[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 28th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16520 4497 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
271/11:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
272/00:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
4
275/04:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 218
3
276/07:36:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
4
278/06:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
6
281/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
6
000/00:00:00
000 0
0 0
0 218
7
284/20:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 219
2
Coasting Arc #1 (Orbit 3113)
---------------------------------------
Vector Time (GMT): 2019/270/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931323
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5806103
93 A = 6795642
55 meter
Y = -319713
29 meter E =
0012545
Z = -3528161
86 I = 51
43664
XDOT = -2399
628238 Wp = 92
29008
YDOT = -5720
075897 meter/sec RA = 212
08067 deg
ZDOT = 4480
633520 TA = 226
14980
MA = 226
25354
Ha = 229
968 n
mi
Hp = 218
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19048897
42 X = -5784959
43
Y = -1048928
10 feet Y = -384523
40 meter
Z = -11575334
20 Z = -3556314
35
XDOT = -7872
796055 XDOT = -2357
250784
YDOT = -18766
653205 feet/sec YDOT = -5746
672789 meter/sec
ZDOT = 14700
241206 ZDOT = 4469
080585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12944194
72 X = 3945390
55
Y = -13907784
30 feet Y = -4239092
65 meter
Z = -11703438
13 Z = -3567207
94
XDOT = 18508
322358 XDOT = 5641
336655
YDOT = 4936
181066 feet/sec YDOT = 1504
547989 meter/sec
ZDOT = 14647
938102 ZDOT = 4464
691533
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 19270
63253005
00016717 00000-0 10270-3 0 9000
2 25544 51
6434 213
2203 0007338 88
9269 271
2723 15
50120314 31146
Satellite: ISS
Catalog Number: 25544
Epoch time: 19270
63253005 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 213
2203 deg
Eccentricity:
0007338
Arg of perigee: 88
9269 deg
Mean anomaly: 271
2723 deg
Mean motion: 15
50120314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3114
Checksum: 270
Coasting Arc #2 (Orbit 3126)
---------------------------------------
Vector Time (GMT): 2019/271/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 964595
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6260139
29 A = 6800634
29 meter
Y = -2481645
67 meter E =
0015438
Z = -925209
95 I = 51
47430
XDOT = 1031
345139 Wp = 61
81551
YDOT = -4771
437959 meter/sec RA = 207
90437 deg
ZDOT = 5902
429757 TA = 288
16490
MA = 288
33292
Ha = 230
001 n
mi
Hp = 218
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20538514
72 X = -6227429
36
Y = -8141882
12 feet Y = -2551468
18 meter
Z = -3035465
72 Z = -955539
76
XDOT = 3383
678277 XDOT = 1055
953222
YDOT = -15654
324011 feet/sec YDOT = -4759
766427 meter/sec
ZDOT = 19364
927023 ZDOT = 5907
500011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19695848
61 X = 6003294
66
Y = 9966846
89 feet Y = 3037894
93 meter
Z = -3173388
43 Z = -967248
79
XDOT = -3930
557529 XDOT = -1198
033935
YDOT = 13857
983004 feet/sec YDOT = 4223
913219 meter/sec
ZDOT = 19388
224166 ZDOT = 5909
530726
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 19271
47062617
00016717 00000-0 10270-3 0 9011
2 25544 51
6403 209
0670 0007394 91
9381 268
2617 15
50110367 31273
Satellite: ISS
Catalog Number: 25544
Epoch time: 19271
47062617 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 209
0670 deg
Eccentricity:
0007394
Arg of perigee: 91
9381 deg
Mean anomaly: 268
2617 deg
Mean motion: 15
50110367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3127
Checksum: 298
Coasting Arc #3 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2019/272/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 964595
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 271392
47 A = 6790399
25 meter
Y = 4562000
14 meter E =
0019705
Z = -5039981
88 I = 51
45928
XDOT = -7206
062800 Wp = 84
01934
YDOT = -1689
555855 meter/sec RA = 205
13274 deg
ZDOT = -1921
846293 TA = 167
26303
MA = 167
21318
Ha = 229
987 n
mi
Hp = 218
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 890395
24 X = 244840
33
Y = 14967192
05 feet Y = 4564885
97 meter
Z = -16535373
61 Z = -5038728
58
XDOT = -23641
938319 XDOT = -7177
298787
YDOT = -5543
162255 feet/sec YDOT = -1769
978538 meter/sec
ZDOT = -6305
269989 ZDOT = -1956
780858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5543140
38 X = 1689549
19
Y = 13937896
17 feet Y = 4248270
75 meter
Z = -16529878
01 Z = -5038306
82
XDOT = -23145
488988 XDOT = -7054
745043
YDOT = 1556
194999 feet/sec YDOT = 474
328236 meter/sec
ZDOT = -6464
195438 ZDOT = -1970
286770
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 19272
05084559
00016717 00000-0 10270-3 0 9026
2 25544 51
6430 206
1896 0007247 98
2953 261
9019 15
50099999 31366
Satellite: ISS
Catalog Number: 25544
Epoch time: 19272
05084559 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 206
1896 deg
Eccentricity:
0007247
Arg of perigee: 98
2953 deg
Mean anomaly: 261
9019 deg
Mean motion: 15
50099999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 336
Coasting Arc #4 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2019/273/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 964595
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -211048
86 A = 6789778
25 meter
Y = -4429110
95 meter E =
0011884
Z = 5133348
34 I = 51
48890
XDOT = 7381
355570 Wp = 111
61725
YDOT = 1420
488157 meter/sec RA = 200
16484 deg
ZDOT = 1521
953478 TA = 323
65118
MA = 323
73184
Ha = 229
914 n
mi
Hp = 218
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -692417
53 X = -186440
87
Y = -14531203
89 feet Y = -4431332
89 meter
Z = 16841694
03 Z = 5132383
39
XDOT = 24217
045833 XDOT = 7357
529755
YDOT = 4660
394216 feet/sec YDOT = 1502
898633 meter/sec
ZDOT = 4993
285689 ZDOT = 1557
751791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5455837
83 X = -1662939
37
Y = -13491121
85 feet Y = -4112093
94 meter
Z = 16837501
34 Z = 5132070
41
XDOT = 23408
265918 XDOT = 7134
839452
YDOT = -3002
019989 feet/sec YDOT = -915
015693 meter/sec
ZDOT = 5156
170611 ZDOT = 1571
600802
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 19273
08234390
00016717 00000-0 10270-3 0 9031
2 25544 51
6434 201
0789 0007253 102
0835 258
1129 15
50147597 31521
Satellite: ISS
Catalog Number: 25544
Epoch time: 19273
08234390 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 201
0789 deg
Eccentricity:
0007253
Arg of perigee: 102
0835 deg
Mean anomaly: 258
1129 deg
Mean motion: 15
50147597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 296
Coasting Arc #5 (Orbit 3166)
---------------------------------------
Vector Time (GMT): 2019/274/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 964595
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 101928
17 A = 6789517
43 meter
Y = 4341557
87 meter E =
0020932
Z = -5237197
01 I = 51
51931
XDOT = -7482
670267 Wp = 89
59123
YDOT = -1134
929003 meter/sec RA = 195
19896 deg
ZDOT = -1090
110237 TA = 169
93656
MA = 169
89458
Ha = 229
919 n
mi
Hp = 218
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 334410
00 X = 78811
86
Y = 14243956
27 feet Y = 4342567
98 meter
Z = -17182404
87 Z = -5236758
40
XDOT = -24549
443132 XDOT = -7464
127792
YDOT = -3723
520351 feet/sec YDOT = -1218
501921 meter/sec
ZDOT = -3576
477156 ZDOT = -1126
413716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5255037
69 X = 1601735
49
Y = 13245701
38 feet Y = 4037289
78 meter
Z = -17180603
35 Z = -5236647
90
XDOT = -23367
903965 XDOT = -7122
537129
YDOT = 4433
130742 feet/sec YDOT = 1351
218250 meter/sec
ZDOT = -3741
692132 ZDOT = -1140
467762
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 19274
04937138
00016717 00000-0 10270-3 0 9049
2 25544 51
6434 196
2880 0007168 104
8805 255
3140 15
50109919 31674
Satellite: ISS
Catalog Number: 25544
Epoch time: 19274
04937138 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 196
2880 deg
Eccentricity:
0007168
Arg of perigee: 104
8805 deg
Mean anomaly: 255
3140 deg
Mean motion: 15
50109919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3167
Checksum: 317
Coasting Arc #6 (Orbit 3182)
---------------------------------------
Vector Time (GMT): 2019/275/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 964595
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1241
92 A = 6789094
98 meter
Y = -4259321
53 meter E =
0010277
Z = 5278829
64 I = 51
55087
XDOT = 7594
732941 Wp = 111
17351
YDOT = 832
001126 meter/sec RA = 190
23499 deg
ZDOT = 668
416036 TA = 332
40984
MA = 332
46435
Ha = 229
854 n
mi
Hp = 218
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4074
53 X = 20745
07
Y = -13974151
99 feet Y = -4259212
13 meter
Z = 17318994
89 Z = 5278877
29
XDOT = 24917
102825 XDOT = 7581
617954
YDOT = 2729
662488 feet/sec YDOT = 916
857501 meter/sec
ZDOT = 2192
965999 ZDOT = 705
277140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5078319
72 X = -1547871
85
Y = -13018196
14 feet Y = -3967946
18 meter
Z = 17319404
21 Z = 5278954
40
XDOT = 23297
223618 XDOT = 7100
993759
YDOT = -5926
905802 feet/sec YDOT = -1806
520889 meter/sec
ZDOT = 2360
753893 ZDOT = 719
557787
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 19275
08086182
00016717 00000-0 10270-3 0 9059
2 25544 51
6433 191
1773 0007216 108
0739 252
1198 15
50159160 31833
Satellite: ISS
Catalog Number: 25544
Epoch time: 19275
08086182 = yrday
fracday
Element set: 905
Inclination: 51
6433 deg
RA of node: 191
1773 deg
Eccentricity:
0007216
Arg of perigee: 108
0739 deg
Mean anomaly: 252
1198 deg
Mean motion: 15
50159160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3183
Checksum: 306
Coasting Arc #7 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2019/275/04:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964595
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3940568
95 A = 6791832
58 meter
Y = -3044982
92 meter E =
0014669
Z = 4606347
87 I = 51
56282
XDOT = 6167
154417 Wp = 84
66648
YDOT = 3442
777466 meter/sec RA = 189
53746 deg
ZDOT = -2990
420673 TA = 35
23336
MA = 35
13647
Ha = 229
817 n
mi
Hp = 218
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12928375
81 X = 3951950
48
Y = -9990101
45 feet Y = -3000852
78 meter
Z = 15112689
85 Z = 4625517
84
XDOT = 20233
446250 XDOT = 6142
723983
YDOT = 11295
201659 feet/sec YDOT = 3511
606152 meter/sec
ZDOT = -9811
091447 ZDOT = -2960
521978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4918469
32 X = -1499149
45
Y = -15495282
73 feet Y = -4722962
18 meter
Z = 15200108
40 Z = 4632993
04
XDOT = 16506
082435 XDOT = 5031
053926
YDOT = -14760
680091 feet/sec YDOT = -4499
055292 meter/sec
ZDOT = -9675
118296 ZDOT = -2948
976057
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 19275
20979874
00016717 00000-0 10270-3 0 9063
2 25544 51
6416 190
5403 0007353 106
0388 254
1573 15
50151197 31850
Satellite: ISS
Catalog Number: 25544
Epoch time: 19275
20979874 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 190
5403 deg
Eccentricity:
0007353
Arg of perigee: 106
0388 deg
Mean anomaly: 254
1573 deg
Mean motion: 15
50151197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 317
Coasting Arc #8 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2019/276/04:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964595
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4064610
12 A = 6792652
75 meter
Y = 3192667
79 meter E =
0016600
Z = -4424364
60 I = 51
59872
XDOT = -6112
704572 Wp = 110
41111
YDOT = -3150
596718 meter/sec RA = 184
57748 deg
ZDOT = 3346
732589 TA = 193
51085
MA = 193
55535
Ha = 229
950 n
mi
Hp = 218
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13335335
05 X = -4078517
92
Y = 10474631
87 feet Y = 3147136
50 meter
Z = -14515631
88 Z = -4444143
18
XDOT = -20054
805026 XDOT = -6093
276203
YDOT = -10336
603406 feet/sec YDOT = -3218
844517 meter/sec
ZDOT = 10980
093795 ZDOT = 3317
086217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5505627
42 X = 1678115
24
Y = 15956506
00 feet Y = 4863543
03 meter
Z = -14605842
17 Z = -4451860
69
XDOT = -15248
581247 XDOT = -4647
767564
YDOT = 15174
955641 feet/sec YDOT = 4625
326479 meter/sec
ZDOT = 10845
237984 ZDOT = 3305
628538
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 19276
17682028
00016717 00000-0 10270-3 0 9073
2 25544 51
6418 185
7488 0007401 109
2097 250
9855 15
50126957 32008
Satellite: ISS
Catalog Number: 25544
Epoch time: 19276
17682028 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 185
7488 deg
Eccentricity:
0007401
Arg of perigee: 109
2097 deg
Mean anomaly: 250
9855 deg
Mean motion: 15
50126957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 325
Coasting Arc #9 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2019/276/07:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 949486
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2772620
60 A = 6791425
11 meter
Y = -3966363
21 meter E =
0014900
Z = 4755745
38 I = 51
59652
XDOT = 6990
617929 Wp = 114
27466
YDOT = -1656
592838 meter/sec RA = 183
87678 deg
ZDOT = 2681
309825 TA = 309
15943
MA = 309
29173
Ha = 229
918 n
mi
Hp = 218
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9096524
27 X = -2751162
64
Y = -13013002
67 feet Y = -3997248
44 meter
Z = 15602839
18 Z = 4742329
11
XDOT = 22935
098193 XDOT = 6995
598355
YDOT = -5435
015874 feet/sec YDOT = -1578
390860 meter/sec
ZDOT = 8796
948246 ZDOT = 2715
280315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5392291
43 X = -1643570
43
Y = 14996843
72 feet Y = 4571037
97 meter
Z = 15541925
70 Z = 4737178
95
XDOT = -16467
121269 XDOT = -5019
178563
YDOT = -15241
131752 feet/sec YDOT = -4645
496958 meter/sec
ZDOT = 8951
717073 ZDOT = 2728
483364
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 19276
37022357
00016717 00000-0 10270-3 0 9089
2 25544 51
6388 184
7910 0007192 110
1058 250
0867 15
50151263 32033
Satellite: ISS
Catalog Number: 25544
Epoch time: 19276
37022357 = yrday
fracday
Element set: 908
Inclination: 51
6388 deg
RA of node: 184
7910 deg
Eccentricity:
0007192
Arg of perigee: 110
1058 deg
Mean anomaly: 250
0867 deg
Mean motion: 15
50151263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 296
Coasting Arc #10 (Orbit 3217)
---------------------------------------
Vector Time (GMT): 2019/277/07:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 949486
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2641226
36 A = 6790806
67 meter
Y = 3861047
77 meter E =
0018257
Z = -4938515
69 I = 51
62819
XDOT = -7045
429544 Wp = 88
48576
YDOT = 1928
522030 meter/sec RA = 178
91733 deg
ZDOT = -2267
084974 TA = 159
33631
MA = 159
26239
Ha = 229
894 n
mi
Hp = 218
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8665440
80 X = 2621843
57
Y = 12667479
55 feet Y = 3890475
29 meter
Z = -16202479
31 Z = -4925732
65
XDOT = -23114
926327 XDOT = -7055
458827
YDOT = 6327
172014 feet/sec YDOT = 1849
678918 meter/sec
ZDOT = -7437
942829 ZDOT = -2301
333875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5104415
00 X = 1555825
69
Y = -14538822
09 feet Y = -4431432
97 meter
Z = -16144436
75 Z = -4920824
32
XDOT = 17600
141273 XDOT = 5364
523060
YDOT = 14587
023263 feet/sec YDOT = 4446
124691 meter/sec
ZDOT = -7594
016679 ZDOT = -2314
656284
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 19277
33724118
00016717 00000-0 10270-3 0 9091
2 25544 51
6394 179
9984 0007278 113
0760 247
1158 15
50126727 32187
Satellite: ISS
Catalog Number: 25544
Epoch time: 19277
33724118 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 179
9984 deg
Eccentricity:
0007278
Arg of perigee: 113
0760 deg
Mean anomaly: 247
1158 deg
Mean motion: 15
50126727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 332
Coasting Arc #11 (Orbit 3232)
---------------------------------------
Vector Time (GMT): 2019/278/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 949486
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3358008
61 A = 6791397
96 meter
Y = 3465714
42 meter E =
0017092
Z = -4793572
48 I = 51
66254
XDOT = -6620
985531 Wp = 89
22407
YDOT = 2777
512778 meter/sec RA = 174
13277 deg
ZDOT = -2637
964772 TA = 154
73481
MA = 154
65112
Ha = 229
879 n
mi
Hp = 218
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11017088
60 X = 3342289
14
Y = 11370454
13 feet Y = 3503178
00 meter
Z = -15726943
82 Z = -4777298
67
XDOT = -21722
393475 XDOT = -6638
738512
YDOT = 9112
574731 feet/sec YDOT = 2703
372905 meter/sec
ZDOT = -8654
740064 ZDOT = -2670
170534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5663192
27 X = 1726141
00
Y = -14863138
63 feet Y = -4530284
66 meter
Z = -15652973
95 Z = -4771026
46
XDOT = 16266
460624 XDOT = 4958
017198
YDOT = 15439
649876 feet/sec YDOT = 4706
005282 meter/sec
ZDOT = -8801
570432 ZDOT = -2682
718668
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 19278
30425381
00016717 00000-0 10270-3 0 9101
2 25544 51
6395 175
2067 0007300 116
0044 244
1859 15
50131901 32335
Satellite: ISS
Catalog Number: 25544
Epoch time: 19278
30425381 = yrday
fracday
Element set: 910
Inclination: 51
6395 deg
RA of node: 175
2067 deg
Eccentricity:
0007300
Arg of perigee: 116
0044 deg
Mean anomaly: 244
1859 deg
Mean motion: 15
50131901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3233
Checksum: 280
Coasting Arc #12 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2019/279/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 949486
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3232964
63 A = 6790660
78 meter
Y = -3351116
33 meter E =
0013762
Z = 4935068
35 I = 51
69315
XDOT = 6650
136546 Wp = 121
14531
YDOT = -3082
135888 meter/sec RA = 169
18010 deg
ZDOT = 2252
001893 TA = 306
81203
MA = 306
93821
Ha = 229
814 n
mi
Hp = 218
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10606839
33 X = -3219223
16
Y = -10994476
16 feet Y = -3387192
62 meter
Z = 16191169
12 Z = 4919397
21
XDOT = 21818
033287 XDOT = 6673
168588
YDOT = -10111
994383 feet/sec YDOT = -3007
640511 meter/sec
ZDOT = 7388
457653 ZDOT = 2284
362009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5244939
99 X = -1598657
71
Y = 14428305
77 feet Y = 4397747
60 meter
Z = 16119928
69 Z = 4913354
27
XDOT = -17513
755330 XDOT = -5338
192625
YDOT = -14828
862326 feet/sec YDOT = -4519
837237 meter/sec
ZDOT = 7536
028323 ZDOT = 2296
981433
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 19279
33573081
00016717 00000-0 10270-3 0 9117
2 25544 51
6391 170
0966 0007119 120
0893 240
0964 15
50166623 32495
Satellite: ISS
Catalog Number: 25544
Epoch time: 19279
33573081 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 170
0966 deg
Eccentricity:
0007119
Arg of perigee: 120
0893 deg
Mean anomaly: 240
0964 deg
Mean motion: 15
50166623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 306
Coasting Arc #13 (Orbit 3263)
---------------------------------------
Vector Time (GMT): 2019/280/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 949486
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3073631
18 A = 6790152
12 meter
Y = 3304645
63 meter E =
0018646
Z = -5089143
69 I = 51
72399
XDOT = -6622
668530 Wp = 92
91492
YDOT = 3364
435074 meter/sec RA = 164
22709 deg
ZDOT = -1821
813451 TA = 159
45953
MA = 159
38446
Ha = 229
746 n
mi
Hp = 218
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10084091
81 X = 3061169
58
Y = 10842013
21 feet Y = 3338947
24 meter
Z = -16696665
66 Z = -5074243
50
XDOT = -21727
915126 XDOT = -6650
949013
YDOT = 11038
172815 feet/sec YDOT = 3290
217515 meter/sec
ZDOT = -5977
078250 ZDOT = -1854
052861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5093472
76 X = 1552490
50
Y = -13983996
67 feet Y = -4262322
18 meter
Z = -16628925
85 Z = -5068496
60
XDOT = 18595
991692 XDOT = 5668
058268
YDOT = 14029
532958 feet/sec YDOT = 4276
201645 meter/sec
ZDOT = -6124
133794 ZDOT = -1866
635981
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 19280
30274039
00016717 00000-0 10270-3 0 9128
2 25544 51
6393 165
3042 0007158 123
4080 236
7756 15
50138656 32640
Satellite: ISS
Catalog Number: 25544
Epoch time: 19280
30274039 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 165
3042 deg
Eccentricity:
0007158
Arg of perigee: 123
4080 deg
Mean anomaly: 236
7756 deg
Mean motion: 15
50138656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3264
Checksum: 302
Coasting Arc #14 (Orbit 3279)
---------------------------------------
Vector Time (GMT): 2019/281/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 949486
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2933919
69 A = 6789569
19 meter
Y = -3254880
23 meter E =
0011589
Z = 5179580
69 I = 51
75558
XDOT = 6580
141358 Wp = 126
88948
YDOT = -3676
024441 meter/sec RA = 159
27809 deg
ZDOT = 1408
246098 TA = 309
53568
MA = 309
63805
Ha = 229
677 n
mi
Hp = 218
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9625720
78 X = -2922464
24
Y = -10678740
92 feet Y = -3287625
05 meter
Z = 16993374
97 Z = 5165356
77
XDOT = 21588
390282 XDOT = 6613
918177
YDOT = -12060
447641 feet/sec YDOT = -3602
251718 meter/sec
ZDOT = 4620
229980 ZDOT = 1440
292316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4919961
96 X = -1499604
41
Y = 13589616
71 feet Y = 4142115
17 meter
Z = 16928706
19 Z = 5159869
65
XDOT = -19713
869875 XDOT = -6008
787538
YDOT = -13111
574238 feet/sec YDOT = -3996
407828 meter/sec
ZDOT = 4766
439723 ZDOT = 1452
810828
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 19281
33421208
00016717 00000-0 10270-3 0 9135
2 25544 51
6406 160
1941 0006995 127
5794 232
5992 15
50179728 32800
Satellite: ISS
Catalog Number: 25544
Epoch time: 19281
33421208 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 160
1941 deg
Eccentricity:
0006995
Arg of perigee: 127
5794 deg
Mean anomaly: 232
5992 deg
Mean motion: 15
50179728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3280
Checksum: 319
Coasting Arc #15 (Orbit 3281)
---------------------------------------
Vector Time (GMT): 2019/281/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949486
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 918932
46 A = 6789003
08 meter
Y = 4142382
76 meter E =
0020920
Z = -5317623
80 I = 51
76157
XDOT = -7247
853715 Wp = 105
22338
YDOT = 2365
444369 meter/sec RA = 158
44830 deg
ZDOT = 586
748359 TA = 170
40303
MA = 170
36300
Ha = 229
590 n
mi
Hp = 218
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3014870
28 X = 898373
00
Y = 13590494
61 feet Y = 4152543
64 meter
Z = -17446272
32 Z = -5313210
14
XDOT = -23779
047623 XDOT = -7276
616233
YDOT = 7760
644254 feet/sec YDOT = 2284
232967 meter/sec
ZDOT = 1925
027424 ZDOT = 551
470880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2450338
26 X = -746863
10
Y = -13728857
63 feet Y = -4184555
80 meter
Z = -17426351
17 Z = -5311551
84
XDOT = 23148
040206 XDOT = 7055
522655
YDOT = -6385
012113 feet/sec YDOT = -1946
151692 meter/sec
ZDOT = 1764
149940 ZDOT = 537
712902
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 19281
46314660
00016717 00000-0 10270-3 0 9143
2 25544 51
6434 159
5560 0007021 127
4165 232
7626 15
50172179 32823
Satellite: ISS
Catalog Number: 25544
Epoch time: 19281
46314660 = yrday
fracday
Element set: 914
Inclination: 51
6434 deg
RA of node: 159
5560 deg
Eccentricity:
0007021
Arg of perigee: 127
4165 deg
Mean anomaly: 232
7626 deg
Mean motion: 15
50172179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3282
Checksum: 300
Coasting Arc #16 (Orbit 3297)
---------------------------------------
Vector Time (GMT): 2019/282/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949486
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -809439
39 A = 6789108
39 meter
Y = -4215814
57 meter E =
0008670
Z = 5252114
99 I = 51
79293
XDOT = 7123
706078 Wp = 108
39236
YDOT = -2647
247625 meter/sec RA = 153
50047 deg
ZDOT = -1028
312482 TA = 351
42545
MA = 351
44026
Ha = 229
517 n
mi
Hp = 218
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2655641
05 X = -787748
75
Y = -13831412
63 feet Y = -4224744
62 meter
Z = 17231348
40 Z = 5248236
02
XDOT = 23371
739100 XDOT = 7157
773914
YDOT = -8685
195621 feet/sec YDOT = -2567
394907 meter/sec
ZDOT = -3373
728615 ZDOT = -993
625091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2317772
09 X = 706456
93
Y = 13913680
24 feet Y = 4240889
74 meter
Z = 17213866
71 Z = 5246786
57
XDOT = -22651
024755 XDOT = -6904
032345
YDOT = 7746
255173 feet/sec YDOT = 2361
058577 meter/sec
ZDOT = -3215
507823 ZDOT = -980
086784
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 19282
49461408
00016717 00000-0 10270-3 0 9151
2 25544 51
6433 154
4451 0006925 131
2589 228
9159 15
50203945 32981
Satellite: ISS
Catalog Number: 25544
Epoch time: 19282
49461408 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 154
4451 deg
Eccentricity:
0006925
Arg of perigee: 131
2589 deg
Mean anomaly: 228
9159 deg
Mean motion: 15
50203945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3298
Checksum: 326
Coasting Arc #17 (Orbit 3312)
---------------------------------------
Vector Time (GMT): 2019/283/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949486
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 711770
43 A = 6789560
37 meter
Y = 4344617
12 meter E =
0019948
Z = -5186329
73 I = 51
82292
XDOT = -6928
103012 Wp = 112
32736
YDOT = 2886
702267 meter/sec RA = 148
55470 deg
ZDOT = 1464
532487 TA = 171
78979
MA = 171
75710
Ha = 229
467 n
mi
Hp = 218
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2335204
82 X = 688327
25
Y = 14253993
18 feet Y = 4352445
11 meter
Z = -17015517
49 Z = -5182929
51
XDOT = -22729
996760 XDOT = -6966
981979
YDOT = 9470
807964 feet/sec YDOT = 2809
010070 meter/sec
ZDOT = 4804
896612 ZDOT = 1430
783447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2228358
55 X = -679203
69
Y = -14289300
60 feet Y = -4355378
82 meter
Z = -17000224
85 Z = -5181668
53
XDOT = 21864
177659 XDOT = 6664
201350
YDOT = -8954
098899 feet/sec YDOT = -2729
209344 meter/sec
ZDOT = 4650
923878 ZDOT = 1417
601598
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 19283
46161573
00016717 00000-0 10270-3 0 9160
2 25544 51
6428 149
6538 0006942 134
4369 225
7351 15
50176842 33139
Satellite: ISS
Catalog Number: 25544
Epoch time: 19283
46161573 = yrday
fracday
Element set: 916
Inclination: 51
6428 deg
RA of node: 149
6538 deg
Eccentricity:
0006942
Arg of perigee: 134
4369 deg
Mean anomaly: 225
7351 deg
Mean motion: 15
50176842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3313
Checksum: 323
Coasting Arc #18 (Orbit 3328)
---------------------------------------
Vector Time (GMT): 2019/284/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949486
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -640002
79 A = 6789902
97 meter
Y = -4468715
13 meter E =
0009251
Z = 5063483
84 I = 51
85256
XDOT = 6744
393274 Wp = 103
03418
YDOT = -3118
045541 meter/sec RA = 143
61133 deg
ZDOT = -1898
449831 TA = 5
31817
MA = 5
30835
Ha = 229
354 n
mi
Hp = 218
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2099746
70 X = -614580
61
Y = -14661138
87 feet Y = -4475729
46 meter
Z = 16612479
79 Z = 5060437
09
XDOT = 22127
274520 XDOT = 6787
980617
YDOT = -10229
808205 feet/sec YDOT = -3042
381443 meter/sec
ZDOT = -6228
509943 ZDOT = -1865
581593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2236337
09 X = 681635
55
Y = 14656425
66 feet Y = 4467278
54 meter
Z = 16598807
10 Z = 5059316
41
XDOT = -21082
820407 XDOT = -6426
043660
YDOT = 10104
272924 feet/sec YDOT = 3079
782387 meter/sec
ZDOT = -6078
524771 ZDOT = -1852
734350
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 19284
49307955
00016717 00000-0 10270-3 0 9171
2 25544 51
6429 144
5431 0006810 139
2391 220
9270 15
50212319 33292
Satellite: ISS
Catalog Number: 25544
Epoch time: 19284
49307955 = yrday
fracday
Element set: 917
Inclination: 51
6429 deg
RA of node: 144
5431 deg
Eccentricity:
0006810
Arg of perigee: 139
2391 deg
Mean anomaly: 220
9270 deg
Mean motion: 15
50212319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3329
Checksum: 307
Coasting Arc #19 (Orbit 3334)
---------------------------------------
Vector Time (GMT): 2019/284/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949486
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3833292
13 A = 6789710
40 meter
Y = 2157935
23 meter E =
0017941
Z = -5186537
74 I = 51
86163
XDOT = -5091
373426 Wp = 100
15327
YDOT = 5514
973919 meter/sec RA = 141
59391 deg
ZDOT = -1475
791910 TA = 155
69011
MA = 155
60537
Ha = 229
479 n
mi
Hp = 219
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12576417
76 X = 3834070
21
Y = 7079839
99 feet Y = 2200805
65 meter
Z = -17016199
95 Z = -5167915
15
XDOT = -16703
981057 XDOT = -5145
496397
YDOT = 18093
746455 feet/sec YDOT = 5457
735822 meter/sec
ZDOT = -4841
836974 ZDOT = -1500
656185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7288020
49 X = 2221388
65
Y = 12571937
97 feet Y = 3831926
69 meter
Z = -16931409
03 Z = -5160693
47
XDOT = -22660
999647 XDOT = -6907
072692
YDOT = 6495
832462 feet/sec YDOT = 1979
929734 meter/sec
ZDOT = -4955
457544 ZDOT = -1510
423459
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 19284
87987915
00016717 00000-0 10270-3 0 9184
2 25544 51
6424 142
6228 0007179 143
3576 216
8067 15
50152800 33353
Satellite: ISS
Catalog Number: 25544
Epoch time: 19284
87987915 = yrday
fracday
Element set: 918
Inclination: 51
6424 deg
RA of node: 142
6228 deg
Eccentricity:
0007179
Arg of perigee: 143
3576 deg
Mean anomaly: 216
8067 deg
Mean motion: 15
50152800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3335
Checksum: 331
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