[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 28th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 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
033/17:25:00
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
039/16:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 215
6
040/11:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 215
6
Coasting Arc #1 (Orbit 3354)
---------------------------------------
Vector Time (GMT): 2019/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3855230
45 A = 6781426
77 meter
Y = 2569009
56 meter E =
0002096
Z = 4950341
58 I = 51
46796
XDOT = -5791
242222 Wp = 71
59812
YDOT = 4541
947359 meter/sec RA = 335
36453 deg
ZDOT = 2152
935654 TA = 357
36831
MA = 357
36942
Ha = 221
993 n
mi
Hp = 217
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12648393
85 X = 3802170
83
Y = 8428509
07 feet Y = 2611824
72 meter
Z = 16241278
15 Z = 4968939
76
XDOT = -19000
138525 XDOT = -5852
058776
YDOT = 14901
402096 feet/sec YDOT = 4476
845585 meter/sec
ZDOT = 7063
437186 ZDOT = 2124
656659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 703841
38 X = 214530
85
Y = 15093209
76 feet Y = 4600410
33 meter
Z = 16324839
19 Z = 4975810
99
XDOT = -22216
977183 XDOT = -6771
734645
YDOT = -6465
486818 feet/sec YDOT = -1970
680382 meter/sec
ZDOT = 6935
246997 ZDOT = 2113
863285
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
55195016
00016717 00000-0 10270-3 0 9009
2 25544 51
6399 335
6965 0005126 321
6683 38
4105 15
53235487 33555
Satellite: ISS
Catalog Number: 25544
Epoch time: 19028
55195016 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 335
6965 deg
Eccentricity:
0005126
Arg of perigee: 321
6683 deg
Mean anomaly: 38
4105 deg
Mean motion: 15
53235487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3355
Checksum: 318
Coasting Arc #2 (Orbit 3369)
---------------------------------------
Vector Time (GMT): 2019/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2682361
63 A = 6780168
76 meter
Y = -3317727
68 meter E =
0012980
Z = -5280262
99 I = 51
43346
XDOT = 6382
613173 Wp = 65
13224
YDOT = -4187
983213 meter/sec RA = 330
36241 deg
ZDOT = -606
762016 TA = 199
02743
MA = 199
07596
Ha = 222
275 n
mi
Hp = 216
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8800399
05 X = -2619414
27
Y = -10884933
34 feet Y = -3347371
64 meter
Z = -17323697
47 Z = -5293139
91
XDOT = 20940
331932 XDOT = 6431
917289
YDOT = -13740
102405 feet/sec YDOT = -4116
332693 meter/sec
ZDOT = -1990
689030 ZDOT = -575
638434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3334183
94 X = 1016259
27
Y = -13520772
97 feet Y = -4121131
60 meter
Z = -17381346
53 Z = -5297834
42
XDOT = 22679
936667 XDOT = 6912
844696
YDOT = 7988
214657 feet/sec YDOT = 2434
807827 meter/sec
ZDOT = -1849
722753 ZDOT = -563
795495
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
51705944
00016717 00000-0 10270-3 0 9014
2 25544 51
6398 330
8918 0005110 326
2721 33
8105 15
53199543 33704
Satellite: ISS
Catalog Number: 25544
Epoch time: 19029
51705944 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 330
8918 deg
Eccentricity:
0005110
Arg of perigee: 326
2721 deg
Mean anomaly: 33
8105 deg
Mean motion: 15
53199543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3370
Checksum: 302
Coasting Arc #3 (Orbit 3385)
---------------------------------------
Vector Time (GMT): 2019/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1446758
76 A = 6780366
26 meter
Y = 4070553
33 meter E =
0006502
Z = 5226564
79 I = 51
40660
XDOT = -6669
831453 Wp = 3
61821
YDOT = 3648
914962 meter/sec RA = 325
35778 deg
ZDOT = -989
146899 TA = 95
92013
MA = 95
84601
Ha = 222
381 n
mi
Hp = 216
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4746583
86 X = 1375745
81
Y = 13354833
77 feet Y = 4086334
76 meter
Z = 17147522
26 Z = 5233420
15
XDOT = -21882
649123 XDOT = -6705
334284
YDOT = 11971
505780 feet/sec YDOT = 3574
129783 meter/sec
ZDOT = -3245
232609 ZDOT = -1021
632044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7558321
84 X = -2303776
50
Y = 11946144
64 feet Y = 3641184
89 meter
Z = 17177909
14 Z = 5235826
70
XDOT = -22114
890764 XDOT = -6740
618705
YDOT = -9083
898840 feet/sec YDOT = -2768
772366 meter/sec
ZDOT = -3392
260945 ZDOT = -1033
961136
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
54650498
00016717 00000-0 10270-3 0 9023
2 25544 51
6405 325
7679 0005226 329
7068 30
3781 15
53214998 33861
Satellite: ISS
Catalog Number: 25544
Epoch time: 19030
54650498 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 325
7679 deg
Eccentricity:
0005226
Arg of perigee: 329
7068 deg
Mean anomaly: 30
3781 deg
Mean motion: 15
53214998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3386
Checksum: 328
Coasting Arc #4 (Orbit 3400)
---------------------------------------
Vector Time (GMT): 2019/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -272802
98 A = 6782162
00 meter
Y = -4772129
72 meter E =
0008785
Z = -4818531
65 I = 51
38590
XDOT = 6633
630307 Wp = 82
18795
YDOT = -2901
099717 meter/sec RA = 320
35238 deg
ZDOT = 2502
694325 TA = 212
50025
MA = 212
55437
Ha = 222
539 n
mi
Hp = 216
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -895022
90 X = -196014
09
Y = -15656593
57 feet Y = -4774750
85 meter
Z = -15808830
86 Z = -4819670
49
XDOT = 21763
878961 XDOT = 6653
421727
YDOT = -9518
043691 feet/sec YDOT = -2826
807279 meter/sec
ZDOT = 8210
939387 ZDOT = 2534
965372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11572868
32 X = 3527410
26
Y = -10576200
46 feet Y = -3223625
90 meter
Z = -15813343
24 Z = -4819907
02
XDOT = 20387
988663 XDOT = 6214
258944
YDOT = 9839
206781 feet/sec YDOT = 2998
990227 meter/sec
ZDOT = 8356
896022 ZDOT = 2547
181907
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
51160818
00016717 00000-0 10270-3 0 9034
2 25544 51
6406 320
9629 0005205 334
6950 25
3947 15
53213160 34012
Satellite: ISS
Catalog Number: 25544
Epoch time: 19031
51160818 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 320
9629 deg
Eccentricity:
0005205
Arg of perigee: 334
6950 deg
Mean anomaly: 25
3947 deg
Mean motion: 15
53213160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3401
Checksum: 280
Coasting Arc #5 (Orbit 3416)
---------------------------------------
Vector Time (GMT): 2019/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -837798
91 A = 6785082
25 meter
Y = 5377074
57 meter E =
0011073
Z = 4050283
53 I = 51
37059
XDOT = -6338
271506 Wp = 50
09733
YDOT = 1928
331460 meter/sec RA = 315
35218 deg
ZDOT = -3857
080767 TA = 80
05984
MA = 79
93488
Ha = 222
684 n
mi
Hp = 216
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2748684
08 X = -917538
20
Y = 17641320
77 feet Y = 5367259
71 meter
Z = 13288331
79 Z = 4046020
45
XDOT = -20794
854022 XDOT = -6340
628437
YDOT = 6326
546784 feet/sec YDOT = 1857
439464 meter/sec
ZDOT = -12654
464459 ZDOT = -3887
874691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15254292
94 X = -4649508
49
Y = 9306297
19 feet Y = 2836559
38 meter
Z = 13268406
23 Z = 4044210
22
XDOT = -17586
074680 XDOT = -5360
235563
YDOT = -10519
942822 feet/sec YDOT = -3206
478572 meter/sec
ZDOT = -12793
625294 ZDOT = -3899
496990
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
54105046
00016717 00000-0 10270-3 0 9041
2 25544 51
6405 315
8393 0005209 337
9854 22
1074 15
53207542 34175
Satellite: ISS
Catalog Number: 25544
Epoch time: 19032
54105046 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 315
8393 deg
Eccentricity:
0005209
Arg of perigee: 337
9854 deg
Mean anomaly: 22
1074 deg
Mean motion: 15
53207542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3417
Checksum: 290
Coasting Arc #6 (Orbit 3431)
---------------------------------------
Vector Time (GMT): 2019/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1771896
48 A = 6788141
98 meter
Y = -5812725
58 meter E =
0006985
Z = -3019117
12 I = 51
35867
XDOT = 5824
671690 Wp = 20
85826
YDOT = -776
360645 meter/sec RA = 310
35603 deg
ZDOT = 4923
111408 TA = 304
41569
MA = 304
48170
Ha = 222
746 n
mi
Hp = 216
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5813308
66 X = 1851429
15
Y = -19070621
97 feet Y = -5792466
20 meter
Z = -9905239
88 Z = -3010317
14
XDOT = 19109
815256 XDOT = 5809
007133
YDOT = -2547
114976 feet/sec YDOT = -711
312848 meter/sec
ZDOT = 16151
940316 ZDOT = 4951
366705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18178115
28 X = 5540689
54
Y = -8236425
69 feet Y = -2510462
55 meter
Z = -9864804
79 Z = -3006792
50
XDOT = 13898
846538 XDOT = 4236
368425
YDOT = 11216
429383 feet/sec YDOT = 3418
767676 meter/sec
ZDOT = 16279
497973 ZDOT = 4961
990982
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
50615065
00016717 00000-0 10270-3 0 9056
2 25544 51
6412 311
0349 0005242 340
8064 19
2890 15
53218606 34328
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
50615065 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 311
0349 deg
Eccentricity:
0005242
Arg of perigee: 340
8064 deg
Mean anomaly: 19
2890 deg
Mean motion: 15
53218606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3432
Checksum: 278
Coasting Arc #7 (Orbit 3435)
---------------------------------------
Vector Time (GMT): 2019/033/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1927003
44 A = 6788616
69 meter
Y = 5880973
58 meter E =
0011558
Z = 2784343
89 I = 51
35445
XDOT = -5704
343062 Wp = 76
60881
YDOT = 550
795823 meter/sec RA = 309
22691 deg
ZDOT = -5090
766105 TA = 71
70048
MA = 71
57477
Ha = 222
689 n
mi
Hp = 216
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6322189
76 X = -2006147
38
Y = 19294532
74 feet Y = 5858981
88 meter
Z = 9134986
52 Z = 2774791
42
XDOT = -18715
036293 XDOT = -5685
350781
YDOT = 1807
072909 feet/sec YDOT = 487
112223 meter/sec
ZDOT = -16701
988534 ZDOT = -5118
428814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5149139
85 X = 1569457
83
Y = 19660477
60 feet Y = 5992513
57 meter
Z = 9091151
46 Z = 2770982
97
XDOT = -13188
365034 XDOT = -4019
813662
YDOT = 11266
171938 feet/sec YDOT = 3433
929207 meter/sec
ZDOT = -16826
843925 ZDOT = -5128
822028
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
76350690
00016717 00000-0 10270-3 0 9065
2 25544 51
6399 309
7515 0005443 339
1281 20
9649 15
53256327 34363
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
76350690 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 309
7515 deg
Eccentricity:
0005443
Arg of perigee: 339
1281 deg
Mean anomaly: 20
9649 deg
Mean motion: 15
53256327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3436
Checksum: 322
Coasting Arc #8 (Orbit 3450)
---------------------------------------
Vector Time (GMT): 2019/034/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2659876
83 A = 6791041
58 meter
Y = -6055620
97 meter E =
0012141
Z = -1509913
10 I = 51
34048
XDOT = 5024
072556 Wp = 17
36666
YDOT = 781
063123 meter/sec RA = 304
23600 deg
ZDOT = 5741
266308 TA = 326
07336
MA = 326
15096
Ha = 222
836 n
mi
Hp = 216
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8726630
00 X = 2734728
92
Y = -19867522
88 feet Y = -6025457
83 meter
Z = -4953783
14 Z = -1496811
07
XDOT = 16483
177678 XDOT = 4987
077986
YDOT = 2562
543056 feet/sec YDOT = 837
038872 meter/sec
ZDOT = 18836
175550 ZDOT = 5765
580852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3835608
35 X = -1169093
43
Y = -21371711
76 feet Y = -6514097
74 meter
Z = -4893929
82 Z = -1491669
81
XDOT = 13439
795508 XDOT = 4096
449671
YDOT = -6732
726708 feet/sec YDOT = -2052
135101 meter/sec
ZDOT = 18945
760303 ZDOT = 5774
667740
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19034
72860595
00016717 00000-0 10270-3 0 9073
2 25544 51
6383 304
9465 0005183 344
4128 15
6864 15
53215074 34518
Satellite: ISS
Catalog Number: 25544
Epoch time: 19034
72860595 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 304
9465 deg
Eccentricity:
0005183
Arg of perigee: 344
4128 deg
Mean anomaly: 15
6864 deg
Mean motion: 15
53215074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3451
Checksum: 315
Coasting Arc #9 (Orbit 3466)
---------------------------------------
Vector Time (GMT): 2019/035/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3249260
20 A = 6791820
30 meter
Y = 5960835
69 meter E =
0008394
Z = 96811
72 I = 51
32534
XDOT = -4248
778900 Wp = 111
86272
YDOT = -2212
117393 meter/sec RA = 299
24887 deg
ZDOT = -5981
737928 TA = 67
09078
MA = 67
00220
Ha = 222
926 n
mi
Hp = 216
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10660302
51 X = -3316144
70
Y = 19556547
54 feet Y = 5924126
22 meter
Z = 317623
77 Z = 80866
03
XDOT = -13939
563319 XDOT = -4194
671485
YDOT = -7257
602996 feet/sec YDOT = -2259
327683 meter/sec
ZDOT = -19625
124437 ZDOT = -6002
244888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2464863
05 X = 751290
26
Y = 22137432
67 feet Y = 6747489
48 meter
Z = 244971
84 Z = 74667
42
XDOT = -13861
830262 XDOT = -4225
085864
YDOT = 1781
173543 feet/sec YDOT = 542
901696 meter/sec
ZDOT = -19717
361473 ZDOT = -6009
851777
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19035
75804100
00016717 00000-0 10270-3 0 9088
2 25544 51
6378 299
8221 0005414 348
7418 11
3612 15
53269740 34670
Satellite: ISS
Catalog Number: 25544
Epoch time: 19035
75804100 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 299
8221 deg
Eccentricity:
0005414
Arg of perigee: 348
7418 deg
Mean anomaly: 11
3612 deg
Mean motion: 15
53269740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3467
Checksum: 312
Coasting Arc #10 (Orbit 3482)
---------------------------------------
Vector Time (GMT): 2019/036/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3645425
60 A = 6791255
09 meter
Y = -5570463
16 meter E =
0016422
Z = 1291903
45 I = 51
30690
XDOT = 3467
821514 Wp = 42
73625
YDOT = 3623
262872 meter/sec RA = 294
25969 deg
ZDOT = 5805
940984 TA = 331
39117
MA = 331
48118
Ha = 222
966 n
mi
Hp = 216
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11960057
74 X = 3701169
99
Y = -18275797
77 feet Y = -5529385
76 meter
Z = 4238528
39 Z = 1309746
56
XDOT = 11377
367171 XDOT = 3398
846207
YDOT = 11887
345381 feet/sec YDOT = 3661
656924 meter/sec
ZDOT = 19048
362810 ZDOT = 5822
618280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1065753
78 X = -324841
75
Y = -21799483
17 feet Y = -6644482
47 meter
Z = 4319674
83 Z = 1316636
89
XDOT = 14496
347868 XDOT = 4418
486830
YDOT = 3100
809102 feet/sec YDOT = 945
126614 meter/sec
ZDOT = 19123
163499 ZDOT = 5828
740235
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19036
78747777
00016717 00000-0 10270-3 0 9099
2 25544 51
6371 294
6968 0005083 352
3415 7
7658 15
53215923 34835
Satellite: ISS
Catalog Number: 25544
Epoch time: 19036
78747777 = yrday
fracday
Element set: 909
Inclination: 51
6371 deg
RA of node: 294
6968 deg
Eccentricity:
0005083
Arg of perigee: 352
3415 deg
Mean anomaly: 7
7658 deg
Mean motion: 15
53215923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3483
Checksum: 348
Coasting Arc #11 (Orbit 3497)
---------------------------------------
Vector Time (GMT): 2019/037/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3929391
48 A = 6788919
46 meter
Y = 4881554
82 meter E =
0004457
Z = -2618307
61 I = 51
28764
XDOT = -2683
823180 Wp = 58
98934
YDOT = -4945
440456 meter/sec RA = 289
26654 deg
ZDOT = -5196
878299 TA = 150
61939
MA = 150
59433
Ha = 223
148 n
mi
Hp = 215
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12891704
34 X = -3970968
43
Y = 16015599
81 feet Y = 4837381
06 meter
Z = -8590248
06 Z = -2637495
76
XDOT = -8805
194161 XDOT = -2603
079544
YDOT = -16225
198346 feet/sec YDOT = -4975
001564 meter/sec
ZDOT = -17050
125653 ZDOT = -5209
718662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -638938
39 X = -194748
42
Y = 20512994
41 feet Y = 6252360
70 meter
Z = -8677364
68 Z = -2644860
75
XDOT = -15200
096026 XDOT = -4632
989269
YDOT = -7704
250604 feet/sec YDOT = -2348
255584 meter/sec
ZDOT = -17107
476212 ZDOT = -5214
358750
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19037
75257045
00016717 00000-0 10270-3 0 9103
2 25544 51
6379 289
8923 0005232 357
8205 2
2923 15
53250459 34987
Satellite: ISS
Catalog Number: 25544
Epoch time: 19037
75257045 = yrday
fracday
Element set: 910
Inclination: 51
6379 deg
RA of node: 289
8923 deg
Eccentricity:
0005232
Arg of perigee: 357
8205 deg
Mean anomaly: 2
2923 deg
Mean motion: 15
53250459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3498
Checksum: 324
Coasting Arc #12 (Orbit 3513)
---------------------------------------
Vector Time (GMT): 2019/038/17:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4084430
50 A = 6785907
13 meter
Y = -3916712
43 meter E =
0012132
Z = 3731756
12 I = 51
26619
XDOT = 1959
373512 Wp = 72
11973
YDOT = 6088
350836 meter/sec RA = 284
26584 deg
ZDOT = 4237
831864 TA = 332
76972
MA = 332
83328
Ha = 223
039 n
mi
Hp = 215
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13400362
53 X = 4109798
37
Y = -12850106
40 feet Y = -3870895
45 meter
Z = 12243294
35 Z = 3751658
07
XDOT = 6428
390788 XDOT = 1870
561708
YDOT = 19974
904319 feet/sec YDOT = 6109
765554 meter/sec
ZDOT = 13903
647848 ZDOT = 4247
133522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2613113
65 X = 796477
04
Y = -18320738
27 feet Y = -5584161
02 meter
Z = 12333506
94 Z = 3759252
92
XDOT = 15935
919823 XDOT = 4857
268362
YDOT = 11677
617975 feet/sec YDOT = 3559
337959 meter/sec
ZDOT = 13944
921597 ZDOT = 4250
412103
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19038
78200149
00016717 00000-0 10270-3 0 9111
2 25544 51
6365 284
7667 0004991
7682 359
3477 15
53243958 35140
Satellite: ISS
Catalog Number: 25544
Epoch time: 19038
78200149 = yrday
fracday
Element set: 911
Inclination: 51
6365 deg
RA of node: 284
7667 deg
Eccentricity:
0004991
Arg of perigee:
7682 deg
Mean anomaly: 359
3477 deg
Mean motion: 15
53243958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3514
Checksum: 335
Coasting Arc #13 (Orbit 3527)
---------------------------------------
Vector Time (GMT): 2019/039/16:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2566827
10 A = 6784675
58 meter
Y = -4738278
48 meter E =
0007995
Z = -4126875
93 I = 51
25470
XDOT = 3947
242157 Wp = 70
96035
YDOT = -5393
355970 meter/sec RA = 279
47230 deg
ZDOT = 3745
820944 TA = 237
81947
MA = 237
89703
Ha = 223
253 n
mi
Hp = 215
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8421348
76 X = -2493605
93
Y = -15545533
06 feet Y = -4766573
37 meter
Z = -13539619
20 Z = -4139166
23
XDOT = 12950
269544 XDOT = 3989
064096
YDOT = -17694
737436 feet/sec YDOT = -5348
981093 meter/sec
ZDOT = 12289
438794 ZDOT = 3765
096643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13164635
94 X = -4012581
03
Y = -11738181
67 feet Y = -3577797
77 meter
Z = -13594537
61 Z = -4143615
06
XDOT = 5149
819359 XDOT = 1569
664941
YDOT = -20077
713203 feet/sec YDOT = -6119
686984 meter/sec
ZDOT = 12376
977055 ZDOT = 3772
502606
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 19039
68275357
00016717 00000-0 10270-3 0 9125
2 25544 51
6361 280
2834 0005128 4
2479 355
8716 15
53229196 35289
Satellite: ISS
Catalog Number: 25544
Epoch time: 19039
68275357 = yrday
fracday
Element set: 912
Inclination: 51
6361 deg
RA of node: 280
2834 deg
Eccentricity:
0005128
Arg of perigee: 4
2479 deg
Mean anomaly: 355
8716 deg
Mean motion: 15
53229196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3528
Checksum: 328
Coasting Arc #14 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2019/040/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3843489
14 A = 6780884
02 meter
Y = 2385179
63 meter E =
0009799
Z = 5049739
58 I = 51
24357
XDOT = -2110
343879 Wp = 29
35732
YDOT = 7158
123214 meter/sec RA = 275
48206 deg
ZDOT = -1764
948791 TA = 77
86337
MA = 77
75361
Ha = 223
233 n
mi
Hp = 215
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12609872
51 X = 3792003
36
Y = 7825392
48 feet Y = 2427872
64 meter
Z = 16567387
08 Z = 5068284
27
XDOT = -6923
700390 XDOT = -2181
658208
YDOT = 23484
656213 feet/sec YDOT = 7134
125024 meter/sec
ZDOT = -5790
514407 ZDOT = -1775
373504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1785285
59 X = 544155
05
Y = 14638587
90 feet Y = 4461841
59 meter
Z = 16650779
75 Z = 5075157
67
XDOT = -21514
774371 XDOT = -6557
703228
YDOT = 9301
331442 feet/sec YDOT = 2835
045824 meter/sec
ZDOT = -5838
306878 ZDOT = -1779
515936
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 19040
51916333
00016717 00000-0 10270-3 0 9136
2 25544 51
6410 276
1241 0005497 4
2564 355
8634 15
53276563 35418
Satellite: ISS
Catalog Number: 25544
Epoch time: 19040
51916333 = yrday
fracday
Element set: 913
Inclination: 51
6410 deg
RA of node: 276
1241 deg
Eccentricity:
0005497
Arg of perigee: 4
2564 deg
Mean anomaly: 355
8634 deg
Mean motion: 15
53276563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 298
Coasting Arc #15 (Orbit 3555)
---------------------------------------
Vector Time (GMT): 2019/041/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3557018
37 A = 6783364
85 meter
Y = -3668009
10 meter E =
0009961
Z = -4469006
20 I = 51
24921
XDOT = 2625
856893 Wp = 77
28246
YDOT = -6442
478500 meter/sec RA = 270
46796 deg
ZDOT = 3205
989293 TA = 225
13328
MA = 225
21422
Ha = 223
447 n
mi
Hp = 215
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11670007
79 X = -3494029
68
Y = -12034150
60 feet Y = -3707434
24 meter
Z = -14662093
84 Z = -4486131
40
XDOT = 8615
016053 XDOT = 2682
130670
YDOT = -21136
740487 feet/sec YDOT = -6412
799501 meter/sec
ZDOT = 10518
337577 ZDOT = 3218
881580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1783344
41 X = 543563
38
Y = -16600293
83 feet Y = -5059769
56 meter
Z = -14738954
70 Z = -4492433
39
XDOT = 20473
764236 XDOT = 6240
403339
YDOT = -7167
896740 feet/sec YDOT = -2184
774926 meter/sec
ZDOT = 10577
168251 ZDOT = 3223
920883
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 19041
48425230
00016717 00000-0 10270-3 0 9145
2 25544 51
6407 271
3191 0005575 8
3800 351
7445 15
53242953 35567
Satellite: ISS
Catalog Number: 25544
Epoch time: 19041
48425230 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 271
3191 deg
Eccentricity:
0005575
Arg of perigee: 8
3800 deg
Mean anomaly: 351
7445 deg
Mean motion: 15
53242953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3556
Checksum: 296
Coasting Arc #16 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2019/042/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3228095
23 A = 6786470
55 meter
Y = 4804694
06 meter E =
0014650
Z = 3536982
61 I = 51
26006
XDOT = -3146
508478 Wp = 65
32943
YDOT = 5399
289068 meter/sec RA = 265
46065 deg
ZDOT = -4442
198800 TA = 72
72084
MA = 72
56059
Ha = 223
561 n
mi
Hp = 215
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10590863
61 X = 3156947
39
Y = 15763431
96 feet Y = 4840395
24 meter
Z = 11604273
66 Z = 3552490
25
XDOT = -10323
190546 XDOT = -3185
073536
YDOT = 17714
202980 feet/sec YDOT = 5363
886764 meter/sec
ZDOT = -14574
143044 ZDOT = -4457
577097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5007066
25 X = -1526153
79
Y = 18274699
84 feet Y = 5570128
51 meter
Z = 11673730
32 Z = 3558153
00
XDOT = -18745
697410 XDOT = -5713
688571
YDOT = 4261
231587 feet/sec YDOT = 1298
823388 meter/sec
ZDOT = -14644
067171 ZDOT = -4463
511674
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 19042
51367812
00016717 00000-0 10270-3 0 9152
2 25544 51
6401 266
1941 0005706 12
5894 347
5399 15
53268461 35723
Satellite: ISS
Catalog Number: 25544
Epoch time: 19042
51367812 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 266
1941 deg
Eccentricity:
0005706
Arg of perigee: 12
5894 deg
Mean anomaly: 347
5399 deg
Mean motion: 15
53268461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 319
Coasting Arc #17 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2019/043/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2891789
57 A = 6789498
28 meter
Y = -5655197
55 meter E =
0010748
Z = -2387513
18 I = 51
27320
XDOT = 3651
488061 Wp = 30
65022
YDOT = -4113
548492 meter/sec RA = 260
46064 deg
ZDOT = 5340
578757 TA = 302
54113
MA = 302
64491
Ha = 223
626 n
mi
Hp = 215
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9487498
57 X = -2816739
55
Y = -18553797
73 feet Y = -5687116
01 meter
Z = -7833048
50 Z = -2401377
78
XDOT = 11979
947707 XDOT = 3671
274264
YDOT = -13495
894001 feet/sec YDOT = -4072
604184 meter/sec
ZDOT = 17521
583848 ZDOT = 5358
364316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7487500
21 X = 2282190
06
Y = -19422118
66 feet Y = -5919861
77 meter
Z = -7895019
66 Z = -2406401
99
XDOT = 16549
923005 XDOT = 5044
416532
YDOT = -748
905223 feet/sec YDOT = -228
266312 meter/sec
ZDOT = 17602
228932 ZDOT = 5365
159378
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 19043
47876489
00016717 00000-0 10270-3 0 9164
2 25544 51
6398 261
3895 0005634 14
4959 345
6354 15
53225336 35876
Satellite: ISS
Catalog Number: 25544
Epoch time: 19043
47876489 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 261
3895 deg
Eccentricity:
0005634
Arg of perigee: 14
4959 deg
Mean anomaly: 345
6354 deg
Mean motion: 15
53225336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 354
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