[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 24th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
025/12:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 217
5
026/08:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 217
4
033/17:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 216
5
037/01:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 216
1
Coasting Arc #1 (Orbit 3276)
---------------------------------------
Vector Time (GMT): 2019/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6740794
85 A = 6791943
87 meter
Y = 475574
48 meter E =
0008276
Z = 639514
35 I = 51
66347
XDOT = -903
806724 Wp = 131
42091
YDOT = -4724
101105 meter/sec RA =
25628 deg
ZDOT = -5968
743674 TA = 41
68034
MA = 41
61731
Ha = 221
529 n
mi
Hp = 217
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22115468
66 X = -6748718
19
Y = 1560283
73 feet Y = 400149
90 meter
Z = 2098144
20 Z = 606751
78
XDOT = -2965
245156 XDOT = -821
921293
YDOT = -15499
019374 feet/sec YDOT = -4733
750170 meter/sec
ZDOT = -19582
492369 ZDOT = -5972
935091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12940902
35 X = -3944387
04
Y = -18018334
03 feet Y = -5491988
21 meter
Z = 1950213
78 Z = 594425
16
XDOT = 10393
374412 XDOT = 3167
900521
YDOT = -9603
181536 feet/sec YDOT = -2927
049732 meter/sec
ZDOT = -19600
755536 ZDOT = -5974
310287
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 19023
53333917
00016717 00000-0 10270-3 0 9006
2 25544 51
6392
6779 0004838 303
1212 56
9475 15
53177644 32770
Satellite: ISS
Catalog Number: 25544
Epoch time: 19023
53333917 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node:
6779 deg
Eccentricity:
0004838
Arg of perigee: 303
1212 deg
Mean anomaly: 56
9475 deg
Mean motion: 15
53177644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3277
Checksum: 310
Coasting Arc #2 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2019/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6742205
61 A = 6791767
73 meter
Y = 40502
35 meter E =
0012663
Z = 749991
82 I = 51
63005
XDOT = -694
898274 Wp = 32
16164
YDOT = 4786
155927 meter/sec RA = 355
29161 deg
ZDOT = 5952
691694 TA = 335
94465
MA = 336
00375
Ha = 221
553 n
mi
Hp = 217
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22120097
16 X = 6737608
66
Y = 132881
73 feet Y = 115872
70 meter
Z = 2460603
09 Z = 782730
95
XDOT = -2279
849979 XDOT = -777
280926
YDOT = 15702
611309 feet/sec YDOT = 4777
924511 meter/sec
ZDOT = 19529
828394 ZDOT = 5949
116095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11808917
92 X = 3599358
18
Y = 18684670
63 feet Y = 5695087
61 meter
Z = 2608345
13 Z = 795023
60
XDOT = -13161
669648 XDOT = -4011
676909
YDOT = 5578
882855 feet/sec YDOT = 1700
443494 meter/sec
ZDOT = 19513
035438 ZDOT = 5947
573202
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 19024
56280803
00016717 00000-0 10270-3 0 9016
2 25544 51
6393 355
5539 0004757 305
4116 54
6592 15
53199388 32937
Satellite: ISS
Catalog Number: 25544
Epoch time: 19024
56280803 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 355
5539 deg
Eccentricity:
0004757
Arg of perigee: 305
4116 deg
Mean anomaly: 54
6592 deg
Mean motion: 15
53199388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 327
Coasting Arc #3 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2019/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6427065
60 A = 6790150
16 meter
Y = -597162
82 meter E =
0001520
Z = -2105242
44 I = 51
59154
XDOT = 2253
319673 Wp = 160
72354
YDOT = -4819
521255 meter/sec RA = 350
32221 deg
ZDOT = -5514
587635 TA = 42
58666
MA = 42
57488
Ha = 221
823 n
mi
Hp = 217
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21086173
22 X = -6409684
40
Y = -1959195
62 feet Y = -668937
61 meter
Z = -6906963
39 Z = -2136419
85
XDOT = 7392
781081 XDOT = 2333
831702
YDOT = -15812
077608 feet/sec YDOT = -4793
872992 meter/sec
ZDOT = -18092
479118 ZDOT = -5503
446446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10018591
23 X = -3053666
61
Y = -18604592
98 feet Y = -5670679
94 meter
Z = -7047569
90 Z = -2148099
30
XDOT = 15971
492191 XDOT = 4868
110820
YDOT = -1769
475047 feet/sec YDOT = -539
335994 meter/sec
ZDOT = -18041
547945 ZDOT = -5499
063814
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 19025
52793651
00016717 00000-0 10270-3 0 9024
2 25544 51
6394 350
7497 0004930 311
2477 48
8250 15
53173557 33089
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
52793651 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 350
7497 deg
Eccentricity:
0004930
Arg of perigee: 311
2477 deg
Mean anomaly: 48
8250 deg
Mean motion: 15
53173557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 317
Coasting Arc #4 (Orbit 3308)
---------------------------------------
Vector Time (GMT): 2019/025/12:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4246427
76 A = 6783507
00 meter
Y = 2848562
03 meter E =
0004573
Z = 4453644
71 I = 51
56898
XDOT = -5890
632335 Wp = 91
77641
YDOT = 3659
869680 meter/sec RA = 350
13701 deg
ZDOT = 3272
647829 TA = 325
19787
MA = 325
22777
Ha = 221
610 n
mi
Hp = 217
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13931849
62 X = 4192625
85
Y = 9345675
97 feet Y = 2895747
81 meter
Z = 14611695
23 Z = 4474141
12
XDOT = -19326
221571 XDOT = -5947
016610
YDOT = 12007
446458 feet/sec YDOT = 3593
681318 meter/sec
ZDOT = 10737
033561 ZDOT = 3243
896919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3859790
13 X = 1176464
03
Y = 16243155
69 feet Y = 4950913
85 meter
Z = 14703796
92 Z = 4481717
30
XDOT = -21222
927363 XDOT = -6468
748260
YDOT = -4567
474119 feet/sec YDOT = -1392
166111 meter/sec
ZDOT = 10606
797201 ZDOT = 3232
951787
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 19025
59227710
00016717 00000-0 10270-3 0 9030
2 25544 51
6400 350
4299 0004951 309
4403 50
6310 15
53202452 33091
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
59227710 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 350
4299 deg
Eccentricity:
0004951
Arg of perigee: 309
4403 deg
Mean anomaly: 50
6310 deg
Mean motion: 15
53202452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3309
Checksum: 275
Coasting Arc #5 (Orbit 3321)
---------------------------------------
Vector Time (GMT): 2019/026/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4760357
45 A = 6784363
89 meter
Y = 2290826
50 meter E =
0005939
Z = 4251161
55 I = 51
54323
XDOT = -5265
638809 Wp = 85
25399
YDOT = 4259
949211 meter/sec RA = 345
97351 deg
ZDOT = 3596
929657 TA = 327
93287
MA = 327
96899
Ha = 221
799 n
mi
Hp = 217
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15617970
64 X = 4713737
56
Y = 7515834
98 feet Y = 2343799
54 meter
Z = 13947380
42 Z = 4274171
92
XDOT = -17275
717876 XDOT = -5330
354999
YDOT = 13976
211323 feet/sec YDOT = 4200
703375 meter/sec
ZDOT = 11800
950319 ZDOT = 3571
194344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10314342
27 X = -3143811
52
Y = 13824791
33 feet Y = 4213796
40 meter
Z = 14050896
45 Z = 4282713
24
XDOT = -9438
690066 XDOT = -2876
912732
YDOT = -18930
086312 feet/sec YDOT = -5769
890308 meter/sec
ZDOT = 11684
250938 ZDOT = 3561
359686
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 19026
42872029
00016717 00000-0 10270-3 0 9043
2 25544 51
6390 346
2661 0004848 313
7169 46
3581 15
53162091 33228
Satellite: ISS
Catalog Number: 25544
Epoch time: 19026
42872029 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 346
2661 deg
Eccentricity:
0004848
Arg of perigee: 313
7169 deg
Mean anomaly: 46
3581 deg
Mean motion: 15
53162091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3322
Checksum: 305
Coasting Arc #6 (Orbit 3336)
---------------------------------------
Vector Time (GMT): 2019/027/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3649826
49 A = 6781699
77 meter
Y = -2896014
96 meter E =
0011212
Z = -4937798
50 I = 51
50280
XDOT = 6156
352600 Wp = 51
08213
YDOT = -3982
384004 meter/sec RA = 340
98162 deg
ZDOT = -2211
364356 TA = 197
24810
MA = 197
28622
Ha = 222
037 n
mi
Hp = 217
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11974496
37 X = -3593186
43
Y = -9501361
41 feet Y = -2936513
20 meter
Z = -16200126
31 Z = -4955390
15
XDOT = 20198
007217 XDOT = 6211
168618
YDOT = -13065
564319 feet/sec YDOT = -3913
232896 meter/sec
ZDOT = -7255
132400 ZDOT = -2181
326363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11401850
72 X = 3475284
10
Y = -10054701
99 feet Y = -3064673
17 meter
Z = -16279106
01 Z = -4961871
51
XDOT = 8655
830241 XDOT = 2638
297057
YDOT = 21360
237334 feet/sec YDOT = 6510
600339 meter/sec
ZDOT = -7119
069204 ZDOT = -2169
892293
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 19027
39384386
00016717 00000-0 10270-3 0 9055
2 25544 51
6394 341
4621 0004764 318
5556 41
5234 15
53173876 33376
Satellite: ISS
Catalog Number: 25544
Epoch time: 19027
39384386 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 341
4621 deg
Eccentricity:
0004764
Arg of perigee: 318
5556 deg
Mean anomaly: 41
5234 deg
Mean motion: 15
53173876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3337
Checksum: 325
Coasting Arc #7 (Orbit 3352)
---------------------------------------
Vector Time (GMT): 2019/028/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2403416
90 A = 6780277
51 meter
Y = 3524254
95 meter E =
0002657
Z = 5270322
35 I = 51
46568
XDOT = -6740
305502 Wp = 351
38276
YDOT = 3591
687768 meter/sec RA = 335
98231 deg
ZDOT = 674
635116 TA = 92
17393
MA = 92
14350
Ha = 222
132 n
mi
Hp = 217
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7885226
05 X = 2338229
09
Y = 11562516
23 feet Y = 3550767
10 meter
Z = 17291083
82 Z = 5281838
80
XDOT = -22113
863196 XDOT = -6783
244777
YDOT = 11783
752521 feet/sec YDOT = 3516
072880 meter/sec
ZDOT = 2213
369803 ZDOT = 641
789392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12628446
06 X = -3849150
36
Y = 5882843
98 feet Y = 1793090
85 meter
Z = 17342567
51 Z = 5286014
58
XDOT = -7781
929589 XDOT = -2371
932139
YDOT = -22766
598529 feet/sec YDOT = -6939
259232 meter/sec
ZDOT = 2064
703017 ZDOT = 629
321480
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 19028
42330687
00016717 00000-0 10270-3 0 9066
2 25544 51
6382 336
3372 0004926 322
0154 38
0650 15
53167627 33531
Satellite: ISS
Catalog Number: 25544
Epoch time: 19028
42330687 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 336
3372 deg
Eccentricity:
0004926
Arg of perigee: 322
0154 deg
Mean anomaly: 38
0650 deg
Mean motion: 15
53167627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3353
Checksum: 301
Coasting Arc #8 (Orbit 3367)
---------------------------------------
Vector Time (GMT): 2019/029/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1137177
92 A = 6780474
41 meter
Y = -4153195
17 meter E =
0011709
Z = -5247259
58 I = 51
43607
XDOT = 6969
842352 Wp = 78
47876
YDOT = -3043
698760 meter/sec RA = 330
98008 deg
ZDOT = 902
591718 TA = 200
16675
MA = 200
21304
Ha = 222
294 n
mi
Hp = 217
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3730898
70 X = -1065163
27
Y = -13625968
40 feet Y = -4165509
11 meter
Z = -17215418
58 Z = -5252608
68
XDOT = 22866
936851 XDOT = 6998
975608
YDOT = -9985
888320 feet/sec YDOT = -2965
594250 meter/sec
ZDOT = 2961
258916 ZDOT = 936
518848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13995814
21 X = 4265924
17
Y = -1700432
94 feet Y = -518291
96 meter
Z = -17238995
59 Z = -5254445
86
XDOT = 6612
972968 XDOT = 2015
634161
YDOT = 22985
565842 feet/sec YDOT = 7006
000469 meter/sec
ZDOT = 3114
721247 ZDOT = 949
367036
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 19029
38842726
00016717 00000-0 10270-3 0 9075
2 25544 51
6380 331
5335 0004947 325
6651 34
4181 15
53159691 33686
Satellite: ISS
Catalog Number: 25544
Epoch time: 19029
38842726 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 331
5335 deg
Eccentricity:
0004947
Arg of perigee: 325
6651 deg
Mean anomaly: 34
4181 deg
Mean motion: 15
53159691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3368
Checksum: 325
Coasting Arc #9 (Orbit 3383)
---------------------------------------
Vector Time (GMT): 2019/030/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -121463
59 A = 6782132
56 meter
Y = 4745337
79 meter E =
0008614
Z = 4844000
53 I = 51
41358
XDOT = -6892
935697 Wp = 23
92310
YDOT = 2313
771780 meter/sec RA = 325
97699 deg
ZDOT = -2430
239172 TA = 90
05163
MA = 89
95292
Ha = 222
404 n
mi
Hp = 216
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -398502
59 X = -198047
37
Y = 15568693
52 feet Y = 4743551
13 meter
Z = 15892390
19 Z = 4843224
67
XDOT = -22614
618430 XDOT = -6906
492079
YDOT = 7591
114764 feet/sec YDOT = 2236
614450 meter/sec
ZDOT = -7973
225630 ZDOT = -2463
754814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15394463
97 X = -4692232
62
Y = -2384264
43 feet Y = -726723
80 meter
Z = 15888261
40 Z = 4842742
08
XDOT = -4979
799648 XDOT = -1517
842933
YDOT = -22190
721193 feet/sec YDOT = -6763
731820 meter/sec
ZDOT = -8124
726786 ZDOT = -2476
416724
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 19030
41788635
00016717 00000-0 10270-3 0 9080
2 25544 51
6383 326
4085 0005030 328
9269 31
1585 15
53186679 33845
Satellite: ISS
Catalog Number: 25544
Epoch time: 19030
41788635 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 326
4085 deg
Eccentricity:
0005030
Arg of perigee: 328
9269 deg
Mean anomaly: 31
1585 deg
Mean motion: 15
53186679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3384
Checksum: 329
Coasting Arc #10 (Orbit 3398)
---------------------------------------
Vector Time (GMT): 2019/031/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1249325
66 A = 6784967
09 meter
Y = -5246275
28 meter E =
0005261
Z = -4119827
64 I = 51
39640
XDOT = 6519
617586 Wp = 65
30105
YDOT = -1405
934187 meter/sec RA = 320
97778 deg
ZDOT = 3773
357382 TA = 243
73003
MA = 243
78410
Ha = 222
591 n
mi
Hp = 216
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4098837
46 X = 1327909
61
Y = -17212189
23 feet Y = -5231864
89 meter
Z = -13516494
87 Z = -4113568
34
XDOT = 21389
821477 XDOT = 6516
526049
YDOT = -4612
644972 feet/sec YDOT = -1333
044715 meter/sec
ZDOT = 12379
781438 ZDOT = 3805
019104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16684964
31 X = 5085577
12
Y = 5954239
30 feet Y = 1814852
14 meter
Z = -13487570
59 Z = -4111011
52
XDOT = 2808
029853 XDOT = 855
887499
YDOT = 20453
672159 feet/sec YDOT = 6234
279274 meter/sec
ZDOT = 12522
794071 ZDOT = 3816
947633
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 19031
38300192
00016717 00000-0 10270-3 0 9096
2 25544 51
6388 321
6044 0005114 333
8834 26
2060 15
53167585 33992
Satellite: ISS
Catalog Number: 25544
Epoch time: 19031
38300192 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 321
6044 deg
Eccentricity:
0005114
Arg of perigee: 333
8834 deg
Mean anomaly: 26
2060 deg
Mean motion: 15
53167585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3399
Checksum: 302
Coasting Arc #11 (Orbit 3414)
---------------------------------------
Vector Time (GMT): 2019/032/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2257759
33 A = 6788056
83 meter
Y = 5606998
96 meter E =
0011478
Z = 3083759
33 I = 51
38144
XDOT = -5913
488988 Wp = 72
11384
YDOT = 306
365825 meter/sec RA = 315
98342 deg
ZDOT = -4868
136986 TA = 72
31974
MA = 72
19446
Ha = 222
679 n
mi
Hp = 216
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7407346
89 X = -2335269
44
Y = 18395665
89 feet Y = 5581317
61 meter
Z = 10117320
65 Z = 3072604
19
XDOT = -19401
210589 XDOT = -5892
829160
YDOT = 1005
137221 feet/sec YDOT = 240
352780 meter/sec
ZDOT = -15971
578039 ZDOT = -4896
811695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17678687
28 X = -5388463
88
Y = -9042324
75 feet Y = -2756100
58 meter
Z = 10066273
77 Z = 3068200
25
XDOT = 13
969783 XDOT = 4
257990
YDOT = -18019
240628 feet/sec YDOT = -5492
264543 meter/sec
ZDOT = -16100
969692 ZDOT = -4907
575562
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 19032
41245700
00016717 00000-0 10270-3 0 9106
2 25544 51
6384 316
4797 0005196 337
2026 22
8894 15
53196234 34155
Satellite: ISS
Catalog Number: 25544
Epoch time: 19032
41245700 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 316
4797 deg
Eccentricity:
0005196
Arg of perigee: 337
2026 deg
Mean anomaly: 22
8894 deg
Mean motion: 15
53196234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3415
Checksum: 305
Coasting Arc #12 (Orbit 3429)
---------------------------------------
Vector Time (GMT): 2019/033/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3047446
84 A = 6790623
22 meter
Y = -5769937
99 meter E =
0010874
Z = -1857863
54 I = 51
36715
XDOT = 5145
406802 Wp = 14
83601
YDOT = 916
446596 meter/sec RA = 310
99437 deg
ZDOT = 5611
403594 TA = 324
64312
MA = 324
71517
Ha = 222
772 n
mi
Hp = 216
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9998185
18 X = 3120765
67
Y = -18930242
77 feet Y = -5735449
31 meter
Z = -6095352
82 Z = -1842882
66
XDOT = 16881
255913 XDOT = 5107
520014
YDOT = 3006
714554 feet/sec YDOT = 973
774098 meter/sec
ZDOT = 18410
116779 ZDOT = 5636
305451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18186182
57 X = 5543148
45
Y = 11331755
48 feet Y = 3453919
07 meter
Z = -6027039
51 Z = -1837041
64
XDOT = -3340
592584 XDOT = -1018
212619
YDOT = 15181
706121 feet/sec YDOT = 4627
384026 meter/sec
ZDOT = 18522
331845 ZDOT = 5645
606746
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 19033
37756966
00016717 00000-0 10270-3 0 9114
2 25544 51
6387 311
6759 0005136 340
7751 19
3206 15
53191180 34301
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
37756966 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 311
6759 deg
Eccentricity:
0005136
Arg of perigee: 340
7751 deg
Mean anomaly: 19
3206 deg
Mean motion: 15
53191180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3430
Checksum: 309
Coasting Arc #13 (Orbit 3435)
---------------------------------------
Vector Time (GMT): 2019/033/17:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5298444
97 A = 6789650
45 meter
Y = 3558067
39 meter E =
0002503
Z = -2320208
07 I = 51
35627
XDOT = -1214
885121 Wp = 67
10215
YDOT = -5315
571129 meter/sec RA = 309
21970 deg
ZDOT = -5380
867044 TA = 138
83874
MA = 138
81985
Ha = 222
750 n
mi
Hp = 216
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17383349
63 X = -5326568
50
Y = 11673449
43 feet Y = 3498659
30 meter
Z = -7612231
21 Z = -2346013
48
XDOT = -3985
843572 XDOT = -1129
218021
YDOT = -17439
537824 feet/sec YDOT = -5328
677670 meter/sec
ZDOT = -17653
763268 ZDOT = -5386
560440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6906136
29 X = -2104990
34
Y = 19722139
76 feet Y = 6011308
20 meter
Z = -7729088
88 Z = -2355826
29
XDOT = -12094
412262 XDOT = -3686
376858
YDOT = -11158
738170 feet/sec YDOT = -3401
183394 meter/sec
ZDOT = -17678
773487 ZDOT = -5388
490159
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 19033
76361258
00016717 00000-0 10270-3 0 9124
2 25544 51
6386 309
7526 0005248 340
4754 19
6196 15
53209191 34363
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
76361258 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 309
7526 deg
Eccentricity:
0005248
Arg of perigee: 340
4754 deg
Mean anomaly: 19
6196 deg
Mean motion: 15
53209191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3436
Checksum: 321
Coasting Arc #14 (Orbit 3451)
---------------------------------------
Vector Time (GMT): 2019/034/17:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5176268
06 A = 6786724
68 meter
Y = -2655145
16 meter E =
0011560
Z = 3481411
53 I = 51
32599
XDOT = 144
673620 Wp = 66
91216
YDOT = 6204
705712 meter/sec RA = 304
22506 deg
ZDOT = 4509
492502 TA = 334
21574
MA = 334
27331
Ha = 222
633 n
mi
Hp = 216
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16982506
77 X = 5188663
64
Y = -8711106
17 feet Y = -2597191
27 meter
Z = 11421953
82 Z = 3506585
26
XDOT = 474
650985 XDOT = 53
376100
YDOT = 20356
646037 feet/sec YDOT = 6205
813011 meter/sec
ZDOT = 14794
922906 ZDOT = 4509
973605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8041514
84 X = 2451053
72
Y = -17233930
52 feet Y = -5252902
02 meter
Z = 11535840
41 Z = 3516124
16
XDOT = 11497
366825 XDOT = 3504
397408
YDOT = 15285
282328 feet/sec YDOT = 4658
954054 meter/sec
ZDOT = 14796
324021 ZDOT = 4509
919562
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 19034
79306163
00016717 00000-0 10270-3 0 9133
2 25544 51
6381 304
6272 0005114 342
9311 17
1668 15
53221599 34529
Satellite: ISS
Catalog Number: 25544
Epoch time: 19034
79306163 = yrday
fracday
Element set: 913
Inclination: 51
6381 deg
RA of node: 304
6272 deg
Eccentricity:
0005114
Arg of perigee: 342
9311 deg
Mean anomaly: 17
1668 deg
Mean motion: 15
53221599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3452
Checksum: 296
Coasting Arc #15 (Orbit 3466)
---------------------------------------
Vector Time (GMT): 2019/035/17:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4921250
86 A = 6783632
10 meter
Y = 1550928
37 meter E =
0011316
Z = -4415314
54 I = 51
29696
XDOT = 804
743486 Wp = 43
17934
YDOT = -6860
574330 meter/sec RA = 299
22311 deg
ZDOT = -3303
753668 TA = 193
24085
MA = 193
27057
Ha = 222
965 n
mi
Hp = 216
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16145836
15 X = -4916781
50
Y = 5088347
68 feet Y = 1495920
49 meter
Z = -14485940
11 Z = -4439208
59
XDOT = 2640
234534 XDOT = 897
447889
YDOT = -22508
445963 feet/sec YDOT = -6851
056793 meter/sec
ZDOT = -10839
086837 ZDOT = -3299
619466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9340924
57 X = -2847113
81
Y = 14006663
64 feet Y = 4269231
08 meter
Z = -14593912
08 Z = -4448224
40
XDOT = -10939
588994 XDOT = -3334
386725
YDOT = -18579
120696 feet/sec YDOT = -5662
915988 meter/sec
ZDOT = -10819
606674 ZDOT = -3297
816114
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 19035
75817127
00016717 00000-0 10270-3 0 9148
2 25544 51
6373 299
8232 0005054 350
1210 9
9842 15
53212827 34676
Satellite: ISS
Catalog Number: 25544
Epoch time: 19035
75817127 = yrday
fracday
Element set: 914
Inclination: 51
6373 deg
RA of node: 299
8232 deg
Eccentricity:
0005054
Arg of perigee: 350
1210 deg
Mean anomaly: 9
9842 deg
Mean motion: 15
53212827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3467
Checksum: 308
Coasting Arc #16 (Orbit 3482)
---------------------------------------
Vector Time (GMT): 2019/036/17:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4544203
85 A = 6781262
30 meter
Y = -287033
80 meter E =
0004343
Z = 5021334
39 I = 51
27303
XDOT = -1614
438846 Wp = 63
64516
YDOT = 7259
619406 meter/sec RA = 294
21263 deg
ZDOT = 1876
646215 TA = 8
08047
MA = 8
07347
Ha = 222
935 n
mi
Hp = 216
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14908805
27 X = 4522685
66
Y = -941711
94 feet Y = -236337
56 meter
Z = 16474194
20 Z = 5043355
54
XDOT = -5296
715374 XDOT = -1704
613413
YDOT = 23817
648971 feet/sec YDOT = 7241
061466 meter/sec
ZDOT = 6156
975771 ZDOT = 1868
584943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10785337
73 X = 3287370
94
Y = -10176044
42 feet Y = -3101658
34 meter
Z = 16573562
69 Z = 5051621
91
XDOT = 10364
672660 XDOT = 3159
152227
YDOT = 20949
051328 feet/sec YDOT = 6385
270845 meter/sec
ZDOT = 6119
754428 ZDOT = 1865
301150
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 19036
78761940
00016717 00000-0 10270-3 0 9154
2 25544 51
6369 294
6981 0005104 352
3343 7
7730 15
53178994 34838
Satellite: ISS
Catalog Number: 25544
Epoch time: 19036
78761940 = yrday
fracday
Element set: 915
Inclination: 51
6369 deg
RA of node: 294
6981 deg
Eccentricity:
0005104
Arg of perigee: 352
3343 deg
Mean anomaly: 7
7730 deg
Mean motion: 15
53178994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3483
Checksum: 336
Coasting Arc #17 (Orbit 3487)
---------------------------------------
Vector Time (GMT): 2019/037/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4354388
26 A = 6780460
97 meter
Y = 355099
20 meter E =
0003835
Z = 5182588
11 I = 51
26926
XDOT = -2007
854919 Wp = 42
85595
YDOT = 7306
090066 meter/sec RA = 292
59468 deg
ZDOT = 1188
638512 TA = 35
69780
MA = 35
67216
Ha = 222
878 n
mi
Hp = 216
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14286050
72 X = 4324920
39
Y = 1165023
61 feet Y = 403628
37 meter
Z = 17003241
83 Z = 5203667
92
XDOT = -6587
450521 XDOT = -2095
178034
YDOT = 23970
111766 feet/sec YDOT = 7283
148609 meter/sec
ZDOT = 3899
732651 ZDOT = 1178
673108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12504117
69 X = -3811255
07
Y = -6771583
38 feet Y = -2063978
62 meter
Z = 17098288
13 Z = 5211558
22
XDOT = 15207
910693 XDOT = 4635
371179
YDOT = -18369
588092 feet/sec YDOT = -5599
050450 meter/sec
ZDOT = 3853
923769 ZDOT = 1174
675965
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 19037
10931935
00016717 00000-0 10270-3 0 9165
2 25544 51
6398 293
0993 0005060 352
4926 7
6150 15
53215190 34885
Satellite: ISS
Catalog Number: 25544
Epoch time: 19037
10931935 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 293
0993 deg
Eccentricity:
0005060
Arg of perigee: 352
4926 deg
Mean anomaly: 7
6150 deg
Mean motion: 15
53215190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3488
Checksum: 314
Coasting Arc #18 (Orbit 3502)
---------------------------------------
Vector Time (GMT): 2019/038/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3908067
27 A = 6780158
17 meter
Y = -1703939
42 meter E =
0015145
Z = -5284360
19 I = 51
25634
XDOT = 2608
558903 Wp = 73
04234
YDOT = -7187
721168 meter/sec RA = 287
57848 deg
ZDOT = 393
784283 TA = 200
70781
MA = 200
76925
Ha = 223
192 n
mi
Hp = 215
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12821743
02 X = -3863055
08
Y = -5590352
42 feet Y = -1747390
70 meter
Z = -17337139
73 Z = -5303234
22
XDOT = 8558
264117 XDOT = 2686
827422
YDOT = -23581
762363 feet/sec YDOT = -7158
112799 meter/sec
ZDOT = 1291
943185 ZDOT = 406
645741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9555136
92 X = 2912405
73
Y = 10069556
48 feet Y = 3069200
81 meter
Z = -17422081
93 Z = -5310250
57
XDOT = -16268
589790 XDOT = -4958
666168
YDOT = 17744
763250 feet/sec YDOT = 5408
603839 meter/sec
ZDOT = 1350
779615 ZDOT = 411
717627
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 19038
07442410
00016717 00000-0 10270-3 0 9178
2 25544 51
6400 288
2950 0005205 357
1948 2
9174 15
53185957 35034
Satellite: ISS
Catalog Number: 25544
Epoch time: 19038
07442410 = yrday
fracday
Element set: 917
Inclination: 51
6400 deg
RA of node: 288
2950 deg
Eccentricity:
0005205
Arg of perigee: 357
1948 deg
Mean anomaly: 2
9174 deg
Mean motion: 15
53185957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3503
Checksum: 306
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