[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 1st 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 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 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
090/20:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
1
000/00:00:00
000 0
0 0
0 216
7
094/11:01:35
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 216
8
094/14:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
0
000/00:00:00
000 0
0 0
0 216
9
097/20:12:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 216
8
101/23:12:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
6
000/00:00:00
000 0
0 0
0 217
1
Coasting Arc #1 (Orbit 286)
---------------------------------------
Vector Time (GMT): 2019/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3086137
06 A = 6790294
22 meter
Y = -5248875
76 meter E =
0006396
Z = -3007355
08 I = 51
87949
XDOT = 5791
632863 Wp = 113
44472
YDOT = -556
185292 meter/sec RA = 36
74351 deg
ZDOT = -4983
486393 TA = 100
81151
MA = 100
73951
Ha = 224
212 n
mi
Hp = 216
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10125121
60 X = -3012605
33
Y = -17220721
01 feet Y = -5282976
14 meter
Z = -9866650
51 Z = -3022167
36
XDOT = 19001
420155 XDOT = 5821
628669
YDOT = -1824
754895 feet/sec YDOT = -491
251778 meter/sec
ZDOT = -16350
020976 ZDOT = -4955
280140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11724438
27 X = -3573608
79
Y = -16133617
66 feet Y = -4917526
66 meter
Z = -9933078
08 Z = -3027602
20
XDOT = 17657
017959 XDOT = 5381
859074
YDOT = -2865
630261 feet/sec YDOT = -873
444104 meter/sec
ZDOT = -16222
311055 ZDOT = -4944
560409
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 19088
52603108
00016717 00000-0 10270-3 0 9008
2 25544 51
6405 37
2364 0001925 124
7236 235
4098 15
52463278 2871
Satellite: ISS
Catalog Number: 25544
Epoch time: 19088
52603108 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 37
2364 deg
Eccentricity:
0001925
Arg of perigee: 124
7236 deg
Mean anomaly: 235
4098 deg
Mean motion: 15
52463278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 287
Checksum: 303
Coasting Arc #2 (Orbit 302)
---------------------------------------
Vector Time (GMT): 2019/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2358470
20 A = 6787720
19 meter
Y = 5043044
30 meter E =
0012906
Z = 3874606
78 I = 51
84403
XDOT = -6453
247083 Wp = 102
99097
YDOT = -173
320554 meter/sec RA = 31
78821 deg
ZDOT = 4139
253817 TA = 303
59904
MA = 303
72215
Ha = 224
144 n
mi
Hp = 216
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7737763
14 X = 2283081
64
Y = 16545420
92 feet Y = 5068997
11 meter
Z = 12711964
51 Z = 3885879
79
XDOT = -21172
070481 XDOT = -6470
935370
YDOT = -568
636988 feet/sec YDOT = -245
583891 meter/sec
ZDOT = 13580
229060 ZDOT = 4107
863689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9531511
55 X = 2905204
72
Y = 15539935
51 feet Y = 4736572
34 meter
Z = 12762392
62 Z = 3889977
27
XDOT = -20050
261878 XDOT = -6111
319820
YDOT = 1222
932150 feet/sec YDOT = 372
749719 meter/sec
ZDOT = 13438
201286 ZDOT = 4095
963752
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 19089
55597148
00016717 00000-0 10270-3 0 9019
2 25544 51
6409 32
1155 0001941 130
6694 229
4627 15
52479468 3037
Satellite: ISS
Catalog Number: 25544
Epoch time: 19089
55597148 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 32
1155 deg
Eccentricity:
0001941
Arg of perigee: 130
6694 deg
Mean anomaly: 229
4627 deg
Mean motion: 15
52479468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 303
Checksum: 320
Coasting Arc #3 (Orbit 317)
---------------------------------------
Vector Time (GMT): 2019/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1464957
26 A = 6785203
92 meter
Y = -4787599
12 meter E =
0011245
Z = -4590206
15 I = 51
80654
XDOT = 6965
026760 Wp = 77
84038
YDOT = 812
118452 meter/sec RA = 26
82544 deg
ZDOT = -3073
974892 TA = 161
45968
MA = 161
41867
Ha = 224
183 n
mi
Hp = 216
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4806290
22 X = -1389015
61
Y = -15707346
18 feet Y = -4803557
05 meter
Z = -15059731
48 Z = -4597137
47
XDOT = 22851
137665 XDOT = 6970
359304
YDOT = 2664
430618 feet/sec YDOT = 890
035819 meter/sec
ZDOT = -10085
219461 ZDOT = -3040
128814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6764668
56 X = -2061870
98
Y = -14937590
08 feet Y = -4552977
46 meter
Z = -15090537
56 Z = -4599595
85
XDOT = 21979
233480 XDOT = 6699
270365
YDOT = 66
882525 feet/sec YDOT = 20
385794 meter/sec
ZDOT = -9932
161541 ZDOT = -3027
322838
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 19090
52153878
00016717 00000-0 10270-3 0 9027
2 25544 51
6407 27
3140 0001916 128
2830 231
8494 15
52475701 3183
Satellite: ISS
Catalog Number: 25544
Epoch time: 19090
52153878 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 27
3140 deg
Eccentricity:
0001916
Arg of perigee: 128
2830 deg
Mean anomaly: 231
8494 deg
Mean motion: 15
52475701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 318
Checksum: 294
Coasting Arc #4 (Orbit 323)
---------------------------------------
Vector Time (GMT): 2019/090/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3525226
03 A = 6788994
89 meter
Y = 4652743
62 meter E =
0013783
Z = 3456389
39 I = 51
80606
XDOT = -6037
380485 Wp = 97
79422
YDOT = 1155
946565 meter/sec RA = 25
08516 deg
ZDOT = 4584
108191 TA = 302
61764
MA = 302
75059
Ha = 224
132 n
mi
Hp = 216
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11565702
21 X = 3456146
65
Y = 15264906
90 feet Y = 4691779
22 meter
Z = 11339860
20 Z = 3473345
29
XDOT = -19807
678756 XDOT = -6072
124767
YDOT = 3792
475607 feet/sec YDOT = 1088
238481 meter/sec
ZDOT = 15039
725036 ZDOT = 4554
696621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2906235
55 X = 885820
60
Y = -18883937
48 feet Y = -5755824
14 meter
Z = 11416040
46 Z = 3479609
13
XDOT = 15238
750589 XDOT = 4644
771180
YDOT = 11391
174706 feet/sec YDOT = 3472
030050 meter/sec
ZDOT = 14906
506807 ZDOT = 4543
503275
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 19090
90776354
00016717 00000-0 10270-3 0 9030
2 25544 51
6379 25
3899 0002204 141
4779 218
6531 15
52482448 3248
Satellite: ISS
Catalog Number: 25544
Epoch time: 19090
90776354 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 25
3899 deg
Eccentricity:
0002204
Arg of perigee: 141
4779 deg
Mean anomaly: 218
6531 deg
Mean motion: 15
52482448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 324
Checksum: 322
Coasting Arc #5 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2019/091/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2664576
12 A = 6786323
02 meter
Y = -4559583
24 meter E =
0009308
Z = -4270767
47 I = 51
76858
XDOT = 6731
556836 Wp = 82
11654
YDOT = -560
193027 meter/sec RA = 20
12273 deg
ZDOT = -3607
300615 TA = 151
06143
MA = 151
00979
Ha = 224
151 n
mi
Hp = 216
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8742047
65 X = -2592646
65
Y = -14959262
60 feet Y = -4588978
63 meter
Z = -14011704
30 Z = -4283535
74
XDOT = 22085
160224 XDOT = 6754
842921
YDOT = -1837
903633 feet/sec YDOT = -484
786203 meter/sec
ZDOT = -11834
975772 ZDOT = -3574
544845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4384672
22 X = -1336448
09
Y = 16714375
15 feet Y = 5094541
55 meter
Z = -14068941
14 Z = -4288213
26
XDOT = -15821
084762 XDOT = -4822
266636
YDOT = -13972
255128 feet/sec YDOT = -4258
743363 meter/sec
ZDOT = -11686
706382 ZDOT = -3562
108105
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 19091
87332552
00016717 00000-0 10270-3 0 9046
2 25544 51
6399 20
5892 0002194 140
4779 219
6533 15
52491190 3390
Satellite: ISS
Catalog Number: 25544
Epoch time: 19091
87332552 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 20
5892 deg
Eccentricity:
0002194
Arg of perigee: 140
4779 deg
Mean anomaly: 219
6533 deg
Mean motion: 15
52491190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 320
Coasting Arc #6 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2019/092/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1698554
36 A = 6784054
08 meter
Y = 4424186
68 meter E =
0008953
Z = 4850187
14 I = 51
72941
XDOT = -7256
916451 Wp = 126
20195
YDOT = 60
260735 meter/sec RA = 15
15216 deg
ZDOT = 2478
077730 TA = 299
44791
MA = 299
53721
Ha = 224
038 n
mi
Hp = 216
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5572684
92 X = 1625396
19
Y = 14515048
15 feet Y = 4442772
57 meter
Z = 15912687
46 Z = 4858259
88
XDOT = -23808
781006 XDOT = -7269
088036
YDOT = 197
705824 feet/sec YDOT = -20
958973 meter/sec
ZDOT = 8130
176280 ZDOT = 2442
796923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6088240
61 X = 1855695
74
Y = -14266311
60 feet Y = -4348371
78 meter
Z = 15948690
91 Z = 4861160
99
XDOT = 16335
895133 XDOT = 4979
180836
YDOT = 15912
518813 feet/sec YDOT = 4850
135734 meter/sec
ZDOT = 7970
555150 ZDOT = 2429
425210
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 19092
90325125
00016717 00000-0 10270-3 0 9050
2 25544 51
6399 15
4668 0002152 147
6231 212
5053 15
52499655 3551
Satellite: ISS
Catalog Number: 25544
Epoch time: 19092
90325125 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 15
4668 deg
Eccentricity:
0002152
Arg of perigee: 147
6231 deg
Mean anomaly: 212
5053 deg
Mean motion: 15
52499655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 355
Checksum: 305
Coasting Arc #7 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2019/093/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -614270
50 A = 6782538
21 meter
Y = -4301073
82 meter E =
0015231
Z = -5221527
39 I = 51
69236
XDOT = 7548
785348 Wp = 88
44360
YDOT = 385
506923 meter/sec RA = 10
17799 deg
ZDOT = -1208
249427 TA = 169
96700
MA = 169
93656
Ha = 224
110 n
mi
Hp = 216
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2015323
17 X = -540765
74
Y = -14111134
58 feet Y = -4307532
62 meter
Z = -17130995
36 Z = -5224332
27
XDOT = 24766
356127 XDOT = 7549
782464
YDOT = 1264
786494 feet/sec YDOT = 469
928166 meter/sec
ZDOT = -3964
072924 ZDOT = -1171
577892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8185580
33 X = -2494964
88
Y = 11651795
90 feet Y = 3551467
39 meter
Z = -17143178
69 Z = -5225240
87
XDOT = -16494
808947 XDOT = -5027
617767
YDOT = -17163
411347 feet/sec YDOT = -5231
407779 meter/sec
ZDOT = -3798
228703 ZDOT = -1157
700109
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 19093
86880312
00016717 00000-0 10270-3 0 9061
2 25544 51
6403 10
6671 0002265 147
1087 213
0206 15
52502871 3705
Satellite: ISS
Catalog Number: 25544
Epoch time: 19093
86880312 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 10
6671 deg
Eccentricity:
0002265
Arg of perigee: 147
1087 deg
Mean anomaly: 213
0206 deg
Mean motion: 15
52502871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 280
Coasting Arc #8 (Orbit 379)
---------------------------------------
Vector Time (GMT): 2019/094/11:01:35
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2612148
20 A = 6784457
39 meter
Y = 4096761
86 meter E =
0009256
Z = 4730731
22 I = 51
68010
XDOT = -7039
198878 Wp = 123
06960
YDOT = 1304
086255 meter/sec RA = 7
16851 deg
ZDOT = 2748
646345 TA = 299
69981
MA = 299
79191
Ha = 223
872 n
mi
Hp = 216
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8570040
03 X = 2543163
59
Y = 13440819
74 feet Y = 4125587
54 meter
Z = 15520771
71 Z = 4743252
08
XDOT = -23094
484507 XDOT = -7066
609803
YDOT = 4278
498211 feet/sec YDOT = 1225
216047 meter/sec
ZDOT = 9017
868586 ZDOT = 2714
385762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7747674
41 X = 2361491
16
Y = 13868254
24 feet Y = 4227043
89 meter
Z = 15576926
58 Z = 4747847
22
XDOT = -22335
974896 XDOT = -6808
005148
YDOT = 2491
137652 feet/sec YDOT = 759
298756 meter/sec
ZDOT = 8862
741723 ZDOT = 2701
363677
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 19094
51250082
00016717 00000-0 10270-3 0 9070
2 25544 51
6414 7
4703 0001799 149
3893 210
7364 15
52519945 3807
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
51250082 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 7
4703 deg
Eccentricity:
0001799
Arg of perigee: 149
3893 deg
Mean anomaly: 210
7364 deg
Mean motion: 15
52519945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 380
Checksum: 311
Coasting Arc #9 (Orbit 381)
---------------------------------------
Vector Time (GMT): 2019/094/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4936316
05 A = 6787658
95 meter
Y = 2541122
23 meter E =
0012071
Z = 3894732
90 I = 51
68747
XDOT = -5220
747565 Wp = 88
07814
YDOT = -3845
008674 meter/sec RA = 6
42140 deg
ZDOT = -4096
907951 TA = 44
87496
MA = 44
77743
Ha = 223
996 n
mi
Hp = 216
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16195262
63 X = -4983283
23
Y = 8337015
20 feet Y = 2485658
71 meter
Z = 12777995
09 Z = 3870639
71
XDOT = -17128
436894 XDOT = -5157
463008
YDOT = -12614
857854 feet/sec YDOT = -3903
037336 meter/sec
ZDOT = -13441
299053 ZDOT = -4122
114321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4703580
97 X = -1433651
48
Y = 17676240
90 feet Y = 5387718
23 meter
Z = 12668715
26 Z = 3861424
41
XDOT = -19488
479983 XDOT = -5940
088699
YDOT = 4556
029440 feet/sec YDOT = 1388
677773 meter/sec
ZDOT = -13554
862903 ZDOT = -4131
522213
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 19094
64123971
00016717 00000-0 10270-3 0 9081
2 25544 51
6429 6
8310 0001607 146
3701 213
7553 15
52531483 3829
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
64123971 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 6
8310 deg
Eccentricity:
0001607
Arg of perigee: 146
3701 deg
Mean anomaly: 213
7553 deg
Mean motion: 15
52531483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 382
Checksum: 294
Coasting Arc #10 (Orbit 396)
---------------------------------------
Vector Time (GMT): 2019/095/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5656873
79 A = 6790313
45 meter
Y = -2242934
01 meter E =
0004859
Z = -3016674
74 I = 51
66282
XDOT = 4234
014952 Wp = 86
33247
YDOT = 4025
899605 meter/sec RA = 1
45251 deg
ZDOT = 4953
525142 TA = 239
17846
MA = 239
22628
Ha = 223
876 n
mi
Hp = 217
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18559297
20 X = 5696187
91
Y = -7358707
40 feet Y = -2179455
39 meter
Z = -9897226
85 Z = -2989099
87
XDOT = 13891
125169 XDOT = 4164
619877
YDOT = 13208
332037 feet/sec YDOT = 4072
859827 meter/sec
ZDOT = 16251
722906 ZDOT = 4973
923570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6676236
81 X = 2034916
98
Y = -18880790
97 feet Y = -5754865
09 meter
Z = -9772245
45 Z = -2978580
41
XDOT = 17635
282430 XDOT = 5375
234085
YDOT = -2210
803563 feet/sec YDOT = -673
852926 meter/sec
ZDOT = 16343
506833 ZDOT = 4981
500883
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 19095
60678350
00016717 00000-0 10270-3 0 9095
2 25544 51
6429 2
0296 0001547 155
8552 204
2673 15
52499570 3976
Satellite: ISS
Catalog Number: 25544
Epoch time: 19095
60678350 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 2
0296 deg
Eccentricity:
0001547
Arg of perigee: 155
8552 deg
Mean anomaly: 204
2673 deg
Mean motion: 15
52499570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 397
Checksum: 325
Coasting Arc #11 (Orbit 412)
---------------------------------------
Vector Time (GMT): 2019/096/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6202251
06 A = 6792470
93 meter
Y = 1932878
02 meter E =
0015157
Z = 1957036
37 I = 51
63699
XDOT = -3094
319487 Wp = 116
26706
YDOT = -4242
519785 meter/sec RA = 356
48581 deg
ZDOT = -5589
373095 TA = 42
14877
MA = 42
03231
Ha = 223
888 n
mi
Hp = 216
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20348592
71 X = -6232910
38
Y = 6341463
33 feet Y = 1863348
86 meter
Z = 6420723
00 Z = 1926833
21
XDOT = -10151
966820 XDOT = -3019
498095
YDOT = -13919
028165 feet/sec YDOT = -4276
704788 meter/sec
ZDOT = -18337
838237 ZDOT = -5604
222177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8265641
02 X = -2519367
38
Y = 19690017
83 feet Y = 6001517
44 meter
Z = 6283903
43 Z = 1915333
77
XDOT = -15673
111523 XDOT = -4777
164392
YDOT = -676
851949 feet/sec YDOT = -206
304474 meter/sec
ZDOT = -18404
489534 ZDOT = -5609
688410
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 19096
63669105
00016717 00000-0 10270-3 0 9109
2 25544 51
6429 356
9078 0001572 154
1038 206
0193 15
52516221 4133
Satellite: ISS
Catalog Number: 25544
Epoch time: 19096
63669105 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 356
9078 deg
Eccentricity:
0001572
Arg of perigee: 154
1038 deg
Mean anomaly: 206
0193 deg
Mean motion: 15
52516221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 413
Checksum: 296
Coasting Arc #12 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2019/097/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6535364
13 A = 6793756
38 meter
Y = -1642771
55 meter E =
0009605
Z = -834253
46 I = 51
60629
XDOT = 1875
590430 Wp = 47
10875
YDOT = 4473
795810 meter/sec RA = 351
51994 deg
ZDOT = 5933
114912 TA = 303
87233
MA = 303
96369
Ha = 223
814 n
mi
Hp = 216
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21441483
35 X = 6557300
73
Y = -5389670
44 feet Y = -1569565
94 meter
Z = -2737052
03 Z = -802453
31
XDOT = 6153
511909 XDOT = 1796
603627
YDOT = 14677
807776 feet/sec YDOT = 4494
328768 meter/sec
ZDOT = 19465
600104 ZDOT = 5942
033768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9338086
44 X = 2846248
75
Y = -20058748
95 feet Y = -6113906
68 meter
Z = -2593056
47 Z = -790363
61
XDOT = 13730
504054 XDOT = 4185
057636
YDOT = 3892
790846 feet/sec YDOT = 1186
522650 meter/sec
ZDOT = 19505
399829 ZDOT = 5945
245868
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 19097
60222457
00016717 00000-0 10270-3 0 9113
2 25544 51
6410 352
1062 0001534 160
5151 199
6060 15
52514489 4289
Satellite: ISS
Catalog Number: 25544
Epoch time: 19097
60222457 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 352
1062 deg
Eccentricity:
0001534
Arg of perigee: 160
5151 deg
Mean anomaly: 199
6060 deg
Mean motion: 15
52514489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 428
Checksum: 286
Coasting Arc #13 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2019/097/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1994451
37 A = 6782432
65 meter
Y = -3862389
67 meter E =
0014674
Z = -5219038
85 I = 51
56045
XDOT = 7247
436827 Wp = 89
24625
YDOT = -2172
152105 meter/sec RA = 350
33423 deg
ZDOT = -1164
735122 TA = 169
56787
MA = 169
53739
Ha = 223
868 n
mi
Hp = 216
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6543475
64 X = -1925761
28
Y = -12671882
13 feet Y = -3884309
31 meter
Z = -17122830
88 Z = -5228560
17
XDOT = 23777
679880 XDOT = 7276
845515
YDOT = -7126
483284 feet/sec YDOT = -2090
941840 meter/sec
ZDOT = -3821
309457 ZDOT = -1129
457751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3720493
61 X = -1134006
45
Y = 13714629
62 feet Y = 4180219
11 meter
Z = -17165426
56 Z = -5232022
02
XDOT = -21443
516126 XDOT = -6535
983715
YDOT = -10389
144163 feet/sec YDOT = -3166
611141 meter/sec
ZDOT = -3661
529868 ZDOT = -1116
034304
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 19097
85970116
00016717 00000-0 10270-3 0 9123
2 25544 51
6408 350
8221 0002139 163
3124 196
8099 15
52528109 4321
Satellite: ISS
Catalog Number: 25544
Epoch time: 19097
85970116 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 350
8221 deg
Eccentricity:
0002139
Arg of perigee: 163
3124 deg
Mean anomaly: 196
8099 deg
Mean motion: 15
52528109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 308
Coasting Arc #14 (Orbit 447)
---------------------------------------
Vector Time (GMT): 2019/098/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 889337
56 A = 6781988
26 meter
Y = 4125847
74 meter E =
0003244
Z = 5306161
17 I = 51
52708
XDOT = -7449
179522 Wp = 119
00278
YDOT = 1813
918540 meter/sec RA = 345
34422 deg
ZDOT = -163
374084 TA = 332
54797
MA = 332
56511
Ha = 223
729 n
mi
Hp = 216
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2917774
16 X = 817360
33
Y = 13536245
88 feet Y = 4135390
74 meter
Z = 17408665
27 Z = 5310306
28
XDOT = -24439
565361 XDOT = -7468
116043
YDOT = 5951
176311 feet/sec YDOT = 1730
510713 meter/sec
ZDOT = -536
004213 ZDOT = -199
605978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6786150
39 X = 2068418
64
Y = -12043908
53 feet Y = -3670983
32 meter
Z = 17426916
40 Z = 5311724
12
XDOT = 21449
601708 XDOT = 6537
838601
YDOT = 11079
811291 feet/sec YDOT = 3377
126481 meter/sec
ZDOT = -700
046607 ZDOT = -213
374206
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 19098
88959851
00016717 00000-0 10270-3 0 9131
2 25544 51
6414 345
6996 0002060 169
3602 190
7594 15
52540173 4484
Satellite: ISS
Catalog Number: 25544
Epoch time: 19098
88959851 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 345
6996 deg
Eccentricity:
0002060
Arg of perigee: 169
3602 deg
Mean anomaly: 190
7594 deg
Mean motion: 15
52540173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 448
Checksum: 339
Coasting Arc #15 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2019/099/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 213387
85 A = 6782732
96 meter
Y = -4425222
07 meter E =
0014553
Z = -5148878
99 I = 51
49819
XDOT = 7381
231601 Wp = 108
75895
YDOT = -1377
575392 meter/sec RA = 340
35372 deg
ZDOT = 1488
746795 TA = 175
63700
MA = 175
62430
Ha = 223
755 n
mi
Hp = 216
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 700091
36 X = 287866
78
Y = -14518445
12 feet Y = -4422419
52 meter
Z = -16892647
61 Z = -5147661
40
XDOT = 24216
639112 XDOT = 7388
855858
YDOT = -4519
604303 feet/sec YDOT = -1294
990626 meter/sec
ZDOT = 4884
339878 ZDOT = 1524
621042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9975181
26 X = -3040435
25
Y = 10581819
56 feet Y = 3225338
60 meter
Z = -16886615
22 Z = -5147040
32
XDOT = -20636
861682 XDOT = -6290
115441
YDOT = -11394
318619 feet/sec YDOT = -3472
988315 meter/sec
ZDOT = 5046
704546 ZDOT = 1538
235546
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 19099
85512356
00016717 00000-0 10270-3 0 9145
2 25544 51
6419 340
8990 0002073 169
1179 191
0018 15
52553148 4639
Satellite: ISS
Catalog Number: 25544
Epoch time: 19099
85512356 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 340
8990 deg
Eccentricity:
0002073
Arg of perigee: 169
1179 deg
Mean anomaly: 191
0018 deg
Mean motion: 15
52553148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 318
Coasting Arc #16 (Orbit 478)
---------------------------------------
Vector Time (GMT): 2019/100/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1259741
86 A = 6784623
16 meter
Y = 4707633
32 meter E =
0007578
Z = 4714699
41 I = 51
47276
XDOT = -7109
358144 Wp = 77
93637
YDOT = 854
165899 meter/sec RA = 335
36234 deg
ZDOT = -2747
171660 TA = 39
34108
MA = 39
28605
Ha = 223
817 n
mi
Hp = 217
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4133011
36 X = -1335191
92
Y = 15444991
20 feet Y = 4693124
19 meter
Z = 15468173
92 Z = 4708396
70
XDOT = -23324
665826 XDOT = -7105
036933
YDOT = 2802
381557 feet/sec YDOT = 774
688214 meter/sec
ZDOT = -9013
030381 ZDOT = -2781
696081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13032157
69 X = 3972201
66
Y = -9310768
74 feet Y = -2837922
31 meter
Z = 15439118
88 Z = 4705843
43
XDOT = 19137
807273 XDOT = 5833
203657
YDOT = 11553
659099 feet/sec YDOT = 3521
555293 meter/sec
ZDOT = -9169
223292 ZDOT = -2794
779260
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 19100
88501403
00016717 00000-0 10270-3 0 9153
2 25544 51
6415 335
7770 0002065 170
0693 190
0500 15
52519478 4797
Satellite: ISS
Catalog Number: 25544
Epoch time: 19100
88501403 = yrday
fracday
Element set: 915
Inclination: 51
6415 deg
RA of node: 335
7770 deg
Eccentricity:
0002065
Arg of perigee: 170
0693 deg
Mean anomaly: 190
0500 deg
Mean motion: 15
52519478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 479
Checksum: 294
Coasting Arc #17 (Orbit 493)
---------------------------------------
Vector Time (GMT): 2019/101/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2199776
56 A = 6787004
63 meter
Y = -4977216
09 meter E =
0008027
Z = -4065083
65 I = 51
45159
XDOT = 6611
997634 Wp = 121
59559
YDOT = -225
660861 meter/sec RA = 330
37408 deg
ZDOT = 3855
822099 TA = 188
47657
MA = 188
49013
Ha = 223
641 n
mi
Hp = 217
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7217114
70 X = 2275015
73
Y = -16329449
10 feet Y = -4952195
97 meter
Z = -13336888
63 Z = -4054215
15
XDOT = 21692
905623 XDOT = 6595
300088
YDOT = -740
357157 feet/sec YDOT = -151
814226 meter/sec
ZDOT = 12650
334969 ZDOT = 3887
900305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15830745
23 X = -4825211
15
Y = 8333608
02 feet Y = 2540083
73 meter
Z = -13287164
24 Z = -4049927
66
XDOT = -16845
146021 XDOT = -5134
400507
YDOT = -11606
386332 feet/sec YDOT = -3537
626554 meter/sec
ZDOT = 12795
389130 ZDOT = 3900
034607
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 19101
85053157
00016717 00000-0 10270-3 0 9160
2 25544 51
6419 330
9763 0002027 179
2871 180
8284 15
52545438 4945
Satellite: ISS
Catalog Number: 25544
Epoch time: 19101
85053157 = yrday
fracday
Element set: 916
Inclination: 51
6419 deg
RA of node: 330
9763 deg
Eccentricity:
0002027
Arg of perigee: 179
2871 deg
Mean anomaly: 180
8284 deg
Mean motion: 15
52545438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 494
Checksum: 319
Coasting Arc #18 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2019/101/23:12:30
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 128559
80 A = 6783605
60 meter
Y = -4646109
76 meter E =
0012977
Z = -4953168
77 I = 51
43521
XDOT = 7035
449885 Wp = 113
13315
YDOT = -2108
330239 meter/sec RA = 329
75868 deg
ZDOT = 2159
763760 TA = 178
01931
MA = 178
01417
Ha = 223
626 n
mi
Hp = 217
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 421784
11 X = 204564
21
Y = -15243142
24 feet Y = -4644247
16 meter
Z = -16250553
70 Z = -4952359
65
XDOT = 23082
184663 XDOT = 7048
011966
YDOT = -6917
093961 feet/sec YDOT = -2029
584670 meter/sec
ZDOT = 7085
839109 ZDOT = 2193
970005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1361830
52 X = 415085
94
Y = 15192543
28 feet Y = 4630687
19 meter
Z = -16246348
17 Z = -4951886
92
XDOT = -20892
156151 XDOT = -6367
929195
YDOT = 9617
364429 feet/sec YDOT = 2931
372678 meter/sec
ZDOT = 7240
735656 ZDOT = 2206
976228
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 19101
97926672
00016717 00000-0 10270-3 0 9175
2 25544 51
6405 330
3377 0001760 178
2919 181
8239 15
52538134 4968
Satellite: ISS
Catalog Number: 25544
Epoch time: 19101
97926672 = yrday
fracday
Element set: 917
Inclination: 51
6405 deg
RA of node: 330
3377 deg
Eccentricity:
0001760
Arg of perigee: 178
2919 deg
Mean anomaly: 181
8239 deg
Mean motion: 15
52538134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 327
Coasting Arc #19 (Orbit 511)
---------------------------------------
Vector Time (GMT): 2019/102/23:12:30
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1085721
69 A = 6785697
28 meter
Y = 5054145
41 meter E =
0008887
Z = 4389018
88 I = 51
41518
XDOT = -6734
754568 Wp = 80
24389
YDOT = 1476
231380 meter/sec RA = 324
76503 deg
ZDOT = -3358
643415 TA = 43
86443
MA = 43
79389
Ha = 223
479 n
mi
Hp = 217
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3562079
03 X = -1163477
31
Y = 16581841
91 feet Y = 5041569
39 meter
Z = 14399668
25 Z = 4383555
95
XDOT = -22095
651469 XDOT = -6734
447235
YDOT = 4843
278807 feet/sec YDOT = 1400
920332 meter/sec
ZDOT = -11019
171310 ZDOT = -3391
357608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1285020
55 X = 391674
27
Y = -16932873
11 feet Y = -5161139
72 meter
Z = 14374382
22 Z = 4381311
70
XDOT = 19884
390959 XDOT = 6060
762364
YDOT = -7991
253653 feet/sec YDOT = -2435
734113 meter/sec
ZDOT = -11167
242101 ZDOT = -3403
775393
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 19103
00914739
00016717 00000-0 10270-3 0 9183
2 25544 51
6413 325
2159 0001682 186
0741 174
0391 15
52580656 5129
Satellite: ISS
Catalog Number: 25544
Epoch time: 19103
00914739 = yrday
fracday
Element set: 918
Inclination: 51
6413 deg
RA of node: 325
2159 deg
Eccentricity:
0001682
Arg of perigee: 186
0741 deg
Mean anomaly: 174
0391 deg
Mean motion: 15
52580656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 512
Checksum: 296
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