[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 1st 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
010/09:34:56
900 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 216
3
Coasting Arc #1 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2019/001/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4563402
23 A = 6780392
23 meter
Y = -1047467
16 meter E =
0009725
Z = -4913167
50 I = 51
97909
XDOT = -903
024055 Wp = 79
32188
YDOT = 7224
288876 meter/sec RA = 111
94116 deg
ZDOT = -2381
165399 TA = 167
44950
MA = 167
42527
Ha = 221
117 n
mi
Hp = 216
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14971792
11 X = 4598641
64
Y = -3436572
06 feet Y = -996238
61 meter
Z = -16119315
96 Z = -4890914
64
XDOT = -2962
677345 XDOT = -972
174558
YDOT = 23701
735157 feet/sec YDOT = 7213
804169 meter/sec
ZDOT = -7812
222438 ZDOT = -2385
719368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5873474
40 X = -1790235
00
Y = -14307266
62 feet Y = -4360854
87 meter
Z = -16018781
29 Z = -4882524
54
XDOT = 22813
599307 XDOT = 6953
585069
YDOT = -603
127849 feet/sec YDOT = -183
833368 meter/sec
ZDOT = -7833
576735 ZDOT = -2387
674189
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 19001
02028722
00016717 00000-0 10270-3 0 9001
2 25544 51
6397 112
8213 0002490 227
3026 132
7917 15
53733019 29275
Satellite: ISS
Catalog Number: 25544
Epoch time: 19001
02028722 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 112
8213 deg
Eccentricity:
0002490
Arg of perigee: 227
3026 deg
Mean anomaly: 132
7917 deg
Mean motion: 15
53733019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 280
Coasting Arc #2 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2019/002/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4183888
38 A = 6778575
09 meter
Y = -508179
07 meter E =
0002968
Z = 5308842
32 I = 51
98467
XDOT = 1736
687875 Wp = 169
36252
YDOT = -7440
598164 meter/sec RA = 106
97197 deg
ZDOT = 653
545626 TA = 274
41043
MA = 274
44434
Ha = 221
077 n
mi
Hp = 216
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13726667
92 X = -4203682
28
Y = -1667254
17 feet Y = -555077
39 meter
Z = 17417461
68 Z = 5288470
39
XDOT = 5697
794864 XDOT = 1816
587090
YDOT = -24411
411300 feet/sec YDOT = -7420
730628 meter/sec
ZDOT = 2144
178563 ZDOT = 662
175192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 875313
91 X = 266795
68
Y = 13914997
78 feet Y = 4241291
32 meter
Z = 17325581
73 Z = 5280837
31
XDOT = -24022
731274 XDOT = -7322
128492
YDOT = -1220
027935 feet/sec YDOT = -371
864515 meter/sec
ZDOT = 2183
970191 ZDOT = 665
674114
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 19002
04938800
00016717 00000-0 10270-3 0 9012
2 25544 51
6396 107
6955 0002674 233
4454 126
6453 15
53757634 29430
Satellite: ISS
Catalog Number: 25544
Epoch time: 19002
04938800 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 107
6955 deg
Eccentricity:
0002674
Arg of perigee: 233
4454 deg
Mean anomaly: 126
6453 deg
Mean motion: 15
53757634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 316
Coasting Arc #3 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2019/003/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3747661
34 A = 6778940
20 meter
Y = 2107281
44 meter E =
0012412
Z = -5251855
91 I = 51
99532
XDOT = -2434
376365 Wp = 106
70667
YDOT = 7171
537237 meter/sec RA = 101
99983 deg
ZDOT = 1139
155370 TA = 174
18141
MA = 174
16697
Ha = 220
938 n
mi
Hp = 216
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12295476
85 X = 3749329
18
Y = 6913653
01 feet Y = 2149200
29 meter
Z = -17230498
38 Z = -5233646
90
XDOT = -7986
799099 XDOT = -2519
922961
YDOT = 23528
665475 feet/sec YDOT = 7143
835903 meter/sec
ZDOT = 3737
386385 ZDOT = 1127
123083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4311791
69 X = 1314234
11
Y = -13535241
94 feet Y = -4125541
74 meter
Z = -17148559
74 Z = -5226881
01
XDOT = 23663
933112 XDOT = 7212
766812
YDOT = 2867
937657 feet/sec YDOT = 874
147398 meter/sec
ZDOT = 3682
246536 ZDOT = 1122
348744
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 19003
01417073
00016717 00000-0 10270-3 0 9025
2 25544 51
6407 102
8886 0002584 236
8328 123
2577 15
53727965 29580
Satellite: ISS
Catalog Number: 25544
Epoch time: 19003
01417073 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 102
8886 deg
Eccentricity:
0002584
Arg of perigee: 236
8328 deg
Mean anomaly: 123
2577 deg
Mean motion: 15
53727965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 319
Coasting Arc #4 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2019/004/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3266259
99 A = 6781115
65 meter
Y = -3610977
91 meter E =
0005455
Z = 4716582
97 I = 52
00898
XDOT = 3027
938768 Wp = 64
37511
YDOT = -6450
184147 meter/sec RA = 97
03287 deg
ZDOT = -2836
503635 TA = 53
63811
MA = 53
58778
Ha = 220
999 n
mi
Hp = 216
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10716076
10 X = -3248548
73
Y = -11847040
40 feet Y = -3647405
04 meter
Z = 15474353
57 Z = 4700759
35
XDOT = 9934
182310 XDOT = 3113
619604
YDOT = -21162
021481 feet/sec YDOT = -6415
844222 meter/sec
ZDOT = -9306
114287 ZDOT = -2821
587757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9238705
28 X = -2815957
37
Y = 13115835
92 feet Y = 3997706
79 meter
Z = 15403358
22 Z = 4694943
59
XDOT = -21862
141932 XDOT = -6663
580861
YDOT = -4531
586612 feet/sec YDOT = -1381
227599 meter/sec
ZDOT = -9238
022693 ZDOT = -2815
749317
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 19004
04326726
00016717 00000-0 10270-3 0 9034
2 25544 51
6411 97
7626 0002512 241
7969 118
2930 15
53736868 29743
Satellite: ISS
Catalog Number: 25544
Epoch time: 19004
04326726 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 97
7626 deg
Eccentricity:
0002512
Arg of perigee: 241
7969 deg
Mean anomaly: 118
2930 deg
Mean motion: 15
53736868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 321
Coasting Arc #5 (Orbit 2988)
---------------------------------------
Vector Time (GMT): 2019/005/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2774113
57 A = 6784442
05 meter
Y = 4908323
93 meter E =
0004213
Z = -3778796
33 I = 52
02398
XDOT = -3531
277717 Wp = 123
44749
YDOT = 5286
827665 meter/sec RA = 92
07213 deg
ZDOT = 4275
888429 TA = 191
61826
MA = 191
62799
Ha = 220
832 n
mi
Hp = 216
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9101422
48 X = 2737376
29
Y = 16103424
97 feet Y = 4939141
05 meter
Z = -12397625
76 Z = -3765409
45
XDOT = -11585
556814 XDOT = -3610
903793
YDOT = 17345
235122 feet/sec YDOT = 5246
892721 meter/sec
ZDOT = 14028
505345 ZDOT = 4258
542181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13531599
43 X = 4124431
51
Y = -12670126
24 feet Y = -3861854
48 meter
Z = -12337788
67 Z = -3760557
99
XDOT = 18659
097746 XDOT = 5687
292993
YDOT = 6347
859237 feet/sec YDOT = 1934
827496 meter/sec
ZDOT = 13949
563988 ZDOT = 4251
827104
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 19005
00804239
00016717 00000-0 10270-3 0 9042
2 25544 51
6418 92
9558 0002477 245
2306 114
8588 15
53749508 29897
Satellite: ISS
Catalog Number: 25544
Epoch time: 19005
00804239 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 92
9558 deg
Eccentricity:
0002477
Arg of perigee: 245
2306 deg
Mean anomaly: 114
8588 deg
Mean motion: 15
53749508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2989
Checksum: 333
Coasting Arc #6 (Orbit 3004)
---------------------------------------
Vector Time (GMT): 2019/006/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2238998
38 A = 6787925
86 meter
Y = -5898967
37 meter E =
0011809
Z = 2486212
00 I = 52
03509
XDOT = 3991
006472 Wp = 112
60123
YDOT = -3776
842791 meter/sec RA = 87
12201 deg
ZDOT = -5351
282651 TA = 39
68831
MA = 39
60195
Ha = 220
878 n
mi
Hp = 216
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7345795
21 X = -2184944
57
Y = -19353567
49 feet Y = -5923703
47 meter
Z = 8156863
51 Z = 2475466
49
XDOT = 13093
853256 XDOT = 4058
936836
YDOT = -12391
216507 feet/sec YDOT = -3731
832125 meter/sec
ZDOT = -17556
701610 ZDOT = -5331
731510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16903700
35 X = -5152247
87
Y = 11981798
20 feet Y = 3652052
09 meter
Z = 8109077
03 Z = 2471646
68
XDOT = -14415
591321 XDOT = -4393
872235
YDOT = -8480
013622 feet/sec YDOT = -2584
708152 meter/sec
ZDOT = -17467
975931 ZDOT = -5324
239064
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 19006
03713489
00016717 00000-0 10270-3 0 9053
2 25544 51
6414 87
8301 0002544 247
5307 112
5576 15
53721184 30055
Satellite: ISS
Catalog Number: 25544
Epoch time: 19006
03713489 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 87
8301 deg
Eccentricity:
0002544
Arg of perigee: 247
5307 deg
Mean anomaly: 112
5576 deg
Mean motion: 15
53721184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3005
Checksum: 292
Coasting Arc #7 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2019/007/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1675001
29 A = 6789992
59 meter
Y = 6500418
07 meter E =
0007830
Z = -992933
63 I = 52
04074
XDOT = -4397
934078 Wp = 27
15353
YDOT = 2036
767162 meter/sec RA = 82
17708 deg
ZDOT = 5940
249000 TA = 322
15114
MA = 322
20618
Ha = 220
685 n
mi
Hp = 216
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5495411
07 X = 1607010
36
Y = 21326830
93 feet Y = 6518769
04 meter
Z = -3257656
26 Z = -984961
65
XDOT = -14428
917580 XDOT = -4449
236929
YDOT = 6682
306962 feet/sec YDOT = 1987
298911 meter/sec
ZDOT = 19489
005905 ZDOT = 5918
761408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19097691
79 X = 5820976
46
Y = -10979044
65 feet Y = -3346412
81 meter
Z = -3222472
91 Z = -982209
74
XDOT = 9507
189027 XDOT = 2897
791215
YDOT = 10870
243216 feet/sec YDOT = 3313
250132 meter/sec
ZDOT = 19391
742510 ZDOT = 5910
603117
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 19007
00190403
00016717 00000-0 10270-3 0 9067
2 25544 51
6425 83
0232 0002632 255
1346 104
9515 15
53758597 30207
Satellite: ISS
Catalog Number: 25544
Epoch time: 19007
00190403 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 83
0232 deg
Eccentricity:
0002632
Arg of perigee: 255
1346 deg
Mean anomaly: 104
9515 deg
Mean motion: 15
53758597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 278
Coasting Arc #8 (Orbit 3035)
---------------------------------------
Vector Time (GMT): 2019/008/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1021194
20 A = 6790365
07 meter
Y = -6679298
74 meter E =
0009822
Z = -614752
50 I = 52
03574
XDOT = 4764
087086 Wp = 152
80412
YDOT = -179
878447 meter/sec RA = 77
23648 deg
ZDOT = -6005
661720 TA = 33
79524
MA = 33
73267
Ha = 220
750 n
mi
Hp = 216
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3350374
68 X = -943442
44
Y = -21913709
79 feet Y = -6690283
65 meter
Z = -2016904
52 Z = -619524
77
XDOT = 15630
206974 XDOT = 4794
916140
YDOT = -590
152385 feet/sec YDOT = -126
430175 meter/sec
ZDOT = -19703
614566 ZDOT = -5982
445096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20084130
75 X = -6121643
05
Y = 9379734
69 feet Y = 2858943
13 meter
Z = -2037611
38 Z = -621063
95
XDOT = -4327
300085 XDOT = -1318
961066
YDOT = -13490
685643 feet/sec YDOT = -4111
960984 meter/sec
ZDOT = -19598
771072 ZDOT = -5973
705423
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 19008
03098972
00016717 00000-0 10270-3 0 9070
2 25544 51
6423 77
8968 0002600 256
6348 103
4515 15
53715788 30361
Satellite: ISS
Catalog Number: 25544
Epoch time: 19008
03098972 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 77
8968 deg
Eccentricity:
0002600
Arg of perigee: 256
6348 deg
Mean anomaly: 103
4515 deg
Mean motion: 15
53715788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3036
Checksum: 325
Coasting Arc #9 (Orbit 3051)
---------------------------------------
Vector Time (GMT): 2019/009/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 295942
12 A = 6788497
98 meter
Y = 6428437
59 meter E =
0011435
Z = 2143403
01 I = 52
02062
XDOT = -5054
127690 Wp = 66
60907
YDOT = -1619
505482 meter/sec RA = 72
29223 deg
ZDOT = 5536
105262 TA = 317
02559
MA = 317
11486
Ha = 220
672 n
mi
Hp = 216
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 970938
72 X = 213624
26
Y = 21090674
49 feet Y = 6431286
58 meter
Z = 7032162
09 Z = 2144641
12
XDOT = -16581
783760 XDOT = -5062
533138
YDOT = -5313
338196 feet/sec YDOT = -1676
071677 meter/sec
ZDOT = 18163
075006 ZDOT = 5511
534101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19854617
41 X = 6051687
39
Y = -7175393
72 feet Y = -2187060
01 meter
Z = 7036936
04 Z = 2144858
10
XDOT = -609
228886 XDOT = -185
692964
YDOT = 16079
014560 feet/sec YDOT = 4900
883638 meter/sec
ZDOT = 18052
341404 ZDOT = 5502
353660
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 19009
06007209
00016717 00000-0 10270-3 0 9088
2 25544 51
6415 72
7695 0002584 266
3153 93
7704 15
53744782 30521
Satellite: ISS
Catalog Number: 25544
Epoch time: 19009
06007209 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 72
7695 deg
Eccentricity:
0002584
Arg of perigee: 266
3153 deg
Mean anomaly: 93
7704 deg
Mean motion: 15
53744782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3052
Checksum: 313
Coasting Arc #10 (Orbit 3066)
---------------------------------------
Vector Time (GMT): 2019/010/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 551541
80 A = 6785251
53 meter
Y = -5785531
02 meter E =
0002290
Z = -3504084
58 I = 51
99901
XDOT = 5223
511986 Wp = 83
47899
YDOT = 3259
764111 meter/sec RA = 67
34138 deg
ZDOT = -4562
257401 TA = 137
45985
MA = 137
44211
Ha = 220
586 n
mi
Hp = 216
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1809520
35 X = 633216
84
Y = -18981400
98 feet Y = -5778906
41 meter
Z = -11496340
50 Z = -3501207
42
XDOT = 17137
506516 XDOT = 5208
832690
YDOT = 10694
764144 feet/sec YDOT = 3318
095254 meter/sec
ZDOT = -14968
036093 ZDOT = -4536
919441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18611073
91 X = -5672655
33
Y = 4184664
91 feet Y = 1275485
86 meter
Z = -11482608
56 Z = -3499899
09
XDOT = 5029
542251 XDOT = 1533
004478
YDOT = -18369
781779 feet/sec YDOT = -5599
109486 meter/sec
ZDOT = -14854
051892 ZDOT = -4527
515017
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 19010
02483408
00016717 00000-0 10270-3 0 9096
2 25544 51
6418 67
9632 0002785 268
5052 91
5781 15
53746031 30672
Satellite: ISS
Catalog Number: 25544
Epoch time: 19010
02483408 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 67
9632 deg
Eccentricity:
0002785
Arg of perigee: 268
5052 deg
Mean anomaly: 91
5781 deg
Mean motion: 15
53746031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3067
Checksum: 312
Coasting Arc #11 (Orbit 3072)
---------------------------------------
Vector Time (GMT): 2019/010/09:34:56
900
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4651433
25 A = 6780624
93 meter
Y = 1098472
55 meter E =
0009048
Z = -4818468
66 I = 51
97841
XDOT = 1025
760755 Wp = 116
03690
YDOT = 7126
674796 meter/sec RA = 65
31315 deg
ZDOT = 2614
818164 TA = 179
64106
MA = 179
64041
Ha = 220
594 n
mi
Hp = 216
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15260607
78 X = 4662209
16
Y = 3603912
57 feet Y = 1150548
63 meter
Z = -15808624
20 Z = -4795847
89
XDOT = 3365
356809 XDOT = 933
290924
YDOT = 23381
478989 feet/sec YDOT = 7137
628396 meter/sec
ZDOT = 8578
799752 ZDOT = 2619
576632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8061937
24 X = -2457278
47
Y = 13568117
32 feet Y = 4135562
16 meter
Z = -15706632
20 Z = -4787381
49
XDOT = -22303
721046 XDOT = -6798
174175
YDOT = -3297
503976 feet/sec YDOT = -1005
079212 meter/sec
ZDOT = 8599
367560 ZDOT = 2621
087232
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 19010
41073794
00016717 00000-0 10270-3 0 9104
2 25544 51
6416 66
0370 0002643 260
8366 99
2487 15
53786527 30734
Satellite: ISS
Catalog Number: 25544
Epoch time: 19010
41073794 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 66
0370 deg
Eccentricity:
0002643
Arg of perigee: 260
8366 deg
Mean anomaly: 99
2487 deg
Mean motion: 15
53786527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3073
Checksum: 312
Coasting Arc #12 (Orbit 3088)
---------------------------------------
Vector Time (GMT): 2019/011/09:34:56
900
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4942481
48 A = 6783992
53 meter
Y = -2504255
84 meter E =
0008687
Z = 3908428
30 I = 51
97468
XDOT = 18
140376 Wp = 79
22607
YDOT = -6471
987128 meter/sec RA = 60
34885 deg
ZDOT = -4114
555994 TA = 53
74129
MA = 53
66105
Ha = 220
724 n
mi
Hp = 216
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16215490
41 X = -4933095
53
Y = -8216062
47 feet Y = -2559473
78 meter
Z = 12822927
48 Z = 3884442
64
XDOT = 59
515669 XDOT = 110
496526
YDOT = -21233
553569 feet/sec YDOT = -6471
267712 meter/sec
ZDOT = -13499
199454 ZDOT = -4114
243818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12515054
14 X = 3814588
50
Y = -13288209
93 feet Y = -4050246
39 meter
Z = 12714958
81 Z = 3875519
45
XDOT = 19344
619908 XDOT = 5896
240148
YDOT = 5274
896897 feet/sec YDOT = 1607
788574 meter/sec
ZDOT = -13496
949494 ZDOT = -4113
870206
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 19011
43981423
00016717 00000-0 10270-3 0 9115
2 25544 51
6416 60
9099 0002591 267
9038 92
1818 15
53773436 30893
Satellite: ISS
Catalog Number: 25544
Epoch time: 19011
43981423 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 60
9099 deg
Eccentricity:
0002591
Arg of perigee: 267
9038 deg
Mean anomaly: 92
1818 deg
Mean motion: 15
53773436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3089
Checksum: 322
Coasting Arc #13 (Orbit 3103)
---------------------------------------
Vector Time (GMT): 2019/012/09:34:56
900
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5056833
59 A = 6787495
71 meter
Y = 3657024
72 meter E =
0003326
Z = -2665738
08 I = 51
96795
XDOT = -1199
413253 Wp = 22
86403
YDOT = 5469
808436 meter/sec RA = 55
39279 deg
ZDOT = 5233
734531 TA = 307
22090
MA = 307
25124
Ha = 220
633 n
mi
Hp = 216
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16590661
37 X = 5028512
39
Y = 11998112
60 feet Y = 3713415
48 meter
Z = -8745859
84 Z = -2641242
87
XDOT = -3935
082852 XDOT = -1285
911297
YDOT = 17945
565736 feet/sec YDOT = 5455
911965 meter/sec
ZDOT = 17171
045049 ZDOT = 5227
698384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16021791
30 X = -4883441
99
Y = 12822669
99 feet Y = 3908349
81 meter
Z = -8635748
56 Z = -2632176
16
XDOT = -15269
038801 XDOT = -4654
003026
YDOT = -7544
631922 feet/sec YDOT = -2299
603810 meter/sec
ZDOT = 17143
075525 ZDOT = 5225
209420
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 19012
40457180
00016717 00000-0 10270-3 0 9122
2 25544 51
6408 56
1038 0002729 271
5796 88
5044 15
53748294 31041
Satellite: ISS
Catalog Number: 25544
Epoch time: 19012
40457180 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 56
1038 deg
Eccentricity:
0002729
Arg of perigee: 271
5796 deg
Mean anomaly: 88
5044 deg
Mean motion: 15
53748294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3104
Checksum: 307
Coasting Arc #14 (Orbit 3119)
---------------------------------------
Vector Time (GMT): 2019/013/09:38:56
900
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4147071
26 A = 6790335
14 meter
Y = -5362890
95 meter E =
0009679
Z = -278620
60 I = 51
95796
XDOT = 3890
008123 Wp = 147
00385
YDOT = -2700
301850 meter/sec RA = 50
44271 deg
ZDOT = -6030
707672 TA = 35
98497
MA = 35
91984
Ha = 220
608 n
mi
Hp = 216
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13605876
84 X = -4085440
32
Y = -17594786
58 feet Y = -5408921
78 meter
Z = -914109
59 Z = -298615
78
XDOT = 12762
493842 XDOT = 3949
208088
YDOT = -8859
258037 feet/sec YDOT = -2656
469898 meter/sec
ZDOT = -19785
786324 ZDOT = -6011
667943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20293444
50 X = 6185441
89
Y = -9093995
52 feet Y = -2771849
83 meter
Z = -1003668
97 Z = -305918
30
XDOT = 4926
558163 XDOT = 1501
614928
YDOT = 13132
882053 feet/sec YDOT = 4002
902450 meter/sec
ZDOT = -19699
471180 ZDOT = -6004
398816
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 19013
43364459
00016717 00000-0 10270-3 0 9133
2 25544 51
6408 50
9768 0002608 275
5669 84
5186 15
53768640 31200
Satellite: ISS
Catalog Number: 25544
Epoch time: 19013
43364459 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 50
9768 deg
Eccentricity:
0002608
Arg of perigee: 275
5669 deg
Mean anomaly: 84
5186 deg
Mean motion: 15
53768640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3120
Checksum: 327
Coasting Arc #15 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2019/014/09:38:56
900
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3439116
92 A = 6788940
84 meter
Y = 5550207
40 meter E =
0012014
Z = 1835985
64 I = 51
93168
XDOT = -5018
521925 Wp = 58
72298
YDOT = 1227
547998 meter/sec RA = 45
49354 deg
ZDOT = 5668
438922 TA = 321
38764
MA = 321
47349
Ha = 220
684 n
mi
Hp = 216
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11283192
00 X = 3367879
21
Y = 18209341
87 feet Y = 5588267
63 meter
Z = 6023574
93 Z = 1852518
62
XDOT = -16464
966946 XDOT = -5059
409663
YDOT = 4027
388444 feet/sec YDOT = 1171
198589 meter/sec
ZDOT = 18597
240558 ZDOT = 5643
961724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20220983
51 X = -6163355
77
Y = 7007619
47 feet Y = 2135922
42 meter
Z = 6097466
94 Z = 1858507
92
XDOT = 191
269058 XDOT = 58
298809
YDOT = -15593
462955 feet/sec YDOT = -4752
887509 meter/sec
ZDOT = 18486
575783 ZDOT = 5634
708299
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 19014
46271425
00016717 00000-0 10270-3 0 9148
2 25544 51
6413 45
8494 0002549 283
6705 76
4163 15
53759680 31366
Satellite: ISS
Catalog Number: 25544
Epoch time: 19014
46271425 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 45
8494 deg
Eccentricity:
0002549
Arg of perigee: 283
6705 deg
Mean anomaly: 76
4163 deg
Mean motion: 15
53759680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 318
Coasting Arc #16 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2019/015/09:38:56
900
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2436075
76 A = 6785849
94 meter
Y = -5437186
98 meter E =
0002215
Z = -3250192
14 I = 51
89662
XDOT = 5982
552842 Wp = 86
20101
YDOT = 178
555445 meter/sec RA = 40
53809 deg
ZDOT = -4785
393379 TA = 131
28638
MA = 131
26731
Ha = 220
705 n
mi
Hp = 216
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7992374
55 X = -2359307
01
Y = -17838539
97 feet Y = -5463999
49 meter
Z = -10663360
03 Z = -3261839
41
XDOT = 19627
798038 XDOT = 6003
356215
YDOT = 585
811826 feet/sec YDOT = 245
573052 meter/sec
ZDOT = -15700
109510 ZDOT = -4756
281990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19067086
35 X = 5811647
92
Y = -4174867
27 feet Y = -1272499
54 meter
Z = -10715199
84 Z = -3265992
91
XDOT = -4842
100631 XDOT = -1475
872272
YDOT = 17821
885049 feet/sec YDOT = 5432
110563 meter/sec
ZDOT = -15568
718916 ZDOT = -4745
345526
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 19015
42746582
00016717 00000-0 10270-3 0 9157
2 25544 51
6404 41
0434 0002481 286
4021 73
6858 15
53770641 31512
Satellite: ISS
Catalog Number: 25544
Epoch time: 19015
42746582 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 41
0434 deg
Eccentricity:
0002481
Arg of perigee: 286
4021 deg
Mean anomaly: 73
6858 deg
Mean motion: 15
53770641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 293
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