[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 21st 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13747 6664 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 995 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
141/12:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
6
000/00:00:00
000 0
0 0
0 216
8
143/14:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
5
000/00:00:00
000 0
0 0
0 216
7
143/16:03:00
458 -2
1 7
1 7
1
N/A 6
7 -0
7 223
7
000/00:20:00
916 -1
1 -0
1 221
4
143/19:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 221
4
143/21:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
6
000/00:00:00
000 0
0 0
0 221
5
144/08:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
7
000/00:00:00
000 0
0 0
0 221
3
147/06:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
0
000/00:00:00
000 0
0 0
0 221
5
Coasting Arc #1 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2019/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4500860
51 A = 6793164
43 meter
Y = -5009324
62 meter E =
0012689
Z = 851116
91 I = 51
91103
XDOT = 4053
927296 Wp = 118
48361
YDOT = 2620
125413 meter/sec RA = 137
62458 deg
ZDOT = -5955
543086 TA = 52
34940
MA = 52
23434
Ha = 223
458 n
mi
Hp = 216
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14766602
73 X = 4552407
38
Y = -16434792
05 feet Y = -4958704
74 meter
Z = 2792378
33 Z = 873105
28
XDOT = 13300
286404 XDOT = 4053
256131
YDOT = 8596
211986 feet/sec YDOT = 2665
456271 meter/sec
ZDOT = -19539
183353 ZDOT = -5935
851645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5739698
45 X = -1749460
09
Y = -21322330
31 feet Y = -6499046
28 meter
Z = 2892475
45 Z = 881626
52
XDOT = 12972
015203 XDOT = 3953
870234
YDOT = -6156
774328 feet/sec YDOT = -1876
584815 meter/sec
ZDOT = -19450
129954 ZDOT = -5928
399610
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 19140
53392535
00016717 00000-0 10270-3 0 9007
2 25544 51
6365 138
5791 0001834 8
4894 351
6288 15
52697407 10955
Satellite: ISS
Catalog Number: 25544
Epoch time: 19140
53392535 = yrday
fracday
Element set: 900
Inclination: 51
6365 deg
RA of node: 138
5791 deg
Eccentricity:
0001834
Arg of perigee: 8
4894 deg
Mean anomaly: 351
6288 deg
Mean motion: 15
52697407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 326
Coasting Arc #2 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2019/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4803182
47 A = 6793299
58 meter
Y = 4779441
24 meter E =
0014039
Z = 371587
84 I = 51
93636
XDOT = -3100
514434 Wp = 45
39277
YDOT = -3594
228616 meter/sec RA = 132
68073 deg
ZDOT = 6022
266602 TA = 318
59525
MA = 318
70157
Ha = 223
393 n
mi
Hp = 216
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15758472
67 X = -4858075
55
Y = 15680581
48 feet Y = 4725421
71 meter
Z = 1219120
22 Z = 348122
88
XDOT = -10172
291451 XDOT = -3089
345421
YDOT = -11792
088634 feet/sec YDOT = -3628
839115 meter/sec
ZDOT = 19758
092525 ZDOT = 6007
231947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4926025
65 X = 1501452
62
Y = 21683942
41 feet Y = 6609265
65 meter
Z = 1112323
44 Z = 339036
19
XDOT = -13880
449430 XDOT = -4230
760986
YDOT = 2119
264428 feet/sec YDOT = 645
951798 meter/sec
ZDOT = 19690
228134 ZDOT = 6001
581535
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 19141
56370928
00016717 00000-0 10270-3 0 9014
2 25544 51
6371 133
4571 0001596 14
1894 345
9302 15
52748083 11110
Satellite: ISS
Catalog Number: 25544
Epoch time: 19141
56370928 = yrday
fracday
Element set: 901
Inclination: 51
6371 deg
RA of node: 133
4571 deg
Eccentricity:
0001596
Arg of perigee: 14
1894 deg
Mean anomaly: 345
9302 deg
Mean motion: 15
52748083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 298
Coasting Arc #3 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2019/141/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4858835
81 A = 6784172
57 meter
Y = -192444
46 meter E =
0007591
Z = 4725139
10 I = 51
90514
XDOT = 2986
712128 Wp = 103
32391
YDOT = -6484
773787 meter/sec RA = 132
64618 deg
ZDOT = 2801
631188 TA = 318
99139
MA = 319
04845
Ha = 223
616 n
mi
Hp = 216
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15941062
36 X = -4879275
04
Y = -631379
48 feet Y = -246894
30 meter
Z = 15502424
86 Z = 4701486
79
XDOT = 9798
924306 XDOT = 3045
395838
YDOT = -21275
504550 feet/sec YDOT = -6451
046545 meter/sec
ZDOT = 9191
703372 ZDOT = 2816
281303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8157917
96 X = -2486533
40
Y = 13830310
82 feet Y = 4215478
74 meter
Z = 15395199
34 Z = 4692456
76
XDOT = -13112
239620 XDOT = -3996
610636
YDOT = -18060
795389 feet/sec YDOT = -5504
930434 meter/sec
ZDOT = 9258
677333 ZDOT = 2822
044851
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 19141
56371164
00016717 00000-0 10270-3 0 9028
2 25544 51
6367 133
4566 0001864 7
9665 352
1516 15
52692196 11113
Satellite: ISS
Catalog Number: 25544
Epoch time: 19141
56371164 = yrday
fracday
Element set: 902
Inclination: 51
6367 deg
RA of node: 133
4566 deg
Eccentricity:
0001864
Arg of perigee: 7
9665 deg
Mean anomaly: 352
1516 deg
Mean motion: 15
52692196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 305
Coasting Arc #4 (Orbit 1125)
---------------------------------------
Vector Time (GMT): 2019/142/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4236752
40 A = 6782324
55 meter
Y = 1156196
32 meter E =
0014611
Z = -5181437
96 I = 51
92056
XDOT = -3614
041682 Wp = 72
02377
YDOT = 6582
701869 meter/sec RA = 127
68285 deg
ZDOT = -1485
300756 TA = 183
70065
MA = 183
71147
Ha = 223
554 n
mi
Hp = 216
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13900106
30 X = 4248677
29
Y = 3793295
02 feet Y = 1203642
04 meter
Z = -16999468
37 Z = -5160828
16
XDOT = -11857
092132 XDOT = -3680
167920
YDOT = 21596
790908 feet/sec YDOT = 6541
917594 meter/sec
ZDOT = -4873
033975 ZDOT = -1503
016228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9797042
54 X = 2986138
57
Y = -10713795
43 feet Y = -3265564
85 meter
Z = -16906108
71 Z = -5152981
94
XDOT = 12986
862056 XDOT = 3958
395555
YDOT = 19697
734897 feet/sec YDOT = 6003
869597 meter/sec
ZDOT = -4953
937591 ZDOT = -1509
960178
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 19142
52913523
00016717 00000-0 10270-3 0 9037
2 25544 51
6366 128
6541 0001924 14
3169 345
8037 15
52684051 11263
Satellite: ISS
Catalog Number: 25544
Epoch time: 19142
52913523 = yrday
fracday
Element set: 903
Inclination: 51
6366 deg
RA of node: 128
6541 deg
Eccentricity:
0001924
Arg of perigee: 14
3169 deg
Mean anomaly: 345
8037 deg
Mean motion: 15
52684051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1126
Checksum: 294
Coasting Arc #5 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2019/143/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3572820
65 A = 6781561
56 meter
Y = -2170695
54 meter E =
0003313
Z = 5337197
83 I = 51
93770
XDOT = 4082
480168 Wp = 61
22622
YDOT = -6491
225209 meter/sec RA = 122
71873 deg
ZDOT = 94
347157 TA = 27
88734
MA = 27
86959
Ha = 223
684 n
mi
Hp = 216
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11721852
52 X = -3574206
98
Y = -7121704
54 feet Y = -2210657
76 meter
Z = 17510491
57 Z = 5319838
71
XDOT = 13393
963807 XDOT = 4154
305194
YDOT = -21296
670634 feet/sec YDOT = -6445
170472 meter/sec
ZDOT = 309
537916 ZDOT = 114
351987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11630753
22 X = -3545053
58
Y = 7455894
83 feet Y = 2272556
75 meter
Z = 17431954
25 Z = 5313259
66
XDOT = -12609
944259 XDOT = -3843
511010
YDOT = -20596
298667 feet/sec YDOT = -6277
751834 meter/sec
ZDOT = 400
837192 ZDOT = 122
175176
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 19143
55891967
00016717 00000-0 10270-3 0 9049
2 25544 51
6367 123
5318 0001914 14
6109 345
5098 15
52683577 11420
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
55891967 = yrday
fracday
Element set: 904
Inclination: 51
6367 deg
RA of node: 123
5318 deg
Eccentricity:
0001914
Arg of perigee: 14
6109 deg
Mean anomaly: 345
5098 deg
Mean motion: 15
52683577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 323
Coasting Arc #6 (Orbit 1142)
---------------------------------------
Vector Time (GMT): 2019/143/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 248497
31 A = 6787855
97 meter
Y = -5718390
77 meter E =
0012603
Z = 3640692
14 I = 51
96183
XDOT = 5716
766923 Wp = 77
29918
YDOT = -2572
697332 meter/sec RA = 122
33159 deg
ZDOT = -4415
561294 TA = 59
74527
MA = 59
62058
Ha = 223
525 n
mi
Hp = 216
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 815279
88 X = 294739
01
Y = -18761124
58 feet Y = -5715353
81 meter
Z = 11944528
03 Z = 3642010
83
XDOT = 18755
796993 XDOT = 5766
559073
YDOT = -8440
608044 feet/sec YDOT = -2508
489473 meter/sec
ZDOT = -14486
749652 ZDOT = -4387
670701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18760412
11 X = -5718173
61
Y = -732428
65 feet Y = -223244
25 meter
Z = 11951013
03 Z = 3642668
77
XDOT = -8497
721992 XDOT = -2590
105663
YDOT = -17483
304135 feet/sec YDOT = -5328
911100 meter/sec
ZDOT = -14360
029835 ZDOT = -4376
937094
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 19143
62328100
00016717 00000-0 10270-3 0 9052
2 25544 51
6382 123
2119 0002013 12
4497 347
6704 15
52703955 11431
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
62328100 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 123
2119 deg
Eccentricity:
0002013
Arg of perigee: 12
4497 deg
Mean anomaly: 347
6704 deg
Mean motion: 15
52703955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1143
Checksum: 277
Coasting Arc #7 (Orbit 1143)
---------------------------------------
Vector Time (GMT): 2019/143/16:13:00
916
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1824494
96 A = 6787897
58 meter
Y = 4332542
99 meter E =
0006751
Z = -4902836
89 I = 51
94968
XDOT = -5309
323068 Wp = 118
82482
YDOT = 4964
296937 meter/sec RA = 121
87951 deg
ZDOT = 2410
436080 TA = 174
73920
MA = 174
73210
Ha = 223
699 n
mi
Hp = 221
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5985875
86 X = 1799726
94
Y = 14214379
89 feet Y = 4352807
90 meter
Z = -16085422
87 Z = -4894033
76
XDOT = -17419
038936 XDOT = -5376
149237
YDOT = 16287
063443 feet/sec YDOT = 4904
550416 meter/sec
ZDOT = 7908
254857 ZDOT = 2384
483636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8522052
88 X = 2597521
72
Y = -12904436
41 feet Y = -3933272
22 meter
Z = -16045880
15 Z = -4890784
27
XDOT = 22269
886252 XDOT = 6787
861330
YDOT = 5017
751921 feet/sec YDOT = 1529
410785 meter/sec
ZDOT = 7790
112326 ZDOT = 2374
426237
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 19143
68764930
00016717 00000-0 10270-3 0 9064
2 25544 51
6393 122
8904 0005473 273
0040 87
0485 15
51153202 11447
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
68764930 = yrday
fracday
Element set: 906
Inclination: 51
6393 deg
RA of node: 122
8904 deg
Eccentricity:
0005473
Arg of perigee: 273
0040 deg
Mean anomaly: 87
0485 deg
Mean motion: 15
51153202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1144
Checksum: 295
Coasting Arc #8 (Orbit 1146)
---------------------------------------
Vector Time (GMT): 2019/143/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4369236
85 A = 6786926
08 meter
Y = -582957
98 meter E =
0002871
Z = 5162541
98 I = 51
94903
XDOT = 2780
025364 Wp = 212
60110
YDOT = -6966
374956 meter/sec RA = 121
14982 deg
ZDOT = 1564
233289 TA = 222
36181
MA = 222
38398
Ha = 223
860 n
mi
Hp = 221
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14334766
56 X = -4387470
12
Y = -1912591
81 feet Y = -631920
44 meter
Z = 16937473
68 Z = 5141273
46
XDOT = 9120
818124 XDOT = 2850
120548
YDOT = -22855
560878 feet/sec YDOT = -6934
895035 meter/sec
ZDOT = 5131
998979 ZDOT = 1577
907017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14412551
43 X = 4392945
68
Y = 2162986
65 feet Y = 659278
33 meter
Z = 16841063
03 Z = 5133156
01
XDOT = -9325
458144 XDOT = -2842
399642
YDOT = 21642
375649 feet/sec YDOT = 6596
596098 meter/sec
ZDOT = 5194
632485 ZDOT = 1583
323982
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 19143
88092548
00016717 00000-0 10270-3 0 9076
2 25544 51
6395 121
9318 0005561 274
1616 85
8899 15
51130054 11475
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
88092548 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 121
9318 deg
Eccentricity:
0005561
Arg of perigee: 274
1616 deg
Mean anomaly: 85
8899 deg
Mean motion: 15
51130054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1147
Checksum: 325
Coasting Arc #9 (Orbit 1146)
---------------------------------------
Vector Time (GMT): 2019/143/21:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2557753
43 A = 6797337
67 meter
Y = 6168582
92 meter E =
0007408
Z = -1242321
68 I = 51
98307
XDOT = -4852
634720 Wp = 358
63984
YDOT = -830
696371 meter/sec RA = 120
88349 deg
ZDOT = 5872
614707 TA = 347
93618
MA = 347
95391
Ha = 223
602 n
mi
Hp = 221
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8391579
50 X = -2620507
67
Y = 20238132
93 feet Y = 6139629
60 meter
Z = -4075858
53 Z = -1254897
96
XDOT = -15920
717585 XDOT = -4871
510929
YDOT = -2725
381795 feet/sec YDOT = -885
068203 meter/sec
ZDOT = 19267
108618 ZDOT = 5848
996429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2253066
30 X = 686734
61
Y = -21781909
47 feet Y = -6639126
01 meter
Z = -4133444
80 Z = -1259873
97
XDOT = 14572
319930 XDOT = 4441
643115
YDOT = -2124
605977 feet/sec YDOT = -647
579902 meter/sec
ZDOT = 19160
062019 ZDOT = 5839
986903
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 19143
88092423
00016717 00000-0 10270-3 0 9089
2 25544 51
6377 121
9301 0005735 273
0604 86
9891 15
51146889 11472
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
88092423 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 121
9301 deg
Eccentricity:
0005735
Arg of perigee: 273
0604 deg
Mean anomaly: 86
9891 deg
Mean motion: 15
51146889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1147
Checksum: 325
Coasting Arc #10 (Orbit 1154)
---------------------------------------
Vector Time (GMT): 2019/144/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 473009
66 A = 6793771
55 meter
Y = -6005303
65 meter E =
0007607
Z = 3133964
14 I = 51
98066
XDOT = 5504
543490 Wp = 95
25027
YDOT = -2123
741273 meter/sec RA = 118
50448 deg
ZDOT = -4890
804191 TA = 48
88700
MA = 48
82135
Ha = 223
733 n
mi
Hp = 221
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1551868
96 X = 524904
45
Y = -19702439
78 feet Y = -5999724
33 meter
Z = 10282034
58 Z = 3136387
18
XDOT = 18059
525886 XDOT = 5551
639495
YDOT = -6967
655095 feet/sec YDOT = -2061
921706 meter/sec
ZDOT = -16045
945507 ZDOT = -4863
951013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1796563
59 X = -547592
58
Y = -19675609
64 feet Y = -5997125
82 meter
Z = 10293561
61 Z = 3137477
58
XDOT = 15328
978853 XDOT = 4672
272754
YDOT = -9746
817584 feet/sec YDOT = -2970
829999 meter/sec
ZDOT = -15923
957411 ZDOT = -4853
622219
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 19144
39632949
00016717 00000-0 10270-3 0 9090
2 25544 51
6389 119
3729 0005308 274
4884 85
5661 15
51174559 11555
Satellite: ISS
Catalog Number: 25544
Epoch time: 19144
39632949 = yrday
fracday
Element set: 909
Inclination: 51
6389 deg
RA of node: 119
3729 deg
Eccentricity:
0005308
Arg of perigee: 274
4884 deg
Mean anomaly: 85
5661 deg
Mean motion: 15
51174559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1155
Checksum: 349
Coasting Arc #11 (Orbit 1169)
---------------------------------------
Vector Time (GMT): 2019/145/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -588627
99 A = 6795186
99 meter
Y = 6278896
08 meter E =
0004245
Z = -2522955
07 I = 52
00192
XDOT = -5257
143379 Wp = 344
50632
YDOT = 1646
229126 meter/sec RA = 113
56805 deg
ZDOT = 5325
434171 TA = 347
37164
MA = 347
38227
Ha = 223
804 n
mi
Hp = 221
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1931194
18 X = -646541
53
Y = 20600052
74 feet Y = 6271990
07 meter
Z = -8277411
64 Z = -2525954
41
XDOT = -17247
845732 XDOT = -5301
029271
YDOT = 5401
014192 feet/sec YDOT = 1587
194129 meter/sec
ZDOT = 17471
896886 ZDOT = 5299
790507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1912278
92 X = 582862
62
Y = 20596115
77 feet Y = 6277696
09 meter
Z = -8291588
03 Z = -2527276
03
XDOT = -14586
490594 XDOT = -4445
962333
YDOT = 8338
732450 feet/sec YDOT = 2541
645651 meter/sec
ZDOT = 17355
424078 ZDOT = 5289
933259
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 19145
36271214
00016717 00000-0 10270-3 0 9104
2 25544 51
6403 114
5770 0005230 277
8952 82
1606 15
51188979 11702
Satellite: ISS
Catalog Number: 25544
Epoch time: 19145
36271214 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 114
5770 deg
Eccentricity:
0005230
Arg of perigee: 277
8952 deg
Mean anomaly: 82
1606 deg
Mean motion: 15
51188979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1170
Checksum: 300
Coasting Arc #12 (Orbit 1185)
---------------------------------------
Vector Time (GMT): 2019/146/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 666822
62 A = 6796505
42 meter
Y = -6500669
76 meter E =
0008846
Z = 1850978
84 I = 52
01630
XDOT = 5040
549843 Wp = 120
20379
YDOT = -1100
910912 meter/sec RA = 108
63452 deg
ZDOT = -5666
463367 TA = 39
56759
MA = 39
50305
Ha = 223
961 n
mi
Hp = 221
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2187738
25 X = 730474
37
Y = -21327656
70 feet Y = -6492857
15 meter
Z = 6072765
22 Z = 1854372
02
XDOT = 16537
237019 XDOT = 5080
010479
YDOT = -3611
912441 feet/sec YDOT = -1044
322796 meter/sec
ZDOT = -18590
759077 ZDOT = -5641
882494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2145389
23 X = -653914
64
Y = -21327398
43 feet Y = -6500591
04 meter
Z = 6088759
94 Z = 1855854
03
XDOT = 14052
413107 XDOT = 4283
175515
YDOT = -6703
979585 feet/sec YDOT = -2043
372978 meter/sec
ZDOT = -18479
146751 ZDOT = -5632
443930
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 19146
39351949
00016717 00000-0 10270-3 0 9113
2 25544 51
6383 109
4616 0005230 282
9344 77
1222 15
51164269 11864
Satellite: ISS
Catalog Number: 25544
Epoch time: 19146
39351949 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 109
4616 deg
Eccentricity:
0005230
Arg of perigee: 282
9344 deg
Mean anomaly: 77
1222 deg
Mean motion: 15
51164269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1186
Checksum: 311
Coasting Arc #13 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2019/147/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4379436
64 A = 6788073
51 meter
Y = -1773007
45 meter E =
0007678
Z = -4880897
46 I = 51
99803
XDOT = 170
432050 Wp = 50
37179
YDOT = 7243
823209 meter/sec RA = 104
13938 deg
ZDOT = -2476
256033 TA = 195
38695
MA = 195
41030
Ha = 224
012 n
mi
Hp = 221
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14368230
43 X = 4422646
17
Y = -5816953
58 feet Y = -1723791
52 meter
Z = -16013443
13 Z = -4859518
94
XDOT = 559
160268 XDOT = 101
445194
YDOT = 23765
824176 feet/sec YDOT = 7245
343573 meter/sec
ZDOT = -8124
199583 ZDOT = -2475
595099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15551782
31 X = 4740183
25
Y = -1235796
70 feet Y = -376670
83 meter
Z = -15916288
16 Z = -4851284
63
XDOT = -6592
643531 XDOT = -2009
437748
YDOT = 21732
555488 feet/sec YDOT = 6624
082913 meter/sec
ZDOT = -8121
883167 ZDOT = -2475
549989
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 19147
29547563
00016717 00000-0 10270-3 0 9123
2 25544 51
6395 104
9845 0005387 284
7476 75
3078 15
51149502 12009
Satellite: ISS
Catalog Number: 25544
Epoch time: 19147
29547563 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 104
9845 deg
Eccentricity:
0005387
Arg of perigee: 284
7476 deg
Mean anomaly: 75
3078 deg
Mean motion: 15
51149502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 326
Coasting Arc #14 (Orbit 1215)
---------------------------------------
Vector Time (GMT): 2019/148/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4263514
54 A = 6786942
71 meter
Y = 1251006
02 meter E =
0001340
Z = 5131228
54 I = 52
00127
XDOT = -139
493795 Wp = 213
83379
YDOT = -7469
554743 meter/sec RA = 99
19658 deg
ZDOT = 1704
322065 TA = 219
76711
MA = 219
77693
Ha = 224
355 n
mi
Hp = 221
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13987908
59 X = -4302111
56
Y = 4104350
47 feet Y = 1203112
22 meter
Z = 16834739
31 Z = 5110424
22
XDOT = -457
656807 XDOT = -64
235429
YDOT = -24506
413200 feet/sec YDOT = -7470
693993 meter/sec
ZDOT = 5591
607824 ZDOT = 1703
826681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14686019
64 X = -4476298
79
Y = -34401
36 feet Y = -10485
54 meter
Z = 16740232
10 Z = 5102422
75
XDOT = 6428
156244 XDOT = 1959
302023
YDOT = -22581
507392 feet/sec YDOT = -6882
843453 meter/sec
ZDOT = 5590
078249 ZDOT = 1703
855850
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 19148
32627907
00016717 00000-0 10270-3 0 9130
2 25544 51
6392 99
8685 0005328 290
4687 69
5892 15
51168711 12162
Satellite: ISS
Catalog Number: 25544
Epoch time: 19148
32627907 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 99
8685 deg
Eccentricity:
0005328
Arg of perigee: 290
4687 deg
Mean anomaly: 69
5892 deg
Mean motion: 15
51168711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1216
Checksum: 346
Coasting Arc #15 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2019/149/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4198735
35 A = 6786293
82 meter
Y = -704242
01 meter E =
0010163
Z = -5293321
02 I = 52
00443
XDOT = 138
736936 Wp = 67
24988
YDOT = 7602
182680 meter/sec RA = 94
25352 deg
ZDOT = -898
926529 TA = 194
16777
MA = 194
19630
Ha = 224
387 n
mi
Hp = 221
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13775378
44 X = 4232010
55
Y = -2310505
28 feet Y = -657102
36 meter
Z = -17366538
77 Z = -5272844
19
XDOT = 455
173674 XDOT = 58
083371
YDOT = 24941
544225 feet/sec YDOT = 7603
283238 meter/sec
ZDOT = -2949
234020 ZDOT = -898
447916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14007156
29 X = 4269381
24
Y = 1455904
29 feet Y = 443759
63 meter
Z = -17273565
65 Z = -5264982
81
XDOT = -6051
648327 XDOT = -1844
542410
YDOT = 23152
483844 feet/sec YDOT = 7056
877076 meter/sec
ZDOT = -2947
810046 ZDOT = -898
492502
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 19149
29265615
00016717 00000-0 10270-3 0 9142
2 25544 51
6405 95
0728 0005419 293
9485 66
1098 15
51155316 12313
Satellite: ISS
Catalog Number: 25544
Epoch time: 19149
29265615 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 95
0728 deg
Eccentricity:
0005419
Arg of perigee: 293
9485 deg
Mean anomaly: 66
1098 deg
Mean motion: 15
51155316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 319
Coasting Arc #16 (Orbit 1246)
---------------------------------------
Vector Time (GMT): 2019/150/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4176904
02 A = 6785988
70 meter
Y = 131730
06 meter E =
0003274
Z = 5348451
66 I = 52
00320
XDOT = -150
020235 Wp = 317
32036
YDOT = -7660
619016 meter/sec RA = 89
30972 deg
ZDOT = 73
885548 TA = 131
99249
MA = 131
96460
Ha = 224
669 n
mi
Hp = 221
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13703753
35 X = -4204046
74
Y = 432185
22 feet Y = 84868
78 meter
Z = 17547413
59 Z = 5328095
68
XDOT = -492
192372 XDOT = -64
704756
YDOT = -25133
264488 feet/sec YDOT = -7661
819625 meter/sec
ZDOT = 242
406655 ZDOT = 73
363381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13494931
08 X = -4113254
99
Y = -3016567
85 feet Y = -919449
88 meter
Z = 17455042
75 Z = 5320297
03
XDOT = 5550
556893 XDOT = 1691
809741
YDOT = -23482
748544 feet/sec YDOT = -7157
541756 meter/sec
ZDOT = 240
809823 ZDOT = 73
398834
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 19150
32345772
00016717 00000-0 10270-3 0 9152
2 25544 51
6387 89
9568 0005293 299
0226 61
0394 15
51166870 12473
Satellite: ISS
Catalog Number: 25544
Epoch time: 19150
32345772 = yrday
fracday
Element set: 915
Inclination: 51
6387 deg
RA of node: 89
9568 deg
Eccentricity:
0005293
Arg of perigee: 299
0226 deg
Mean anomaly: 61
0394 deg
Mean motion: 15
51166870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1247
Checksum: 329
Coasting Arc #17 (Orbit 1261)
---------------------------------------
Vector Time (GMT): 2019/151/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4211991
59 A = 6786219
11 meter
Y = 428357
53 meter E =
0009894
Z = -5311903
35 I = 52
00345
XDOT = 164
697210 Wp = 81
75307
YDOT = 7618
327696 meter/sec RA = 84
36652 deg
ZDOT = 747
510590 TA = 195
34837
MA = 195
37840
Ha = 224
736 n
mi
Hp = 221
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13818870
06 X = 4232691
18
Y = 1405372
47 feet Y = 475575
23 meter
Z = -17427504
42 Z = -5291392
46
XDOT = 540
345176 XDOT = 75
863612
YDOT = 24994
513438 feet/sec YDOT = 7619
672682 meter/sec
ZDOT = 2452
462565 ZDOT = 748
095628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13229832
73 X = 4032453
02
Y = 4597961
09 feet Y = 1401458
54 meter
Z = -17334486
77 Z = -5283551
57
XDOT = -4952
136484 XDOT = -1509
411200
YDOT = 23469
905875 feet/sec YDOT = 7153
627311 meter/sec
ZDOT = 2454
328103 ZDOT = 748
079206
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 19151
28983241
00016717 00000-0 10270-3 0 9168
2 25544 51
6399 85
1614 0005506 301
5440 58
5173 15
51151988 12627
Satellite: ISS
Catalog Number: 25544
Epoch time: 19151
28983241 = yrday
fracday
Element set: 916
Inclination: 51
6399 deg
RA of node: 85
1614 deg
Eccentricity:
0005506
Arg of perigee: 301
5440 deg
Mean anomaly: 58
5173 deg
Mean motion: 15
51151988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1262
Checksum: 309
Coasting Arc #18 (Orbit 1277)
---------------------------------------
Vector Time (GMT): 2019/152/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4290751
01 A = 6786773
97 meter
Y = -992947
27 meter E =
0006067
Z = 5165441
08 I = 52
00080
XDOT = -156
170244 Wp = 356
27462
YDOT = -7498
935754 meter/sec RA = 79
42248 deg
ZDOT = -1565
452856 TA = 108
78499
MA = 108
71916
Ha = 224
940 n
mi
Hp = 220
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14077267
09 X = -4304419
93
Y = -3257701
03 feet Y = -1041006
50 meter
Z = 16946985
17 Z = 5144564
57
XDOT = -512
369568 XDOT = -64
699178
YDOT = -24602
807592 feet/sec YDOT = -7500
170525 meter/sec
ZDOT = -5136
000184 ZDOT = -1565
990213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13157600
93 X = -4010436
76
Y = -6233586
07 feet Y = -1899997
03 meter
Z = 16852368
19 Z = 5136601
82
XDOT = 4372
438041 XDOT = 1332
719115
YDOT = -23170
263318 feet/sec YDOT = -7062
296259 meter/sec
ZDOT = -5137
639938 ZDOT = -1565
952653
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 19152
32062961
00016717 00000-0 10270-3 0 9172
2 25544 51
6395 80
0450 0005453 306
9611 53
1040 15
51176843 12783
Satellite: ISS
Catalog Number: 25544
Epoch time: 19152
32062961 = yrday
fracday
Element set: 917
Inclination: 51
6395 deg
RA of node: 80
0450 deg
Eccentricity:
0005453
Arg of perigee: 306
9611 deg
Mean anomaly: 53
1040 deg
Mean motion: 15
51176843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1278
Checksum: 289
Coasting Arc #19 (Orbit 1292)
---------------------------------------
Vector Time (GMT): 2019/153/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4419110
77 A = 6787855
94 meter
Y = 1508046
03 meter E =
0007293
Z = -4932914
23 I = 51
99658
XDOT = 124
240695 Wp = 88
81715
YDOT = 7289
684857 meter/sec RA = 74
48059 deg
ZDOT = 2342
968092 TA = 204
01313
MA = 204
04715
Ha = 225
141 n
mi
Hp = 220
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14498394
90 X = 4425880
66
Y = 4947657
58 feet Y = 1557502
17 meter
Z = -16184101
80 Z = -4911430
85
XDOT = 407
613829 XDOT = 31
335111
YDOT = 23916
288902 feet/sec YDOT = 7290
554403 meter/sec
ZDOT = 7686
903190 ZDOT = 2343
346998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13335436
41 X = 4064641
02
Y = 7745276
05 feet Y = 2360760
14 meter
Z = -16086788
25 Z = -4903253
06
XDOT = -3829
752963 XDOT = -1167
308703
YDOT = 22539
876482 feet/sec YDOT = 6870
154352 meter/sec
ZDOT = 7687
824696 ZDOT = 2343
248967
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 19153
28700116
00016717 00000-0 10270-3 0 9180
2 25544 51
6391 75
2500 0005546 310
9446 49
1224 15
51149356 12930
Satellite: ISS
Catalog Number: 25544
Epoch time: 19153
28700116 = yrday
fracday
Element set: 918
Inclination: 51
6391 deg
RA of node: 75
2500 deg
Eccentricity:
0005546
Arg of perigee: 310
9446 deg
Mean anomaly: 49
1224 deg
Mean motion: 15
51149356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1293
Checksum: 294
Coasting Arc #20 (Orbit 1308)
---------------------------------------
Vector Time (GMT): 2019/154/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4579957
13 A = 6789102
19 meter
Y = -2005540
15 meter E =
0008314
Z = 4593228
56 I = 51
99012
XDOT = -38
292148 Wp = 27
76727
YDOT = -7011
183352 meter/sec RA = 69
53844 deg
ZDOT = -3090
069844 TA = 93
06808
MA = 92
97294
Ha = 225
191 n
mi
Hp = 220
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15026106
06 X = -4579501
87
Y = -6579856
13 feet Y = -2056754
63 meter
Z = 15069647
49 Z = 4570981
31
XDOT = -125
630407 XDOT = 55
121795
YDOT = -23002
570051 feet/sec YDOT = -7011
088749 meter/sec
ZDOT = -10138
024421 ZDOT = -3090
030105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13682117
97 X = -4170309
56
Y = -9214313
67 feet Y = -2808522
81 meter
Z = 14968925
05 Z = 4562528
35
XDOT = 3445
253022 XDOT = 1050
113121
YDOT = -21634
176094 feet/sec YDOT = -6594
096874 meter/sec
ZDOT = -10137
056789 ZDOT = -3089
774909
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 19154
31779590
00016717 00000-0 10270-3 0 9198
2 25544 51
6381 70
1342 0005660 314
0909 45
9775 15
51186402 13099
Satellite: ISS
Catalog Number: 25544
Epoch time: 19154
31779590 = yrday
fracday
Element set: 919
Inclination: 51
6381 deg
RA of node: 70
1342 deg
Eccentricity:
0005660
Arg of perigee: 314
0909 deg
Mean anomaly: 45
9775 deg
Mean motion: 15
51186402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1309
Checksum: 311
Coasting Arc #21 (Orbit 1323)
---------------------------------------
Vector Time (GMT): 2019/155/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 945394
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4770745
97 A = 6790705
22 meter
Y = 2424441
84 meter E =
0003922
Z = -4182238
44 I = 51
98325
XDOT = -91
893369 Wp = 63
76432
YDOT = 6669
824077 meter/sec RA = 64
59780 deg
ZDOT = 3766
086696 TA = 244
82771
MA = 244
86840
Ha = 225
462 n
mi
Hp = 220
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15652053
70 X = 4763595
78
Y = 7954205
52 feet Y = 2477752
43 meter
Z = -13721254
72 Z = -4159080
65
XDOT = -301
487431 XDOT = -184
764148
YDOT = 21882
624924 feet/sec YDOT = 6668
276518 meter/sec
ZDOT = 12355
927480 ZDOT = 3765
415927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14220981
93 X = 4334555
29
Y = 10434795
67 feet Y = 3180525
72 meter
Z = -13616450
12 Z = -4150294
00
XDOT = -3218
115338 XDOT = -980
881555
YDOT = 20485
108572 feet/sec YDOT = 6243
861093 meter/sec
ZDOT = 12352
117519 ZDOT = 3764
925420
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 19155
28416503
00016717 00000-0 10270-3 0 9209
2 25544 51
6388 65
3388 0005614 319
1622 40
9108 15
51156773 13249
Satellite: ISS
Catalog Number: 25544
Epoch time: 19155
28416503 = yrday
fracday
Element set: 920
Inclination: 51
6388 deg
RA of node: 65
3388 deg
Eccentricity:
0005614
Arg of perigee: 319
1622 deg
Mean anomaly: 40
9108 deg
Mean motion: 15
51156773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1324
Checksum: 302
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