2 (Orbit 1001)
---------------------------------------
Vector Time (GMT): 2019/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -833886
40 A = 6781581
91 meter
Y = -4119308
25 meter E =
0002533
Z = 5320415
67 I = 51
69862
XDOT = 7495
897612 Wp = 55
19832
YDOT = -1614
696706 meter/sec RA = 167
40764 deg
ZDOT = -73
877381 TA = 35
51353
MA = 35
49667
Ha = 223
255 n
mi
Hp = 217
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2735847
77 X = -813604
96
Y = -13514790
86 feet Y = -4128520
08 meter
Z = 17455431
99 Z = 5316414
10
XDOT = 24592
839936 XDOT = 7513
755359
YDOT = -5297
561373 feet/sec YDOT = -1530
772479 meter/sec
ZDOT = -242
379860 ZDOT = -37
421510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12303494
60 X = -3750105
15
Y = -6275386
57 feet Y = -1912737
83 meter
Z = 17437605
49 Z = 5314982
15
XDOT = 10881
061997 XDOT = 3316
547697
YDOT = -21560
759866 feet/sec YDOT = -6571
719607 meter/sec
ZDOT = -77
114530 ZDOT = -23
504509
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
54825311
00016717 00000-0 10270-3 0 9015
2 25544 51
6396 168
3538 0001456 346
6126 13
4987 15
52674915 10020
Satellite: ISS
Catalog Number: 25544
Epoch time: 19134
54825311 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 168
3538 deg
Eccentricity:
0001456
Arg of perigee: 346
6126 deg
Mean anomaly: 13
4987 deg
Mean motion: 15
52674915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1002
Checksum: 309
Coasting Arc #3 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2019/134/18:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2337251
20 A = 6782050
52 meter
Y = -3658732
29 meter E =
0002949
Z = 5207983
21 I = 51
70813
XDOT = 7053
077470 Wp = 105
66773
YDOT = -2743
992670 meter/sec RA = 166
15136 deg
ZDOT = 1236
216467 TA = 332
47162
MA = 332
48724
Ha = 223
184 n
mi
Hp = 217
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7668147
00 X = -2321462
22
Y = -12003714
86 feet Y = -3684780
91 meter
Z = 17086559
10 Z = 5196667
89
XDOT = 23140
017946 XDOT = 7077
232474
YDOT = -9002
600624 feet/sec YDOT = -2664
985187 meter/sec
ZDOT = 4055
828303 ZDOT = 1270
536575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -962535
90 X = -293380
94
Y = 14272461
64 feet Y = 4350246
31 meter
Z = 17035566
15 Z = 5192440
56
XDOT = -22856
513812 XDOT = -6966
665410
YDOT = -6573
628150 feet/sec YDOT = -2003
641860 meter/sec
ZDOT = 4211
505609 ZDOT = 1283
666910
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
80570321
00016717 00000-0 10270-3 0 9023
2 25544 51
6391 167
0741 0001729 339
0435 21
0646 15
52701450 10065
Satellite: ISS
Catalog Number: 25544
Epoch time: 19134
80570321 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 167
0741 deg
Eccentricity:
0001729
Arg of perigee: 339
0435 deg
Mean anomaly: 21
0646 deg
Mean motion: 15
52701450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 272
Coasting Arc #4 (Orbit 1020)
---------------------------------------
Vector Time (GMT): 2019/135/18:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1197071
29 A = 6781631
16 meter
Y = 4033888
84 meter E =
0014571
Z = -5330894
47 I = 51
73784
XDOT = -7281
916531 Wp = 84
53650
YDOT = 2357
492257 meter/sec RA = 161
17262 deg
ZDOT = 150
441320 TA = 186
88761
MA = 186
90766
Ha = 223
279 n
mi
Hp = 217
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3927399
23 X = 1177769
08
Y = 13234543
44 feet Y = 4047167
55 meter
Z = -17489811
27 Z = -5325126
25
XDOT = -23890
802266 XDOT = -7308
468243
YDOT = 7734
554650 feet/sec YDOT = 2275
912302 meter/sec
ZDOT = 493
573886 ZDOT = 115
003613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4467906
86 X = 1361818
01
Y = -13096506
16 feet Y = -3991815
08 meter
Z = -17463975
43 Z = -5323019
71
XDOT = 22944
265291 XDOT = 6993
412061
YDOT = 7391
132934 feet/sec YDOT = 2252
817318 meter/sec
ZDOT = 332
842620 ZDOT = 101
450431
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
77114380
00016717 00000-0 10270-3 0 9030
2 25544 51
6384 162
2716 0001746 348
0930 12
0181 15
52663326 10215
Satellite: ISS
Catalog Number: 25544
Epoch time: 19135
77114380 = yrday
fracday
Element set: 903
Inclination: 51
6384 deg
RA of node: 162
2716 deg
Eccentricity:
0001746
Arg of perigee: 348
0930 deg
Mean anomaly: 12
0181 deg
Mean motion: 15
52663326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1021
Checksum: 279
Coasting Arc #5 (Orbit 1028)
---------------------------------------
Vector Time (GMT): 2019/136/05:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3828641
48 A = 6788513
49 meter
Y = -4409970
77 meter E =
0012031
Z = 3451738
83 I = 51
77693
XDOT = 5944
270588 Wp = 84
25903
YDOT = 1559
545813 meter/sec RA = 158
70587 deg
ZDOT = -4585
939370 TA = 55
37469
MA = 55
26130
Ha = 223
201 n
mi
Hp = 217
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12561159
72 X = 3860903
60
Y = -14468408
04 feet Y = -4366975
95 meter
Z = 11324602
45 Z = 3470415
42
XDOT = 19502
200091 XDOT = 5948
665790
YDOT = 5116
620123 feet/sec YDOT = 1626
043542 meter/sec
ZDOT = -15045
732841 ZDOT = -4557
053170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18775455
69 X = 5722758
89
Y = -3559289
63 feet Y = -1084871
48 meter
Z = 11409553
30 Z = 3477631
85
XDOT = 11904
745331 XDOT = 3628
566377
YDOT = 14831
594569 feet/sec YDOT = 4520
670024 meter/sec
ZDOT = -14914
967642 ZDOT = -4546
082137
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
28604476
00016717 00000-0 10270-3 0 9048
2 25544 51
6390 159
7072 0001095 343
9473 16
1644 15
52649164 10292
Satellite: ISS
Catalog Number: 25544
Epoch time: 19136
28604476 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 159
7072 deg
Eccentricity:
0001095
Arg of perigee: 343
9473 deg
Mean anomaly: 16
1644 deg
Mean motion: 15
52649164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1029
Checksum: 314
Coasting Arc #6 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2019/137/05:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4564436
20 A = 6791046
16 meter
Y = 4392728
33 meter E =
0006124
Z = -2442096
26 I = 51
81702
XDOT = -5005
419235 Wp = 37
27570
YDOT = -2229
184429 meter/sec RA = 153
74664 deg
ZDOT = 5357
473701 TA = 295
49129
MA = 295
55462
Ha = 223
223 n
mi
Hp = 217
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14975184
38 X = -4601355
14
Y = 14411838
34 feet Y = 4341479
31 meter
Z = -8012126
85 Z = -2464358
42
XDOT = -16421
979117 XDOT = -5006
143941
YDOT = -7313
597207 feet/sec YDOT = -2285
162867 meter/sec
ZDOT = 17577
013456 ZDOT = 5333
156937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20610239
48 X = -6282000
99
Y = 2354387
14 feet Y = 717617
20 meter
Z = -8113340
76 Z = -2472946
26
XDOT = -8501
947185 XDOT = -2591
393502
YDOT = -14365
088838 feet/sec YDOT = -4378
479078 meter/sec
ZDOT = 17466
992731 ZDOT = 5323
939385
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
25148092
00016717 00000-0 10270-3 0 9054
2 25544 51
6400 154
9052 0001386 344
5670 15
5440 15
52647361 10449
Satellite: ISS
Catalog Number: 25544
Epoch time: 19137
25148092 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 154
9052 deg
Eccentricity:
0001386
Arg of perigee: 344
5670 deg
Mean anomaly: 15
5440 deg
Mean motion: 15
52647361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1044
Checksum: 287
Coasting Arc #7 (Orbit 1045)
---------------------------------------
Vector Time (GMT): 2019/137/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5850885
00 A = 6788654
49 meter
Y = -88945
80 meter E =
0012150
Z = 3429927
83 I = 51
81120
XDOT = 2793
695291 Wp = 83
99189
YDOT = -5454
285705 meter/sec RA = 153
41453 deg
ZDOT = 4611
359642 TA = 316
05286
MA = 316
14942
Ha = 223
298 n
mi
Hp = 217
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19195816
93 X = -5866116
51
Y = -291816
92 feet Y = -154459
84 meter
Z = 11253044
05 Z = 3401468
91
XDOT = 9165
666966 XDOT = 2832
079208
YDOT = -17894
638141 feet/sec YDOT = -5422
830281 meter/sec
ZDOT = 15129
132684 ZDOT = 4625
023544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18933087
51 X = -5770805
07
Y = -3603938
61 feet Y = -1098480
49 meter
Z = 11124089
56 Z = 3390622
50
XDOT = 11746
055192 XDOT = 3580
197622
YDOT = -14685
642085 feet/sec YDOT = -4476
183708 meter/sec
ZDOT = 15191
465968 ZDOT = 4630
358827
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
38020437
00016717 00000-0 10270-3 0 9061
2 25544 51
6398 154
2659 0001340 343
7622 16
3487 15
52687214 10462
Satellite: ISS
Catalog Number: 25544
Epoch time: 19137
38020437 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 154
2659 deg
Eccentricity:
0001340
Arg of perigee: 343
7622 deg
Mean anomaly: 16
3487 deg
Mean motion: 15
52687214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1046
Checksum: 307
Coasting Arc #8 (Orbit 1060)
---------------------------------------
Vector Time (GMT): 2019/138/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5209876
50 A = 6785937
83 meter
Y = 758923
00 meter E =
0008539
Z = -4290478
02 I = 51
83037
XDOT = -3769
279655 Wp = 60
81250
YDOT = 5620
131307 meter/sec RA = 148
45252 deg
ZDOT = -3584
196374 TA = 172
65630
MA = 172
64379
Ha = 223
287 n
mi
Hp = 217
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17092770
68 X = 5221843
95
Y = 2489904
85 feet Y = 817250
74 meter
Z = -14076371
47 Z = -4265140
79
XDOT = -12366
403069 XDOT = -3814
435061
YDOT = 18438
751007 feet/sec YDOT = 5577
728386 meter/sec
ZDOT = -11759
174456 ZDOT = -3602
615702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16592417
61 X = 5057368
89
Y = 5125626
32 feet Y = 1562290
90 meter
Z = -13961600
97 Z = -4255495
98
XDOT = -14625
636943 XDOT = -4457
894140
YDOT = 15098
119274 feet/sec YDOT = 4601
906755 meter/sec
ZDOT = -11843
090943 ZDOT = -3609
774120
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
34563986
00016717 00000-0 10270-3 0 9070
2 25544 51
6390 149
4639 0001430 349
9318 10
1805 15
52664157 10612
Satellite: ISS
Catalog Number: 25544
Epoch time: 19138
34563986 = yrday
fracday
Element set: 907
Inclination: 51
6390 deg
RA of node: 149
4639 deg
Eccentricity:
0001430
Arg of perigee: 349
9318 deg
Mean anomaly: 10
1805 deg
Mean motion: 15
52664157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1061
Checksum: 316
Coasting Arc #9 (Orbit 1076)
---------------------------------------
Vector Time (GMT): 2019/139/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4442853
90 A = 6783456
76 meter
Y = -1497959
87 meter E =
0006162
Z = 4898073
76 I = 51
85017
XDOT = 4550
220216 Wp = 109
95220
YDOT = -5695
604199 meter/sec RA = 143
48700 deg
ZDOT = 2380
985299 TA = 316
77020
MA = 316
81855
Ha = 223
414 n
mi
Hp = 216
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14576292
31 X = -4449565
62
Y = -4914566
49 feet Y = -1547681
01 meter
Z = 16069795
79 Z = 4876475
20
XDOT = 14928
544015 XDOT = 4602
006195
YDOT = -18686
365483 feet/sec YDOT = -5644
431145 meter/sec
ZDOT = 7811
631557 ZDOT = 2403
214144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13864133
52 X = -4225787
90
Y = -6894931
48 feet Y = -2101575
12 meter
Z = 15972016
77 Z = 4868270
71
XDOT = 16811
854005 XDOT = 5124
253101
YDOT = -15440
558125 feet/sec YDOT = -4706
282116 meter/sec
ZDOT = 7912
844596 ZDOT = 2411
835033
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
37543495
00016717 00000-0 10270-3 0 9088
2 25544 51
6389 144
3414 0001475 353
8719 6
2415 15
52693442 10772
Satellite: ISS
Catalog Number: 25544
Epoch time: 19139
37543495 = yrday
fracday
Element set: 908
Inclination: 51
6389 deg
RA of node: 144
3414 deg
Eccentricity:
0001475
Arg of perigee: 353
8719 deg
Mean anomaly: 6
2415 deg
Mean motion: 15
52693442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1077
Checksum: 324
Coasting Arc #10 (Orbit 1091)
---------------------------------------
Vector Time (GMT): 2019/140/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3613472
10 A = 6782033
68 meter
Y = 2318908
71 meter E =
0014470
Z = -5262544
03 I = 51
87063
XDOT = -5109
816449 Wp = 76
23645
YDOT = 5605
020709 meter/sec RA = 138
51956 deg
ZDOT = -1037
827003 TA = 183
83381
MA = 183
84491
Ha = 223
362 n
mi
Hp = 217
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11855223
43 X = 3612835
73
Y = 7607968
20 feet Y = 2359314
18 meter
Z = -17265564
40 Z = -5244992
13
XDOT = -16764
489662 XDOT = -5167
072354
YDOT = 18389
175556 feet/sec YDOT = 5547
559157 meter/sec
ZDOT = -3404
944237 ZDOT = -1062
787311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10961523
33 X = 3341072
31
Y = 9000400
04 feet Y = 2743321
93 meter
Z = -17186186
95 Z = -5238349
78
XDOT = -18188
546478 XDOT = -5543
868967
YDOT = 15427
019127 feet/sec YDOT = 4702
155430 meter/sec
ZDOT = -3518
558793 ZDOT = -1072
456720
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
34086883
00016717 00000-0 10270-3 0 9091
2 25544 51
6383 139
5394 0001489 356
8679 3
2463 15
52655075 10929
Satellite: ISS
Catalog Number: 25544
Epoch time: 19140
34086883 = yrday
fracday
Element set: 909
Inclination: 51
6383 deg
RA of node: 139
5394 deg
Eccentricity:
0001489
Arg of perigee: 356
8679 deg
Mean anomaly: 3
2463 deg
Mean motion: 15
52655075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1092
Checksum: 334
Coasting Arc #11 (Orbit 1107)
---------------------------------------
Vector Time (GMT): 2019/141/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2747265
69 A = 6781532
51 meter
Y = -3171715
88 meter E =
0003384
Z = 5325402
98 I = 51
89480
XDOT = 5478
723952 Wp = 48
44085
YDOT = -5353
474485 meter/sec RA = 133
55175 deg
ZDOT = -359
738704 TA = 44
99068
MA = 44
96327
Ha = 223
440 n
mi
Hp = 216
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9013338
88 X = -2737462
60
Y = -10405892
01 feet Y = -3202383
65 meter
Z = 17471794
54 Z = 5312081
02
XDOT = 17974
816116 XDOT = 5539
928268
YDOT = -17563
892666 feet/sec YDOT = -5291
865295 meter/sec
ZDOT = -1180
245093 ZDOT = -332
976904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7998708
15 X = -2438006
24
Y = -11297841
18 feet Y = -3443581
99 meter
Z = 17411660
55 Z = 5307074
14
XDOT = 18887
634733 XDOT = 5756
951067
YDOT = -15015
260035 feet/sec YDOT = -4576
651259 meter/sec
ZDOT = -1058
456408 ZDOT = -322
617513
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 19141
37066023
00016717 00000-0 10270-3 0 9101
2 25544 51
6394 134
4169 0001613 1
6522 358
4635 15
52703665 11089
Satellite: ISS
Catalog Number: 25544
Epoch time: 19141
37066023 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 134
4169 deg
Eccentricity:
0001613
Arg of perigee: 1
6522 deg
Mean anomaly: 358
4635 deg
Mean motion: 15
52703665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1108
Checksum: 284
Coasting Arc #12 (Orbit 1122)
---------------------------------------
Vector Time (GMT): 2019/142/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1918881
81 A = 6782561
41 meter
Y = 4027815
22 meter E =
0013408
Z = -5120430
32 I = 51
91996
XDOT = -5634
798519 Wp = 95
47207
YDOT = 4884
553637 meter/sec RA = 128
58628 deg
ZDOT = 1733
283884 TA = 191
22817
MA = 191
25811
Ha = 223
517 n
mi
Hp = 216
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6295543
98 X = 1898571
38
Y = 13214616
87 feet Y = 4049160
65 meter
Z = -16799312
08 Z = -5111157
83
XDOT = -18486
871782 XDOT = -5697
419585
YDOT = 16025
438441 feet/sec YDOT = 4821
191001 meter/sec
ZDOT = 5686
626916 ZDOT = 1705
760538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5235899
23 X = 1595902
09
Y = 13720228
26 feet Y = 4181925
57 meter
Z = -16757611
86 Z = -5107720
09
XDOT = -18846
350035 XDOT = -5744
367491
YDOT = 13974
041999 feet/sec YDOT = 4259
288001 meter/sec
ZDOT = 5561
398752 ZDOT = 1695
114340
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 19142
33609066
00016717 00000-0 10270-3 0 9119
2 25544 51
6393 129
6148 0001775 10
2120 349
9068 15
52668462 11237
Satellite: ISS
Catalog Number: 25544
Epoch time: 19142
33609066 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 129
6148 deg
Eccentricity:
0001775
Arg of perigee: 10
2120 deg
Mean anomaly: 349
9068 deg
Mean motion: 15
52668462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1123
Checksum: 300
Coasting Arc #13 (Orbit 1138)
---------------------------------------
Vector Time (GMT): 2019/143/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1122831
03 A = 6784448
31 meter
Y = -4838362
83 meter E =
0009530
Z = 4617129
52 I = 51
94637
XDOT = 5647
928810 Wp = 57
49990
YDOT = -4210
508183 meter/sec RA = 123
62561 deg
ZDOT = -3029
218679 TA = 62
65884
MA = 62
56187
Ha = 223
484 n
mi
Hp = 216
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3683828
85 X = -1091071
15
Y = -15873893
81 feet Y = -4850742
14 meter
Z = 15148062
74 Z = 4611751
72
XDOT = 18529
950165 XDOT = 5709
306455
YDOT = -13814
003226 feet/sec YDOT = -4147
005510 meter/sec
ZDOT = -9938
381492 ZDOT = -3001
634540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2669353
10 X = -813618
83
Y = -16098171
15 feet Y = -4906722
57 meter
Z = 15124098
12 Z = 4609825
11
XDOT = 18340
317796 XDOT = 5590
128864
YDOT = -12289
710818 feet/sec YDOT = -3745
903857 meter/sec
ZDOT = -9812
912738 ZDOT = -2990
975803
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 19143
36588003
00016717 00000-0 10270-3 0 9121
2 25544 51
6390 124
4930 0001710 11
9786 348
1407 15
52710971 11399
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
36588003 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 124
4930 deg
Eccentricity:
0001710
Arg of perigee: 11
9786 deg
Mean anomaly: 348
1407 deg
Mean motion: 15
52710971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1139
Checksum: 294
Coasting Arc #14 (Orbit 1142)
---------------------------------------
Vector Time (GMT): 2019/143/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 225056
25 A = 6787826
74 meter
Y = -5707744
35 meter E =
0012563
Z = 3658854
39 I = 51
96178
XDOT = 5718
038458 Wp = 77
01040
YDOT = -2602
619773 meter/sec RA = 122
33277 deg
ZDOT = -4396
333734 TA = 59
76720
MA = 59
64288
Ha = 223
537 n
mi
Hp = 216
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 738373
53 X = 271092
42
Y = -18726195
38 feet Y = -5704970
68 meter
Z = 12004115
44 Z = 3660058
71
XDOT = 18759
968693 XDOT = 5768
071717
YDOT = -8538
778782 feet/sec YDOT = -2538
396349 meter/sec
ZDOT = -14423
667107 ZDOT = -4368
436383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18725467
71 X = -5707522
56
Y = -655129
35 feet Y = -199683
43 meter
Z = 12010080
81 Z = 3660672
63
XDOT = -8590
252194 XDOT = -2618
308869
YDOT = -17489
586594 feet/sec YDOT = -5330
825994 meter/sec
ZDOT = -14296
914003 ZDOT = -4357
699388
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 19143
62332885
00016717 00000-0 10270-3 0 9136
2 25544 51
6384 123
2126 0001999 12
4378 347
6823 15
52694857 11433
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
62332885 = yrday
fracday
Element set: 913
Inclination: 51
6384 deg
RA of node: 123
2126 deg
Eccentricity:
0001999
Arg of perigee: 12
4378 deg
Mean anomaly: 347
6823 deg
Mean motion: 15
52694857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1143
Checksum: 323
Coasting Arc #15 (Orbit 1143)
---------------------------------------
Vector Time (GMT): 2019/143/16:12:46
849
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1920813
31 A = 6787698
91 meter
Y = 4241197
65 meter E =
0007090
Z = -4945773
37 I = 51
94921
XDOT = -5266
040679 Wp = 117
46316
YDOT = 5063
350388 meter/sec RA = 121
88227 deg
ZDOT = 2296
167151 TA = 174
92230
MA = 174
91510
Ha = 223
706 n
mi
Hp = 221
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6301880
93 X = 1897268
14
Y = 13914690
46 feet Y = 4262546
51 meter
Z = -16226290
59 Z = -4936499
41
XDOT = -17277
036347 XDOT = -5333
422653
YDOT = 16612
041956 feet/sec YDOT = 5004
084788 meter/sec
ZDOT = 7533
356796 ZDOT = 2270
423620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8110795
94 X = 2472170
60
Y = -12996091
36 feet Y = -3961208
65 meter
Z = -16184604
38 Z = -4933067
42
XDOT = 22449
691757 XDOT = 6842
666047
YDOT = 4772
373873 feet/sec YDOT = 1454
619556 meter/sec
ZDOT = 7416
153022 ZDOT = 2260
443441
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 19143
68769762
00016717 00000-0 10270-3 0 9141
2 25544 51
6396 122
8911 0005395 272
3194 87
7339 15
51161361 11443
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
68769762 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 122
8911 deg
Eccentricity:
0005395
Arg of perigee: 272
3194 deg
Mean anomaly: 87
7339 deg
Mean motion: 15
51161361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1144
Checksum: 328
Coasting Arc #16 (Orbit 1146)
---------------------------------------
Vector Time (GMT): 2019/143/19:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4943880
28 A = 6790005
77 meter
Y = 1528164
08 meter E =
0004477
Z = 4394775
48 I = 51
95937
XDOT = 962
050118 Wp = 127
10903
YDOT = -6781
804553 meter/sec RA = 121
17913 deg
ZDOT = 3435
407179 TA = 288
16964
MA = 288
21838
Ha = 223
869 n
mi
Hp = 221
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16220079
66 X = -4981948
63
Y = 5013661
69 feet Y = 1472664
75 meter
Z = 14418554
72 Z = 4370667
64
XDOT = 3156
332407 XDOT = 1021
127357
YDOT = -22250
014937 feet/sec YDOT = -6770
716343 meter/sec
ZDOT = 11271
020930 ZDOT = 3440
223109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16500897
35 X = 5029473
51
Y = -4369569
48 feet Y = -1331844
78 meter
Z = 14309079
54 Z = 4361407
44
XDOT = -4271
251354 XDOT = -1301
877413
YDOT = 20907
728340 feet/sec YDOT = 6372
675598 meter/sec
ZDOT = 11293
463889 ZDOT = 3442
247794
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 19143
88097289
00016717 00000-0 10270-3 0 9152
2 25544 51
6398 121
9325 0005496 274
1227 85
9295 15
51135745 11474
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
88097289 = yrday
fracday
Element set: 915
Inclination: 51
6398 deg
RA of node: 121
9325 deg
Eccentricity:
0005496
Arg of perigee: 274
1227 deg
Mean anomaly: 85
9295 deg
Mean motion: 15
51135745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1147
Checksum: 340
Coasting Arc #17 (Orbit 1146)
---------------------------------------
Vector Time (GMT): 2019/143/21:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2538063
99 A = 6797285
30 meter
Y = 6171889
92 meter E =
0007284
Z = -1266257
79 I = 51
98310
XDOT = -4865
787571 Wp = 358
83614
YDOT = -798
774704 meter/sec RA = 120
88449 deg
ZDOT = 5866
061579 TA = 347
47634
MA = 347
49443
Ha = 223
607 n
mi
Hp = 221
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8326981
60 X = -2600740
40
Y = 20248982
68 feet Y = 6143157
22 meter
Z = -4154389
07 Z = -1278738
24
XDOT = -15963
869984 XDOT = -4884
987929
YDOT = -2620
651917 feet/sec YDOT = -853
295432 meter/sec
ZDOT = 19245
608855 ZDOT = 5842
378626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2187551
84 X = 666765
80
Y = -21773755
08 feet Y = -6636640
55 meter
Z = -4211540
98 Z = -1283677
69
XDOT = 14584
309597 XDOT = 4445
297565
YDOT = -2232
468755 feet/sec YDOT = -680
456476 meter/sec
ZDOT = 19138
266094 ZDOT = 5833
343506
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 19143
88097144
00016717 00000-0 10270-3 0 9163
2 25544 51
6380 121
9308 0005655 272
3684 87
6820 15
51156048 11472
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
88097144 = yrday
fracday
Element set: 916
Inclination: 51
6380 deg
RA of node: 121
9308 deg
Eccentricity:
0005655
Arg of perigee: 272
3684 deg
Mean anomaly: 87
6820 deg
Mean motion: 15
51156048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1147
Checksum: 319
Coasting Arc #18 (Orbit 1154)
---------------------------------------
Vector Time (GMT): 2019/144/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 452051
13 A = 6793696
00 meter
Y = -5997028
43 meter E =
0007655
Z = 3152602
79 I = 51
98062
XDOT = 5506
891358 Wp = 95
23773
YDOT = -2152
910192 meter/sec RA = 118
50560 deg
ZDOT = -4875
517495 TA = 48
65211
MA = 48
58628
Ha = 223
739 n
mi
Hp = 221
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1483107
39 X = 503764
41
Y = -19675290
14 feet Y = -5991684
51 meter
Z = 10343185
02 Z = 3154923
58
XDOT = 18067
228865 XDOT = 5554
239109
YDOT = -7063
353649 feet/sec YDOT = -2091
062964 meter/sec
ZDOT = -15995
792305 ZDOT = -4848
652304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1860289
24 X = -567016
16
Y = -19637388
01 feet Y = -5985475
86 meter
Z = 10354247
53 Z = 3155974
65
XDOT = 15323
201337 XDOT = 4670
511768
YDOT = -9837
765956 feet/sec YDOT = -2998
551063 meter/sec
ZDOT = -15873
747116 ZDOT = -4838
318121
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 19144
39637371
00016717 00000-0 10270-3 0 9173
2 25544 51
6391 119
3736 0005229 273
7398 86
3155 15
51183557 11555
Satellite: ISS
Catalog Number: 25544
Epoch time: 19144
39637371 = yrday
fracday
Element set: 917
Inclination: 51
6391 deg
RA of node: 119
3736 deg
Eccentricity:
0005229
Arg of perigee: 273
7398 deg
Mean anomaly: 86
3155 deg
Mean motion: 15
51183557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1155
Checksum: 332
Coasting Arc #19 (Orbit 1169)
---------------------------------------
Vector Time (GMT): 2019/145/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -571212
69 A = 6795123
93 meter
Y = 6273392
56 meter E =
0004091
Z = -2540708
46 I = 52
00192
XDOT = -5259
575366 Wp = 344
88898
YDOT = 1672
737182 meter/sec RA = 113
56908 deg
ZDOT = 5314
636839 TA = 346
77350
MA = 346
78422
Ha = 223
799 n
mi
Hp = 221
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1874057
37 X = -628979
74
Y = 20581996
59 feet Y = 6266682
13 meter
Z = -8335657
67 Z = -2543622
85
XDOT = -17255
824690 XDOT = -5303
705050
YDOT = 5487
982879 feet/sec YDOT = 1613
673627 meter/sec
ZDOT = 17436
472569 ZDOT = 5288
980772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1965547
25 X = 599098
80
Y = 20567868
20 feet Y = 6269086
23 meter
Z = -8349448
20 Z = -2544911
81
XDOT = -14580
302907 XDOT = -4444
076326
YDOT = 8421
767762 feet/sec YDOT = 2566
954814 meter/sec
ZDOT = 17319
941090 ZDOT = 5279
118044
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 19145
36275078
00016717 00000-0 10270-3 0 9184
2 25544 51
6406 114
5777 0005152 277
1533 82
9033 15
51197639 11708
Satellite: ISS
Catalog Number: 25544
Epoch time: 19145
36275078 = yrday
fracday
Element set: 918
Inclination: 51
6406 deg
RA of node: 114
5777 deg
Eccentricity:
0005152
Arg of perigee: 277
1533 deg
Mean anomaly: 82
9033 deg
Mean motion: 15
51197639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1170
Checksum: 316
Coasting Arc #20 (Orbit 1185)
---------------------------------------
Vector Time (GMT): 2019/146/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 652679
89 A = 6796453
96 meter
Y = -6497425
31 meter E =
0008936
Z = 1866953
27 I = 52
01635
XDOT = 5042
991484 Wp = 120
12879
YDOT = -1124
247413 meter/sec RA = 108
63547 deg
ZDOT = -5659
827634 TA = 39
45995
MA = 39
39491
Ha = 223
945 n
mi
Hp = 221
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2141338
23 X = 716218
82
Y = -21317012
16 feet Y = -6489771
49 meter
Z = 6125174
76 Z = 1870277
47
XDOT = 16545
247650 XDOT = 5082
680661
YDOT = -3688
475763 feet/sec YDOT = -1067
630715 meter/sec
ZDOT = -18568
988300 ZDOT = -5635
234347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2189080
94 X = -667231
87
Y = -21307649
13 feet Y = -6494571
46 meter
Z = 6140856
27 Z = 1871732
99
XDOT = 14046
305598 XDOT = 4281
313946
YDOT = -6777
387243 feet/sec YDOT = -2065
747632 meter/sec
ZDOT = -18457
317502 ZDOT = -5625
790375
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 19146
39355217
00016717 00000-0 10270-3 0 9193
2 25544 51
6386 109
4623 0005150 282
2021 77
8553 15
51173353 11869
Satellite: ISS
Catalog Number: 25544
Epoch time: 19146
39355217 = yrday
fracday
Element set: 919
Inclination: 51
6386 deg
RA of node: 109
4623 deg
Eccentricity:
0005150
Arg of perigee: 282
2021 deg
Mean anomaly: 77
8553 deg
Mean motion: 15
51173353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1186
Checksum: 306
Coasting Arc #21 (Orbit 1200)
---------------------------------------
Vector Time (GMT): 2019/147/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -681066
35 A = 6797232
50 meter
Y = 6654995
35 meter E =
0008543
Z = -1172231
84 I = 52
02925
XDOT = -4867
313371 Wp = 4
45215
YDOT = 538
371685 meter/sec RA = 103
70361 deg
ZDOT = 5895
496304 TA = 342
90090
MA = 342
92967
Ha = 223
950 n
mi
Hp = 221
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2234469
64 X = -749739
72
Y = 21833974
25 feet Y = 6646995
31 meter
Z = -3845905
00 Z = -1175706
47
XDOT = -15968
875888 XDOT = -4901
608976
YDOT = 1766
311301 feet/sec YDOT = 483
749740 meter/sec
ZDOT = 19342
179474 ZDOT = 5871
769395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2561151
31 X = 780638
92
Y = 21795170
20 feet Y = 6643167
88 meter
Z = -3862296
11 Z = -1177227
85
XDOT = -13746
755213 XDOT = -4190
010989
YDOT = 5017
450165 feet/sec YDOT = 1529
318810 meter/sec
ZDOT = 19234
486166 ZDOT = 5862
671383
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 19147
35992713
00016717 00000-0 10270-3 0 9200
2 25544 51
6389 104
6666 0005198 283
9260 76
1313 15
51212237 12010
Satellite: ISS
Catalog Number: 25544
Epoch time: 19147
35992713 = yrday
fracday
Element set: 920
Inclination: 51
6389 deg
RA of node: 104
6666 deg
Eccentricity:
0005198
Arg of perigee: 283
9260 deg
Mean anomaly: 76
1313 deg
Mean motion: 15
51212237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1201
Checksum: 304
Coasting Arc #22 (Orbit 1216)
---------------------------------------
Vector Time (GMT): 2019/148/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 694168
63 A = 6797844
08 meter
Y = -6743397
57 meter E =
0008079
Z = 438794
62 I = 52
03711
XDOT = 4738
968754 Wp = 142
64506
YDOT = 92
695314 meter/sec RA = 98
77224 deg
ZDOT = -6020
777493 TA = 32
65553
MA = 32
60560
Ha = 224
218 n
mi
Hp = 221
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2277456
12 X = 767392
20
Y = -22124007
77 feet Y = -6735225
50 meter
Z = 1439614
90 Z = 442344
00
XDOT = 15547
797750 XDOT = 4766
825753
YDOT = 304
118483 feet/sec YDOT = 145
845991 meter/sec
ZDOT = -19753
206999 ZDOT = -5997
689562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2945741
27 X = -897861
94
Y = -22043879
42 feet Y = -6718974
45 meter
Z = 1456367
41 Z = 443900
79
XDOT = 13712
075914 XDOT = 4179
440738
YDOT = -3141
539261 feet/sec YDOT = -957
541167 meter/sec
ZDOT = -19648
467995 ZDOT = -5988
853045
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 19148
39072528
00016717 00000-0 10270-3 0 9219
2 25544 51
6383 99
5501 0005250 290
9866 69
0724 15
51174960 12177
Satellite: ISS
Catalog Number: 25544
Epoch time: 19148
39072528 = yrday
fracday
Element set: 921
Inclination: 51
6383 deg
RA of node: 99
5501 deg
Eccentricity:
0005250
Arg of perigee: 290
9866 deg
Mean anomaly: 69
0724 deg
Mean motion: 15
51174960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1217
Checksum: 320
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