[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 17th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14537 7374 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
108/01:53:30
000 0
0 0
0 0
0
N/A 0
0 0
0 230
6
000/00:00:00
000 0
0 0
0 222
1
110/05:09:32
060 1
2 -3
2 3
2
N/A -2
9 0
3 228
6
000/00:01:04
120 0
5 -0
1 222
2
113/03:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 222
3
Coasting Arc #1 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2020/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936071
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4437630
25 A = 6794014
80 meter
Y = 95474
53 meter E =
0008209
Z = 5138636
48 I = 51
26408
XDOT = -1838
257730 Wp = 123
30866
YDOT = 7298
306589 meter/sec RA = 293
00171 deg
ZDOT = 1445
774380 TA = 312
66132
MA = 312
73046
Ha = 230
702 n
mi
Hp = 222
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14559154
37 X = 4411272
37
Y = 313236
63 feet Y = 144951
97 meter
Z = 16859043
58 Z = 5160128
64
XDOT = -6031
029298 XDOT = -1926
755645
YDOT = 23944
575423 feet/sec YDOT = 7277
255084 meter/sec
ZDOT = 4743
354266 ZDOT = 1436
629818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13304413
57 X = 4055185
26
Y = -5632783
99 feet Y = -1716872
56 meter
Z = 16957557
84 Z = 5168663
63
XDOT = 3871
343176 XDOT = 1179
985400
YDOT = 23356
350618 feet/sec YDOT = 7119
015668 meter/sec
ZDOT = 4700
993840 ZDOT = 1432
862922
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 20107
55089307
00016717 00000-0 10270-3 0 9004
2 25544 51
6391 293
5156 0003663 121
9812 238
1694 15
48654124 22456
Satellite: ISS
Catalog Number: 25544
Epoch time: 20107
55089307 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 293
5156 deg
Eccentricity:
0003663
Arg of perigee: 121
9812 deg
Mean anomaly: 238
1694 deg
Mean motion: 15
48654124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 304
Coasting Arc #2 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2020/108/01:53:30
000
Vector Time (MET): N/A
Weight (LBS) : 920963
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4602661
69 A = 6795242
13 meter
Y = -1347995
20 meter E =
0010740
Z = 4808108
79 I = 51
26157
XDOT = -509
600502 Wp = 120
97706
YDOT = 7225
024052 meter/sec RA = 290
13545 deg
ZDOT = 2503
815834 TA = 304
20922
MA = 304
31095
Ha = 230
584 n
mi
Hp = 222
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15100596
08 X = 4594038
34
Y = -4422556
43 feet Y = -1296573
06 meter
Z = 15774635
14 Z = 4830445
72
XDOT = -1671
917656 XDOT = -602
517040
YDOT = 23704
147153 feet/sec YDOT = 7218
805870 meter/sec
ZDOT = 8214
618877 ZDOT = 2501
114548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5456433
12 X = -1663120
81
Y = 14648240
34 feet Y = 4464783
66 meter
Z = 15877106
59 Z = 4839342
09
XDOT = -16861
053611 XDOT = -5139
249141
YDOT = -15204
521924 feet/sec YDOT = -4634
338282 meter/sec
ZDOT = 8201
810157 ZDOT = 2499
911736
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 20108
13164268
00016717 00000-0 10270-3 0 9010
2 25544 51
6392 290
6466 0003592 124
2972 235
8519 15
48711407 22541
Satellite: ISS
Catalog Number: 25544
Epoch time: 20108
13164268 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 290
6466 deg
Eccentricity:
0003592
Arg of perigee: 124
2972 deg
Mean anomaly: 235
8519 deg
Mean motion: 15
48711407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 305
Coasting Arc #3 (Orbit 2268)
---------------------------------------
Vector Time (GMT): 2020/109/01:53:30
000
Vector Time (MET): N/A
Weight (LBS) : 920963
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4475988
00 A = 6795454
57 meter
Y = 1836187
39 meter E =
0013790
Z = -4784564
44 I = 51
25186
XDOT = -196
930418 Wp = 84
13986
YDOT = -7196
887054 meter/sec RA = 285
16517 deg
ZDOT = -2582
822502 TA = 160
23077
MA = 160
17727
Ha = 230
732 n
mi
Hp = 221
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14685000
01 X = -4472947
50
Y = 6024236
85 feet Y = 1786150
53 meter
Z = -15697389
89 Z = -4806299
67
XDOT = -646
097172 XDOT = -103
892214
YDOT = -23611
834166 feet/sec YDOT = -7198
569157 meter/sec
ZDOT = -8473
827107 ZDOT = -2583
552869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3662592
49 X = 1116358
19
Y = -15342259
73 feet Y = -4676320
77 meter
Z = -15797125
90 Z = -4814963
97
XDOT = 18358
765068 XDOT = 5595
751593
YDOT = 13093
746297 feet/sec YDOT = 3990
973871 meter/sec
ZDOT = -8476
770123 ZDOT = -2583
719534
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 20109
09956074
00016717 00000-0 10270-3 0 9021
2 25544 51
6394 285
8601 0003650 126
8392 233
3093 15
48687145 22696
Satellite: ISS
Catalog Number: 25544
Epoch time: 20109
09956074 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 285
8601 deg
Eccentricity:
0003650
Arg of perigee: 126
8392 deg
Mean anomaly: 233
3093 deg
Mean motion: 15
48687145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2269
Checksum: 321
Coasting Arc #4 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2020/110/01:53:30
000
Vector Time (MET): N/A
Weight (LBS) : 920963
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4277598
49 A = 6795500
39 meter
Y = -2336579
22 meter E =
0011059
Z = 4729539
17 I = 51
24574
XDOT = 909
117221 Wp = 122
14515
YDOT = 7119
652233 meter/sec RA = 280
19600 deg
ZDOT = 2684
730814 TA = 301
10495
MA = 301
21341
Ha = 230
460 n
mi
Hp = 222
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14034115
77 X = 4280435
47
Y = -7665942
34 feet Y = -2288727
99 meter
Z = 15516860
81 Z = 4750325
08
XDOT = 2982
668048 XDOT = 816
394698
YDOT = 23358
439086 feet/sec YDOT = 7129
300307 meter/sec
ZDOT = 8808
171962 ZDOT = 2688
921422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1679929
17 X = -512042
41
Y = 15809207
22 feet Y = 4818646
36 meter
Z = 15612266
06 Z = 4758618
69
XDOT = -19679
043257 XDOT = -5998
172385
YDOT = -10841
721388 feet/sec YDOT = -3304
556679 meter/sec
ZDOT = 8826
999269 ZDOT = 2690
469377
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 20110
13200193
00016717 00000-0 10270-3 0 9033
2 25544 51
6403 280
7559 0003493 132
2500 227
8947 15
48735502 22855
Satellite: ISS
Catalog Number: 25544
Epoch time: 20110
13200193 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 280
7559 deg
Eccentricity:
0003493
Arg of perigee: 132
2500 deg
Mean anomaly: 227
8947 deg
Mean motion: 15
48735502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 282
Coasting Arc #5 (Orbit 2286)
---------------------------------------
Vector Time (GMT): 2020/110/05:10:04
120
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3762856
39 A = 6792191
80 meter
Y = 2401827
83 meter E =
0004291
Z = 5115860
26 I = 51
24130
XDOT = -2438
152102 Wp = 74
04254
YDOT = 7100
575171 meter/sec RA = 279
48434 deg
ZDOT = -1538
057204 TA = 30
88460
MA = 30
85937
Ha = 228
584 n
mi
Hp = 222
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12345329
36 X = 3710868
82
Y = 7880012
58 feet Y = 2443616
33 meter
Z = 16784318
43 Z = 5134012
38
XDOT = -7999
186686 XDOT = -2509
900615
YDOT = 23295
850300 feet/sec YDOT = 7072
908776 meter/sec
ZDOT = -5046
119435 ZDOT = -1550
075398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4594958
62 X = -1400543
39
Y = 13805519
29 feet Y = 4207922
28 meter
Z = 16867397
33 Z = 5141182
71
XDOT = -23537
266638 XDOT = -7174
158871
YDOT = -1592
040020 feet/sec YDOT = -485
253798 meter/sec
ZDOT = -5101
587500 ZDOT = -1554
963870
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 20110
26103557
00016717 00000-0 10270-3 0 9044
2 25544 51
6421 280
1179 0001605 173
9221 186
1949 15
49317202 22877
Satellite: ISS
Catalog Number: 25544
Epoch time: 20110
26103557 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 280
1179 deg
Eccentricity:
0001605
Arg of perigee: 173
9221 deg
Mean anomaly: 186
1949 deg
Mean motion: 15
49317202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2287
Checksum: 285
Coasting Arc #6 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2020/111/05:10:04
120
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3931291
86 A = 6792394
01 meter
Y = -2199592
26 meter E =
0013996
Z = -5096317
85 I = 51
23790
XDOT = 1899
763047 Wp = 108
71275
YDOT = -7223
739924 meter/sec RA = 274
50751 deg
ZDOT = 1651
664612 TA = 177
36591
MA = 177
35853
Ha = 228
769 n
mi
Hp = 222
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12897939
17 X = -3881648
06
Y = -7216510
06 feet Y = -2243277
43 meter
Z = -16720202
92 Z = -5115293
94
XDOT = 6232
818395 XDOT = 1972
376968
YDOT = -23699
934135 feet/sec YDOT = -7202
089333 meter/sec
ZDOT = 5418
847152 ZDOT = 1661
069671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3570438
17 X = 1088269
55
Y = -14239883
06 feet Y = -4340316
36 meter
Z = -16807074
10 Z = -5122796
18
XDOT = 23455
833254 XDOT = 7149
337976
YDOT = -568
416606 feet/sec YDOT = -173
253381 meter/sec
ZDOT = 5462
325639 ZDOT = 1664
916855
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 20111
22858282
00016717 00000-0 10270-3 0 9054
2 25544 51
6426 275
3292 0001599 173
5540 186
5631 15
49292486 23022
Satellite: ISS
Catalog Number: 25544
Epoch time: 20111
22858282 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 275
3292 deg
Eccentricity:
0001599
Arg of perigee: 173
5540 deg
Mean anomaly: 186
5631 deg
Mean motion: 15
49292486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 310
Coasting Arc #7 (Orbit 2317)
---------------------------------------
Vector Time (GMT): 2020/112/05:10:04
120
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4075886
36 A = 6792410
51 meter
Y = 1982459
64 meter E =
0004597
Z = 5055643
10 I = 51
23646
XDOT = -1363
301833 Wp = 71
26508
YDOT = 7329
872712 meter/sec RA = 269
53171 deg
ZDOT = -1772
367334 TA = 36
00457
MA = 35
97361
Ha = 228
472 n
mi
Hp = 222
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13372330
57 X = 4028857
33
Y = 6504132
69 feet Y = 2027776
36 meter
Z = 16586755
57 Z = 5075328
03
XDOT = -4472
775044 XDOT = -1436
556092
YDOT = 24048
138820 feet/sec YDOT = 7314
217636 meter/sec
ZDOT = -5814
853458 ZDOT = -1779
168010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2507562
82 X = -764305
15
Y = 14554616
38 feet Y = 4436247
07 meter
Z = 16676891
13 Z = 5083116
42
XDOT = -23261
631733 XDOT = -7090
145352
YDOT = 2701
603386 feet/sec YDOT = 823
448712 meter/sec
ZDOT = -5846
383273 ZDOT = -1781
977622
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 20112
26063119
00016717 00000-0 10270-3 0 9067
2 25544 51
6422 270
2225 0001570 182
5026 177
6117 15
49328368 23182
Satellite: ISS
Catalog Number: 25544
Epoch time: 20112
26063119 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 270
2225 deg
Eccentricity:
0001570
Arg of perigee: 182
5026 deg
Mean anomaly: 177
6117 deg
Mean motion: 15
49328368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2318
Checksum: 283
Coasting Arc #8 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2020/113/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1074722
49 A = 6801671
06 meter
Y = 6398166
56 meter E =
0007811
Z = -2032138
92 I = 51
26806
XDOT = -4666
522408 Wp = 147
62060
YDOT = -2531
845400 meter/sec RA = 264
98502 deg
ZDOT = -5519
906728 TA = 54
90965
MA = 54
83643
Ha = 228
639 n
mi
Hp = 222
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3525992
42 X = -1136317
72
Y = 20991360
10 feet Y = 6385803
78 meter
Z = -6667122
43 Z = -2037509
38
XDOT = -15310
112888 XDOT = -4611
050851
YDOT = -8306
579397 feet/sec YDOT = -2583
719793 meter/sec
ZDOT = -18109
930209 ZDOT = -5542
440336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19875273
79 X = -6057983
45
Y = -7596738
54 feet Y = -2315485
91 meter
Z = -6692039
91 Z = -2039733
76
XDOT = 10615
259888 XDOT = 3235
531214
YDOT = -11775
639649 feet/sec YDOT = -3589
214965 meter/sec
ZDOT = -18213
102058 ZDOT = -5551
353507
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 20113
16367468
00016717 00000-0 10270-3 0 9072
2 25544 51
6421 265
7523 0001575 184
3987 175
7150 15
49290990 23323
Satellite: ISS
Catalog Number: 25544
Epoch time: 20113
16367468 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 265
7523 deg
Eccentricity:
0001575
Arg of perigee: 184
3987 deg
Mean anomaly: 175
7150 deg
Mean motion: 15
49290990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 319
Coasting Arc #9 (Orbit 2347)
---------------------------------------
Vector Time (GMT): 2020/114/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 590475
74 A = 6801544
81 meter
Y = -6431063
34 meter E =
0013269
Z = 2116249
36 I = 51
27188
XDOT = 4858
054040 Wp = 75
75874
YDOT = 2257
054285 meter/sec RA = 260
01017 deg
ZDOT = 5477
673401 TA = 307
76708
MA = 307
88721
Ha = 228
629 n
mi
Hp = 222
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1937256
36 X = 652066
22
Y = -21099289
17 feet Y = -6424115
81 meter
Z = 6943075
33 Z = 2119267
41
XDOT = 15938
497507 XDOT = 4805
846110
YDOT = 7405
033743 feet/sec YDOT = 2311
088685 meter/sec
ZDOT = 17971
369426 ZDOT = 5501
145449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20399444
24 X = 6217750
60
Y = 5709579
22 feet Y = 1740279
75 meter
Z = 6957200
63 Z = 2120554
75
XDOT = -9752
202445 XDOT = -2972
471305
YDOT = 12710
887185 feet/sec YDOT = 3874
278414 meter/sec
ZDOT = 18078
862253 ZDOT = 5510
437215
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 20114
19572094
00016717 00000-0 10270-3 0 9080
2 25544 51
6422 260
6449 0001491 186
8385 173
2745 15
49287972 23487
Satellite: ISS
Catalog Number: 25544
Epoch time: 20114
19572094 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 260
6449 deg
Eccentricity:
0001491
Arg of perigee: 186
8385 deg
Mean anomaly: 173
2745 deg
Mean motion: 15
49287972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2348
Checksum: 331
Coasting Arc #10 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2020/115/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -138363
06 A = 6801324
86 meter
Y = 6419725
89 meter E =
0007005
Z = -2234236
67 I = 51
27917
XDOT = -5030
456359 Wp = 146
71589
YDOT = -1990
128789 meter/sec RA = 255
03625 deg
ZDOT = -5420
659468 TA = 58
19449
MA = 58
12630
Ha = 228
580 n
mi
Hp = 222
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -453947
06 X = -199287
22
Y = 21062092
82 feet Y = 6417837
97 meter
Z = -7330172
80 Z = -2235056
76
XDOT = -16504
121914 XDOT = -4981
497350
YDOT = -6529
293927 feet/sec YDOT = -2046
109179 meter/sec
ZDOT = -17784
315839 ZDOT = -5444
976972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20703994
55 X = -6310577
54
Y = -3886282
16 feet Y = -1184538
80 meter
Z = -7334212
69 Z = -2235468
03
XDOT = 8869
640973 XDOT = 2703
466569
YDOT = -13565
564123 feet/sec YDOT = -4134
783945 meter/sec
ZDOT = -17895
704024 ZDOT = -5454
610587
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 20115
16326244
00016717 00000-0 10270-3 0 9093
2 25544 51
6432 255
8571 0001488 191
2336 168
8781 15
49288814 23635
Satellite: ISS
Catalog Number: 25544
Epoch time: 20115
16326244 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 255
8571 deg
Eccentricity:
0001488
Arg of perigee: 191
2336 deg
Mean anomaly: 168
8781 deg
Mean motion: 15
49288814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 322
Coasting Arc #11 (Orbit 2378)
---------------------------------------
Vector Time (GMT): 2020/116/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -337815
45 A = 6801182
24 meter
Y = -6379292
76 meter E =
0013093
Z = 2317804
09 I = 51
28798
XDOT = 5193
755650 Wp = 78
08299
YDOT = 1686
082958 meter/sec RA = 250
06276 deg
ZDOT = 5374
376149 TA = 307
83599
MA = 307
95441
Ha = 228
558 n
mi
Hp = 222
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1108318
40 X = -277713
97
Y = -20929438
17 feet Y = -6382734
45 meter
Z = 7604344
11 Z = 2316308
92
XDOT = 17039
880742 XDOT = 5148
409244
YDOT = 5531
768236 feet/sec YDOT = 1743
909566 meter/sec
ZDOT = 17632
467680 ZDOT = 5399
495733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20869019
65 X = 6360877
19
Y = 1963128
30 feet Y = 598361
50 meter
Z = 7597759
37 Z = 2315797
06
XDOT = -7842
525333 XDOT = -2390
401722
YDOT = 14387
798903 feet/sec YDOT = 4385
401106 meter/sec
ZDOT = 17747
555654 ZDOT = 5409
454963
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 20116
19530724
00016717 00000-0 10270-3 0 9109
2 25544 51
6427 250
7501 0001418 194
8611 165
2498 15
49287088 23799
Satellite: ISS
Catalog Number: 25544
Epoch time: 20116
19530724 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 250
7501 deg
Eccentricity:
0001418
Arg of perigee: 194
8611 deg
Mean anomaly: 165
2498 deg
Mean motion: 15
49287088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2379
Checksum: 312
Coasting Arc #12 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2020/117/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 776152
10 A = 6800967
82 meter
Y = 6300696
85 meter E =
0006182
Z = -2433831
97 I = 51
30083
XDOT = -5337
852891 Wp = 147
08896
YDOT = -1390
057094 meter/sec RA = 245
09057 deg
ZDOT = -5312
298162 TA = 60
21330
MA = 60
15183
Ha = 228
464 n
mi
Hp = 222
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2546430
77 X = 717460
52
Y = 20671577
60 feet Y = 6309048
27 meter
Z = -7985013
01 Z = -2430203
95
XDOT = -17512
640717 XDOT = -5296
107596
YDOT = -4560
554769 feet/sec YDOT = -1449
515129 meter/sec
ZDOT = -17428
799744 ZDOT = -5338
126468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20833616
71 X = -6350086
37
Y = -141788
61 feet Y = -43217
17 meter
Z = -7968636
89 Z = -2428840
53
XDOT = 6800
098609 XDOT = 2072
670056
YDOT = -15123
185523 feet/sec YDOT = -4609
546947 meter/sec
ZDOT = -17547
161219 ZDOT = -5348
374739
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 20117
16284674
00016717 00000-0 10270-3 0 9118
2 25544 51
6438 245
9627 0001604 204
9828 155
1244 15
49281029 23949
Satellite: ISS
Catalog Number: 25544
Epoch time: 20117
16284674 = yrday
fracday
Element set: 911
Inclination: 51
6438 deg
RA of node: 245
9627 deg
Eccentricity:
0001604
Arg of perigee: 204
9828 deg
Mean anomaly: 155
1244 deg
Mean motion: 15
49281029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 311
Coasting Arc #13 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2020/118/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1231415
52 A = 6800761
63 meter
Y = -6190246
78 meter E =
0012805
Z = 2518238
03 I = 51
31566
XDOT = 5468
074363 Wp = 80
15220
YDOT = 1060
940695 meter/sec RA = 240
11813 deg
ZDOT = 5261
058863 TA = 308
19013
MA = 308
30539
Ha = 228
443 n
mi
Hp = 222
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4040077
17 X = -1174335
16
Y = -20309208
58 feet Y = -6203698
33 meter
Z = 8261935
81 Z = 2512394
50
XDOT = 17939
876520 XDOT = 5430
248631
YDOT = 3480
776560 feet/sec YDOT = 1121
876792 meter/sec
ZDOT = 17260
691808 ZDOT = 5287
529199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20644212
50 X = 6292355
97
Y = -1743753
38 feet Y = -531496
03 meter
Z = 8235385
51 Z = 2510145
50
XDOT = -5626
682578 XDOT = -1715
012850
YDOT = 15800
867781 feet/sec YDOT = 4816
104500 meter/sec
ZDOT = 17382
024448 ZDOT = 5298
041052
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 20118
19488698
00016717 00000-0 10270-3 0 9125
2 25544 51
6439 240
8551 0001336 207
6460 152
4619 15
49295657 24101
Satellite: ISS
Catalog Number: 25544
Epoch time: 20118
19488698 = yrday
fracday
Element set: 912
Inclination: 51
6439 deg
RA of node: 240
8551 deg
Eccentricity:
0001336
Arg of perigee: 207
6460 deg
Mean anomaly: 152
4619 deg
Mean motion: 15
49295657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 320
Coasting Arc #14 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2020/119/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1644488
39 A = 6800551
94 meter
Y = 6048933
80 meter E =
0005346
Z = -2633206
20 I = 51
33213
XDOT = -5578
911342 Wp = 143
30582
YDOT = -739
658967 meter/sec RA = 235
14824 deg
ZDOT = -5192
949599 TA = 66
43161
MA = 66
37548
Ha = 228
397 n
mi
Hp = 222
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5395303
10 X = 1589515
94
Y = 19845583
33 feet Y = 6067016
44 meter
Z = -8639127
94 Z = -2625350
94
XDOT = -18303
514901 XDOT = -5545
000976
YDOT = -2426
702646 feet/sec YDOT = -801
856366 meter/sec
ZDOT = -17037
236217 ZDOT = -5219
967742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20281966
29 X = -6181943
32
Y = 3495067
87 feet Y = 1065296
69 meter
Z = -8603333
59 Z = -2622296
08
XDOT = 4442
377975 XDOT = 1354
036807
YDOT = -16385
394144 feet/sec YDOT = -4994
268135 meter/sec
ZDOT = -17161
109310 ZDOT = -5230
706118
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 20119
16242274
00016717 00000-0 10270-3 0 9132
2 25544 51
6434 236
0680 0001489 213
4869 146
6187 15
49282567 24250
Satellite: ISS
Catalog Number: 25544
Epoch time: 20119
16242274 = yrday
fracday
Element set: 913
Inclination: 51
6434 deg
RA of node: 236
0680 deg
Eccentricity:
0001489
Arg of perigee: 213
4869 deg
Mean anomaly: 146
6187 deg
Mean motion: 15
49282567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 316
Coasting Arc #15 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2020/120/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2069347
38 A = 6800337
20 meter
Y = -5874459
13 meter E =
0012498
Z = 2716846
46 I = 51
35091
XDOT = 5671
426023 Wp = 82
39235
YDOT = 386
747592 meter/sec RA = 230
17849 deg
ZDOT = 5137
254102 TA = 308
40159
MA = 308
51376
Ha = 228
360 n
mi
Hp = 222
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6789197
44 X = -2016700
61
Y = -19273159
87 feet Y = -5897305
86 meter
Z = 8913538
26 Z = 2706921
78
XDOT = 18607
040759 XDOT = 5641
725784
YDOT = 1268
856928 feet/sec YDOT = 450
003092 meter/sec
ZDOT = 16854
508209 ZDOT = 5164
731740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19760283
07 X = 6022934
28
Y = -5280601
93 feet Y = -1609527
47 meter
Z = 8868230
58 Z = 2703036
68
XDOT = -3135
012105 XDOT = -955
551690
YDOT = 16889
529283 feet/sec YDOT = 5147
928526 meter/sec
ZDOT = 16980
518734 ZDOT = 5175
662110
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 20120
19446071
00016717 00000-0 10270-3 0 9149
2 25544 51
6426 230
9605 0001299 219
7787 140
3268 15
49295736 24419
Satellite: ISS
Catalog Number: 25544
Epoch time: 20120
19446071 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 230
9605 deg
Eccentricity:
0001299
Arg of perigee: 219
7787 deg
Mean anomaly: 140
3268 deg
Mean motion: 15
49295736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 312
Coasting Arc #16 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2020/121/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2449146
80 A = 6800088
43 meter
Y = 5676647
78 meter E =
0004505
Z = -2829594
56 I = 51
37285
XDOT = -5743
450455 Wp = 138
83079
YDOT = -42
238716 meter/sec RA = 225
21081 deg
ZDOT = -5063
903566 TA = 73
35786
MA = 73
30841
Ha = 228
269 n
mi
Hp = 222
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8035258
52 X = 2399231
41
Y = 18624172
50 feet Y = 5703756
96 meter
Z = -9283446
72 Z = -2817818
41
XDOT = -18843
341387 XDOT = -5717
953645
YDOT = -138
578463 feet/sec YDOT = -106
323189 meter/sec
ZDOT = -16613
856845 ZDOT = -5091
741162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19097606
12 X = -5820950
34
Y = 6906742
34 feet Y = 2105175
07 meter
Z = -9229621
59 Z = -2813188
66
XDOT = 1824
851879 XDOT = 556
214853
YDOT = -17291
222806 feet/sec YDOT = -5270
364711 meter/sec
ZDOT = -16741
547614 ZDOT = -5102
823713
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 20121
16199366
00016717 00000-0 10270-3 0 9150
2 25544 51
6430 226
1729 0001532 226
5133 133
5890 15
49291746 24567
Satellite: ISS
Catalog Number: 25544
Epoch time: 20121
16199366 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 226
1729 deg
Eccentricity:
0001532
Arg of perigee: 226
5133 deg
Mean anomaly: 133
5890 deg
Mean motion: 15
49291746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 301
Coasting Arc #17 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2020/122/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920642
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2833305
18 A = 6799847
90 meter
Y = -5445348
18 meter E =
0012101
Z = 2913462
56 I = 51
39660
XDOT = 5794
033456 Wp = 84
44041
YDOT = -328
983183 meter/sec RA = 220
24325 deg
ZDOT = 5002
913028 TA = 308
83621
MA = 308
94417
Ha = 228
245 n
mi
Hp = 222
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9295620
67 X = -2786355
06
Y = -17865315
55 feet Y = -5476769
84 meter
Z = 9558604
19 Z = 2899813
23
XDOT = 19009
296117 XDOT = 5772
980306
YDOT = -1079
341153 feet/sec YDOT = -264
308133 meter/sec
ZDOT = 16413
756655 ZDOT = 5031
007056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18275880
61 X = 5570488
41
Y = -8529954
79 feet Y = -2599930
22 meter
Z = 9496159
05 Z = 2894429
28
XDOT = -412
673157 XDOT = -125
782778
YDOT = 17594
175717 feet/sec YDOT = 5362
704759 meter/sec
ZDOT = 16542
652194 ZDOT = 5042
200389
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 20122
19402682
00016717 00000-0 10270-3 0 9163
2 25544 51
6429 221
0647 0001310 235
1843 124
9184 15
49308452 24727
Satellite: ISS
Catalog Number: 25544
Epoch time: 20122
19402682 = yrday
fracday
Element set: 916
Inclination: 51
6429 deg
RA of node: 221
0647 deg
Eccentricity:
0001310
Arg of perigee: 235
1843 deg
Mean anomaly: 124
9184 deg
Mean motion: 15
49308452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2472
Checksum: 284
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