[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 26th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
026/08:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 217
4
033/17:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 216
5
040/11:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 215
6
Coasting Arc #1 (Orbit 3309)
---------------------------------------
Vector Time (GMT): 2019/025/14:35:17
515
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1130828
90 A = 6780015
64 meter
Y = 4072952
86 meter E =
0003057
Z = 5302110
68 I = 51
55598
XDOT = -7483
224382 Wp = 332
57603
YDOT = 1630
050789 meter/sec RA = 349
77013 deg
ZDOT = 346
585143 TA = 114
13099
MA = 114
09901
Ha = 221
732 n
mi
Hp = 217
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3710068
58 X = 1059445
76
Y = 13362706
23 feet Y = 4085199
55 meter
Z = 17395376
25 Z = 5307430
27
XDOT = -24551
261097 XDOT = -7502
579390
YDOT = 5347
935658 feet/sec YDOT = 1546
259942 meter/sec
ZDOT = 1137
090364 ZDOT = 310
188136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -578371
87 X = -176287
75
Y = 13826627
25 feet Y = 4214355
99 meter
Z = 17418826
21 Z = 5309258
23
XDOT = -24023
708654 XDOT = -7322
426398
YDOT = -2218
946258 feet/sec YDOT = -676
334819 meter/sec
ZDOT = 972
628735 ZDOT = 296
457238
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 19025
65661760
00016717 00000-0 10270-3 0 9001
2 25544 51
6409 350
1103 0005083 310
9371 49
1341 15
53222627 33104
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
65661760 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 350
1103 deg
Eccentricity:
0005083
Arg of perigee: 310
9371 deg
Mean anomaly: 49
1341 deg
Mean motion: 15
53222627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3310
Checksum: 269
Coasting Arc #2 (Orbit 3321)
---------------------------------------
Vector Time (GMT): 2019/026/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4755665
95 A = 6784299
71 meter
Y = 2294525
06 meter E =
0005948
Z = 4254272
97 I = 51
54321
XDOT = -5270
997619 Wp = 84
75271
YDOT = 4257
442309 meter/sec RA = 345
97319 deg
ZDOT = 3592
185527 TA = 328
49126
MA = 328
52687
Ha = 221
795 n
mi
Hp = 217
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15602578
58 X = 4708989
93
Y = 7527969
35 feet Y = 2347445
32 meter
Z = 13957588
49 Z = 4277260
42
XDOT = -17293
299274 XDOT = -5335
662334
YDOT = 13967
986578 feet/sec YDOT = 4198
136834 meter/sec
ZDOT = 11785
385588 ZDOT = 3566
424309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10323338
16 X = -3146553
47
Y = 13807317
24 feet Y = 4208470
30 meter
Z = 14061000
57 Z = 4285792
97
XDOT = -9428
584817 XDOT = -2873
832652
YDOT = -18945
038579 feet/sec YDOT = -5774
447759 meter/sec
ZDOT = 11668
569658 ZDOT = 3556
580032
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 19026
42870957
00016717 00000-0 10270-3 0 9018
2 25544 51
6390 346
2659 0004875 314
3931 45
6822 15
53180197 33226
Satellite: ISS
Catalog Number: 25544
Epoch time: 19026
42870957 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 346
2659 deg
Eccentricity:
0004875
Arg of perigee: 314
3931 deg
Mean anomaly: 45
6822 deg
Mean motion: 15
53180197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3322
Checksum: 318
Coasting Arc #3 (Orbit 3336)
---------------------------------------
Vector Time (GMT): 2019/027/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3638313
64 A = 6781630
92 meter
Y = -2903421
45 meter E =
0011286
Z = -4941906
04 I = 51
50276
XDOT = 6165
003549 Wp = 51
04858
YDOT = -3975
512624 meter/sec RA = 340
98110 deg
ZDOT = -2199
568234 TA = 197
40258
MA = 197
44129
Ha = 222
034 n
mi
Hp = 217
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11936724
56 X = -3581571
67
Y = -9525660
93 feet Y = -2943790
38 meter
Z = -16213602
49 Z = -4959441
52
XDOT = 20226
389598 XDOT = 6219
684789
YDOT = -13043
020421 feet/sec YDOT = -3906
265529 meter/sec
ZDOT = -7216
431213 ZDOT = -2169
488546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11419276
94 X = 3480595
61
Y = -10013225
53 feet Y = -3052031
14 meter
Z = -16292327
75 Z = -4965901
50
XDOT = 8631
806922 XDOT = 2630
974750
YDOT = 21382
792581 feet/sec YDOT = 6517
475179 meter/sec
ZDOT = -7080
180825 ZDOT = -2158
039115
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 19027
39382193
00016717 00000-0 10270-3 0 9026
2 25544 51
6394 341
4618 0004792 319
2322 40
8471 15
53191687 33377
Satellite: ISS
Catalog Number: 25544
Epoch time: 19027
39382193 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 341
4618 deg
Eccentricity:
0004792
Arg of perigee: 319
2322 deg
Mean anomaly: 40
8471 deg
Mean motion: 15
53191687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3337
Checksum: 317
Coasting Arc #4 (Orbit 3352)
---------------------------------------
Vector Time (GMT): 2019/028/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2384022
34 A = 6780217
87 meter
Y = 3534507
21 meter E =
0002749
Z = 5272177
89 I = 51
46567
XDOT = -6749
089066 Wp = 351
89333
YDOT = 3578
843399 meter/sec RA = 335
98158 deg
ZDOT = 655
292166 TA = 91
84986
MA = 91
81837
Ha = 222
130 n
mi
Hp = 217
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7821595
59 X = 2318712
31
Y = 11596152
25 feet Y = 3560801
80 meter
Z = 17297171
56 Z = 5283599
83
XDOT = -22142
680664 XDOT = -6791
790103
YDOT = 11741
612200 feet/sec YDOT = 3503
131618 meter/sec
ZDOT = 2149
908680 ZDOT = 622
404353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12651805
13 X = -3856270
20
Y = 5814729
40 feet Y = 1772329
52 meter
Z = 17348227
51 Z = 5287739
74
XDOT = -7740
859553 XDOT = -2359
413992
YDOT = -22786
410931 feet/sec YDOT = -6945
298052 meter/sec
ZDOT = 2001
053738 ZDOT = 609
921179
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 19028
42327319
00016717 00000-0 10270-3 0 9031
2 25544 51
6383 336
3369 0004955 322
6712 37
4095 15
53185346 33530
Satellite: ISS
Catalog Number: 25544
Epoch time: 19028
42327319 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 336
3369 deg
Eccentricity:
0004955
Arg of perigee: 322
6712 deg
Mean anomaly: 37
4095 deg
Mean motion: 15
53185346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3353
Checksum: 315
Coasting Arc #5 (Orbit 3367)
---------------------------------------
Vector Time (GMT): 2019/029/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1110521
14 A = 6780440
24 meter
Y = -4164772
64 meter E =
0011711
Z = -5243729
65 I = 51
43614
XDOT = 6975
302063 Wp = 78
42074
YDOT = -3023
505221 meter/sec RA = 330
97918 deg
ZDOT = 928
215023 TA = 200
47245
MA = 200
51942
Ha = 222
293 n
mi
Hp = 217
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3643442
07 X = -1038396
16
Y = -13663952
24 feet Y = -4176787
88 meter
Z = -17203837
42 Z = -5248948
98
XDOT = 22884
849288 XDOT = 7004
084641
YDOT = -9919
636552 feet/sec YDOT = -2945
341618 meter/sec
ZDOT = 3045
324880 ZDOT = 962
167823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14021374
49 X = 4273714
95
Y = -1608649
67 feet Y = -490316
42 meter
Z = -17226827
52 Z = -5250737
03
XDOT = 6551
647639 XDOT = 1996
942200
YDOT = 22991
741713 feet/sec YDOT = 7007
882874 meter/sec
ZDOT = 3198
900316 ZDOT = 975
024816
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 19029
38838274
00016717 00000-0 10270-3 0 9045
2 25544 51
6381 331
5330 0004977 326
3306 33
7530 15
53176986 33686
Satellite: ISS
Catalog Number: 25544
Epoch time: 19029
38838274 = yrday
fracday
Element set: 904
Inclination: 51
6381 deg
RA of node: 331
5330 deg
Eccentricity:
0004977
Arg of perigee: 326
3306 deg
Mean anomaly: 33
7530 deg
Mean motion: 15
53176986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3368
Checksum: 325
Coasting Arc #6 (Orbit 3383)
---------------------------------------
Vector Time (GMT): 2019/030/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -154546
08 A = 6782131
79 meter
Y = 4756350
24 meter E =
0008720
Z = 4832209
55 I = 51
41376
XDOT = -6892
100663 Wp = 24
45801
YDOT = 2284
771380 meter/sec RA = 325
97598 deg
ZDOT = -2459
947207 TA = 89
82830
MA = 89
72837
Ha = 222
403 n
mi
Hp = 216
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -507040
95 X = -231193
28
Y = 15604823
64 feet Y = 4754193
28 meter
Z = 15853705
87 Z = 4831272
83
XDOT = -22611
878815 XDOT = -6905
188512
YDOT = 7495
969096 feet/sec YDOT = 2207
626009 meter/sec
ZDOT = -8070
692937 ZDOT = -2493
457656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15417229
22 X = -4699171
47
Y = -2496116
65 feet Y = -760816
36 meter
Z = 15848849
99 Z = 4830729
48
XDOT = -4893
912201 XDOT = -1491
664439
YDOT = -22174
185792 feet/sec YDOT = -6758
691829 meter/sec
ZDOT = -8222
166820 ZDOT = -2506
116447
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 19030
41783043
00016717 00000-0 10270-3 0 9055
2 25544 51
6384 326
4080 0005060 329
5869 30
4989 15
53203823 33848
Satellite: ISS
Catalog Number: 25544
Epoch time: 19030
41783043 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 326
4080 deg
Eccentricity:
0005060
Arg of perigee: 329
5869 deg
Mean anomaly: 30
4989 deg
Mean motion: 15
53203823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3384
Checksum: 307
Coasting Arc #7 (Orbit 3398)
---------------------------------------
Vector Time (GMT): 2019/031/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1286556
46 A = 6784994
38 meter
Y = -5254187
50 meter E =
0005262
Z = -4098109
37 I = 51
39667
XDOT = 6510
373856 Wp = 63
89037
YDOT = -1367
687528 meter/sec RA = 320
97677 deg
ZDOT = 3803
451742 TA = 245
51133
MA = 245
56621
Ha = 222
591 n
mi
Hp = 216
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4220985
75 X = 1365120
62
Y = -17238147
96 feet Y = -5239360
89 meter
Z = -13445240
73 Z = -4091669
27
XDOT = 21359
494279 XDOT = 6506
709142
YDOT = -4487
163805 feet/sec YDOT = -1294
904632 meter/sec
ZDOT = 12478
516215 ZDOT = 3835
067172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16698140
58 X = 5089593
25
Y = 6077946
21 feet Y = 1852558
00 meter
Z = -13415499
80 Z = -4089044
34
XDOT = 2695
459546 XDOT = 821
576070
YDOT = 20408
858903 feet/sec YDOT = 6220
620194 meter/sec
ZDOT = 12621
315000 ZDOT = 3846
976812
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 19031
38293550
00016717 00000-0 10270-3 0 9062
2 25544 51
6389 321
6039 0005146 334
5318 25
5580 15
53184292 33990
Satellite: ISS
Catalog Number: 25544
Epoch time: 19031
38293550 = yrday
fracday
Element set: 906
Inclination: 51
6389 deg
RA of node: 321
6039 deg
Eccentricity:
0005146
Arg of perigee: 334
5318 deg
Mean anomaly: 25
5580 deg
Mean motion: 15
53184292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3399
Checksum: 316
Coasting Arc #8 (Orbit 3414)
---------------------------------------
Vector Time (GMT): 2019/032/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2297076
35 A = 6788093
70 meter
Y = 5608881
42 meter E =
0011531
Z = 3051170
95 I = 51
38174
XDOT = -5894
124799 Wp = 72
59291
YDOT = 258
739730 meter/sec RA = 315
98247 deg
ZDOT = -4894
312289 TA = 72
27275
MA = 72
14692
Ha = 222
678 n
mi
Hp = 216
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7536339
72 X = -2374446
29
Y = 18401841
93 feet Y = 5582761
19 meter
Z = 10010403
37 Z = 3039825
16
XDOT = -19337
679788 XDOT = -5872
806700
YDOT = 848
883630 feet/sec YDOT = 192
946911 meter/sec
ZDOT = -16057
455016 ZDOT = -4922
891338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17673705
87 X = -5386945
55
Y = -9170651
64 feet Y = -2795214
62 meter
Z = 9958496
26 Z = 3035349
66
XDOT = 154
722488 XDOT = 47
159414
YDOT = -17942
188226 feet/sec YDOT = -5468
778971 meter/sec
ZDOT = -16186
408982 ZDOT = -4933
617458
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 19032
41237957
00016717 00000-0 10270-3 0 9077
2 25544 51
6385 316
4791 0005227 337
8424 22
2501 15
53212727 34158
Satellite: ISS
Catalog Number: 25544
Epoch time: 19032
41237957 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 316
4791 deg
Eccentricity:
0005227
Arg of perigee: 337
8424 deg
Mean anomaly: 22
2501 deg
Mean motion: 15
53212727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3415
Checksum: 299
Coasting Arc #9 (Orbit 3429)
---------------------------------------
Vector Time (GMT): 2019/033/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3086139
31 A = 6790640
10 meter
Y = -5762779
89 meter E =
0011065
Z = -1815343
42 I = 51
36738
XDOT = 5115
802011 Wp = 15
12263
YDOT = 972
130984 meter/sec RA = 310
99350 deg
ZDOT = 5629
246634 TA = 324
84629
MA = 324
91925
Ha = 222
770 n
mi
Hp = 216
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10125128
98 X = 3159168
69
Y = -18906758
16 feet Y = -5727860
13 meter
Z = -5955851
13 Z = -1800175
30
XDOT = 16784
127334 XDOT = 5077
208075
YDOT = 3189
406115 feet/sec YDOT = 1029
123470 meter/sec
ZDOT = 18468
656936 ZDOT = 5654
002970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18153976
01 X = 5533331
89
Y = 11455823
49 feet Y = 3491735
00 meter
Z = -5886694
07 Z = -1794264
35
XDOT = -3507
011896 XDOT = -1068
937226
YDOT = 15074
059553 feet/sec YDOT = 4594
573352 meter/sec
ZDOT = 18580
208465 ZDOT = 5663
247540
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 19033
37748206
00016717 00000-0 10270-3 0 9088
2 25544 51
6388 311
6752 0005164 341
4198 18
6765 15
53208020 34303
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
37748206 = yrday
fracday
Element set: 908
Inclination: 51
6388 deg
RA of node: 311
6752 deg
Eccentricity:
0005164
Arg of perigee: 341
4198 deg
Mean anomaly: 18
6765 deg
Mean motion: 15
53208020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3430
Checksum: 305
Coasting Arc #10 (Orbit 3435)
---------------------------------------
Vector Time (GMT): 2019/033/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1920925
05 A = 6788612
50 meter
Y = 5880361
41 meter E =
0011573
Z = 2789822
76 I = 51
35452
XDOT = -5706
981440 Wp = 76
51005
YDOT = 558
827436 meter/sec RA = 309
22745 deg
ZDOT = -5086
934860 TA = 71
72962
MA = 71
60373
Ha = 222
697 n
mi
Hp = 216
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6302247
52 X = -2000089
20
Y = 19292524
32 feet Y = 5858437
57 meter
Z = 9152961
80 Z = 2780299
76
XDOT = -18723
692389 XDOT = -5688
097384
YDOT = 1833
423345 feet/sec YDOT = 495
113726 meter/sec
ZDOT = -16689
418833 ZDOT = -5114
610648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5164674
61 X = 1574192
82
Y = 19648003
73 feet Y = 5988711
54 meter
Z = 9109259
79 Z = 2776502
38
XDOT = -13182
261400 XDOT = -4017
953275
YDOT = 11291
901609 feet/sec YDOT = 3441
771610 meter/sec
ZDOT = -16814
334238 ZDOT = -5125
009076
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 19033
76351947
00016717 00000-0 10270-3 0 9094
2 25544 51
6399 309
7519 0005440 339
2592 20
8339 15
53253322 34367
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
76351947 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 309
7519 deg
Eccentricity:
0005440
Arg of perigee: 339
2592 deg
Mean anomaly: 20
8339 deg
Mean motion: 15
53253322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3436
Checksum: 325
Coasting Arc #11 (Orbit 3450)
---------------------------------------
Vector Time (GMT): 2019/034/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2653679
96 A = 6791041
20 meter
Y = -6056570
54 meter E =
0012126
Z = -1517065
62 I = 51
34056
XDOT = 5028
276108 Wp = 17
38985
YDOT = 771
473645 meter/sec RA = 304
23654 deg
ZDOT = 5738
857157 TA = 325
96951
MA = 326
04721
Ha = 222
845 n
mi
Hp = 216
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8706299
09 X = 2728577
87
Y = -19870638
25 feet Y = -6026476
44 meter
Z = -4977249
42 Z = -1503993
58
XDOT = 16496
968858 XDOT = 4991
400159
YDOT = 2531
081513 feet/sec YDOT = 827
497064 meter/sec
ZDOT = 18828
271513 ZDOT = 5763
192408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3854081
08 X = -1174723
91
Y = -21363025
66 feet Y = -6511450
22 meter
Z = -4917531
27 Z = -1498863
53
XDOT = 13434
332057 XDOT = 4094
784411
YDOT = -6765
207753 feet/sec YDOT = -2062
035323 meter/sec
ZDOT = 18937
950862 ZDOT = 5772
287423
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 19034
72862036
00016717 00000-0 10270-3 0 9109
2 25544 51
6384 304
9469 0005181 344
5550 15
5444 15
53212064 34510
Satellite: ISS
Catalog Number: 25544
Epoch time: 19034
72862036 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 304
9469 deg
Eccentricity:
0005181
Arg of perigee: 344
5550 deg
Mean anomaly: 15
5444 deg
Mean motion: 15
53212064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3451
Checksum: 293
Coasting Arc #12 (Orbit 3466)
---------------------------------------
Vector Time (GMT): 2019/035/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3243326
85 A = 6791828
30 meter
Y = 5963924
49 meter E =
0008426
Z = 105247
00 I = 51
32545
XDOT = -4254
586932 Wp = 111
75609
YDOT = -2201
419922 meter/sec RA = 299
24942 deg
ZDOT = -5981
560406 TA = 67
10621
MA = 67
01728
Ha = 222
934 n
mi
Hp = 216
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10640836
13 X = -3310287
31
Y = 19566681
38 feet Y = 5927280
94 meter
Z = 345298
56 Z = 89329
95
XDOT = -13958
618544 XDOT = -4200
599570
YDOT = -7222
506307 feet/sec YDOT = -2248
695833 meter/sec
ZDOT = -19624
542013 ZDOT = -6002
095869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2486473
01 X = 757876
97
Y = 22134694
27 feet Y = 6746654
81 meter
Z = 272775
43 Z = 83141
95
XDOT = -13857
544193 XDOT = -4223
779470
YDOT = 1819
282624 feet/sec YDOT = 554
517344 meter/sec
ZDOT = -19716
908924 ZDOT = -6009
713840
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 19035
75805743
00016717 00000-0 10270-3 0 9116
2 25544 51
6379 299
8225 0005413 348
8712 11
2320 15
53266801 34672
Satellite: ISS
Catalog Number: 25544
Epoch time: 19035
75805743 = yrday
fracday
Element set: 911
Inclination: 51
6379 deg
RA of node: 299
8225 deg
Eccentricity:
0005413
Arg of perigee: 348
8712 deg
Mean anomaly: 11
2320 deg
Mean motion: 15
53266801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3467
Checksum: 312
Coasting Arc #13 (Orbit 3482)
---------------------------------------
Vector Time (GMT): 2019/036/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3639969
69 A = 6791274
53 meter
Y = -5576178
74 meter E =
0016433
Z = 1282683
37 I = 51
30704
XDOT = 3475
171633 Wp = 42
67376
YDOT = 3611
973229 meter/sec RA = 294
26028 deg
ZDOT = 5808
569954 TA = 331
35070
MA = 331
44089
Ha = 222
974 n
mi
Hp = 216
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11942157
76 X = 3695823
18
Y = -18294549
67 feet Y = -5535161
74 meter
Z = 4208278
79 Z = 1300500
24
XDOT = 11401
481736 XDOT = 3406
309255
YDOT = 11850
305869 feet/sec YDOT = 3650
450106 meter/sec
ZDOT = 19056
988037 ZDOT = 5825
283227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1091089
40 X = -332564
05
Y = -21804280
65 feet Y = -6645944
74 meter
Z = 4289307
55 Z = 1307380
94
XDOT = 14493
736796 XDOT = 4417
690976
YDOT = 3058
549064 feet/sec YDOT = 932
245755 meter/sec
ZDOT = 19131
952350 ZDOT = 5831
419076
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 19036
78749627
00016717 00000-0 10270-3 0 9129
2 25544 51
6371 294
6973 0005082 352
4869 7
6206 15
53212786 34836
Satellite: ISS
Catalog Number: 25544
Epoch time: 19036
78749627 = yrday
fracday
Element set: 912
Inclination: 51
6371 deg
RA of node: 294
6973 deg
Eccentricity:
0005082
Arg of perigee: 352
4869 deg
Mean anomaly: 7
6206 deg
Mean motion: 15
53212786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3483
Checksum: 339
Coasting Arc #14 (Orbit 3497)
---------------------------------------
Vector Time (GMT): 2019/037/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3924711
10 A = 6788949
09 meter
Y = 4890225
67 meter E =
0004449
Z = -2609158
13 I = 51
28782
XDOT = -2692
567617 Wp = 59
44107
YDOT = -4934
499101 meter/sec RA = 289
26720 deg
ZDOT = -5202
759612 TA = 150
05382
MA = 150
02836
Ha = 223
156 n
mi
Hp = 215
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12876348
74 X = -3966429
79
Y = 16044047
48 feet Y = 4846103
45 meter
Z = -8560230
09 Z = -2628323
89
XDOT = -8833
883259 XDOT = -2611
917114
YDOT = -16189
301511 feet/sec YDOT = -4964
158516 meter/sec
ZDOT = -17069
421299 ZDOT = -5215
642678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -609732
05 X = -185846
33
Y = 20526634
08 feet Y = 6256518
07 meter
Z = -8647246
71 Z = -2635680
80
XDOT = -15200
368646 XDOT = -4633
072363
YDOT = -7660
527105 feet/sec YDOT = -2334
928661 meter/sec
ZDOT = -17126
965741 ZDOT = -5220
299158
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 19037
75259094
00016717 00000-0 10270-3 0 9132
2 25544 51
6379 289
8927 0005232 357
9598 2
1532 15
53247312 34986
Satellite: ISS
Catalog Number: 25544
Epoch time: 19037
75259094 = yrday
fracday
Element set: 913
Inclination: 51
6379 deg
RA of node: 289
8927 deg
Eccentricity:
0005232
Arg of perigee: 357
9598 deg
Mean anomaly: 2
1532 deg
Mean motion: 15
53247312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3498
Checksum: 342
Coasting Arc #15 (Orbit 3513)
---------------------------------------
Vector Time (GMT): 2019/038/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4080646
36 A = 6785943
27 meter
Y = -3928509
51 meter E =
0012178
Z = 3723508
55 I = 51
26639
XDOT = 1969
453015 Wp = 72
05128
YDOT = 6078
615214 meter/sec RA = 284
26658 deg
ZDOT = 4247
137012 TA = 332
71191
MA = 332
77583
Ha = 223
048 n
mi
Hp = 215
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13387947
39 X = 4106186
50
Y = -12888810
72 feet Y = -3882733
88 meter
Z = 12216235
39 Z = 3743392
53
XDOT = 6461
460023 XDOT = 1880
704130
YDOT = 19942
963302 feet/sec YDOT = 6100
143000 meter/sec
ZDOT = 13934
176550 ZDOT = 4256
487785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2579679
64 X = 786286
35
Y = -18343760
16 feet Y = -5591178
10 meter
Z = 12306368
28 Z = 3750981
05
XDOT = 15940
546871 XDOT = 4858
678686
YDOT = 11634
664433 feet/sec YDOT = 3546
245719 meter/sec
ZDOT = 13975
672933 ZDOT = 4259
785110
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 19038
78202413
00016717 00000-0 10270-3 0 9140
2 25544 51
6365 284
7672 0004990
9249 359
1912 15
53240618 35148
Satellite: ISS
Catalog Number: 25544
Epoch time: 19038
78202413 = yrday
fracday
Element set: 914
Inclination: 51
6365 deg
RA of node: 284
7672 deg
Eccentricity:
0004990
Arg of perigee:
9249 deg
Mean anomaly: 359
1912 deg
Mean motion: 15
53240618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3514
Checksum: 312
Coasting Arc #16 (Orbit 3528)
---------------------------------------
Vector Time (GMT): 2019/039/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4183159
99 A = 6782893
12 meter
Y = 2742469
45 meter E =
0013267
Z = -4594328
94 I = 51
24987
XDOT = -1283
959719 Wp = 49
87340
YDOT = -6938
497963 meter/sec RA = 279
25978 deg
ZDOT = -2970
026815 TA = 190
28258
MA = 190
30974
Ha = 223
310 n
mi
Hp = 215
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13724278
20 X = -4191199
94
Y = 8997603
17 feet Y = 2695645
21 meter
Z = -15073257
68 Z = -4614668
41
XDOT = -4212
466271 XDOT = -1191
849621
YDOT = -22764
100929 feet/sec YDOT = -6952
341253 meter/sec
ZDOT = -9744
182464 ZDOT = -2976
039552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4954042
44 X = -1509992
14
Y = 15555925
23 feet Y = 4741446
01 meter
Z = -15165303
35 Z = -4622384
46
XDOT = -16387
291033 XDOT = -4994
846307
YDOT = -14752
534116 feet/sec YDOT = -4496
572398 meter/sec
ZDOT = -9770
544271 ZDOT = -2978
061894
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 19039
74711811
00016717 00000-0 10270-3 0 9155
2 25544 51
6374 279
9638 0005066 5
8606 354
2605 15
53238560 35296
Satellite: ISS
Catalog Number: 25544
Epoch time: 19039
74711811 = yrday
fracday
Element set: 915
Inclination: 51
6374 deg
RA of node: 279
9638 deg
Eccentricity:
0005066
Arg of perigee: 5
8606 deg
Mean anomaly: 354
2605 deg
Mean motion: 15
53238560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3529
Checksum: 325
Coasting Arc #17 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2019/040/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3848227
16 A = 6780876
79 meter
Y = 2368977
60 meter E =
0009772
Z = 5053735
33 I = 51
24363
XDOT = -2099
293688 Wp = 29
31900
YDOT = 7164
983783 meter/sec RA = 275
48298 deg
ZDOT = -1750
287442 TA = 77
75451
MA = 77
64510
Ha = 223
241 n
mi
Hp = 215
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12625417
21 X = 3796902
80
Y = 7772236
21 feet Y = 2411724
50 meter
Z = 16580496
48 Z = 5072303
42
XDOT = -6887
446483 XDOT = -2170
756771
YDOT = 23507
164641 feet/sec YDOT = 7141
108333 meter/sec
ZDOT = -5742
412866 ZDOT = -1760
658839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1836319
51 X = 559710
19
Y = 14617141
68 feet Y = 4455304
78 meter
Z = 16663996
48 Z = 5079186
13
XDOT = -21511
215334 XDOT = -6556
618434
YDOT = 9339
700476 feet/sec YDOT = 2846
740705 meter/sec
ZDOT = -5789
965591 ZDOT = -1764
781512
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 19040
51918971
00016717 00000-0 10270-3 0 9169
2 25544 51
6410 276
1246 0005494 4
3951 355
7248 15
53273072 35413
Satellite: ISS
Catalog Number: 25544
Epoch time: 19040
51918971 = yrday
fracday
Element set: 916
Inclination: 51
6410 deg
RA of node: 276
1246 deg
Eccentricity:
0005494
Arg of perigee: 4
3951 deg
Mean anomaly: 355
7248 deg
Mean motion: 15
53273072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 306
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