[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 21st 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 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
020/01:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 217
9
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
7
000/00:00:00
000 0
0 0
0 216
5
Coasting Arc #1 (Orbit 3203)
---------------------------------------
Vector Time (GMT): 2019/018/18:48:39
601
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1043954
25 A = 6782170
60 meter
Y = 4627526
35 meter E =
0002901
Z = 4846719
27 I = 51
78511
XDOT = -7177
114377 Wp = 148
33925
YDOT = -1004
001777 meter/sec RA = 23
73265 deg
ZDOT = 2501
415205 TA = 277
10791
MA = 277
14090
Ha = 220
958 n
mi
Hp = 217
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3425046
76 X = 968587
96
Y = 15182173
05 feet Y = 4638778
67 meter
Z = 15901309
95 Z = 4851607
79
XDOT = -23546
963178 XDOT = -7177
504280
YDOT = -3293
969084 feet/sec YDOT = -1084
263706 meter/sec
ZDOT = 8206
742797 ZDOT = 2466
550809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12162982
43 X = 3707277
04
Y = 9675208
32 feet Y = 2949003
50 meter
Z = 15922725
41 Z = 4853246
70
XDOT = -19672
269711 XDOT = -5996
107808
YDOT = 11466
646620 feet/sec YDOT = 3495
033890 meter/sec
ZDOT = 8049
512558 ZDOT = 2453
491428
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 19018
83636545
00016717 00000-0 10270-3 0 9006
2 25544 51
6414 24
0608 0004702 283
2659 76
7968 15
53158051 32047
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
83636545 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 24
0608 deg
Eccentricity:
0004702
Arg of perigee: 283
2659 deg
Mean anomaly: 76
7968 deg
Mean motion: 15
53158051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3204
Checksum: 307
Coasting Arc #2 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2019/019/18:48:39
601
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 272502
68 A = 6780413
02 meter
Y = -4284320
17 meter E =
0010170
Z = -5257048
69 I = 51
74904
XDOT = 7404
999246 Wp = 70
81516
YDOT = 1689
126855 meter/sec RA = 18
75402 deg
ZDOT = -991
044406 TA = 189
69181
MA = 189
71144
Ha = 220
992 n
mi
Hp = 217
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 894037
66 X = 345926
28
Y = -14056168
53 feet Y = -4280861
76 meter
Z = -17247535
08 Z = -5255547
12
XDOT = 24294
616949 XDOT = 7390
374465
YDOT = 5541
754774 feet/sec YDOT = 1771
853045 meter/sec
ZDOT = -3251
458025 ZDOT = -955
109648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8293660
83 X = -2527907
82
Y = -11394953
10 feet Y = -3473181
70 meter
Z = -17240153
06 Z = -5254798
65
XDOT = 21327
208449 XDOT = 6500
533135
YDOT = -10840
006917 feet/sec YDOT = -3304
034108 meter/sec
ZDOT = -3089
494775 ZDOT = -941
678007
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 19019
80150010
00016717 00000-0 10270-3 0 9013
2 25544 51
6420 19
2569 0004880 287
2691 72
7927 15
53179398 32197
Satellite: ISS
Catalog Number: 25544
Epoch time: 19019
80150010 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 19
2569 deg
Eccentricity:
0004880
Arg of perigee: 287
2691 deg
Mean anomaly: 72
7927 deg
Mean motion: 15
53179398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3219
Checksum: 314
Coasting Arc #3 (Orbit 3223)
---------------------------------------
Vector Time (GMT): 2019/020/01:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2289170
65 A = 6783239
50 meter
Y = 4475434
17 meter E =
0004072
Z = 4552797
38 I = 51
74658
XDOT = -6991
213767 Wp = 125
89871
YDOT = 395
529634 meter/sec RA = 17
34317 deg
ZDOT = 3122
124986 TA = 292
84347
MA = 292
88647
Ha = 220
856 n
mi
Hp = 217
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7510402
40 X = 2216840
41
Y = 14683182
98 feet Y = 4500628
38 meter
Z = 14936999
28 Z = 4563741
90
XDOT = -22937
053041 XDOT = -7010
282355
YDOT = 1297
669403 feet/sec YDOT = 317
242071 meter/sec
ZDOT = 10243
192212 ZDOT = 3088
118656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2842243
47 X = 866315
81
Y = -16200751
12 feet Y = -4937988
94 meter
Z = 14985768
90 Z = 4567662
36
XDOT = 18033
075094 XDOT = 5496
481289
YDOT = 12509
631430 feet/sec YDOT = 3812
935660 meter/sec
ZDOT = 10089
639734 ZDOT = 3075
322191
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 19020
12321084
00016717 00000-0 10270-3 0 9022
2 25544 51
6390 17
6496 0004751 282
6517 77
4104 15
53182579 32247
Satellite: ISS
Catalog Number: 25544
Epoch time: 19020
12321084 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 17
6496 deg
Eccentricity:
0004751
Arg of perigee: 282
6517 deg
Mean anomaly: 77
4104 deg
Mean motion: 15
53182579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3224
Checksum: 293
Coasting Arc #4 (Orbit 3238)
---------------------------------------
Vector Time (GMT): 2019/021/01:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -981010
15 A = 6781004
27 meter
Y = -4350719
47 meter E =
0009845
Z = -5116642
18 I = 51
70777
XDOT = 7469
172088 Wp = 63
65311
YDOT = 285
208006 meter/sec RA = 12
36411 deg
ZDOT = -1672
803823 TA = 190
18050
MA = 190
20045
Ha = 221
092 n
mi
Hp = 217
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3218537
23 X = -907433
08
Y = -14274014
02 feet Y = -4361277
97 meter
Z = -16786883
81 Z = -5121229
12
XDOT = 24505
157770 XDOT = 7473
553045
YDOT = 935
721804 feet/sec YDOT = 368
758130 meter/sec
ZDOT = -5488
201519 ZDOT = -1636
511611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5817643
23 X = -1773217
66
Y = 13400989
91 feet Y = 4084621
73 meter
Z = -16806975
42 Z = -5122766
11
XDOT = -18395
241472 XDOT = -5606
869601
YDOT = -14670
705238 feet/sec YDOT = -4471
630956 meter/sec
ZDOT = -5324
429355 ZDOT = -1622
886067
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 19021
08834435
00016717 00000-0 10270-3 0 9038
2 25544 51
6398 12
8462 0004560 288
3162 71
7494 15
53175508 32391
Satellite: ISS
Catalog Number: 25544
Epoch time: 19021
08834435 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 12
8462 deg
Eccentricity:
0004560
Arg of perigee: 288
3162 deg
Mean anomaly: 71
7494 deg
Mean motion: 15
53175508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3239
Checksum: 313
Coasting Arc #5 (Orbit 3254)
---------------------------------------
Vector Time (GMT): 2019/022/01:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -415958
89 A = 6780198
70 meter
Y = 4186145
84 meter E =
0002446
Z = 5318940
22 I = 51
67177
XDOT = -7612
561888 Wp = 310
33942
YDOT = -896
525285 meter/sec RA = 7
37766 deg
ZDOT = 111
842355 TA = 138
60421
MA = 138
58568
Ha = 221
270 n
mi
Hp = 217
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1364694
52 X = -488574
36
Y = 13734074
27 feet Y = 4181087
97 meter
Z = 17450591
28 Z = 5316743
59
XDOT = -24975
596746 XDOT = -7602
514168
YDOT = -2941
355923 feet/sec YDOT = -981
598082 meter/sec
ZDOT = 366
936861 ZDOT = 74
888777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9047500
29 X = 2757678
09
Y = -10440129
19 feet Y = -3182151
38 meter
Z = 17440090
72 Z = 5315739
65
XDOT = 18082
692041 XDOT = 5511
604534
YDOT = 15996
484059 feet/sec YDOT = 4875
728341 meter/sec
ZDOT = 200
269774 ZDOT = 61
042227
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 19022
11781903
00016717 00000-0 10270-3 0 9045
2 25544 51
6395 7
7208 0004597 292
1673 67
8991 15
53150701 32553
Satellite: ISS
Catalog Number: 25544
Epoch time: 19022
11781903 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 7
7208 deg
Eccentricity:
0004597
Arg of perigee: 292
1673 deg
Mean anomaly: 67
8991 deg
Mean motion: 15
53150701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3255
Checksum: 312
Coasting Arc #6 (Orbit 3269)
---------------------------------------
Vector Time (GMT): 2019/023/01:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1809838
07 A = 6780867
84 meter
Y = -4014949
28 meter E =
0009276
Z = -5164199
44 I = 51
64192
XDOT = 7378
073196 Wp = 94
28217
YDOT = 1458
937555 meter/sec RA = 2
39056 deg
ZDOT = 1453
022314 TA = 189
70787
MA = 189
72580
Ha = 221
282 n
mi
Hp = 217
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5937788
95 X = 1879683
95
Y = -13172405
76 feet Y = -3994319
74 meter
Z = -16942911
56 Z = -5155238
65
XDOT = 24206
276889 XDOT = 7354
152826
YDOT = 4786
540535 feet/sec YDOT = 1541
310525 meter/sec
ZDOT = 4767
133575 ZDOT = 1488
803141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12352856
13 X = -3765150
55
Y = 7587108
37 feet Y = 2312550
63 meter
Z = -16901910
99 Z = -5151702
47
XDOT = -16880
537578 XDOT = -5145
187854
YDOT = -16516
267702 feet/sec YDOT = -5034
158396 meter/sec
ZDOT = 4928
422143 ZDOT = 1502
183069
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
08294898
00016717 00000-0 10270-3 0 9055
2 25544 51
6404 2
9176 0004609 294
8670 65
1992 15
53178236 32707
Satellite: ISS
Catalog Number: 25544
Epoch time: 19023
08294898 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 2
9176 deg
Eccentricity:
0004609
Arg of perigee: 294
8670 deg
Mean anomaly: 65
1992 deg
Mean motion: 15
53178236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3270
Checksum: 326
Coasting Arc #7 (Orbit 3285)
---------------------------------------
Vector Time (GMT): 2019/024/01:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3137729
50 A = 6783156
99 meter
Y = 3823008
35 meter E =
0006783
Z = 4641905
74 I = 51
61691
XDOT = -6793
385675 Wp = 32
07816
YDOT = -2012
636364 meter/sec RA = 357
40282 deg
ZDOT = -2926
870984 TA = 87
10856
MA = 87
03094
Ha = 221
550 n
mi
Hp = 217
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10294388
13 X = -3202793
46
Y = 12542678
31 feet Y = 3787556
28 meter
Z = 15229349
55 Z = 4626506
21
XDOT = -22288
010746 XDOT = -6756
158177
YDOT = -6603
137676 feet/sec YDOT = -2088
396587 meter/sec
ZDOT = -9602
595092 ZDOT = -2959
779418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15532329
77 X = 4734254
11
Y = -4916085
80 feet Y = -1498422
95 meter
Z = 15159324
73 Z = 4620562
18
XDOT = 14748
636947 XDOT = 4495
384541
YDOT = 16453
231755 feet/sec YDOT = 5014
945039 meter/sec
ZDOT = -9750
834688 ZDOT = -2972
054413
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
11242090
00016717 00000-0 10270-3 0 9068
2 25544 51
6414 357
7924 0004535 299
4511 60
6189 15
53141304 32864
Satellite: ISS
Catalog Number: 25544
Epoch time: 19024
11242090 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 357
7924 deg
Eccentricity:
0004535
Arg of perigee: 299
4511 deg
Mean anomaly: 60
6189 deg
Mean motion: 15
53141304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3286
Checksum: 296
Coasting Arc #8 (Orbit 3300)
---------------------------------------
Vector Time (GMT): 2019/025/01:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4291400
39 A = 6786096
23 meter
Y = -3620064
90 meter E =
0002292
Z = -3812428
89 I = 51
59368
XDOT = 5882
754452 Wp = 56
51785
YDOT = 2566
494830 meter/sec RA = 352
42034 deg
ZDOT = 4187
888122 TA = 257
68387
MA = 257
70954
Ha = 221
651 n
mi
Hp = 217
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14079397
59 X = 4350080
28
Y = -11876853
35 feet Y = -3571747
43 meter
Z = -12507968
80 Z = -3791440
77
XDOT = 19300
375499 XDOT = 5833
275990
YDOT = 8420
258629 feet/sec YDOT = 2632
003306 meter/sec
ZDOT = 13739
790427 ZDOT = 4216
343487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18295808
84 X = -5576562
54
Y = 2631555
20 feet Y = 802098
02 meter
Z = -12412762
05 Z = -3783409
87
XDOT = -11695
187811 XDOT = -3564
693245
YDOT = -15944
942579 feet/sec YDOT = -4860
018498 meter/sec
ZDOT = 13867
849077 ZDOT = 4226
920399
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
07754733
00016717 00000-0 10270-3 0 9077
2 25544 51
6413 352
9892 0004707 303
7282 56
3421 15
53155600 33012
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
07754733 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 352
9892 deg
Eccentricity:
0004707
Arg of perigee: 303
7282 deg
Mean anomaly: 56
3421 deg
Mean motion: 15
53155600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3301
Checksum: 293
Coasting Arc #9 (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 = 4248074
71 A = 6783511
17 meter
Y = 2847577
35 meter E =
0004579
Z = 4452712
68 I = 51
56894
XDOT = -5889
133615 Wp = 91
91988
YDOT = 3660
829611 meter/sec RA = 350
13773 deg
ZDOT = 3274
260941 TA = 325
03592
MA = 325
06598
Ha = 221
606 n
mi
Hp = 217
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13937252
98 X = 4194288
21
Y = 9342445
38 feet Y = 2894781
63 meter
Z = 14608637
41 Z = 4473217
13
XDOT = -19321
304512 XDOT = -5945
536572
YDOT = 12010
595836 feet/sec YDOT = 3594
657904 meter/sec
ZDOT = 10742
325923 ZDOT = 3245
517265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3865969
59 X = 1178347
53
Y = 16244447
42 feet Y = 4951307
57 meter
Z = 14700775
51 Z = 4480796
38
XDOT = -21221
370712 XDOT = -6468
273793
YDOT = -4562
302272 feet/sec YDOT = -1390
589732 meter/sec
ZDOT = 10612
122077 ZDOT = 3234
574809
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
59228040
00016717 00000-0 10270-3 0 9082
2 25544 51
6399 350
4305 0004943 309
3230 50
7483 15
53202233 33093
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
59228040 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 350
4305 deg
Eccentricity:
0004943
Arg of perigee: 309
3230 deg
Mean anomaly: 50
7483 deg
Mean motion: 15
53202233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3309
Checksum: 289
Coasting Arc #10 (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 = 4761902
39 A = 6784368
77 meter
Y = 2289621
96 meter E =
0005943
Z = 4250091
74 I = 51
54319
XDOT = -5263
881182 Wp = 85
35713
YDOT = 4260
752198 meter/sec RA = 345
97423 deg
ZDOT = 3598
539046 TA = 327
81043
MA = 327
84670
Ha = 221
795 n
mi
Hp = 217
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15623039
34 X = 4715301
05
Y = 7511883
07 feet Y = 2342612
38 meter
Z = 13943870
55 Z = 4273109
67
XDOT = -17269
951384 XDOT = -5328
614300
YDOT = 13978
845794 feet/sec YDOT = 4201
525922 meter/sec
ZDOT = 11806
230466 ZDOT = 3572
812230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10311423
27 X = -3142921
81
Y = 13830538
32 feet Y = 4215548
08 meter
Z = 14047420
82 Z = 4281653
87
XDOT = -9441
941105 XDOT = -2877
903649
YDOT = -18925
169065 feet/sec YDOT = -5768
391531 meter/sec
ZDOT = 11689
569313 ZDOT = 3562
980726
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
42872374
00016717 00000-0 10270-3 0 9091
2 25544 51
6389 346
2667 0004839 313
5997 46
4754 15
53161750 33223
Satellite: ISS
Catalog Number: 25544
Epoch time: 19026
42872374 = yrday
fracday
Element set: 909
Inclination: 51
6389 deg
RA of node: 346
2667 deg
Eccentricity:
0004839
Arg of perigee: 313
5997 deg
Mean anomaly: 46
4754 deg
Mean motion: 15
53161750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3322
Checksum: 338
Coasting Arc #11 (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 = -3651762
80 A = 6781704
38 meter
Y = -2894786
82 meter E =
0011200
Z = -4937084
96 I = 51
50276
XDOT = 6154
912634 Wp = 51
10609
YDOT = -3983
495246 meter/sec RA = 340
98234 deg
ZDOT = -2213
385040 TA = 197
20342
MA = 197
24141
Ha = 222
034 n
mi
Hp = 217
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11980849
10 X = -3595139
80
Y = -9497332
09 feet Y = -2935306
81 meter
Z = -16197785
31 Z = -4954686
06
XDOT = 20193
282920 XDOT = 6209
751001
YDOT = -13069
210124 feet/sec YDOT = -3914
360115 meter/sec
ZDOT = -7261
761941 ZDOT = -2183
353987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11398976
63 X = 3474408
08
Y = -10061668
38 feet Y = -3066796
52 meter
Z = -16276807
80 Z = -4961171
02
XDOT = 8659
719123 XDOT = 2639
482389
YDOT = 21356
463930 feet/sec YDOT = 6509
450206 meter/sec
ZDOT = -7125
729907 ZDOT = -2171
922476
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
39384760
00016717 00000-0 10270-3 0 9107
2 25544 51
6393 341
4627 0004755 318
4431 41
6359 15
53173301 33374
Satellite: ISS
Catalog Number: 25544
Epoch time: 19027
39384760 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 341
4627 deg
Eccentricity:
0004755
Arg of perigee: 318
4431 deg
Mean anomaly: 41
6359 deg
Mean motion: 15
53173301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3337
Checksum: 305
Coasting Arc #12 (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 = 2405827
78 A = 6780281
01 meter
Y = 3522984
85 meter E =
0002641
Z = 5270076
71 I = 51
46564
XDOT = -6739
233753 Wp = 351
32841
YDOT = 3593
233607 meter/sec RA = 335
98304 deg
ZDOT = 677
076655 TA = 92
20470
MA = 92
17446
Ha = 222
129 n
mi
Hp = 217
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7893135
77 X = 2340655
19
Y = 11558349
24 feet Y = 3549524
05 meter
Z = 17290277
93 Z = 5281604
91
XDOT = -22110
346959 XDOT = -6782
202253
YDOT = 11788
824169 feet/sec YDOT = 3517
630540 meter/sec
ZDOT = 2221
380101 ZDOT = 644
236066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12625556
45 X = -3848269
61
Y = 5891309
23 feet Y = 1795671
05 meter
Z = 17341814
79 Z = 5285785
15
XDOT = -7786
860000 XDOT = -2373
434928
YDOT = -22764
174821 feet/sec YDOT = -6938
520486 meter/sec
ZDOT = 2072
736272 ZDOT = 631
770016
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
42331109
00016717 00000-0 10270-3 0 9112
2 25544 51
6381 336
3378 0004918 321
9088 38
1716 15
53166789 33533
Satellite: ISS
Catalog Number: 25544
Epoch time: 19028
42331109 = yrday
fracday
Element set: 911
Inclination: 51
6381 deg
RA of node: 336
3378 deg
Eccentricity:
0004918
Arg of perigee: 321
9088 deg
Mean anomaly: 38
1716 deg
Mean motion: 15
53166789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3353
Checksum: 319
Coasting Arc #13 (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 = -1139997
79 A = 6780475
78 meter
Y = -4151961
79 meter E =
0011708
Z = -5247628
40 I = 51
43601
XDOT = 6969
281675 Wp = 78
51157
YDOT = -3045
790552 meter/sec RA = 330
98082 deg
ZDOT = 899
832794 TA = 200
10731
MA = 200
15348
Ha = 222
292 n
mi
Hp = 217
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3740150
22 X = -1067994
93
Y = -13621921
89 feet Y = -4164307
33 meter
Z = -17216628
60 Z = -5252991
22
XDOT = 22865
097358 XDOT = 6998
451764
YDOT = -9992
751154 feet/sec YDOT = -2967
692105 meter/sec
ZDOT = 2952
207328 ZDOT = 933
757289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13993082
20 X = 4265091
46
Y = -1710146
17 feet Y = -521252
55 meter
Z = -17240267
71 Z = -5254833
60
XDOT = 6619
307987 XDOT = 2017
565075
YDOT = 22984
950376 feet/sec YDOT = 7005
812875 meter/sec
ZDOT = 3105
658058 ZDOT = 946
604576
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
38843207
00016717 00000-0 10270-3 0 9126
2 25544 51
6380 331
5340 0004939 325
5604 34
5227 15
53158641 33686
Satellite: ISS
Catalog Number: 25544
Epoch time: 19029
38843207 = yrday
fracday
Element set: 912
Inclination: 51
6380 deg
RA of node: 331
5340 deg
Eccentricity:
0004939
Arg of perigee: 325
5604 deg
Mean anomaly: 34
5227 deg
Mean motion: 15
53158641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3368
Checksum: 306
Coasting Arc #14 (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 = -118205
71 A = 6782131
47 meter
Y = 4744229
44 meter E =
0008599
Z = 4845166
35 I = 51
41351
XDOT = -6893
036760 Wp = 23
88325
YDOT = 2316
587679 meter/sec RA = 325
97772 deg
ZDOT = -2427
266887 TA = 90
06034
MA = 89
96180
Ha = 222
401 n
mi
Hp = 216
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -387814
01 X = -194783
01
Y = 15565057
20 feet Y = 4742479
25 meter
Z = 15896215
07 Z = 4844406
33
XDOT = -22614
950001 XDOT = -6906
639060
YDOT = 7600
353276 feet/sec YDOT = 2239
428962 meter/sec
ZDOT = -7963
474038 ZDOT = -2460
783131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15392144
36 X = -4691525
60
Y = -2373240
14 feet Y = -723363
59 meter
Z = 15892157
89 Z = 4843929
73
XDOT = -4988
119128 XDOT = -1520
378710
YDOT = -22192
401702 feet/sec YDOT = -6764
244039 meter/sec
ZDOT = -8114
978287 ZDOT = -2473
445382
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
41789193
00016717 00000-0 10270-3 0 9136
2 25544 51
6382 326
4091 0005023 328
8260 31
2593 15
53185379 33849
Satellite: ISS
Catalog Number: 25544
Epoch time: 19030
41789193 = yrday
fracday
Element set: 913
Inclination: 51
6382 deg
RA of node: 326
4091 deg
Eccentricity:
0005023
Arg of perigee: 328
8260 deg
Mean anomaly: 31
2593 deg
Mean motion: 15
53185379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3384
Checksum: 309
Coasting Arc #15 (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 = 1245772
33 A = 6784964
15 meter
Y = -5245487
73 meter E =
0005258
Z = -4121920
13 I = 51
39633
XDOT = 6520
514836 Wp = 65
48661
YDOT = -1409
563707 meter/sec RA = 320
97851 deg
ZDOT = 3770
428611 TA = 243
50858
MA = 243
56252
Ha = 222
589 n
mi
Hp = 216
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4087179
57 X = 1324357
90
Y = -17209605
43 feet Y = -5231117
08 meter
Z = -13523360
01 Z = -4115678
09
XDOT = 21392
765210 XDOT = 6517
478044
YDOT = -4624
552845 feet/sec YDOT = -1336
663895 meter/sec
ZDOT = 12370
172609 ZDOT = 3802
094824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16683601
01 X = 5085161
59
Y = 5942422
04 feet Y = 1811250
24 meter
Z = -13494513
69 Z = -4113127
77
XDOT = 2818
699867 XDOT = 859
139719
YDOT = 20458
000053 feet/sec YDOT = 6235
598416 meter/sec
ZDOT = 12513
205981 ZDOT = 3814
025183
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
38300837
00016717 00000-0 10270-3 0 9148
2 25544 51
6387 321
6050 0005107 333
7879 26
3014 15
53166071 33997
Satellite: ISS
Catalog Number: 25544
Epoch time: 19031
38300837 = yrday
fracday
Element set: 914
Inclination: 51
6387 deg
RA of node: 321
6050 deg
Eccentricity:
0005107
Arg of perigee: 333
7879 deg
Mean anomaly: 26
3014 deg
Mean motion: 15
53166071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3399
Checksum: 299
Coasting Arc #16 (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 = -2253988
36 A = 6788053
66 meter
Y = 5606774
93 meter E =
0011471
Z = 3086915
23 I = 51
38136
XDOT = -5915
361008 Wp = 72
08884
YDOT = 310
925784 meter/sec RA = 315
98413 deg
ZDOT = -4865
576818 TA = 72
30273
MA = 72
17754
Ha = 222
677 n
mi
Hp = 216
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7394974
92 X = -2331511
57
Y = 18394930
88 feet Y = 5581135
68 meter
Z = 10127674
65 Z = 3075778
38
XDOT = -19407
352389 XDOT = -5894
764468
YDOT = 1020
097717 feet/sec YDOT = 244
891451 meter/sec
ZDOT = -15963
178538 ZDOT = -4894
260774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17679022
89 X = -5388566
18
Y = -9030004
94 feet Y = -2752345
51 meter
Z = 10076710
29 Z = 3071381
30
XDOT =
501048 XDOT =
152720
YDOT = -18026
688317 feet/sec YDOT = -5494
534599 meter/sec
ZDOT = -16092
612496 ZDOT = -4905
028289
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
41246454
00016717 00000-0 10270-3 0 9158
2 25544 51
6383 316
4803 0005189 337
1109 22
9811 15
53194481 34157
Satellite: ISS
Catalog Number: 25544
Epoch time: 19032
41246454 = yrday
fracday
Element set: 915
Inclination: 51
6383 deg
RA of node: 316
4803 deg
Eccentricity:
0005189
Arg of perigee: 337
1109 deg
Mean anomaly: 22
9811 deg
Mean motion: 15
53194481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3415
Checksum: 299
Coasting Arc #17 (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 = 3043664
58 A = 6790622
54 meter
Y = -5770595
54 meter E =
0010851
Z = -1862067
47 I = 51
36708
XDOT = 5148
311071 Wp = 14
80921
YDOT = 910
984144 meter/sec RA = 310
99507 deg
ZDOT = 5609
606967 TA = 324
62140
MA = 324
69335
Ha = 222
771 n
mi
Hp = 216
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9985776
18 X = 3117011
46
Y = -18932400
06 feet Y = -5736148
99 meter
Z = -6109145
24 Z = -1847104
90
XDOT = 16890
784353 XDOT = 5110
493876
YDOT = 2988
793123 feet/sec YDOT = 968
344512 meter/sec
ZDOT = 18404
222332 ZDOT = 5634
523100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18189192
73 X = 5544065
94
Y = 11319619
01 feet Y = 3450219
87 meter
Z = -6040914
42 Z = -1841270
72
XDOT = -3324
265005 XDOT = -1013
235973
YDOT = 15192
278232 feet/sec YDOT = 4630
606405 meter/sec
ZDOT = 18516
502495 ZDOT = 5643
829961
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
37757835
00016717 00000-0 10270-3 0 9165
2 25544 51
6386 311
6765 0005129 340
6850 19
4107 15
53189142 34304
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
37757835 = yrday
fracday
Element set: 916
Inclination: 51
6386 deg
RA of node: 311
6765 deg
Eccentricity:
0005129
Arg of perigee: 340
6850 deg
Mean anomaly: 19
4107 deg
Mean motion: 15
53189142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3430
Checksum: 313
Coasting Arc #18 (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 = -5297525
30 A = 6789664
91 meter
Y = 3562206
17 meter E =
0002491
Z = -2315947
41 I = 51
35625
XDOT = -1220
163369 Wp = 67
57021
YDOT = -5312
005052 meter/sec RA = 309
22041 deg
ZDOT = -5383
208861 TA = 138
31952
MA = 138
30054
Ha = 222
749 n
mi
Hp = 216
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17380332
34 X = -5325715
87
Y = 11687028
10 feet Y = 3502807
99 meter
Z = -7598252
66 Z = -2341748
51
XDOT = -4003
160659 XDOT = -1134
524379
YDOT = -17427
838097 feet/sec YDOT = -5325
170776 meter/sec
ZDOT = -17661
446394 ZDOT = -5388
927964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6895669
89 X = -2101800
18
Y = 19731272
70 feet Y = 6014091
92 meter
Z = -7715091
44 Z = -2351559
87
XDOT = -12100
583220 XDOT = -3688
257765
YDOT = -11139
798119 feet/sec YDOT = -3395
410467 meter/sec
ZDOT = -17686
573028 ZDOT = -5390
867459
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
76362177
00016717 00000-0 10270-3 0 9170
2 25544 51
6385 309
7532 0005241 340
3845 19
7105 15
53207144 34369
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
76362177 = yrday
fracday
Element set: 917
Inclination: 51
6385 deg
RA of node: 309
7532 deg
Eccentricity:
0005241
Arg of perigee: 340
3845 deg
Mean anomaly: 19
7105 deg
Mean motion: 15
53207144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3436
Checksum: 303
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