[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 22nd 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15204 0235 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
297/21:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 220
7
301/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 221
1
304/19:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
3
000/00:00:00
000 0
0 0
0 221
8
305/15:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
2
000/00:00:00
000 0
0 0
0 221
9
306/13:59:43
634 0
0 0
0 0
0
N/A 0
0 0
0 227
0
000/00:00:00
000 0
0 0
0 222
1
308/07:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 222
3
308/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 222
3
Coasting Arc #1 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2019/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4195144
43 A = 6789045
09 meter
Y = 471044
62 meter E =
0008964
Z = 5314659
72 I = 52
00424
XDOT = 9
192098 Wp = 156
39807
YDOT = -7634
592006 meter/sec RA = 94
03245 deg
ZDOT = 675
535992 TA = 287
13125
MA = 287
22939
Ha = 228
867 n
mi
Hp = 220
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13763597
22 X = -4225915
99
Y = 1545421
98 feet Y = 423959
49 meter
Z = 17436547
63 Z = 5294206
28
XDOT = 30
157802 XDOT = 91
282217
YDOT = -25047
874034 feet/sec YDOT = -7634
030220 meter/sec
ZDOT = 2216
325433 ZDOT = 675
780011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11425439
24 X = 3482473
88
Y = -8033109
96 feet Y = -2448491
92 meter
Z = 17343200
78 Z = 5286207
60
XDOT = 11449
944811 XDOT = 3489
943178
YDOT = 21133
427267 feet/sec YDOT = 6441
468631 meter/sec
ZDOT = 2217
984200 ZDOT = 676
041584
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 19294
54952117
00016717 00000-0 10270-3 0 9006
2 25544 51
6383 94
6997 0006932 172
8938 187
2312 15
50172118 34855
Satellite: ISS
Catalog Number: 25544
Epoch time: 19294
54952117 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 94
6997 deg
Eccentricity:
0006932
Arg of perigee: 172
8938 deg
Mean anomaly: 187
2312 deg
Mean motion: 15
50172118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 335
Coasting Arc #2 (Orbit 3499)
---------------------------------------
Vector Time (GMT): 2019/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4178930
52 A = 6788776
33 meter
Y = -290005
40 meter E =
0016570
Z = -5355182
31 I = 52
00635
XDOT = 278
850605 Wp = 113
47989
YDOT = 7643
304738 meter/sec RA = 89
09983 deg
ZDOT = -203
221709 TA = 154
62940
MA = 154
54795
Ha = 228
611 n
mi
Hp = 220
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13710401
97 X = 4207875
63
Y = -951461
27 feet Y = -243111
88 meter
Z = -17569495
78 Z = -5334812
12
XDOT = 914
864188 XDOT = 194
347377
YDOT = 25076
459113 feet/sec YDOT = 7645
950552 meter/sec
ZDOT = -666
737890 ZDOT = -202
072492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11534797
64 X = -3515806
32
Y = 7686788
33 feet Y = 2342933
08 meter
Z = -17476536
03 Z = -5326848
18
XDOT = -12676
958245 XDOT = -3863
936873
YDOT = -20476
489242 feet/sec YDOT = -6241
233921 meter/sec
ZDOT = -662
054258 ZDOT = -201
794138
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 19295
51649028
00016717 00000-0 10270-3 0 9019
2 25544 51
6396 89
9086 0007014 176
9346 183
1849 15
50219844 35001
Satellite: ISS
Catalog Number: 25544
Epoch time: 19295
51649028 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 89
9086 deg
Eccentricity:
0007014
Arg of perigee: 176
9346 deg
Mean anomaly: 183
1849 deg
Mean motion: 15
50219844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3500
Checksum: 334
Coasting Arc #3 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2019/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4181400
49 A = 6788881
11 meter
Y = 145108
62 meter E =
0006858
Z = 5344050
71 I = 52
00493
XDOT = -581
390629 Wp = 159
24220
YDOT = -7638
264505 meter/sec RA = 84
16523 deg
ZDOT = -253
636390 TA = 293
12833
MA = 293
20058
Ha = 228
655 n
mi
Hp = 220
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13718505
53 X = -4208671
05
Y = 476078
16 feet Y = 98196
96 meter
Z = 17532974
78 Z = 5323672
60
XDOT = -1907
449569 XDOT = -494
702091
YDOT = -25059
922916 feet/sec YDOT = -7644
281328 meter/sec
ZDOT = -832
140386 ZDOT = -256
249777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11650509
09 X = 3551075
17
Y = -7479422
76 feet Y = -2279728
06 meter
Z = 17439986
30 Z = 5315707
82
XDOT = 13892
954312 XDOT = 4234
572474
YDOT = 19721
108855 feet/sec YDOT = 6010
993979 meter/sec
ZDOT = -843
492683 ZDOT = -257
096570
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 19296
54792400
00016717 00000-0 10270-3 0 9027
2 25544 51
6398 84
7958 0006924 180
4172 179
6974 15
50182387 35167
Satellite: ISS
Catalog Number: 25544
Epoch time: 19296
54792400 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 84
7958 deg
Eccentricity:
0006924
Arg of perigee: 180
4172 deg
Mean anomaly: 179
6974 deg
Mean motion: 15
50182387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 348
Coasting Arc #4 (Orbit 3530)
---------------------------------------
Vector Time (GMT): 2019/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4235535
55 A = 6788914
49 meter
Y = 31802
78 meter E =
0016308
Z = -5318488
17 I = 52
00163
XDOT = 862
244708 Wp = 120
63469
YDOT = 7567
599831 meter/sec RA = 79
23213 deg
ZDOT = 725
508280 TA = 156
31415
MA = 156
23899
Ha = 228
363 n
mi
Hp = 220
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13896114
02 X = 4260699
70
Y = 104339
83 feet Y = 79307
94 meter
Z = -17449108
17 Z = -5297852
17
XDOT = 2828
886836 XDOT = 774
033368
YDOT = 24828
083436 feet/sec YDOT = 7576
748880 meter/sec
ZDOT = 2380
276509 ZDOT = 729
482121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11975828
37 X = -3650232
49
Y = 7278000
71 feet Y = 2218334
62 meter
Z = -17354955
72 Z = -5289790
50
XDOT = -14912
513344 XDOT = -4545
334067
YDOT = -18770
002771 feet/sec YDOT = -5721
096845 meter/sec
ZDOT = 2397
829066 ZDOT = 730
858299
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 19297
51488809
00016717 00000-0 10270-3 0 9031
2 25544 51
6405 80
0045 0006909 183
9498 176
1599 15
50229504 35319
Satellite: ISS
Catalog Number: 25544
Epoch time: 19297
51488809 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 80
0045 deg
Eccentricity:
0006909
Arg of perigee: 183
9498 deg
Mean anomaly: 176
1599 deg
Mean motion: 15
50229504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3531
Checksum: 334
Coasting Arc #5 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2019/297/21:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3018458
07 A = 6791030
54 meter
Y = 3711524
71 meter E =
0011548
Z = 4819043
59 I = 52
00425
XDOT = -3521
748399 Wp = 149
76769
YDOT = -6280
523503 meter/sec RA = 77
22438 deg
ZDOT = 2618
812697 TA = 274
46267
MA = 274
59459
Ha = 228
234 n
mi
Hp = 220
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9903077
66 X = -3083145
63
Y = 12176918
32 feet Y = 3677408
78 meter
Z = 15810510
47 Z = 4804223
52
XDOT = -11554
292648 XDOT = -3463
976923
YDOT = -20605
392069 feet/sec YDOT = -6319
582998 meter/sec
ZDOT = 8591
905174 ZDOT = 2601
845847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9823971
36 X = -2994346
47
Y = 12328036
75 feet Y = 3757585
60 meter
Z = 15742605
41 Z = 4798346
13
XDOT = -11023
720920 XDOT = -3360
030136
YDOT = -19710
303398 feet/sec YDOT = -6007
700476 meter/sec
ZDOT = 8514
976417 ZDOT = 2595
364812
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 19297
96613744
00016717 00000-0 10270-3 0 9049
2 25544 51
6389 77
7716 0006465 186
4087 173
6982 15
50208468 35388
Satellite: ISS
Catalog Number: 25544
Epoch time: 19297
96613744 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 77
7716 deg
Eccentricity:
0006465
Arg of perigee: 186
4087 deg
Mean anomaly: 173
6982 deg
Mean motion: 15
50208468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 361
Coasting Arc #6 (Orbit 3552)
---------------------------------------
Vector Time (GMT): 2019/298/21:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2973873
85 A = 6790306
78 meter
Y = -3520464
11 meter E =
0011326
Z = -4995482
29 I = 51
99339
XDOT = 3792
208116 Wp = 105
18028
YDOT = 6282
810083 meter/sec RA = 72
29077 deg
ZDOT = -2177
122170 TA = 143
69887
MA = 143
62198
Ha = 228
129 n
mi
Hp = 220
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9756803
98 X = 3037285
39
Y = -11550079
09 feet Y = -3486853
95 meter
Z = -16389377
59 Z = -4980881
80
XDOT = 12441
627676 XDOT = 3732
245502
YDOT = 20612
893974 feet/sec YDOT = 6324
881807 meter/sec
ZDOT = -7142
789271 ZDOT = -2158
846803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9488441
26 X = 2892076
90
Y = -11864116
31 feet Y = -3616182
65 meter
Z = -16322483
74 Z = -4975093
04
XDOT = 12284
476547 XDOT = 3744
308451
YDOT = 19505
867358 feet/sec YDOT = 5945
388371 meter/sec
ZDOT = -7059
904846 ZDOT = -2151
858997
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 19298
93310141
00016717 00000-0 10270-3 0 9053
2 25544 51
6390 72
9792 0006465 189
4465 170
6565 15
50212859 35534
Satellite: ISS
Catalog Number: 25544
Epoch time: 19298
93310141 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 72
9792 deg
Eccentricity:
0006465
Arg of perigee: 189
4465 deg
Mean anomaly: 170
6565 deg
Mean motion: 15
50212859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3553
Checksum: 331
Coasting Arc #7 (Orbit 3568)
---------------------------------------
Vector Time (GMT): 2019/299/21:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2935802
11 A = 6789746
36 meter
Y = 3357962
93 meter E =
0009591
Z = 5119195
94 I = 51
98098
XDOT = -4082
831419 Wp = 163
43182
YDOT = -6244
352086 meter/sec RA = 67
35696 deg
ZDOT = 1744
809242 TA = 269
71154
MA = 269
82145
Ha = 227
973 n
mi
Hp = 221
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9631896
68 X = -2998000
41
Y = 11016938
75 feet Y = 3324785
29 meter
Z = 16795262
26 Z = 5104783
29
XDOT = -13395
116204 XDOT = -4021
177324
YDOT = -20486
719441 feet/sec YDOT = -6289
664345 meter/sec
ZDOT = 5724
439771 ZDOT = 1725
126086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9187347
84 X = -2800303
62
Y = 11487063
34 feet Y = 3501256
91 meter
Z = 16729232
59 Z = 5099070
09
XDOT = -13593
948283 XDOT = -4143
435437
YDOT = -19125
959553 feet/sec YDOT = -5829
592472 meter/sec
ZDOT = 5635
147116 ZDOT = 1717
592841
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 19299
96452782
00016717 00000-0 10270-3 0 9066
2 25544 51
6396 67
8679 0006424 194
4924 165
6044 15
50217016 35691
Satellite: ISS
Catalog Number: 25544
Epoch time: 19299
96452782 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 67
8679 deg
Eccentricity:
0006424
Arg of perigee: 194
4924 deg
Mean anomaly: 165
6044 deg
Mean motion: 15
50217016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3569
Checksum: 351
Coasting Arc #8 (Orbit 3583)
---------------------------------------
Vector Time (GMT): 2019/300/21:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2962507
21 A = 6789270
00 meter
Y = -3168695
05 meter E =
0012507
Z = -5232376
02 I = 51
96654
XDOT = 4349
267823 Wp = 107
01102
YDOT = 6167
028595 meter/sec RA = 62
42095 deg
ZDOT = -1278
289044 TA = 150
78224
MA = 150
71223
Ha = 227
826 n
mi
Hp = 221
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9719511
86 X = 3023136
98
Y = -10395981
14 feet Y = -3135227
46 meter
Z = -17166587
98 Z = -5217837
46
XDOT = 14269
251388 XDOT = 4286
192458
YDOT = 20233
033447 feet/sec YDOT = 6215
312440 meter/sec
ZDOT = -4193
861694 ZDOT = -1257
314859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9119731
99 X = 2779694
31
Y = -11029859
71 feet Y = -3361901
24 meter
Z = -17099993
01 Z = -5212077
87
XDOT = 14810
618416 XDOT = 4514
276493
YDOT = 18569
072839 feet/sec YDOT = 5659
853401 meter/sec
ZDOT = -4098
692758 ZDOT = -1249
281553
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 19300
93148700
00016717 00000-0 10270-3 0 9079
2 25544 51
6407 63
0754 0006324 197
5261 162
5672 15
50220942 35845
Satellite: ISS
Catalog Number: 25544
Epoch time: 19300
93148700 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 63
0754 deg
Eccentricity:
0006324
Arg of perigee: 197
5261 deg
Mean anomaly: 162
5672 deg
Mean motion: 15
50220942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3584
Checksum: 298
Coasting Arc #9 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2019/301/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3177169
72 A = 6800592
13 meter
Y = 6000558
98 meter E =
0007744
Z = 352790
49 I = 51
99750
XDOT = -4321
451169 Wp = 75
52863
YDOT = 1927
757247 meter/sec RA = 59
77296 deg
ZDOT = 6020
792758 TA = 288
24705
MA = 288
33132
Ha = 227
835 n
mi
Hp = 221
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10423785
18 X = 3108119
89
Y = 19686873
28 feet Y = 6035702
26 meter
Z = 1157449
11 Z = 368056
50
XDOT = -14177
989398 XDOT = -4371
933240
YDOT = 6324
662885 feet/sec YDOT = 1879
149682 meter/sec
ZDOT = 19753
257079 ZDOT = 5999
677479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15675582
27 X = -4777917
48
Y = -15822123
38 feet Y = -4822583
21 meter
Z = 1226579
73 Z = 373861
50
XDOT = 10708
845714 XDOT = 3264
056174
YDOT = -9059
764931 feet/sec YDOT = -2761
416351 meter/sec
ZDOT = 19656
760733 ZDOT = 5991
380671
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 19301
51166199
00016717 00000-0 10270-3 0 9087
2 25544 51
6422 60
1967 0006765 198
5320 161
5585 15
50240572 35935
Satellite: ISS
Catalog Number: 25544
Epoch time: 19301
51166199 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 60
1967 deg
Eccentricity:
0006765
Arg of perigee: 198
5320 deg
Mean anomaly: 161
5585 deg
Mean motion: 15
50240572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3593
Checksum: 316
Coasting Arc #10 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2019/302/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3367667
61 A = 6800365
59 meter
Y = -5845274
53 meter E =
0014618
Z = -783201
30 I = 51
97840
XDOT = 4463
036778 Wp = 164
09336
YDOT = -1776
117555 meter/sec RA = 54
84395 deg
ZDOT = -5974
755199 TA = 24
32451
MA = 24
25558
Ha = 227
665 n
mi
Hp = 221
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11048778
25 X = -3298249
29
Y = -19177409
88 feet Y = -5882546
03 meter
Z = -2569558
05 Z = -799391
98
XDOT = 14642
509113 XDOT = 4511
589031
YDOT = -5827
157333 feet/sec YDOT = -1725
937305 meter/sec
ZDOT = -19602
215221 ZDOT = -5952
956860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16375261
44 X = 4991179
69
Y = 14876728
88 feet Y = 4534426
96 meter
Z = -2642901
69 Z = -805556
44
XDOT = -11194
135487 XDOT = -3411
972497
YDOT = 8879
666114 feet/sec YDOT = 2706
522232 meter/sec
ZDOT = -19502
612786 ZDOT = -5944
396377
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 19302
47861954
00016717 00000-0 10270-3 0 9095
2 25544 51
6416 55
4052 0006713 202
9086 157
1766 15
50246610 36080
Satellite: ISS
Catalog Number: 25544
Epoch time: 19302
47861954 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 55
4052 deg
Eccentricity:
0006713
Arg of perigee: 202
9086 deg
Mean anomaly: 157
1766 deg
Mean motion: 15
50246610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 309
Coasting Arc #11 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2019/303/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3561661
51 A = 6800015
59 meter
Y = 5668198
21 meter E =
0008716
Z = 1182316
47 I = 51
95868
XDOT = -4613
925594 Wp = 82
14509
YDOT = 1664
873544 meter/sec RA = 49
91321 deg
ZDOT = 5881
628849 TA = 290
61306
MA = 290
70652
Ha = 227
547 n
mi
Hp = 221
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11685241
18 X = 3492270
17
Y = 18596450
83 feet Y = 5707639
21 meter
Z = 3878991
03 Z = 1199449
71
XDOT = -15137
551161 XDOT = -4660
770243
YDOT = 5462
183542 feet/sec YDOT = 1613
015349 meter/sec
ZDOT = 19296
682577 ZDOT = 5859
101762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17035369
68 X = -5192380
68
Y = -13840543
58 feet Y = -4218597
68 meter
Z = 3956633
60 Z = 1205981
92
XDOT = 11678
968109 XDOT = 3559
749480
YDOT = -8854
840398 feet/sec YDOT = -2698
955353 meter/sec
ZDOT = 19193
762264 ZDOT = 5850
258738
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 19303
51003849
00016717 00000-0 10270-3 0 9104
2 25544 51
6432 50
2942 0006760 206
5166 153
5640 15
50248925 36240
Satellite: ISS
Catalog Number: 25544
Epoch time: 19303
51003849 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 50
2942 deg
Eccentricity:
0006760
Arg of perigee: 206
5166 deg
Mean anomaly: 153
5640 deg
Mean motion: 15
50248925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 288
Coasting Arc #12 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2019/304/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3697007
13 A = 6799507
52 meter
Y = -5467960
41 meter E =
0012048
Z = -1601826
79 I = 51
93501
XDOT = 4809
087567 Wp = 172
51223
YDOT = -1569
429290 meter/sec RA = 44
98090 deg
ZDOT = -5758
457287 TA = 24
91822
MA = 24
86010
Ha = 227
358 n
mi
Hp = 221
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12129288
49 X = -3627807
07
Y = -17939502
65 feet Y = -5508915
98 meter
Z = -5255337
22 Z = -1619617
99
XDOT = 15777
846349 XDOT = 4854
252007
YDOT = -5149
046227 feet/sec YDOT = -1515
397956 meter/sec
ZDOT = -18892
576402 ZDOT = -5734
986342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17457353
74 X = 5321001
42
Y = 12780141
60 feet Y = 3895387
16 meter
Z = -5335985
87 Z = -1626408
49
XDOT = -12286
692319 XDOT = -3744
983819
YDOT = 8962
254182 feet/sec YDOT = 2731
695075 meter/sec
ZDOT = -18785
356148 ZDOT = -5725
776554
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 19304
47699158
00016717 00000-0 10270-3 0 9115
2 25544 51
6435 45
5026 0006638 210
3962 149
6805 15
50250990 36394
Satellite: ISS
Catalog Number: 25544
Epoch time: 19304
47699158 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 45
5026 deg
Eccentricity:
0006638
Arg of perigee: 210
3962 deg
Mean anomaly: 149
6805 deg
Mean motion: 15
50250990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 323
Coasting Arc #13 (Orbit 3644)
---------------------------------------
Vector Time (GMT): 2019/304/19:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5295219
18 A = 6793197
82 meter
Y = -415130
45 meter E =
0006902
Z = 4227867
87 I = 51
90221
XDOT = -2455
074979 Wp = 110
96697
YDOT = -6255
800345 meter/sec RA = 43
09775 deg
ZDOT = -3686
682991 TA = 16
71883
MA = 16
69609
Ha = 227
298 n
mi
Hp = 221
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17372766
33 X = -5310720
60
Y = -1361976
55 feet Y = -474432
16 meter
Z = 13870957
57 Z = 4202107
44
XDOT = -8054
707937 XDOT = -2367
030082
YDOT = -20524
279348 feet/sec YDOT = -6282
762300 meter/sec
ZDOT = -12095
416637 ZDOT = -3698
395471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15243368
34 X = -4646178
67
Y = -8634405
58 feet Y = -2631766
82 meter
Z = 13753480
14 Z = 4192060
75
XDOT = 846
595855 XDOT = 258
042417
YDOT = -20858
053936 feet/sec YDOT = -6357
534840 meter/sec
ZDOT = -12148
255437 ZDOT = -3702
788257
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 19304
86377118
00016717 00000-0 10270-3 0 9128
2 25544 51
6409 43
5898 0006195 213
8924 146
1832 15
50251257 36450
Satellite: ISS
Catalog Number: 25544
Epoch time: 19304
86377118 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 43
5898 deg
Eccentricity:
0006195
Arg of perigee: 213
8924 deg
Mean anomaly: 146
1832 deg
Mean motion: 15
50251257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3645
Checksum: 322
Coasting Arc #14 (Orbit 3657)
---------------------------------------
Vector Time (GMT): 2019/305/15:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5822473
86 A = 6796546
07 meter
Y = -1550536
82 meter E =
0011179
Z = 3129039
53 I = 51
89443
XDOT = -1084
359473 Wp = 123
77655
YDOT = -5805
342054 meter/sec RA = 38
94546 deg
ZDOT = -4888
023137 TA = 20
37126
MA = 20
32670
Ha = 227
173 n
mi
Hp = 221
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19102604
54 X = -5819901
99
Y = -5087063
05 feet Y = -1615633
57 meter
Z = 10265877
72 Z = 3100761
79
XDOT = -3557
609821 XDOT = -995
618120
YDOT = -19046
397814 feet/sec YDOT = -5816
971748 meter/sec
ZDOT = -16036
821316 ZDOT = -4893
075337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2194732
23 X = 668954
38
Y = -19712934
24 feet Y = -6008502
36 meter
Z = 10137027
68 Z = 3089766
04
XDOT = 16890
155045 XDOT = 5148
119258
YDOT = -6388
805200 feet/sec YDOT = -1947
307825 meter/sec
ZDOT = -16059
310115 ZDOT = -4894
877723
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 19305
70179457
00016717 00000-0 10270-3 0 9139
2 25544 51
6428 39
4369 0006227 216
2773 143
7956 15
50266926 36586
Satellite: ISS
Catalog Number: 25544
Epoch time: 19305
70179457 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 39
4369 deg
Eccentricity:
0006227
Arg of perigee: 216
2773 deg
Mean anomaly: 143
7956 deg
Mean motion: 15
50266926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 339
Coasting Arc #15 (Orbit 3671)
---------------------------------------
Vector Time (GMT): 2019/306/13:59:43
634
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -567433
67 A = 6791331
44 meter
Y = -4869698
42 meter E =
0006234
Z = -4704183
78 I = 51
85211
XDOT = 6828
097448 Wp = 103
12955
YDOT = 1961
006280 meter/sec RA = 34
44569 deg
ZDOT = -2858
196198 TA = 138
55925
MA = 138
51195
Ha = 227
045 n
mi
Hp = 222
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1861659
01 X = -490086
46
Y = -15976700
85 feet Y = -4875611
22 meter
Z = -15433673
83 Z = -4706752
51
XDOT = 22401
894513 XDOT = 6819
545165
YDOT = 6433
747638 feet/sec YDOT = 2037
315169 meter/sec
ZDOT = -9377
284114 ZDOT = -2825
048060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15653888
83 X = 4771305
31
Y = 3650935
79 feet Y = 1112805
23 meter
Z = -15444917
11 Z = -4707610
74
XDOT = -13265
353985 XDOT = -4043
279895
YDOT = 17909
583898 feet/sec YDOT = 5458
841172 meter/sec
ZDOT = -9226
260581 ZDOT = -2812
164225
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 19306
60428101
00016717 00000-0 10270-3 0 9143
2 25544 51
6425 34
9639 0006469 219
2981 140
7701 15
50232689 36725
Satellite: ISS
Catalog Number: 25544
Epoch time: 19306
60428101 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 34
9639 deg
Eccentricity:
0006469
Arg of perigee: 219
2981 deg
Mean anomaly: 140
7701 deg
Mean motion: 15
50232689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3672
Checksum: 312
Coasting Arc #16 (Orbit 3687)
---------------------------------------
Vector Time (GMT): 2019/307/13:59:43
634
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 503133
83 A = 6790529
09 meter
Y = 4695074
52 meter E =
0008256
Z = 4881771
03 I = 51
82189
XDOT = -7040
515515 Wp = 169
27183
YDOT = -1784
891703 meter/sec RA = 29
50156 deg
ZDOT = 2433
684320 TA = 256
84354
MA = 256
93568
Ha = 226
773 n
mi
Hp = 222
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1650701
55 X = 426881
52
Y = 15403787
78 feet Y = 4700274
43 meter
Z = 16016309
14 Z = 4884030
01
XDOT = -23098
804183 XDOT = -7031
854704
YDOT = -5855
943908 feet/sec YDOT = -1863
575355 meter/sec
ZDOT = 7984
528608 ZDOT = 2399
504697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15102944
97 X = -4603377
63
Y = -3403994
04 feet Y = -1037537
38 meter
Z = 16026151
44 Z = 4884770
96
XDOT = 12622
766495 XDOT = 3847
419228
YDOT = -19014
520742 feet/sec YDOT = -5795
625922 meter/sec
ZDOT = 7828
789229 ZDOT = 2386
214957
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 19307
63568917
00016717 00000-0 10270-3 0 9158
2 25544 51
6429 29
8523 0006396 224
0750 135
9892 15
50260665 36880
Satellite: ISS
Catalog Number: 25544
Epoch time: 19307
63568917 = yrday
fracday
Element set: 915
Inclination: 51
6429 deg
RA of node: 29
8523 deg
Eccentricity:
0006396
Arg of perigee: 224
0750 deg
Mean anomaly: 135
9892 deg
Mean motion: 15
50260665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3688
Checksum: 342
Coasting Arc #17 (Orbit 3698)
---------------------------------------
Vector Time (GMT): 2019/308/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1140421
68 A = 6791003
42 meter
Y = 4716735
12 meter E =
0008375
Z = 4752340
50 I = 51
80102
XDOT = -7076
324325 Wp = 164
28222
YDOT = -1055
244219 meter/sec RA = 25
99740 deg
ZDOT = 2736
456586 TA = 258
63294
MA = 258
72705
Ha = 226
694 n
mi
Hp = 222
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3741540
95 X = 1064508
53
Y = 15474852
77 feet Y = 4729063
58 meter
Z = 15591668
32 Z = 4757696
01
XDOT = -23216
287157 XDOT = -7077
290688
YDOT = -3462
087332 feet/sec YDOT = -1134
382125 meter/sec
ZDOT = 8977
875938 ZDOT = 2702
079695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5288489
10 X = 1611931
48
Y = -14991807
19 feet Y = -4569502
83 meter
Z = 15615630
56 Z = 4759644
20
XDOT = 16636
669134 XDOT = 5070
856752
YDOT = 15087
633793 feet/sec YDOT = 4598
710780 meter/sec
ZDOT = 8821
170296 ZDOT = 2688
692706
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 19308
34478166
00016717 00000-0 10270-3 0 9164
2 25544 51
6412 26
3346 0006413 225
4543 134
6085 15
50272880 36996
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
34478166 = yrday
fracday
Element set: 916
Inclination: 51
6412 deg
RA of node: 26
3346 deg
Eccentricity:
0006413
Arg of perigee: 225
4543 deg
Mean anomaly: 134
6085 deg
Mean motion: 15
50272880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3699
Checksum: 314
Coasting Arc #18 (Orbit 3700)
---------------------------------------
Vector Time (GMT): 2019/308/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3950807
83 A = 6796472
65 meter
Y = -4566910
92 meter E =
0005631
Z = -3111750
78 I = 51
81745
XDOT = 5678
219739 Wp = 182
36149
YDOT = -1580
190869 meter/sec RA = 25
23031 deg
ZDOT = -4895
328101 TA = 33
28233
MA = 33
24693
Ha = 226
713 n
mi
Hp = 222
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12961967
96 X = -3884330
35
Y = -14983303
53 feet Y = -4610719
89 meter
Z = -10209156
09 Z = -3130781
15
XDOT = 18629
329854 XDOT = 5719
246929
YDOT = -5184
353245 feet/sec YDOT = -1516
463533 meter/sec
ZDOT = -16060
787734 ZDOT = -4867
645501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17835741
65 X = 5436334
05
Y = 8522186
49 feet Y = 2597562
44 meter
Z = -10295509
87 Z = -3138071
41
XDOT = -14440
486017 XDOT = -4401
460138
YDOT = 10992
189452 feet/sec YDOT = 3350
419345 meter/sec
ZDOT = -15934
357985 ZDOT = -4856
792314
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 19308
47370729
00016717 00000-0 10270-3 0 9175
2 25544 51
6443 25
6975 0006528 225
8112 134
2503 15
50248617 37019
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
47370729 = yrday
fracday
Element set: 917
Inclination: 51
6443 deg
RA of node: 25
6975 deg
Eccentricity:
0006528
Arg of perigee: 225
8112 deg
Mean anomaly: 134
2503 deg
Mean motion: 15
50248617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3701
Checksum: 308
Coasting Arc #19 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2019/309/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3934884
46 A = 6795478
92 meter
Y = 4341783
99 meter E =
0008589
Z = 3439509
40 I = 51
78376
XDOT = -5889
453225 Wp = 120
06606
YDOT = 1683
889766 meter/sec RA = 20
28626 deg
ZDOT = 4599
267559 TA = 280
04794
MA = 280
14484
Ha = 226
520 n
mi
Hp = 222
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12909725
92 X = 3869333
50
Y = 14244698
14 feet Y = 4385420
12 meter
Z = 11284479
67 Z = 3458464
62
XDOT = -19322
353099 XDOT = -5930
186196
YDOT = 5524
572722 feet/sec YDOT = 1617
801974 meter/sec
ZDOT = 15089
460494 ZDOT = 4570
559545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17616614
50 X = -5369544
10
Y = -7568250
94 feet Y = -2306802
89 meter
Z = 11370505
76 Z = 3465730
15
XDOT = 14777
496620 XDOT = 4504
180970
YDOT = -11861
624868 feet/sec YDOT = -3615
423260 meter/sec
ZDOT = 14958
350116 ZDOT = 4559
305115
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 19309
50511030
00016717 00000-0 10270-3 0 9183
2 25544 51
6443 20
5863 0006434 229
7099 130
3490 15
50278717 37164
Satellite: ISS
Catalog Number: 25544
Epoch time: 19309
50511030 = yrday
fracday
Element set: 918
Inclination: 51
6443 deg
RA of node: 20
5863 deg
Eccentricity:
0006434
Arg of perigee: 229
7099 deg
Mean anomaly: 130
3490 deg
Mean motion: 15
50278717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 301
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