[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 12th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13725 3851 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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
193/19:17:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 217
5
194/07:47:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 217
7
201/16:28:21
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 218
5
201/22:50:20
000 0
0 -0
0 0
0
N/A -0
0 0
0 227
4
000/00:00:40
000 0
0 -0
0 218
6
202/23:35:13
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
7
203/20:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 219
0
204/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
9
Coasting Arc #1 (Orbit 1917)
---------------------------------------
Vector Time (GMT): 2019/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1340614
76 A = 6788952
79 meter
Y = -4667316
35 meter E =
0014618
Z = 4737671
90 I = 51
31208
XDOT = 5713
706720 Wp = 125
52863
YDOT = 4362
816112 meter/sec RA = 234
64746 deg
ZDOT = 2667
054488 TA = 297
93481
MA = 298
08273
Ha = 228
221 n
mi
Hp = 217
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4398342
39 X = 1369693
52
Y = -15312717
69 feet Y = -4652162
71 meter
Z = 15543542
98 Z = 4744254
07
XDOT = 18745
756956 XDOT = 5651
540797
YDOT = 14313
701154 feet/sec YDOT = 4426
362834 meter/sec
ZDOT = 8750
178765 ZDOT = 2694
659019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15871932
62 X = -4837765
06
Y = 982468
99 feet Y = 299456
55 meter
Z = 15573791
36 Z = 4746891
61
XDOT = 7441
725867 XDOT = 2268
238044
YDOT = -21198
051922 feet/sec YDOT = -6461
166226 meter/sec
ZDOT = 8875
062553 ZDOT = 2705
119066
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 19193
55313194
00016717 00000-0 10270-3 0 9001
2 25544 51
6408 235
4288 0007074 133
7216 226
4522 15
50983871 19188
Satellite: ISS
Catalog Number: 25544
Epoch time: 19193
55313194 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 235
4288 deg
Eccentricity:
0007074
Arg of perigee: 133
7216 deg
Mean anomaly: 226
4522 deg
Mean motion: 15
50983871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1918
Checksum: 313
Coasting Arc #2 (Orbit 1921)
---------------------------------------
Vector Time (GMT): 2019/193/19:17:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5311318
95 A = 6793338
48 meter
Y = -2437926
17 meter E =
0011250
Z = -3477371
23 I = 51
33191
XDOT = -118
219555 Wp = 117
01455
YDOT = -6175
715905 meter/sec RA = 233
09020 deg
ZDOT = 4516
590347 TA = 202
07195
MA = 202
12043
Ha = 228
200 n
mi
Hp = 217
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17425587
10 X = -5266771
56
Y = -7998445
43 feet Y = -2497071
49 meter
Z = -11408698
25 Z = -3503063
64
XDOT = -387
859432 XDOT = -71
091118
YDOT = -20261
535120 feet/sec YDOT = -6176
775045 meter/sec
ZDOT = 14818
209800 ZDOT = 4516
129677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18536238
97 X = 5649845
64
Y = -4622250
89 feet Y = -1408862
07 meter
Z = -11525070
60 Z = -3512841
52
XDOT = 12726
254838 XDOT = 3878
962475
YDOT = 14142
734221 feet/sec YDOT = 4310
705391 meter/sec
ZDOT = 14816
625750 ZDOT = 4516
107529
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 19193
81086534
00016717 00000-0 10270-3 0 9016
2 25544 51
6401 234
1509 0006851 133
4369 226
7353 15
50964666 19222
Satellite: ISS
Catalog Number: 25544
Epoch time: 19193
81086534 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 234
1509 deg
Eccentricity:
0006851
Arg of perigee: 133
4369 deg
Mean anomaly: 226
7353 deg
Mean motion: 15
50964666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1922
Checksum: 312
Coasting Arc #3 (Orbit 1929)
---------------------------------------
Vector Time (GMT): 2019/194/07:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4867245
06 A = 6798099
15 meter
Y = -4637274
01 meter E =
0010956
Z = -1009454
37 I = 51
36019
XDOT = 2702
819930 Wp = 78
66832
YDOT = -4103
059364 meter/sec RA = 230
50832 deg
ZDOT = 5873
225342 TA = 270
37252
MA = 270
49806
Ha = 228
235 n
mi
Hp = 217
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15968651
76 X = -4810124
65
Y = -15214153
56 feet Y = -4691383
42 meter
Z = -3311858
16 Z = -1032959
43
XDOT = 8867
519456 XDOT = 2719
971955
YDOT = -13461
480852 feet/sec YDOT = -4072
739508 meter/sec
ZDOT = 19269
112013 ZDOT = 5886
395594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22007257
80 X = -6707812
18
Y = 1197355
91 feet Y = 364954
08 meter
Z = -3418136
20 Z = -1041847
91
XDOT = -3734
956844 XDOT = -1138
414846
YDOT = -13980
940192 feet/sec YDOT = -4261
390570 meter/sec
ZDOT = 19329
205207 ZDOT = 5891
541747
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 19194
32632866
00016717 00000-0 10270-3 0 9029
2 25544 51
6420 231
5910 0007117 138
2604 221
9091 15
50956415 19309
Satellite: ISS
Catalog Number: 25544
Epoch time: 19194
32632866 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 231
5910 deg
Eccentricity:
0007117
Arg of perigee: 138
2604 deg
Mean anomaly: 221
9091 deg
Mean motion: 15
50956415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1930
Checksum: 292
Coasting Arc #4 (Orbit 1945)
---------------------------------------
Vector Time (GMT): 2019/195/07:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4928239
33 A = 6798497
42 meter
Y = 4657444
54 meter E =
0019826
Z = 318754
53 I = 51
38305
XDOT = -3079
398445 Wp = 135
67932
YDOT = 3682
221142 meter/sec RA = 225
53374 deg
ZDOT = -5980
426568 TA = 40
87526
MA = 40
72675
Ha = 228
182 n
mi
Hp = 217
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16168764
19 X = 4874243
85
Y = 15280329
85 feet Y = 4712253
61 meter
Z = 1045782
59 Z = 342563
45
XDOT = -10103
013272 XDOT = -3091
295925
YDOT = 12080
778024 feet/sec YDOT = 3647
719579 meter/sec
ZDOT = -19620
822073 ZDOT = -5995
413299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22177058
95 X = 6759567
57
Y = -1690758
52 feet Y = -515343
20 meter
Z = 1153459
60 Z = 351574
49
XDOT = 2115
375978 XDOT = 644
766598
YDOT = 13885
061309 feet/sec YDOT = 4232
166687 meter/sec
ZDOT = -19689
126862 ZDOT = -6001
245867
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 19195
35725551
00016717 00000-0 10270-3 0 9038
2 25544 51
6415 226
4764 0007218 142
9798 217
1852 15
50963911 19469
Satellite: ISS
Catalog Number: 25544
Epoch time: 19195
35725551 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 226
4764 deg
Eccentricity:
0007218
Arg of perigee: 142
9798 deg
Mean anomaly: 217
1852 deg
Mean motion: 15
50963911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1946
Checksum: 331
Coasting Arc #5 (Orbit 1961)
---------------------------------------
Vector Time (GMT): 2019/196/07:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4984978
25 A = 6798488
62 meter
Y = -4607881
20 meter E =
0013713
Z = 324792
11 I = 51
40763
XDOT = 3464
304481 Wp = 79
24626
YDOT = -3311
640025 meter/sec RA = 220
56055 deg
ZDOT = 5975
134685 TA = 284
25922
MA = 284
41148
Ha = 228
083 n
mi
Hp = 217
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16354915
53 X = -4934658
75
Y = -15117720
46 feet Y = -4663345
42 meter
Z = 1065590
91 Z = 300698
74
XDOT = 11365
828351 XDOT = 3472
055227
YDOT = -10864
960712 feet/sec YDOT = -3272
857371 meter/sec
ZDOT = 19603
460253 ZDOT = 5991
981044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22154471
85 X = -6752683
02
Y = 2329918
55 feet Y = 710159
17 meter
Z = 956595
27 Z = 291570
24
XDOT = -588
288144 XDOT = -179
310226
YDOT = -13993
465694 feet/sec YDOT = -4265
208343 meter/sec
ZDOT = 19680
180271 ZDOT = 5998
518947
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 19196
38817959
00016717 00000-0 10270-3 0 9047
2 25544 51
6419 221
3618 0007012 145
0988 215
0624 15
50969738 19627
Satellite: ISS
Catalog Number: 25544
Epoch time: 19196
38817959 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 221
3618 deg
Eccentricity:
0007012
Arg of perigee: 145
0988 deg
Mean anomaly: 215
0624 deg
Mean motion: 15
50969738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1962
Checksum: 338
Coasting Arc #6 (Orbit 1976)
---------------------------------------
Vector Time (GMT): 2019/197/07:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4947441
88 A = 6798115
30 meter
Y = 4538133
39 meter E =
0016828
Z = -1017229
34 I = 51
43091
XDOT = -3917
795698 Wp = 144
87415
YDOT = 2966
105832 meter/sec RA = 215
58964 deg
ZDOT = -5884
222130 TA = 46
17239
MA = 46
03340
Ha = 228
058 n
mi
Hp = 217
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16231764
69 X = 4901268
52
Y = 14888889
07 feet Y = 4593201
14 meter
Z = -3337366
59 Z = -993308
37
XDOT = -12853
660427 XDOT = -3922
090581
YDOT = 9731
318345 feet/sec YDOT = 2922
271191 meter/sec
ZDOT = -19305
190716 ZDOT = -5903
262960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21866679
40 X = 6664963
88
Y = -2776385
03 feet Y = -846242
16 meter
Z = -3229123
23 Z = -984236
76
XDOT = -1003
863168 XDOT = -305
977494
YDOT = 14402
936746 feet/sec YDOT = 4390
015120 meter/sec
ZDOT = -19391
851583 ZDOT = -5910
636363
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 19197
35467042
00016717 00000-0 10270-3 0 9050
2 25544 51
6404 216
5672 0007092 149
0654 211
0916 15
50970690 19774
Satellite: ISS
Catalog Number: 25544
Epoch time: 19197
35467042 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 216
5672 deg
Eccentricity:
0007092
Arg of perigee: 149
0654 deg
Mean anomaly: 211
0916 deg
Mean motion: 15
50970690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1977
Checksum: 318
Coasting Arc #7 (Orbit 1992)
---------------------------------------
Vector Time (GMT): 2019/198/07:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4895126
11 A = 6797418
33 meter
Y = -4416440
03 meter E =
0015664
Z = 1641117
79 I = 51
45655
XDOT = 4357
003569 Wp = 90
19620
YDOT = -2694
884367 meter/sec RA = 210
61912 deg
ZDOT = 5696
538044 TA = 287
79266
MA = 287
96351
Ha = 227
960 n
mi
Hp = 218
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16060125
04 X = -4853347
88
Y = -14489632
65 feet Y = -4470947
40 meter
Z = 5384244
73 Z = 1617440
43
XDOT = 14294
631131 XDOT = 4359
144666
YDOT = -8841
484145 feet/sec YDOT = -2646
150132 meter/sec
ZDOT = 18689
429278 ZDOT = 5717
707128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21406603
75 X = -6524732
82
Y = 3282830
48 feet Y = 1000606
73 meter
Z = 5277073
21 Z = 1608451
91
XDOT = 2369
220434 XDOT = 722
138388
YDOT = -15002
908731 feet/sec YDOT = -4572
886581 meter/sec
ZDOT = 18785
739819 ZDOT = 5725
893497
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 19198
38559301
00016717 00000-0 10270-3 0 9065
2 25544 51
6405 211
4524 0007019 152
4985 207
6539 15
50976157 19933
Satellite: ISS
Catalog Number: 25544
Epoch time: 19198
38559301 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 211
4524 deg
Eccentricity:
0007019
Arg of perigee: 152
4985 deg
Mean anomaly: 207
6539 deg
Mean motion: 15
50976157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1993
Checksum: 332
Coasting Arc #8 (Orbit 2007)
---------------------------------------
Vector Time (GMT): 2019/199/07:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4734854
32 A = 6796341
46 meter
Y = 4296549
70 meter E =
0012756
Z = -2291070
27 I = 51
48193
XDOT = -4836
636210 Wp = 147
27364
YDOT = 2456
844879 meter/sec RA = 205
64980 deg
ZDOT = -5412
859719 TA = 58
26638
MA = 58
14212
Ha = 227
900 n
mi
Hp = 218
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15534298
94 X = 4697585
67
Y = 14096291
67 feet Y = 4349290
07 meter
Z = -7516634
75 Z = -2268160
61
XDOT = -15868
229034 XDOT = -4837
457806
YDOT = 8060
514696 feet/sec YDOT = 2402
754295 meter/sec
ZDOT = -17758
726113 ZDOT = -5436
355461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20721166
67 X = 6315811
60
Y = -3493079
46 feet Y = -1064690
62 meter
Z = -7412916
33 Z = -2259456
90
XDOT = -3691
323295 XDOT = -1125
115340
YDOT = 15842
814785 feet/sec YDOT = 4828
889946 meter/sec
ZDOT = -17865
593065 ZDOT = -5445
432766
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 19199
35208143
00016717 00000-0 10270-3 0 9079
2 25544 51
6402 206
6572 0006980 156
0024 204
1454 15
50978290 20085
Satellite: ISS
Catalog Number: 25544
Epoch time: 19199
35208143 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 206
6572 deg
Eccentricity:
0006980
Arg of perigee: 156
0024 deg
Mean anomaly: 204
1454 deg
Mean motion: 15
50978290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2008
Checksum: 298
Coasting Arc #9 (Orbit 2023)
---------------------------------------
Vector Time (GMT): 2019/200/07:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4556623
16 A = 6795096
61 meter
Y = -4148034
13 meter E =
0016214
Z = 2856566
29 I = 51
50882
XDOT = 5280
660404 Wp = 105
35226
YDOT = -2301
526382 meter/sec RA = 200
68105 deg
ZDOT = 5053
122376 TA = 287
15138
MA = 287
32885
Ha = 227
790 n
mi
Hp = 218
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14949551
04 X = -4523775
29
Y = -13609035
85 feet Y = -4198806
12 meter
Z = 9371936
66 Z = 2834511
77
XDOT = 17325
001325 XDOT = 5281
459558
YDOT = -7550
939575 feet/sec YDOT = -2242
470392 meter/sec
ZDOT = 16578
485487 ZDOT = 5078
774972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19923493
36 X = -6072680
78
Y = 3689346
81 feet Y = 1124512
91 meter
Z = 9272068
95 Z = 2826126
61
XDOT = 4699
736804 XDOT = 1432
479778
YDOT = -16813
503698 feet/sec YDOT = -5124
755927 meter/sec
ZDOT = 16695
146875 ZDOT = 5088
680767
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 19200
38299985
00016717 00000-0 10270-3 0 9080
2 25544 51
6407 201
5423 0006898 158
9549 201
1887 15
50991093 20241
Satellite: ISS
Catalog Number: 25544
Epoch time: 19200
38299985 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 201
5423 deg
Eccentricity:
0006898
Arg of perigee: 158
9549 deg
Mean anomaly: 201
1887 deg
Mean motion: 15
50991093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2024
Checksum: 335
Coasting Arc #10 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2019/201/07:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4269510
66 A = 6793631
11 meter
Y = 4025636
68 meter E =
0009652
Z = -3422364
67 I = 51
53477
XDOT = -5727
931523 Wp = 134
09404
YDOT = 2180
826246 meter/sec RA = 195
71359 deg
ZDOT = -4595
170561 TA = 85
95393
MA = 85
84360
Ha = 227
762 n
mi
Hp = 218
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14007580
89 X = 4240801
10
Y = 13207469
41 feet Y = 4073221
11 meter
Z = -11228230
55 Z = -3401694
81
XDOT = -18792
426257 XDOT = -5729
572133
YDOT = 7154
941752 feet/sec YDOT = 2116
763720 meter/sec
ZDOT = -15076
018901 ZDOT = -4622
997908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18982819
32 X = 5785963
33
Y = -3520718
36 feet Y = -1073114
96 meter
Z = -11134623
69 Z = -3393833
30
XDOT = -5566
864300 XDOT = -1696
780239
YDOT = 17911
332905 feet/sec YDOT = 5459
374270 meter/sec
ZDOT = -15202
561112 ZDOT = -4633
740627
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 19201
34948725
00016717 00000-0 10270-3 0 9091
2 25544 51
6400 196
7475 0006921 161
8735 198
2664 15
50979302 20397
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
34948725 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 196
7475 deg
Eccentricity:
0006921
Arg of perigee: 161
8735 deg
Mean anomaly: 198
2664 deg
Mean motion: 15
50979302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 332
Coasting Arc #11 (Orbit 2044)
---------------------------------------
Vector Time (GMT): 2019/201/16:28:21
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 166493
87 A = 6786626
47 meter
Y = -4271736
74 meter E =
0009173
Z = 5267819
28 I = 51
52362
XDOT = 7527
226028 Wp = 149
79068
YDOT = 1240
541935 meter/sec RA = 193
89823 deg
ZDOT = 759
725300 TA = 292
88878
MA = 292
98559
Ha = 227
501 n
mi
Hp = 218
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 546239
73 X = 188661
67
Y = -14014884
31 feet Y = -4269751
37 meter
Z = 17282871
65 Z = 5268681
52
XDOT = 24695
623452 XDOT = 7509
104251
YDOT = 4070
019471 feet/sec YDOT = 1324
615275 meter/sec
ZDOT = 2492
537074 ZDOT = 796
245076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 637330
36 X = 194258
30
Y = 14005845
93 feet Y = 4268981
84 meter
Z = 17287079
06 Z = 5269101
70
XDOT = -23895
093872 XDOT = -7283
224612
YDOT = -2227
547310 feet/sec YDOT = -678
956420 meter/sec
ZDOT = 2658
334019 ZDOT = 810
260209
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 19201
73608089
00016717 00000-0 10270-3 0 9102
2 25544 51
6401 194
8312 0006566 163
9223 196
2138 15
51021912 20454
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
73608089 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 194
8312 deg
Eccentricity:
0006566
Arg of perigee: 163
9223 deg
Mean anomaly: 196
2138 deg
Mean motion: 15
51021912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2045
Checksum: 290
Coasting Arc #12 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2019/201/22:50:40
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4650342
71 A = 6790564
91 meter
Y = -2452469
87 meter E =
0011406
Z = 4286205
43 I = 51
54385
XDOT = 5431
032430 Wp = 108
06483
YDOT = 4093
552358 meter/sec RA = 192
54566 deg
ZDOT = -3545
885563 TA = 18
13925
MA = 18
09859
Ha = 227
388 n
mi
Hp = 218
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15257029
90 X = 4656601
73
Y = -8046161
00 feet Y = -2400431
81 meter
Z = 14062353
78 Z = 4308809
62
XDOT = 17818
347866 XDOT = 5402
077105
YDOT = 13430
289890 feet/sec YDOT = 4154
124351 meter/sec
ZDOT = -11633
482817 ZDOT = -3519
574181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10603916
21 X = 3232073
66
Y = 13497096
84 feet Y = 4113915
12 meter
Z = 14165196
80 Z = 4317551
98
XDOT = -9062
638979 XDOT = -2762
292361
YDOT = 19218
920488 feet/sec YDOT = 5857
926965 meter/sec
ZDOT = -11514
243574 ZDOT = -3509
541441
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 19201
99380935
00016717 00000-0 10270-3 0 9118
2 25544 51
6386 193
5498 0006614 166
0713 194
0621 15
50993606 20493
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
99380935 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 193
5498 deg
Eccentricity:
0006614
Arg of perigee: 166
0713 deg
Mean anomaly: 194
0621 deg
Mean motion: 15
50993606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 325
Coasting Arc #13 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2019/202/22:50:40
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5038711
39 A = 6792038
95 meter
Y = 2425052
95 meter E =
0011290
Z = -3868612
12 I = 51
58135
XDOT = -5077
588982 Wp = 138
18840
YDOT = -3973
095810 meter/sec RA = 187
57699 deg
ZDOT = 4121
546317 TA = 175
24613
MA = 175
23540
Ha = 227
494 n
mi
Hp = 218
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16531205
35 X = -5046663
30
Y = 7956210
45 feet Y = 2368662
33 meter
Z = -12692296
97 Z = -3893107
02
XDOT = -16658
756501 XDOT = -5052
803145
YDOT = -13035
091240 feet/sec YDOT = -4029
738656 meter/sec
ZDOT = 13522
133585 ZDOT = 4096
941660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10995402
26 X = -3351398
61
Y = -14589101
55 feet Y = -4446758
15 meter
Z = -12803737
06 Z = -3902579
06
XDOT = 8472
372656 XDOT = 2582
379186
YDOT = -18158
463575 feet/sec YDOT = -5534
699698 meter/sec
ZDOT = 13410
620868 ZDOT = 4087
557241
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 19202
96029459
00016717 00000-0 10270-3 0 9128
2 25544 51
6384 188
7535 0006754 168
1305 192
0006 15
50994047 20646
Satellite: ISS
Catalog Number: 25544
Epoch time: 19202
96029459 = yrday
fracday
Element set: 912
Inclination: 51
6384 deg
RA of node: 188
7535 deg
Eccentricity:
0006754
Arg of perigee: 168
1305 deg
Mean anomaly: 192
0006 deg
Mean motion: 15
50994047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 318
Coasting Arc #14 (Orbit 2064)
---------------------------------------
Vector Time (GMT): 2019/202/23:35:13
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4422737
49 A = 6790651
11 meter
Y = -2849039
80 meter E =
0011283
Z = 4282005
71 I = 51
57736
XDOT = 5764
887610 Wp = 109
83798
YDOT = 3596
832266 meter/sec RA = 187
42412 deg
ZDOT = -3557
312491 TA = 16
48008
MA = 16
44343
Ha = 227
440 n
mi
Hp = 218
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14510293
59 X = 4433468
32
Y = -9347243
44 feet Y = -2799521
92 meter
Z = 14048575
15 Z = 4303515
22
XDOT = 18913
673260 XDOT = 5741
517494
YDOT = 11800
630794 feet/sec YDOT = 3661
168847 meter/sec
ZDOT = -11670
972739 ZDOT = -3529
365836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14127115
83 X = 4305944
91
Y = 9776692
11 feet Y = 2979935
75 meter
Z = 14146481
32 Z = 4311847
51
XDOT = -2975
849761 XDOT = -907
039007
YDOT = 21022
423770 feet/sec YDOT = 6407
634765 meter/sec
ZDOT = -11544
251962 ZDOT = -3518
687998
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 19203
02472725
00016717 00000-0 10270-3 0 9135
2 25544 51
6382 188
4333 0006829 168
7249 191
4056 15
50971264 20658
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
02472725 = yrday
fracday
Element set: 913
Inclination: 51
6382 deg
RA of node: 188
4333 deg
Eccentricity:
0006829
Arg of perigee: 168
7249 deg
Mean anomaly: 191
4056 deg
Mean motion: 15
50971264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2065
Checksum: 317
Coasting Arc #15 (Orbit 2078)
---------------------------------------
Vector Time (GMT): 2019/203/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4016210
17 A = 6791236
14 meter
Y = -3532568
08 meter E =
0014102
Z = 4181321
60 I = 51
61070
XDOT = 6176
661288 Wp = 129
23131
YDOT = -2612
019105 meter/sec RA = 183
06459 deg
ZDOT = 3708
884947 TA = 282
55944
MA = 282
71713
Ha = 227
400 n
mi
Hp = 218
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13176542
54 X = -3996719
73
Y = -11589790
29 feet Y = -3577371
43 meter
Z = 13718246
72 Z = 4161859
76
XDOT = 20264
636772 XDOT = 6187
395130
YDOT = -8569
616486 feet/sec YDOT = -2542
887539 meter/sec
ZDOT = 12168
257699 ZDOT = 3738
914347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14932721
46 X = 4551493
50
Y = -9347202
74 feet Y = -2849027
39 meter
Z = 13630056
35 Z = 4154441
18
XDOT = 1680
178982 XDOT = 512
118554
YDOT = 20709
541986 feet/sec YDOT = 6312
268397 meter/sec
ZDOT = 12304
865744 ZDOT = 3750
523079
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 19203
92677731
00016717 00000-0 10270-3 0 9149
2 25544 51
6405 183
9609 0006360 171
5630 188
5629 15
50970580 20794
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
92677731 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 183
9609 deg
Eccentricity:
0006360
Arg of perigee: 171
5630 deg
Mean anomaly: 188
5629 deg
Mean motion: 15
50970580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2079
Checksum: 327
Coasting Arc #16 (Orbit 2087)
---------------------------------------
Vector Time (GMT): 2019/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 67915
80 A = 6786508
94 meter
Y = -4212554
96 meter E =
0007307
Z = 5317526
73 I = 51
61273
XDOT = 7665
909561 Wp = 153
69400
YDOT = 61
285707 meter/sec RA = 180
12803 deg
ZDOT = -55
735929 TA = 296
80008
MA = 296
87480
Ha = 227
373 n
mi
Hp = 218
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 222820
85 X = 89187
47
Y = -13820718
38 feet Y = -4211676
85 meter
Z = 17445953
85 Z = 5317908
06
XDOT = 25150
621918 XDOT = 7664
925234
YDOT = 201
068591 feet/sec YDOT = 147
005791 meter/sec
ZDOT = -182
860658 ZDOT = -18
500649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13375528
73 X = -4076861
16
Y = 3476639
98 feet Y = 1059679
87 meter
Z = 17447963
13 Z = 5318139
16
XDOT = -6065
045891 XDOT = -1848
625988
YDOT = -23370
137136 feet/sec YDOT = -7123
217799 meter/sec
ZDOT = -13
677837 ZDOT = -4
169005
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 19204
50666625
00016717 00000-0 10270-3 0 9155
2 25544 51
6384 181
0842 0006584 172
4744 187
6507 15
50986776 20881
Satellite: ISS
Catalog Number: 25544
Epoch time: 19204
50666625 = yrday
fracday
Element set: 915
Inclination: 51
6384 deg
RA of node: 181
0842 deg
Eccentricity:
0006584
Arg of perigee: 172
4744 deg
Mean anomaly: 187
6507 deg
Mean motion: 15
50986776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2088
Checksum: 340
Coasting Arc #17 (Orbit 2102)
---------------------------------------
Vector Time (GMT): 2019/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -578607
11 A = 6786768
28 meter
Y = 4241804
75 meter E =
0016973
Z = -5280023
47 I = 51
64678
XDOT = -7607
350107 Wp = 118
83463
YDOT = -8
089879 meter/sec RA = 175
16125 deg
ZDOT = 821
162894 TA = 159
06593
MA = 158
99636
Ha = 227
273 n
mi
Hp = 219
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1898317
30 X = -600350
00
Y = 13916682
25 feet Y = 4235213
11 meter
Z = -17322911
64 Z = -5282886
65
XDOT = -24958
497726 XDOT = -7610
682970
YDOT = -26
541599 feet/sec YDOT = -93
179298 meter/sec
ZDOT = 2694
103984 ZDOT = 784
201469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13867854
72 X = 4226922
12
Y = -2121240
96 feet Y = -646554
24 meter
Z = -17336200
96 Z = -5284074
05
XDOT = 6701
374925 XDOT = 2042
579077
YDOT = 23005
371407 feet/sec YDOT = 7012
037205 meter/sec
ZDOT = 2526
142046 ZDOT = 769
968096
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 19205
47314835
00016717 00000-0 10270-3 0 9166
2 25544 51
6384 176
2893 0006565 175
8386 184
2820 15
50970916 21039
Satellite: ISS
Catalog Number: 25544
Epoch time: 19205
47314835 = yrday
fracday
Element set: 916
Inclination: 51
6384 deg
RA of node: 176
2893 deg
Eccentricity:
0006565
Arg of perigee: 175
8386 deg
Mean anomaly: 184
2820 deg
Mean motion: 15
50970916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2103
Checksum: 329
Coasting Arc #18 (Orbit 2118)
---------------------------------------
Vector Time (GMT): 2019/206/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1046464
37 A = 6787238
04 meter
Y = -4302638
04 meter E =
0005405
Z = 5139621
99 I = 51
68205
XDOT = 7505
365215 Wp = 135
10804
YDOT = -41
328881 meter/sec RA = 170
19705 deg
ZDOT = -1565
482157 TA = 329
96112
MA = 329
99212
Ha = 227
109 n
mi
Hp = 219
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3433282
07 X = 1069534
67
Y = -14116266
52 feet Y = -4290807
12 meter
Z = 16862276
86 Z = 5144761
00
XDOT = 24623
901623 XDOT = 7512
873747
YDOT = -135
593443 feet/sec YDOT = 42
643482 meter/sec
ZDOT = -5136
096315 ZDOT = -1529
005907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14469354
78 X = -4410259
34
Y = 946773
80 feet Y = 288576
65 meter
Z = 16885916
58 Z = 5146827
37
XDOT = -7261
435837 XDOT = -2213
285643
YDOT = -22488
337707 feet/sec YDOT = -6854
445333 meter/sec
ZDOT = -4970
315179 ZDOT = -1514
952067
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 19206
50406025
00016717 00000-0 10270-3 0 9175
2 25544 51
6386 171
1743 0006512 180
3797 179
7350 15
50996083 21195
Satellite: ISS
Catalog Number: 25544
Epoch time: 19206
50406025 = yrday
fracday
Element set: 917
Inclination: 51
6386 deg
RA of node: 171
1743 deg
Eccentricity:
0006512
Arg of perigee: 180
3797 deg
Mean anomaly: 179
7350 deg
Mean motion: 15
50996083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2119
Checksum: 314
Coasting Arc #19 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2019/207/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1516655
63 A = 6788210
95 meter
Y = 4425336
69 meter E =
0015018
Z = -4932240
49 I = 51
71817
XDOT = -7301
180736 Wp = 131
30515
YDOT = 55
396341 meter/sec RA = 165
23564 deg
ZDOT = 2289
674130 TA = 161
13031
MA = 161
07459
Ha = 227
008 n
mi
Hp = 219
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4975904
30 X = -1542070
35
Y = 14518821
15 feet Y = 4408234
72 meter
Z = -16181891
36 Z = -4939669
12
XDOT = -23954
005040 XDOT = -7312
379459
YDOT = 181
746526 feet/sec YDOT = -26
313414 meter/sec
ZDOT = 7512
054232 ZDOT = 2254
180731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15311079
71 X = 4666817
10
Y = 152038
85 feet Y = 46341
44 meter
Z = -16215952
69 Z = -4942622
38
XDOT = 7587
831675 XDOT = 2312
771095
YDOT = 21661
080406 feet/sec YDOT = 6602
297308 meter/sec
ZDOT = 7350
717348 ZDOT = 2240
498648
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 19207
47053840
00016717 00000-0 10270-3 0 9186
2 25544 51
6390 166
3791 0006386 183
3737 176
7372 15
50979807 21348
Satellite: ISS
Catalog Number: 25544
Epoch time: 19207
47053840 = yrday
fracday
Element set: 918
Inclination: 51
6390 deg
RA of node: 166
3791 deg
Eccentricity:
0006386
Arg of perigee: 183
3737 deg
Mean anomaly: 176
7372 deg
Mean motion: 15
50979807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 338
Coasting Arc #20 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2019/208/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1929617
08 A = 6789307
07 meter
Y = -4568494
17 meter E =
0007154
Z = 4629752
73 I = 51
75346
XDOT = 7064
742971 Wp = 113
25985
YDOT = -37
106719 meter/sec RA = 160
27801 deg
ZDOT = -2980
206660 TA = 6
40775
MA = 6
39860
Ha = 226
817 n
mi
Hp = 219
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6330764
69 X = 1958071
26
Y = -14988497
93 feet Y = -4546757
24 meter
Z = 15189477
46 Z = 4639194
64
XDOT = 23178
290586 XDOT = 7079
108940
YDOT = -121
741204 feet/sec YDOT = 41
976849 meter/sec
ZDOT = -9777
580905 ZDOT = -2945
854111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16197846
36 X = -4937103
57
Y = -1023814
03 feet Y = -312058
52 meter
Z = 15232710
04 Z = 4642930
02
XDOT = -7738
524575 XDOT = -2358
702290
YDOT = -20762
915916 feet/sec YDOT = -6328
536771 meter/sec
ZDOT = -9621
408127 ZDOT = -2932
605197
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 19208
50144754
00016717 00000-0 10270-3 0 9197
2 25544 51
6383 161
2643 0006344 188
0593 172
0457 15
51002744 21493
Satellite: ISS
Catalog Number: 25544
Epoch time: 19208
50144754 = yrday
fracday
Element set: 919
Inclination: 51
6383 deg
RA of node: 161
2643 deg
Eccentricity:
0006344
Arg of perigee: 188
0593 deg
Mean anomaly: 172
0457 deg
Mean motion: 15
51002744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 304
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