[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 4th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 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
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
107/20:46:01
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 217
3
Coasting Arc #1 (Orbit 364)
---------------------------------------
Vector Time (GMT): 2019/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1664468
49 A = 6782259
66 meter
Y = 3911241
95 meter E =
0003873
Z = 5281650
08 I = 51
70452
XDOT = -7330
096425 Wp = 85
82542
YDOT = -2134
018705 meter/sec RA = 11
90788 deg
ZDOT = -728
969911 TA = 11
13519
MA = 11
12662
Ha = 224
037 n
mi
Hp = 216
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5460854
63 X = -1733736
69
Y = 12832158
63 feet Y = 3892241
98 meter
Z = 17328248
29 Z = 5273396
05
XDOT = -24048
872785 XDOT = -7302
147510
YDOT = -7001
373704 feet/sec YDOT = -2215
832783 meter/sec
ZDOT = -2391
633566 ZDOT = -764
508591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3110058
60 X = -947945
86
Y = 13642628
14 feet Y = 4158273
06 meter
Z = 17290449
68 Z = 5270129
06
XDOT = -23917
270316 XDOT = -7289
983992
YDOT = -2214
704361 feet/sec YDOT = -675
041889 meter/sec
ZDOT = -2552
153650 ZDOT = -777
896433
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
54697014
00016717 00000-0 10270-3 0 9005
2 25544 51
6419 12
2716 0001658 140
2742 219
8532 15
52510467 3657
Satellite: ISS
Catalog Number: 25544
Epoch time: 19093
54697014 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 12
2716 deg
Eccentricity:
0001658
Arg of perigee: 140
2742 deg
Mean anomaly: 219
8532 deg
Mean motion: 15
52510467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 365
Checksum: 296
Coasting Arc #2 (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 = 2627020
53 A = 6784514
14 meter
Y = 4093982
76 meter E =
0009281
Z = 4724896
39 I = 51
68018
XDOT = -7032
151217 Wp = 122
40966
YDOT = 1315
163271 meter/sec RA = 7
16867 deg
ZDOT = 2761
471637 TA = 300
22265
MA = 300
31451
Ha = 223
898 n
mi
Hp = 216
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8618833
76 X = 2558094
23
Y = 13431701
96 feet Y = 4122975
07 meter
Z = 15501628
57 Z = 4737489
63
XDOT = -23071
362259 XDOT = -7059
748830
YDOT = 4314
840127 feet/sec YDOT = 1236
370832 meter/sec
ZDOT = 9059
946316 ZDOT = 2727
244835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7797006
93 X = 2376527
71
Y = 13861719
24 feet Y = 4225052
03 meter
Z = 15558111
19 Z = 4742112
29
XDOT = -22315
553418 XDOT = -6801
780682
YDOT = 2525
035250 feet/sec YDOT = 769
630744 meter/sec
ZDOT = 8904
970951 ZDOT = 2714
235146
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
51252585
00016717 00000-0 10270-3 0 9014
2 25544 51
6413 7
4704 0001757 146
9794 213
1468 15
52508377 3803
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
51252585 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 7
4704 deg
Eccentricity:
0001757
Arg of perigee: 146
9794 deg
Mean anomaly: 213
1468 deg
Mean motion: 15
52508377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 380
Checksum: 311
Coasting Arc #3 (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 = -4924857
01 A = 6787662
19 meter
Y = 2549587
65 meter E =
0012082
Z = 3903755
25 I = 51
68738
XDOT = -5234
609849 Wp = 87
57817
YDOT = -3837
820362 meter/sec RA = 6
42150 deg
ZDOT = -4085
877069 TA = 45
23239
MA = 45
13416
Ha = 224
022 n
mi
Hp = 216
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16157667
35 X = -4971963
53
Y = 8364788
89 feet Y = 2494251
50 meter
Z = 12807595
96 Z = 3879717
38
XDOT = -17173
916826 XDOT = -5171
458225
YDOT = -12591
274153 feet/sec YDOT = -3896
004784 meter/sec
ZDOT = -13405
108494 ZDOT = -4111
151100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4657913
53 X = -1419732
04
Y = 17667051
26 feet Y = 5384917
22 meter
Z = 12698565
38 Z = 3870522
73
XDOT = -19502
232770 XDOT = -5944
280548
YDOT = 4602
454504 feet/sec YDOT = 1402
828133 meter/sec
ZDOT = -13518
979245 ZDOT = -4120
584874
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
64126569
00016717 00000-0 10270-3 0 9021
2 25544 51
6429 6
8311 0001568 143
6272 216
4987 15
52520180 3822
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
64126569 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 6
8311 deg
Eccentricity:
0001568
Arg of perigee: 143
6272 deg
Mean anomaly: 216
4987 deg
Mean motion: 15
52520180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 382
Checksum: 307
Coasting Arc #4 (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 = 5644645
16 A = 6790311
93 meter
Y = -2254533
32 meter E =
0004920
Z = -3030948
85 I = 51
66270
XDOT = 4254
697605 Wp = 86
18059
YDOT = 4017
674289 meter/sec RA = 1
45264 deg
ZDOT = 4942
430716 TA = 239
14395
MA = 239
19235
Ha = 223
906 n
mi
Hp = 217
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18519177
02 X = 5684159
24
Y = -7396762
86 feet Y = -2191190
32 meter
Z = -9944057
91 Z = -3003432
89
XDOT = 13958
981644 XDOT = 4185
446862
YDOT = 13181
346093 feet/sec YDOT = 4064
866605 meter/sec
ZDOT = 16215
323870 ZDOT = 4962
929965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6621395
77 X = 2018201
43
Y = -18875750
44 feet Y = -5753328
73 meter
Z = -9819341
60 Z = -2992935
32
XDOT = 17659
999426 XDOT = 5382
767825
YDOT = -2275
890705 feet/sec YDOT = -693
691487 meter/sec
ZDOT = 16307
564764 ZDOT = 4970
545740
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
60681684
00016717 00000-0 10270-3 0 9033
2 25544 51
6428 2
0298 0001503 153
1261 206
9969 15
52487679 3971
Satellite: ISS
Catalog Number: 25544
Epoch time: 19095
60681684 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 2
0298 deg
Eccentricity:
0001503
Arg of perigee: 153
1261 deg
Mean anomaly: 206
9969 deg
Mean motion: 15
52487679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 397
Checksum: 328
Coasting Arc #5 (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 = -6191297
09 A = 6792473
35 meter
Y = 1947913
05 meter E =
0015164
Z = 1976854
41 I = 51
63688
XDOT = -3122
400182 Wp = 115
69273
YDOT = -4233
689598 meter/sec RA = 356
48594 deg
ZDOT = -5580
384004 TA = 42
49349
MA = 42
37620
Ha = 223
919 n
mi
Hp = 216
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20312654
49 X = -6222221
62
Y = 6390790
86 feet Y = 1878504
91 meter
Z = 6485742
82 Z = 1946703
81
XDOT = -10244
095084 XDOT = -3047
719109
YDOT = -13890
057736 feet/sec YDOT = -4268
189403 meter/sec
ZDOT = -18308
346470 ZDOT = -5595
369835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8205034
22 X = -2500894
43
Y = 19694582
79 feet Y = 6002908
83 meter
Z = 6349159
20 Z = 1935223
72
XDOT = -15710
004522 XDOT = -4788
409378
YDOT = -591
955781 feet/sec YDOT = -180
428122 meter/sec
ZDOT = -18375
617244 ZDOT = -5600
888136
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
63673259
00016717 00000-0 10270-3 0 9047
2 25544 51
6429 356
9080 0001531 151
2104 208
9132 15
52504266 4133
Satellite: ISS
Catalog Number: 25544
Epoch time: 19096
63673259 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 356
9080 deg
Eccentricity:
0001531
Arg of perigee: 151
2104 deg
Mean anomaly: 208
9132 deg
Mean motion: 15
52504266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 413
Checksum: 294
Coasting Arc #6 (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 = 6527246
18 A = 6793778
84 meter
Y = -1661925
63 meter E =
0009624
Z = -859691
15 I = 51
60623
XDOT = 1911
252360 Wp = 46
93696
YDOT = 4464
790397 meter/sec RA = 351
52008 deg
ZDOT = 5928
495122 TA = 303
76674
MA = 303
85838
Ha = 223
850 n
mi
Hp = 217
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21414849
67 X = 6549521
14
Y = -5452511
93 feet Y = -1588808
92 meter
Z = -2820509
01 Z = -827929
60
XDOT = 6270
512991 XDOT = 1832
386048
YDOT = 14648
262457 feet/sec YDOT = 4485
722824 meter/sec
ZDOT = 19450
443313 ZDOT = 5937
587506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9272857
27 X = 2826366
89
Y = -20078107
86 feet Y = -6119807
28 meter
Z = -2676685
78 Z = -815853
82
XDOT = 13779
944071 XDOT = 4200
126953
YDOT = 3788
005265 feet/sec YDOT = 1154
584005 meter/sec
ZDOT = 19491
028801 ZDOT = 5940
865579
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
60227418
00016717 00000-0 10270-3 0 9058
2 25544 51
6410 352
1064 0001489 157
6035 202
5182 15
52500824 4285
Satellite: ISS
Catalog Number: 25544
Epoch time: 19097
60227418 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 352
1064 deg
Eccentricity:
0001489
Arg of perigee: 157
6035 deg
Mean anomaly: 202
5182 deg
Mean motion: 15
52500824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 428
Checksum: 287
Coasting Arc #7 (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 = -2026801
58 A = 6782494
60 meter
Y = -3852695
84 meter E =
0014689
Z = -5213838
59 I = 51
56053
XDOT = 7235
996020 Wp = 88
79754
YDOT = -2193
936852 meter/sec RA = 350
33486 deg
ZDOT = -1194
320843 TA = 169
72795
MA = 169
69790
Ha = 223
901 n
mi
Hp = 216
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6649611
50 X = -1958242
74
Y = -12640078
22 feet Y = -3874977
98 meter
Z = -17105769
64 Z = -5223517
38
XDOT = 23740
144424 XDOT = 7265
792875
YDOT = -7197
955551 feet/sec YDOT = -2112
852357 meter/sec
ZDOT = -3918
375470 ZDOT = -1159
098103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3620316
91 X = -1103472
60
Y = 13762219
17 feet Y = 4194724
40 meter
Z = -17149078
53 Z = -5227039
14
XDOT = -21460
566006 XDOT = -6541
180519
YDOT = -10318
676397 feet/sec YDOT = -3145
132566 meter/sec
ZDOT = -3758
840330 ZDOT = -1145
694533
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
85975298
00016717 00000-0 10270-3 0 9062
2 25544 51
6407 350
8223 0002093 161
3015 198
8214 15
52514494 4321
Satellite: ISS
Catalog Number: 25544
Epoch time: 19097
85975298 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 350
8223 deg
Eccentricity:
0002093
Arg of perigee: 161
3015 deg
Mean anomaly: 198
8214 deg
Mean motion: 15
52514494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 317
Coasting Arc #8 (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 = 928039
14 A = 6782021
56 meter
Y = 4116347
66 meter E =
0003292
Z = 5306918
24 I = 51
52707
XDOT = -7443
176026 Wp = 118
71135
YDOT = 1841
249895 meter/sec RA = 345
34502 deg
ZDOT = -128
052951 TA = 332
50208
MA = 332
51950
Ha = 223
762 n
mi
Hp = 216
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3044747
84 X = 856161
58
Y = 13505077
61 feet Y = 4126324
00 meter
Z = 17411149
08 Z = 5311251
59
XDOT = -24419
868853 XDOT = -7462
590194
YDOT = 6040
846113 feet/sec YDOT = 1757
906535 meter/sec
ZDOT = -420
121231 ZDOT = -164
256844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6669982
44 X = 2033010
65
Y = -12103857
03 feet Y = -3689255
62 meter
Z = 17430252
50 Z = 5312740
96
XDOT = 21489
910067 XDOT = 6550
124588
YDOT = 11008
259081 feet/sec YDOT = 3355
317368 meter/sec
ZDOT = -584
040270 ZDOT = -178
015474
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
88965932
00016717 00000-0 10270-3 0 9071
2 25544 51
6414 345
6999 0002011 167
3732 192
7471 15
52527185 4489
Satellite: ISS
Catalog Number: 25544
Epoch time: 19098
88965932 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 345
6999 deg
Eccentricity:
0002011
Arg of perigee: 167
3732 deg
Mean anomaly: 192
7471 deg
Mean motion: 15
52527185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 448
Checksum: 344
Coasting Arc #9 (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 = 169088
39 A = 6782734
56 meter
Y = -4416897
64 meter E =
0014651
Z = -5157757
21 I = 51
49806
XDOT = 7382
632548 Wp = 108
16103
YDOT = -1411
162598 meter/sec RA = 340
35464 deg
ZDOT = 1449
419343 TA = 175
84684
MA = 175
83467
Ha = 223
793 n
mi
Hp = 216
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 554751
94 X = 243520
65
Y = -14491134
01 feet Y = -4414590
74 meter
Z = -16921775
62 Z = -5156754
93
XDOT = 24221
235393 XDOT = 7390
823315
YDOT = -4629
798549 feet/sec YDOT = -1328
558999 meter/sec
ZDOT = 4755
312805 ZDOT = 1485
301772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9846574
42 X = -3001235
88
Y = 10654428
14 feet Y = 3247469
70 meter
Z = -16916717
70 Z = -5156215
56
XDOT = -20706
733596 XDOT = -6311
412400
YDOT = -11322
922674 feet/sec YDOT = -3451
226831 meter/sec
ZDOT = 4917
718473 ZDOT = 1498
920590
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
85519314
00016717 00000-0 10270-3 0 9089
2 25544 51
6419 340
8993 0002029 166
9290 193
1915 15
52539044 4630
Satellite: ISS
Catalog Number: 25544
Epoch time: 19099
85519314 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 340
8993 deg
Eccentricity:
0002029
Arg of perigee: 166
9290 deg
Mean anomaly: 193
1915 deg
Mean motion: 15
52539044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 333
Coasting Arc #10 (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 = -1211526
24 A = 6784588
85 meter
Y = 4701707
03 meter E =
0007541
Z = 4733201
38 I = 51
47252
XDOT = -7120
068758 Wp = 77
37806
YDOT = 894
878259 meter/sec RA = 335
36328 deg
ZDOT = -2706
138195 TA = 39
45955
MA = 39
40465
Ha = 223
855 n
mi
Hp = 217
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3974823
61 X = -1287003
49
Y = 15425548
00 feet Y = 4687736
93 meter
Z = 15528875
92 Z = 4727132
81
XDOT = -23359
805635 XDOT = -7116
401327
YDOT = 2935
952294 feet/sec YDOT = 815
277146 meter/sec
ZDOT = -8878
406150 ZDOT = -2740
716232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12897482
32 X = 3931152
61
Y = -9395233
02 feet Y = -2863667
03 meter
Z = 15500880
21 Z = 4724668
29
XDOT = 19243
888755 XDOT = 5865
537292
YDOT = 11482
581814 feet/sec YDOT = 3499
890937 meter/sec
ZDOT = -9034
846314 ZDOT = -2753
821156
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
88509320
00016717 00000-0 10270-3 0 9092
2 25544 51
6415 335
7774 0002022 167
8318 192
2883 15
52505429 4791
Satellite: ISS
Catalog Number: 25544
Epoch time: 19100
88509320 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 335
7774 deg
Eccentricity:
0002022
Arg of perigee: 167
8318 deg
Mean anomaly: 192
2883 deg
Mean motion: 15
52505429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 479
Checksum: 317
Coasting Arc #11 (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 = 2149233
76 A = 6786945
09 meter
Y = -4975337
54 meter E =
0008217
Z = -4094427
92 I = 51
45125
XDOT = 6633
045477 Wp = 121
11198
YDOT = -273
867879 meter/sec RA = 330
37500 deg
ZDOT = 3816
124842 TA = 188
46637
MA = 188
48024
Ha = 223
684 n
mi
Hp = 217
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7051291
88 X = 2224598
22
Y = -16323285
90 feet Y = -4950881
93 meter
Z = -13433162
46 Z = -4083804
63
XDOT = 21761
960228 XDOT = 6617
078260
YDOT = -898
516665 feet/sec YDOT = -199
781789 meter/sec
ZDOT = 12520
094625 ZDOT = 3848
307066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15697020
52 X = -4784451
85
Y = 8430758
20 feet Y = 2569695
10 meter
Z = -13384546
93 Z = -4079609
90
XDOT = -16990
730419 XDOT = -5178
774632
YDOT = -11534
903538 feet/sec YDOT = -3515
838598 meter/sec
ZDOT = 12665
624744 ZDOT = 3860
482422
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
85062004
00016717 00000-0 10270-3 0 9105
2 25544 51
6419 330
9768 0001981 177
0247 183
0917 15
52531020 4941
Satellite: ISS
Catalog Number: 25544
Epoch time: 19101
85062004 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 330
9768 deg
Eccentricity:
0001981
Arg of perigee: 177
0247 deg
Mean anomaly: 183
0917 deg
Mean motion: 15
52531020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 494
Checksum: 290
Coasting Arc #12 (Orbit 509)
---------------------------------------
Vector Time (GMT): 2019/102/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2969248
31 A = 6789650
44 meter
Y = 5175073
54 meter E =
0013159
Z = 3226407
30 I = 51
43202
XDOT = -5998
694905 Wp = 101
69928
YDOT = -467
944310 meter/sec RA = 325
38865 deg
ZDOT = -4756
143076 TA = 40
82869
MA = 40
73017
Ha = 223
721 n
mi
Hp = 217
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9741628
30 X = -3042568
88
Y = 16978587
72 feet Y = 5141459
39 meter
Z = 10585325
77 Z = 3211805
67
XDOT = -19680
757562 XDOT = -5969
913663
YDOT = -1535
250362 feet/sec YDOT = -534
865024 meter/sec
ZDOT = -15604
143950 ZDOT = -4785
212604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18074458
98 X = 5509095
10
Y = -7608651
71 feet Y = -2319117
04 meter
Z = 10518708
86 Z = 3206102
46
XDOT = 14121
059179 XDOT = 4304
098838
YDOT = 11727
695150 feet/sec YDOT = 3574
601482 meter/sec
ZDOT = -15735
511322 ZDOT = -4796
183851
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 19102
88051317
00016717 00000-0 10270-3 0 9115
2 25544 51
6421 325
8550 0001972 177
5375 182
5787 15
52522334 5109
Satellite: ISS
Catalog Number: 25544
Epoch time: 19102
88051317 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 325
8550 deg
Eccentricity:
0001972
Arg of perigee: 177
5375 deg
Mean anomaly: 182
5787 deg
Mean motion: 15
52522334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 510
Checksum: 298
Coasting Arc #13 (Orbit 524)
---------------------------------------
Vector Time (GMT): 2019/103/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3621459
15 A = 6791986
53 meter
Y = -5297555
23 meter E =
0004921
Z = -2223364
11 I = 51
41330
XDOT = 5236
205399 Wp = 54
25225
YDOT = 1301
391924 meter/sec RA = 320
40568 deg
ZDOT = 5439
344710 TA = 280
98725
MA = 281
04261
Ha = 223
597 n
mi
Hp = 217
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11881427
67 X = 3691228
62
Y = -17380430
55 feet Y = -5256667
48 meter
Z = -7294501
68 Z = -2205602
88
XDOT = 17179
151570 XDOT = 5194
842435
YDOT = 4269
658544 feet/sec YDOT = 1359
715679 meter/sec
ZDOT = 17845
619126 ZDOT = 5464
679692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19887636
17 X = -6061751
51
Y = 6993095
03 feet Y = 2131495
36 meter
Z = -7213597
83 Z = -2198704
62
XDOT = -10742
847414 XDOT = -3274
419892
YDOT = -12063
920736 feet/sec YDOT = -3677
083040 meter/sec
ZDOT = 17960
004898 ZDOT = 5474
209493
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
84603336
00016717 00000-0 10270-3 0 9127
2 25544 51
6424 321
0540 0001673 185
2918 174
8216 15
52510617 5254
Satellite: ISS
Catalog Number: 25544
Epoch time: 19103
84603336 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 321
0540 deg
Eccentricity:
0001673
Arg of perigee: 185
2918 deg
Mean anomaly: 174
8216 deg
Mean motion: 15
52510617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 525
Checksum: 285
Coasting Arc #14 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2019/104/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4129223
04 A = 6793517
85 meter
Y = 5275959
72 meter E =
0014568
Z = 1077271
04 I = 51
39248
XDOT = -4402
317978 Wp = 129
69860
YDOT = -2238
673250 meter/sec RA = 315
42528 deg
ZDOT = -5866
472811 TA = 38
57979
MA = 38
47578
Ha = 223
566 n
mi
Hp = 217
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13547319
70 X = -4193146
20
Y = 17309579
15 feet Y = 5229426
49 meter
Z = 3534353
81 Z = 1057057
41
XDOT = -14443
300452 XDOT = -4348
461322
YDOT = -7344
728512 feet/sec YDOT = -2287
602163 meter/sec
ZDOT = -19246
958040 ZDOT = -5887
726659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21064502
21 X = 6420460
27
Y = -6330862
86 feet Y = -1929647
00 meter
Z = 3442380
02 Z = 1049237
43
XDOT = 7006
493213 XDOT = 2135
579131
YDOT = 12714
661247 feet/sec YDOT = 3875
428748 meter/sec
ZDOT = -19342
787586 ZDOT = -5895
681656
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 19104
87592110
00016717 00000-0 10270-3 0 9139
2 25544 51
6412 315
9330 0001865 185
0607 175
0526 15
52529836 5414
Satellite: ISS
Catalog Number: 25544
Epoch time: 19104
87592110 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 315
9330 deg
Eccentricity:
0001865
Arg of perigee: 185
0607 deg
Mean anomaly: 175
0526 deg
Mean motion: 15
52529836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 297
Coasting Arc #15 (Orbit 556)
---------------------------------------
Vector Time (GMT): 2019/105/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4458765
66 A = 6793987
18 meter
Y = -5119033
36 meter E =
0011003
Z = 90791
35 I = 51
37140
XDOT = 3551
683824 Wp = 51
28327
YDOT = 3208
363612 meter/sec RA = 310
44407 deg
ZDOT = 5987
000451 TA = 309
69758
MA = 309
79454
Ha = 223
495 n
mi
Hp = 217
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14628496
26 X = 4515235
75
Y = -16794728
87 feet Y = -5068856
57 meter
Z = 297871
88 Z = 112587
80
XDOT = 11652
505983 XDOT = 3486
461539
YDOT = 10526
127335 feet/sec YDOT = 3247
716716 meter/sec
ZDOT = 19642
389931 ZDOT = 6004
094563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21536094
37 X = -6564201
56
Y = 5673059
52 feet Y = 1729148
54 meter
Z = 396967
27 Z = 120995
62
XDOT = -3200
088362 XDOT = -975
386933
YDOT = -13611
566017 feet/sec YDOT = -4148
805322 meter/sec
ZDOT = 19719
309310 ZDOT = 6010
445478
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 19105
90580516
00016717 00000-0 10270-3 0 9142
2 25544 51
6414 310
8113 0001655 192
2649 167
8463 15
52525407 5578
Satellite: ISS
Catalog Number: 25544
Epoch time: 19105
90580516 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 310
8113 deg
Eccentricity:
0001655
Arg of perigee: 192
2649 deg
Mean anomaly: 167
8463 deg
Mean motion: 15
52525407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 557
Checksum: 304
Coasting Arc #16 (Orbit 571)
---------------------------------------
Vector Time (GMT): 2019/106/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4660215
21 A = 6793188
18 meter
Y = 4764541
38 meter E =
0009924
Z = -1289815
81 I = 51
34745
XDOT = -2704
196578 Wp = 149
55322
YDOT = -4209
538919 meter/sec RA = 305
46159 deg
ZDOT = -5807
475020 TA = 44
52809
MA = 44
44838
Ha = 223
382 n
mi
Hp = 217
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15289419
97 X = -4706882
08
Y = 15631697
44 feet Y = 4712166
56 meter
Z = -4231679
16 Z = -1312567
14
XDOT = -8872
036018 XDOT = -2628
713786
YDOT = -13810
823224 feet/sec YDOT = -4239
357533 meter/sec
ZDOT = -19053
395736 ZDOT = -5820
427363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21329213
24 X = 6501144
20
Y = -4721817
59 feet Y = -1439210
00 meter
Z = -4335036
03 Z = -1321318
98
XDOT = -591
833320 XDOT = -180
390796
YDOT = 14790
092319 feet/sec YDOT = 4508
020139 meter/sec
ZDOT = -19111
488096 ZDOT = -5825
181572
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 19106
87131720
00016717 00000-0 10270-3 0 9159
2 25544 51
6406 306
0099 0001659 194
4017 165
7087 15
52547402 5721
Satellite: ISS
Catalog Number: 25544
Epoch time: 19106
87131720 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 306
0099 deg
Eccentricity:
0001659
Arg of perigee: 194
4017 deg
Mean anomaly: 165
7087 deg
Mean motion: 15
52547402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 572
Checksum: 304
Coasting Arc #17 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2019/107/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4720660
08 A = 6791425
10 meter
Y = -4248654
07 meter E =
0012959
Z = 2390747
96 I = 51
32288
XDOT = 1924
832814 Wp = 79
78134
YDOT = 5155
392207 meter/sec RA = 300
47465 deg
ZDOT = 5338
589592 TA = 307
04406
MA = 307
16252
Ha = 223
345 n
mi
Hp = 217
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15487729
93 X = 4756205
88
Y = -13939153
78 feet Y = -4195665
40 meter
Z = 7843661
28 Z = 2413766
00
XDOT = 6315
068288 XDOT = 1841
108608
YDOT = 16914
016427 feet/sec YDOT = 5176
449340 meter/sec
ZDOT = 17515
057715 ZDOT = 5347
736000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20489612
95 X = -6245234
03
Y = 3563062
93 feet Y = 1086021
58 meter
Z = 7948154
02 Z = 2422597
35
XDOT = 4035
043313 XDOT = 1229
881202
YDOT = -16120
670392 feet/sec YDOT = -4913
580335 meter/sec
ZDOT = 17555
851930 ZDOT = 5351
023668
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 19107
90119417
00016717 00000-0 10270-3 0 9164
2 25544 51
6402 300
8880 0001569 197
5256 162
5841 15
52555528 5884
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
90119417 = yrday
fracday
Element set: 916
Inclination: 51
6402 deg
RA of node: 300
8880 deg
Eccentricity:
0001569
Arg of perigee: 197
5256 deg
Mean anomaly: 162
5841 deg
Mean motion: 15
52555528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 322
Coasting Arc #18 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2019/107/20:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1896955
97 A = 6792352
25 meter
Y = 6235258
46 meter E =
0014121
Z = 1886731
20 I = 51
32543
XDOT = -5246
301189 Wp = 118
84158
YDOT = 103
762514 meter/sec RA = 300
31939 deg
ZDOT = -5592
489822 TA = 40
29263
MA = 40
18808
Ha = 223
325 n
mi
Hp = 217
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6223608
83 X = -1975704
18
Y = 20456884
72 feet Y = 6213605
22 meter
Z = 6190062
99 Z = 1877324
66
XDOT = -17212
274243 XDOT = -5219
906170
YDOT = 340
428195 feet/sec YDOT = 45
241828 meter/sec
ZDOT = -18348
063722 ZDOT = -5617
910465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13956982
05 X = 4254088
13
Y = -16215819
21 feet Y = -4942581
70 meter
Z = 6146883
63 Z = 1873570
13
XDOT = 14602
555767 XDOT = 4450
858998
YDOT = 5538
231019 feet/sec YDOT = 1688
052814 meter/sec
ZDOT = -18462
975818 ZDOT = -5627
515029
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 19107
90119405
00016717 00000-0 10270-3 0 9172
2 25544 51
6400 300
8884 0001405 199
0084 161
1015 15
52579820 5880
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
90119405 = yrday
fracday
Element set: 917
Inclination: 51
6400 deg
RA of node: 300
8884 deg
Eccentricity:
0001405
Arg of perigee: 199
0084 deg
Mean anomaly: 161
1015 deg
Mean motion: 15
52579820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 296
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