[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 11th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14148 2991 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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
190/22:57:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 217
3
201/16:28:21
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 218
5
201/22:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
6
202/23:35:11
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
7
203/02:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 218
7
203/20:57:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
9
204/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
9
Coasting Arc #1 (Orbit 1855)
---------------------------------------
Vector Time (GMT): 2019/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 837141
43 A = 6794699
92 meter
Y = -6029639
73 meter E =
0019214
Z = 3004535
36 I = 51
27618
XDOT = 4961
268292 Wp = 96
62271
YDOT = 3154
847969 meter/sec RA = 254
59132 deg
ZDOT = 4919
580554 TA = 297
93920
MA = 298
13358
Ha = 228
414 n
mi
Hp = 217
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2746527
01 X = 889910
20
Y = -19782282
56 feet Y = -6019983
44 meter
Z = 9857399
47 Z = 3008729
46
XDOT = 16277
126943 XDOT = 4901
724867
YDOT = 10350
551081 feet/sec YDOT = 3209
994990 meter/sec
ZDOT = 16140
356148 ZDOT = 4943
535890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19789379
36 X = -6031802
83
Y = 2622304
78 feet Y = 799278
50 meter
Z = 9876964
13 Z = 3010498
67
XDOT = 5921
022742 XDOT = 1804
727732
YDOT = -16880
093378 feet/sec YDOT = -5145
052461 meter/sec
ZDOT = 16248
727179 ZDOT = 4952
612044
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 19189
55827166
00016717 00000-0 10270-3 0 9005
2 25544 51
6416 255
2474 0007124 121
7590 238
4256 15
50970751 18563
Satellite: ISS
Catalog Number: 25544
Epoch time: 19189
55827166 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 255
2474 deg
Eccentricity:
0007124
Arg of perigee: 121
7590 deg
Mean anomaly: 238
4256 deg
Mean motion: 15
50970751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1856
Checksum: 322
Coasting Arc #2 (Orbit 1870)
---------------------------------------
Vector Time (GMT): 2019/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -912539
58 A = 6793216
71 meter
Y = 5721100
33 meter E =
0011648
Z = -3553558
97 I = 51
28020
XDOT = -5120
916324 Wp = 108
03644
YDOT = -3563
761709 meter/sec RA = 249
60645 deg
ZDOT = -4438
080681 TA = 114
04179
MA = 113
91985
Ha = 228
421 n
mi
Hp = 217
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2993896
27 X = -959185
68
Y = 18770014
22 feet Y = 5710635
18 meter
Z = -11658658
03 Z = -3558104
49
XDOT = -16800
906575 XDOT = -5059
127179
YDOT = -11692
131591 feet/sec YDOT = -3620
681510 meter/sec
ZDOT = -14560
632155 ZDOT = -4462
806206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18835230
80 X = 5740978
35
Y = -2453172
19 feet Y = -747726
88 meter
Z = -11679776
65 Z = -3559995
92
XDOT = -6731
005802 XDOT = -2051
610568
YDOT = 17933
938923 feet/sec YDOT = 5466
264584 meter/sec
ZDOT = -14672
473578 ZDOT = -4472
169947
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 19190
52477387
00016717 00000-0 10270-3 0 9011
2 25544 51
6407 250
4526 0007187 124
9708 235
2119 15
50955741 18715
Satellite: ISS
Catalog Number: 25544
Epoch time: 19190
52477387 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 250
4526 deg
Eccentricity:
0007187
Arg of perigee: 124
9708 deg
Mean anomaly: 235
2119 deg
Mean motion: 15
50955741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1871
Checksum: 320
Coasting Arc #3 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2019/190/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2869890
06 A = 6787791
72 meter
Y = 3575952
66 meter E =
0018161
Z = -5020622
13 I = 51
26961
XDOT = -4218
275309 Wp = 92
27330
YDOT = -6083
669928 meter/sec RA = 247
32389 deg
ZDOT = -1928
641570 TA = 158
90938
MA = 158
83440
Ha = 228
280 n
mi
Hp = 217
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9415649
82 X = -2885276
87
Y = 11732128
14 feet Y = 3543773
97 meter
Z = -16471857
38 Z = -5034599
93
XDOT = -13839
485922 XDOT = -4140
564254
YDOT = -19959
547007 feet/sec YDOT = -6130
406954 meter/sec
ZDOT = -6327
564206 ZDOT = -1948
944052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11883617
42 X = -3622126
59
Y = -9109001
61 feet Y = -2776423
69 meter
Z = -16535570
88 Z = -5040042
01
XDOT = 19064
346195 XDOT = 5810
812720
YDOT = -13258
964700 feet/sec YDOT = -4041
332441 meter/sec
ZDOT = -6419
130712 ZDOT = -1956
551041
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 19190
97580728
00016717 00000-0 10270-3 0 9025
2 25544 51
6425 248
2171 0006900 124
4102 235
7703 15
50984542 18783
Satellite: ISS
Catalog Number: 25544
Epoch time: 19190
97580728 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 248
2171 deg
Eccentricity:
0006900
Arg of perigee: 124
4102 deg
Mean anomaly: 235
7703 deg
Mean motion: 15
50984542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1878
Checksum: 312
Coasting Arc #4 (Orbit 1893)
---------------------------------------
Vector Time (GMT): 2019/191/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3035138
70 A = 6787041
18 meter
Y = -3154468
70 meter E =
0011031
Z = 5180183
70 I = 51
28172
XDOT = 4350
436366 Wp = 127
09344
YDOT = 6197
463915 meter/sec RA = 242
33305 deg
ZDOT = 1216
624862 TA = 311
12756
MA = 311
22273
Ha = 228
168 n
mi
Hp = 217
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9957804
12 X = 3045024
95
Y = -10349306
77 feet Y = -3120472
93 meter
Z = 16995353
36 Z = 5194950
88
XDOT = 14273
085191 XDOT = 4274
901555
YDOT = 20332
886860 feet/sec YDOT = 6245
691075 meter/sec
ZDOT = 3991
551386 ZDOT = 1237
574769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10674666
06 X = 3253638
21
Y = 9488249
87 feet Y = 2892018
56 meter
Z = 17062610
24 Z = 5200683
60
XDOT = -19148
593078 XDOT = -5836
491170
YDOT = 14146
030478 feet/sec YDOT = 4311
710090 meter/sec
ZDOT = 4086
062624 ZDOT = 1245
431888
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 19192
00673907
00016717 00000-0 10270-3 0 9034
2 25544 51
6432 243
1023 0006908 128
6023 231
5748 15
50980517 18946
Satellite: ISS
Catalog Number: 25544
Epoch time: 19192
00673907 = yrday
fracday
Element set: 903
Inclination: 51
6432 deg
RA of node: 243
1023 deg
Eccentricity:
0006908
Arg of perigee: 128
6023 deg
Mean anomaly: 231
5748 deg
Mean motion: 15
50980517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1894
Checksum: 304
Coasting Arc #5 (Orbit 1908)
---------------------------------------
Vector Time (GMT): 2019/192/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3287029
86 A = 6786596
23 meter
Y = 2727691
89 meter E =
0020132
Z = -5290802
06 I = 51
29628
XDOT = -4426
692921 Wp = 100
24432
YDOT = -6220
629599 meter/sec RA = 237
34228 deg
ZDOT = -461
901348 TA = 165
34682
MA = 165
28837
Ha = 228
171 n
mi
Hp = 217
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10784218
69 X = -3291587
72
Y = 8949120
39 feet Y = 2690909
20 meter
Z = -17358274
47 Z = -5306779
89
XDOT = -14523
270739 XDOT = -4354
559407
YDOT = -20408
889762 feet/sec YDOT = -6269
728603 meter/sec
ZDOT = -1515
424369 ZDOT = -483
230069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9479888
68 X = -2889470
07
Y = -10197457
24 feet Y = -3108184
97 meter
Z = -17430989
58 Z = -5312965
62
XDOT = 18899
363776 XDOT = 5760
526079
YDOT = -14842
574472 feet/sec YDOT = -4524
016699 meter/sec
ZDOT = -1611
670680 ZDOT = -491
237223
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 19192
97323614
00016717 00000-0 10270-3 0 9048
2 25544 51
6428 238
3072 0006806 131
0714 229
1026 15
50989141 19094
Satellite: ISS
Catalog Number: 25544
Epoch time: 19192
97323614 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 238
3072 deg
Eccentricity:
0006806
Arg of perigee: 131
0714 deg
Mean anomaly: 229
1026 deg
Mean motion: 15
50989141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1909
Checksum: 306
Coasting Arc #6 (Orbit 1924)
---------------------------------------
Vector Time (GMT): 2019/193/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3547743
37 A = 6786515
66 meter
Y = -2332986
35 meter E =
0008450
Z = 5287641
60 I = 51
31424
XDOT = 4498
696881 Wp = 121
29132
YDOT = 6205
010919 meter/sec RA = 232
35340 deg
ZDOT = -284
631759 TA = 331
41062
MA = 331
45693
Ha = 228
015 n
mi
Hp = 217
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11639577
99 X = 3547883
53
Y = -7654154
70 feet Y = -2293312
97 meter
Z = 17347905
53 Z = 5304875
13
XDOT = 14759
504202 XDOT = 4430
358894
YDOT = 20357
647373 feet/sec YDOT = 6254
936443 meter/sec
ZDOT = -933
831229 ZDOT = -262
943976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8420214
00 X = 2566481
23
Y = 10974520
46 feet Y = 3345033
84 meter
Z = 17426289
99 Z = 5311533
19
XDOT = -18504
087630 XDOT = -5640
045910
YDOT = 15504
040959 feet/sec YDOT = 4725
631684 meter/sec
ZDOT = -835
934385 ZDOT = -254
792801
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 19194
00416549
00016717 00000-0 10270-3 0 9055
2 25544 51
6420 233
1930 0006825 135
5626 224
6074 15
50990097 19257
Satellite: ISS
Catalog Number: 25544
Epoch time: 19194
00416549 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 233
1930 deg
Eccentricity:
0006825
Arg of perigee: 135
5626 deg
Mean anomaly: 224
6074 deg
Mean motion: 15
50990097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1925
Checksum: 306
Coasting Arc #7 (Orbit 1939)
---------------------------------------
Vector Time (GMT): 2019/194/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3878420
97 A = 6786859
69 meter
Y = 1964205
37 meter E =
0019861
Z = -5228861
62 I = 51
33613
XDOT = -4492
433277 Wp = 110
97690
YDOT = -6103
098093 meter/sec RA = 227
36504 deg
ZDOT = 1035
812107 TA = 169
03246
MA = 168
98910
Ha = 228
038 n
mi
Hp = 217
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12724478
24 X = -3874698
33
Y = 6444243
33 feet Y = 1920855
78 meter
Z = -17155057
81 Z = -5247692
03
XDOT = -14738
954321 XDOT = -4428
884157
YDOT = -20023
287706 feet/sec YDOT = -6152
980470 meter/sec
ZDOT = 3398
333683 ZDOT = 1014
143119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7494878
94 X = -2284439
10
Y = -12013444
89 feet Y = -3661698
00 meter
Z = -17240665
85 Z = -5254954
95
XDOT = 17815
252576 XDOT = 5430
088985
YDOT = -15868
703110 feet/sec YDOT = -4836
780708 meter/sec
ZDOT = 3300
491689 ZDOT = 1005
989867
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 19194
97066165
00016717 00000-0 10270-3 0 9067
2 25544 51
6415 228
3977 0006713 139
1134 221
0522 15
50987665 19401
Satellite: ISS
Catalog Number: 25544
Epoch time: 19194
97066165 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 228
3977 deg
Eccentricity:
0006713
Arg of perigee: 139
1134 deg
Mean anomaly: 221
0522 deg
Mean motion: 15
50987665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1940
Checksum: 322
Coasting Arc #8 (Orbit 1955)
---------------------------------------
Vector Time (GMT): 2019/195/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4207701
72 A = 6787449
56 meter
Y = -1636644
73 meter E =
0008578
Z = 5060349
40 I = 51
36198
XDOT = 4458
144970 Wp = 105
71495
YDOT = 5984
544842 meter/sec RA = 222
37918 deg
ZDOT = -1771
185454 TA = 1
48235
MA = 1
47980
Ha = 227
776 n
mi
Hp = 217
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13804795
68 X = 4201110
36
Y = -5369569
34 feet Y = -1589628
94 meter
Z = 16602196
21 Z = 5080772
33
XDOT = 14626
459874 XDOT = 4399
496067
YDOT = 19634
333470 feet/sec YDOT = 6034
071306 meter/sec
ZDOT = -5810
975898 ZDOT = -1749
671189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6742436
75 X = 2055094
72
Y = 13071097
66 feet Y = 3984070
57 meter
Z = 16695015
14 Z = 5088640
61
XDOT = -17075
785512 XDOT = -5204
699424
YDOT = 16107
051198 feet/sec YDOT = 4909
429205 meter/sec
ZDOT = -5713
802694 ZDOT = -1741
567061
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 19196
00158715
00016717 00000-0 10270-3 0 9077
2 25544 51
6417 223
2829 0006587 143
3424 216
8179 15
51006565 19560
Satellite: ISS
Catalog Number: 25544
Epoch time: 19196
00158715 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 223
2829 deg
Eccentricity:
0006587
Arg of perigee: 143
3424 deg
Mean anomaly: 216
8179 deg
Mean motion: 15
51006565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1956
Checksum: 321
Coasting Arc #9 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2019/196/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4582485
83 A = 6788506
33 meter
Y = 1359291
01 meter E =
0017437
Z = -4836998
07 I = 51
38887
XDOT = -4333
090153 Wp = 121
63908
YDOT = -5798
396276 meter/sec RA = 217
39454 deg
ZDOT = 2473
280655 TA = 172
81597
MA = 172
79095
Ha = 227
912 n
mi
Hp = 217
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15034402
32 X = -4573850
16
Y = 4459616
17 feet Y = 1308095
49 meter
Z = -15869416
23 Z = -4859236
53
XDOT = -14216
175042 XDOT = -4279
942412
YDOT = -19023
609828 feet/sec YDOT = -5846
555154 meter/sec
ZDOT = 8114
437846 ZDOT = 2452
360622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6210419
84 X = -1892935
97
Y = -14287571
69 feet Y = -4354851
85 meter
Z = -15970465
91 Z = -4867798
01
XDOT = 16139
567711 XDOT = 4919
340238
YDOT = -15988
559662 feet/sec YDOT = -4873
312985 meter/sec
ZDOT = 8019
922297 ZDOT = 2444
472316
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 19196
96808028
00016717 00000-0 10270-3 0 9082
2 25544 51
6399 218
4866 0006647 146
0417 214
1160 15
50987052 19711
Satellite: ISS
Catalog Number: 25544
Epoch time: 19196
96808028 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 218
4866 deg
Eccentricity:
0006647
Arg of perigee: 146
0417 deg
Mean anomaly: 214
1160 deg
Mean motion: 15
50987052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1971
Checksum: 337
Coasting Arc #10 (Orbit 1986)
---------------------------------------
Vector Time (GMT): 2019/197/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4938111
04 A = 6789662
35 meter
Y = -1126662
83 meter E =
0011501
Z = 4510601
13 I = 51
42012
XDOT = 4163
218420 Wp = 101
83096
YDOT = 5619
774563 meter/sec RA = 212
41491 deg
ZDOT = -3149
585140 TA = 19
87736
MA = 19
83258
Ha = 227
622 n
mi
Hp = 218
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16201151
72 X = 4928433
13
Y = -3696400
35 feet Y = -1071496
18 meter
Z = 14798560
13 Z = 4534564
49
XDOT = 13658
853085 XDOT = 4115
365712
YDOT = 18437
580587 feet/sec YDOT = 5666
063495 meter/sec
ZDOT = -10333
284580 ZDOT = -3129
477566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5859584
73 X = 1786001
43
Y = 15445766
28 feet Y = 4707869
56 meter
Z = 14907435
91 Z = 4543786
46
XDOT = -15263
137496 XDOT = -4652
204309
YDOT = 15689
903719 feet/sec YDOT = 4782
282654 meter/sec
ZDOT = -10242
418668 ZDOT = -3121
889210
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 19197
99900405
00016717 00000-0 10270-3 0 9099
2 25544 51
6398 213
3724 0006529 150
5533 209
5987 15
51011098 19876
Satellite: ISS
Catalog Number: 25544
Epoch time: 19197
99900405 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 213
3724 deg
Eccentricity:
0006529
Arg of perigee: 150
5533 deg
Mean anomaly: 209
5987 deg
Mean motion: 15
51011098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1987
Checksum: 339
Coasting Arc #11 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2019/198/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5309950
85 A = 6791132
11 meter
Y = 958660
04 meter E =
0013267
Z = -4138509
91 I = 51
45289
XDOT = -3904
513870 Wp = 130
67505
YDOT = -5400
944968 meter/sec RA = 207
43659 deg
ZDOT = 3758
109969 TA = 178
23297
MA = 178
22828
Ha = 227
753 n
mi
Hp = 218
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17421098
60 X = -5300174
07
Y = 3145210
11 feet Y = 899335
65 meter
Z = -13577788
41 Z = -4164279
24
XDOT = -12810
084875 XDOT = -3862
083180
YDOT = -17719
635721 feet/sec YDOT = -5444
371228 meter/sec
ZDOT = 12329
757115 ZDOT = 3739
246058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5768454
02 X = -1758224
79
Y = -16640881
84 feet Y = -5072140
79 meter
Z = -13694865
86 Z = -4174195
11
XDOT = 14315
058075 XDOT = 4363
229701
YDOT = -15040
395737 feet/sec YDOT = -4584
312621 meter/sec
ZDOT = 12244
497667 ZDOT = 3732
122889
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 19198
96549547
00016717 00000-0 10270-3 0 9105
2 25544 51
6392 208
5760 0006638 154
6015 205
5463 15
50989222 20023
Satellite: ISS
Catalog Number: 25544
Epoch time: 19198
96549547 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 208
5760 deg
Eccentricity:
0006638
Arg of perigee: 154
6015 deg
Mean anomaly: 205
5463 deg
Mean motion: 15
50989222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2002
Checksum: 322
Coasting Arc #12 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2019/199/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5643322
28 A = 6792577
07 meter
Y = -828579
82 meter E =
0014899
Z = 3671860
80 I = 51
48867
XDOT = 3590
059617 Wp = 109
64995
YDOT = 5214
166917 meter/sec RA = 202
46259 deg
ZDOT = -4331
555176 TA = 26
58054
MA = 26
50422
Ha = 227
468 n
mi
Hp = 218
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18514836
88 X = 5634332
82
Y = -2718437
74 feet Y = -765522
91 meter
Z = 12046787
42 Z = 3699251
41
XDOT = 11778
410818 XDOT = 3552
526302
YDOT = 17106
846842 feet/sec YDOT = 5254
104106 meter/sec
ZDOT = -14211
139029 ZDOT = -4314
206979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5821723
94 X = 1774461
46
Y = 17699796
53 feet Y = 5394897
98 meter
Z = 12171232
83 Z = 3709791
77
XDOT = -13539
456595 XDOT = -4126
826370
YDOT = 14192
738100 feet/sec YDOT = 4325
946573 meter/sec
ZDOT = -14132
727081 ZDOT = -4307
655214
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 19199
99641559
00016717 00000-0 10270-3 0 9116
2 25544 51
6398 203
4604 0006472 158
1787 201
9641 15
51012918 20186
Satellite: ISS
Catalog Number: 25544
Epoch time: 19199
99641559 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 203
4604 deg
Eccentricity:
0006472
Arg of perigee: 158
1787 deg
Mean anomaly: 201
9641 deg
Mean motion: 15
51012918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2018
Checksum: 326
Coasting Arc #13 (Orbit 2032)
---------------------------------------
Vector Time (GMT): 2019/200/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5963971
87 A = 6794122
66 meter
Y = 766404
81 meter E =
0008689
Z = -3175208
02 I = 51
52291
XDOT = -3203
622889 Wp = 130
35778
YDOT = -5017
456769 meter/sec RA = 197
49232 deg
ZDOT = 4809
484186 TA = 193
02470
MA = 193
04715
Ha = 227
650 n
mi
Hp = 218
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19566836
84 X = -5956675
72
Y = 2514451
48 feet Y = 699752
58 meter
Z = -10417349
13 Z = -3204160
33
XDOT = -10510
573783 XDOT = -3170
639438
YDOT = -16461
472339 feet/sec YDOT = -5053
097955 meter/sec
ZDOT = 15779
147591 ZDOT = 4794
002168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6124340
02 X = -1866698
84
Y = -18679345
19 feet Y = -5693464
41 meter
Z = -10548898
33 Z = -3215304
21
XDOT = 12816
076227 XDOT = 3906
340034
YDOT = -13067
628956 feet/sec YDOT = -3983
013306 meter/sec
ZDOT = 15709
178250 ZDOT = 4788
157531
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 19200
96290462
00016717 00000-0 10270-3 0 9120
2 25544 51
6379 198
6647 0006714 161
1993 198
9407 15
50984471 20332
Satellite: ISS
Catalog Number: 25544
Epoch time: 19200
96290462 = yrday
fracday
Element set: 912
Inclination: 51
6379 deg
RA of node: 198
6647 deg
Eccentricity:
0006714
Arg of perigee: 161
1993 deg
Mean anomaly: 198
9407 deg
Mean motion: 15
50984471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2033
Checksum: 336
Coasting Arc #14 (Orbit 2044)
---------------------------------------
Vector Time (GMT): 2019/201/16:28:21
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 157331
13 A = 6786637
59 meter
Y = -4273264
06 meter E =
0009197
Z = 5266911
78 I = 51
52365
XDOT = 7527
439419 Wp = 150
05052
YDOT = 1233
955219 meter/sec RA = 193
89872 deg
ZDOT = 767
917131 TA = 292
54981
MA = 292
64713
Ha = 227
503 n
mi
Hp = 218
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 516178
25 X = 179521
10
Y = -14019895
20 feet Y = -4271381
02 meter
Z = 17279894
28 Z = 5267729
56
XDOT = 24696
323553 XDOT = 7509
351490
YDOT = 4048
409512 feet/sec YDOT = 1318
031134 meter/sec
ZDOT = 2519
413159 ZDOT = 804
438025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 667665
30 X = 203504
38
Y = 14008557
24 feet Y = 4269808
25 meter
Z = 17283899
87 Z = 5268132
68
XDOT = -23893
770173 XDOT = -7282
821149
YDOT = -2208
174291 feet/sec YDOT = -673
051524 meter/sec
ZDOT = 2685
215630 ZDOT = 818
453724
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 19201
73609496
00016717 00000-0 10270-3 0 9138
2 25544 51
6401 194
8314 0006583 164
2566 195
8791 15
51019640 20454
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
73609496 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 194
8314 deg
Eccentricity:
0006583
Arg of perigee: 164
2566 deg
Mean anomaly: 195
8791 deg
Mean motion: 15
51019640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2045
Checksum: 316
Coasting Arc #15 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2019/201/22:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4421333
15 A = 6790060
75 meter
Y = -2618614
59 meter E =
0010614
Z = 4427792
83 I = 51
54208
XDOT = 5669
655139 Wp = 107
97816
YDOT = 3960
182358 meter/sec RA = 192
54929 deg
ZDOT = -3315
975917 TA = 15
55103
MA = 15
51844
Ha = 227
405 n
mi
Hp = 218
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14505686
19 X = 4428779
33
Y = -8591255
21 feet Y = -2569130
84 meter
Z = 14526879
36 Z = 4449287
46
XDOT = 18601
230771 XDOT = 5641
056710
YDOT = 12992
724272 feet/sec YDOT = 4023
424775 meter/sec
ZDOT = -10879
186078 ZDOT = -3288
504562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10969741
97 X = 3343577
35
Y = 12690071
69 feet Y = 3867933
85 meter
Z = 14624693
62 Z = 4457606
61
XDOT = -8613
388701 XDOT = -2625
360876
YDOT = 19852
493821 feet/sec YDOT = 6051
040117 meter/sec
ZDOT = -10754
668775 ZDOT = -3278
023043
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 19201
99382391
00016717 00000-0 10270-3 0 9149
2 25544 51
6386 193
5500 0006644 166
3318 193
8014 15
50987863 20495
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
99382391 = yrday
fracday
Element set: 914
Inclination: 51
6386 deg
RA of node: 193
5500 deg
Eccentricity:
0006644
Arg of perigee: 166
3318 deg
Mean anomaly: 193
8014 deg
Mean motion: 15
50987863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 328
Coasting Arc #16 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2019/202/22:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4823285
99 A = 6791493
57 meter
Y = 2586698
60 meter E =
0012091
Z = -4034852
82 I = 51
57950
XDOT = -5336
009039 Wp = 137
86136
YDOT = -3841
794338 meter/sec RA = 187
57999 deg
ZDOT = 3913
836184 TA = 172
90414
MA = 172
88701
Ha = 227
495 n
mi
Hp = 218
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15824429
09 X = -4832253
99
Y = 8486543
97 feet Y = 2532711
35 meter
Z = -13237706
11 Z = -4058303
75
XDOT = -17506
591334 XDOT = -5311
663324
YDOT = -12604
312133 feet/sec YDOT = -3901
329467 meter/sec
ZDOT = 12840
669894 ZDOT = 3887
975180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11337491
24 X = -3455667
33
Y = -13822400
26 feet Y = -4213067
60 meter
Z = -13344414
23 Z = -4067377
46
XDOT = 7999
540319 XDOT = 2438
259889
YDOT = -18850
946991 feet/sec YDOT = -5745
768643 meter/sec
ZDOT = 12723
440956 ZDOT = 3878
104803
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 19202
96031043
00016717 00000-0 10270-3 0 9153
2 25544 51
6384 188
7536 0006769 168
4310 191
6998 15
50991852 20648
Satellite: ISS
Catalog Number: 25544
Epoch time: 19202
96031043 = yrday
fracday
Element set: 915
Inclination: 51
6384 deg
RA of node: 188
7536 deg
Eccentricity:
0006769
Arg of perigee: 168
4310 deg
Mean anomaly: 191
6998 deg
Mean motion: 15
50991852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 335
Coasting Arc #17 (Orbit 2064)
---------------------------------------
Vector Time (GMT): 2019/202/23:35:11
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4403203
50 A = 6790614
62 meter
Y = -2861181
56 meter E =
0011194
Z = 4294036
50 I = 51
57723
XDOT = 5783
899414 Wp = 109
97774
YDOT = 3584
540320 meter/sec RA = 187
42475 deg
ZDOT = -3538
747679 TA = 16
12068
MA = 16
08509
Ha = 227
443 n
mi
Hp = 218
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14446205
70 X = 4414013
11
Y = -9387078
61 feet Y = -2811881
68 meter
Z = 14088046
26 Z = 4315451
31
XDOT = 18976
047946 XDOT = 5760
575161
YDOT = 11760
302886 feet/sec YDOT = 3649
089759 meter/sec
ZDOT = -11610
064564 ZDOT = -3510
708563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14138060
83 X = 4309280
94
Y = 9704087
99 feet Y = 2957806
02 meter
Z = 14185523
03 Z = 4323747
42
XDOT = -2923
503992 XDOT = -891
084017
YDOT = 21063
063619 feet/sec YDOT = 6420
021791 meter/sec
ZDOT = -11482
922925 ZDOT = -3499
994907
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 19203
02474320
00016717 00000-0 10270-3 0 9161
2 25544 51
6383 188
4334 0006846 169
0391 191
0910 15
50968855 20658
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
02474320 = yrday
fracday
Element set: 916
Inclination: 51
6383 deg
RA of node: 188
4334 deg
Eccentricity:
0006846
Arg of perigee: 169
0391 deg
Mean anomaly: 191
0910 deg
Mean motion: 15
50968855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2065
Checksum: 313
Coasting Arc #18 (Orbit 2066)
---------------------------------------
Vector Time (GMT): 2019/203/02:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -170714
41 A = 6786570
37 meter
Y = -4246571
45 meter E =
0009052
Z = 5288394
00 I = 51
57101
XDOT = 7630
297943 Wp = 154
76783
YDOT = 442
581152 meter/sec RA = 186
85074 deg
ZDOT = 593
316882 TA = 289
51346
MA = 289
61120
Ha = 227
524 n
mi
Hp = 218
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -560086
66 X = -148902
99
Y = -13932321
03 feet Y = -4248358
88 meter
Z = 17350374
01 Z = 5287617
45
XDOT = 25033
785903 XDOT = 7621
899823
YDOT = 1452
037899 feet/sec YDOT = 527
861508 meter/sec
ZDOT = 1946
577696 ZDOT = 630
361020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5008822
99 X = 1526689
25
Y = -13017203
03 feet Y = -3967643
48 meter
Z = 17347128
35 Z = 5287404
72
XDOT = 21351
717019 XDOT = 6508
003347
YDOT = 11070
801489 feet/sec YDOT = 3374
380294 meter/sec
ZDOT = 2114
840119 ZDOT = 644
603268
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 19203
15360740
00016717 00000-0 10270-3 0 9176
2 25544 51
6413 187
7933 0006989 169
9393 190
1899 15
51013576 20678
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
15360740 = yrday
fracday
Element set: 917
Inclination: 51
6413 deg
RA of node: 187
7933 deg
Eccentricity:
0006989
Arg of perigee: 169
9393 deg
Mean anomaly: 190
1899 deg
Mean motion: 15
51013576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2067
Checksum: 338
Coasting Arc #19 (Orbit 2078)
---------------------------------------
Vector Time (GMT): 2019/203/20:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3250598
70 A = 6789766
31 meter
Y = -3809712
25 meter E =
0013228
Z = 4582150
56 I = 51
60580
XDOT = 6725
238158 Wp = 137
93442
YDOT = -2057
673245 meter/sec RA = 183
05576 deg
ZDOT = 3045
403911 TA = 281
52722
MA = 281
67571
Ha = 227
432 n
mi
Hp = 218
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10664693
89 X = -3230013
04
Y = -12499055
95 feet Y = -3845947
90 meter
Z = 15033302
35 Z = 4566410
36
XDOT = 22064
429652 XDOT = 6732
955150
YDOT = -6750
896472 feet/sec YDOT = -1982
423937 meter/sec
ZDOT = 9991
482647 ZDOT = 3078
090759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15019590
51 X = 4577971
19
Y = -6819938
29 feet Y = -2078717
19 meter
Z = 14962039
21 Z = 4560429
55
XDOT = -200
016456 XDOT = -60
965016
YDOT = 21911
987786 feet/sec YDOT = 6678
773877 meter/sec
ZDOT = 10140
128087 ZDOT = 3090
711041
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 19203
92679489
00016717 00000-0 10270-3 0 9185
2 25544 51
6406 183
9611 0006402 171
4945 188
6316 15
50960785 20793
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
92679489 = yrday
fracday
Element set: 918
Inclination: 51
6406 deg
RA of node: 183
9611 deg
Eccentricity:
0006402
Arg of perigee: 171
4945 deg
Mean anomaly: 188
6316 deg
Mean motion: 15
50960785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2079
Checksum: 342
Coasting Arc #20 (Orbit 2086)
---------------------------------------
Vector Time (GMT): 2019/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 55846
05 A = 6786516
30 meter
Y = -4212662
82 meter E =
0007329
Z = 5317632
28 I = 51
61275
XDOT = 7666
001842 Wp = 154
09401
YDOT = 52
885272 meter/sec RA = 180
12860 deg
ZDOT = -45
036902 TA = 296
29778
MA = 296
37305
Ha = 227
374 n
mi
Hp = 218
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 183221
96 X = 77119
32
Y = -13821072
26 feet Y = -4211919
67 meter
Z = 17446300
13 Z = 5317954
98
XDOT = 25150
924678 XDOT = 7665
059475
YDOT = 173
508110 feet/sec YDOT = 138
606623 meter/sec
ZDOT = -147
758866 ZDOT = -7
801073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13365616
26 X = -4073839
84
Y = 3514981
26 feet Y = 1071366
29 meter
Z = 17448043
03 Z = 5318163
52
XDOT = -6088
885488 XDOT = -1855
892297
YDOT = -23363
788282 feet/sec YDOT = -7121
282668 meter/sec
ZDOT = 21
427002 ZDOT = 6
530950
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 19204
50668446
00016717 00000-0 10270-3 0 9192
2 25544 51
6384 181
0844 0006600 172
8080 187
3166 15
50984278 20871
Satellite: ISS
Catalog Number: 25544
Epoch time: 19204
50668446 = yrday
fracday
Element set: 919
Inclination: 51
6384 deg
RA of node: 181
0844 deg
Eccentricity:
0006600
Arg of perigee: 172
8080 deg
Mean anomaly: 187
3166 deg
Mean motion: 15
50984278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2087
Checksum: 327
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