[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 10th 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 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 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
065/14:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
3
065/21:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
4
066/14:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
4
000/00:00:00
000 0
0 0
0 215
3
066/21:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
5
066/23:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
4
000/00:00:00
000 0
0 0
0 215
4
073/19:14:09
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
4
074/01:07:11
000 0
0 0
0 0
0
N/A 0
0 0
0 224
4
000/00:00:00
000 0
0 0
0 215
5
074/14:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
6
Coasting Arc #1 (Orbit 3929)
---------------------------------------
Vector Time (GMT): 2019/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926995
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2560798
52 A = 6781285
31 meter
Y = -3349231
44 meter E =
0006184
Z = 5306144
97 I = 51
80569
XDOT = 6458
383757 Wp = 97
03385
YDOT = -4106
823447 meter/sec RA = 150
63233 deg
ZDOT = 523
397818 TA = 347
97855
MA = 347
99331
Ha = 224
460 n
mi
Hp = 215
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8401569
95 X = -2548929
96
Y = -10988292
14 feet Y = -3377801
10 meter
Z = 17408612
09 Z = 5293735
03
XDOT = 21188
923088 XDOT = 6501
285096
YDOT = -13473
830207 feet/sec YDOT = -4034
361347 meter/sec
ZDOT = 1717
184441 ZDOT = 554
874295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4944324
37 X = -1507030
07
Y = -12993260
84 feet Y = -3960345
90 meter
Z = 17352738
87 Z = 5289114
81
XDOT = 23237
812782 XDOT = 7082
885336
YDOT = -6353
302753 feet/sec YDOT = -1936
486679 meter/sec
ZDOT = 1859
828892 ZDOT = 566
875846
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 19065
54926169
00016717 00000-0 10270-3 0 9000
2 25544 51
6414 151
5343 0003551 83
4893 276
6664 15
52811870 39304
Satellite: ISS
Catalog Number: 25544
Epoch time: 19065
54926169 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 151
5343 deg
Eccentricity:
0003551
Arg of perigee: 83
4893 deg
Mean anomaly: 276
6664 deg
Mean motion: 15
52811870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3930
Checksum: 318
Coasting Arc #2 (Orbit 3930)
---------------------------------------
Vector Time (GMT): 2019/065/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 926995
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1935522
27 A = 6785607
67 meter
Y = 4950316
90 meter E =
0011667
Z = -4229498
66 I = 51
82175
XDOT = -6696
045880 Wp = 100
98849
YDOT = 517
384469 meter/sec RA = 150
08768 deg
ZDOT = 3676
272512 TA = 206
63028
MA = 206
69026
Ha = 224
510 n
mi
Hp = 215
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6350138
67 X = -1970190
09
Y = 16241197
17 feet Y = 4928478
19 meter
Z = -13876307
94 Z = -4238985
31
XDOT = -21968
654461 XDOT = -6719
190715
YDOT = 1697
455606 feet/sec YDOT = 442
375626 meter/sec
ZDOT = 12061
261523 ZDOT = 3643
689976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -127553
35 X = -38878
26
Y = 17403501
83 feet Y = 5304587
36 meter
Z = -13919573
37 Z = -4242685
96
XDOT = -18764
119299 XDOT = -5719
303562
YDOT = 9374
527594 feet/sec YDOT = 2857
356011 meter/sec
ZDOT = 11913
878081 ZDOT = 3631
350039
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 19065
61362107
00016717 00000-0 10270-3 0 9015
2 25544 51
6400 151
2155 0003908 80
6328 279
5265 15
52793378 39317
Satellite: ISS
Catalog Number: 25544
Epoch time: 19065
61362107 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 151
2155 deg
Eccentricity:
0003908
Arg of perigee: 80
6328 deg
Mean anomaly: 279
5265 deg
Mean motion: 15
52793378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3931
Checksum: 306
Coasting Arc #3 (Orbit 3935)
---------------------------------------
Vector Time (GMT): 2019/065/21:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 926995
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3063233
46 A = 6781502
10 meter
Y = -2979731
83 meter E =
0006761
Z = 5260024
60 I = 51
81512
XDOT = 6085
998594 Wp = 100
10003
YDOT = -4572
462141 meter/sec RA = 148
72580 deg
ZDOT = 951
815818 TA = 340
80530
MA = 340
83075
Ha = 224
515 n
mi
Hp = 215
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10049978
55 X = -3055235
42
Y = -9776023
07 feet Y = -3013941
69 meter
Z = 17257298
57 Z = 5245164
62
XDOT = 19967
186988 XDOT = 6132
053529
YDOT = -15001
516211 feet/sec YDOT = -4504
146625 meter/sec
ZDOT = 3122
755307 ZDOT = 981
491192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2859866
53 X = -871687
32
Y = 13809461
29 feet Y = 4209123
80 meter
Z = 17190316
81 Z = 5239608
56
XDOT = -22312
287562 XDOT = -6800
785249
YDOT = -8684
509843 feet/sec YDOT = -2647
038600 meter/sec
ZDOT = 3257
294610 ZDOT = 992
823397
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 19065
93540989
00016717 00000-0 10270-3 0 9027
2 25544 51
6390 149
6155 0003699 78
1559 282
0007 15
52813376 39360
Satellite: ISS
Catalog Number: 25544
Epoch time: 19065
93540989 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 149
6155 deg
Eccentricity:
0003699
Arg of perigee: 78
1559 deg
Mean anomaly: 282
0007 deg
Mean motion: 15
52813376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 341
Coasting Arc #4 (Orbit 3946)
---------------------------------------
Vector Time (GMT): 2019/066/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 926995
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2866010
25 A = 6788444
09 meter
Y = -5173440
41 meter E =
0016313
Z = 3318282
76 I = 51
85881
XDOT = 6039
894917 Wp = 89
91777
YDOT = 306
819185 meter/sec RA = 145
12686 deg
ZDOT = -4718
298216 TA = 51
60944
MA = 51
46304
Ha = 224
418 n
mi
Hp = 215
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9402920
78 X = 2907529
99
Y = -16973229
69 feet Y = -5141158
11 meter
Z = 10886754
45 Z = 3332306
04
XDOT = 19815
928204 XDOT = 6058
933609
YDOT = 1006
624622 feet/sec YDOT = 374
467372 meter/sec
ZDOT = -15479
981023 ZDOT = -4688
912921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2414399
09 X = 735908
84
Y = -19216731
45 feet Y = -5857259
74 meter
Z = 10950560
59 Z = 3337730
87
XDOT = 17485
063505 XDOT = 5329
447356
YDOT = -6585
858232 feet/sec YDOT = -2007
369589 meter/sec
ZDOT = -15347
105673 ZDOT = -4677
797809
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 19066
64334557
00016717 00000-0 10270-3 0 9039
2 25544 51
6392 146
0932 0003781 83
7724 276
3858 15
52811078 39473
Satellite: ISS
Catalog Number: 25544
Epoch time: 19066
64334557 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 146
0932 deg
Eccentricity:
0003781
Arg of perigee: 83
7724 deg
Mean anomaly: 276
3858 deg
Mean motion: 15
52811078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3947
Checksum: 336
Coasting Arc #5 (Orbit 3950)
---------------------------------------
Vector Time (GMT): 2019/066/21:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 926995
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2033087
49 A = 6781359
46 meter
Y = 3697305
27 meter E =
0018473
Z = -5324765
09 I = 51
84184
XDOT = -6376
731139 Wp = 91
45656
YDOT = 4202
961229 meter/sec RA = 143
75288 deg
ZDOT = 484
618091 TA = 183
15705
MA = 183
16872
Ha = 224
495 n
mi
Hp = 215
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6670234
53 X = 2017456
46
Y = 12130266
65 feet Y = 3719952
61 meter
Z = -17469701
74 Z = -5314927
69
XDOT = -20921
033919 XDOT = -6425
609885
YDOT = 13789
242876 feet/sec YDOT = 4131
378925 meter/sec
ZDOT = 1589
954368 ZDOT = 453
523516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6440671
18 X = 1963116
58
Y = -12316496
21 feet Y = -3754068
05 meter
Z = -17425485
71 Z = -5311288
04
XDOT = 22095
162551 XDOT = 6734
605546
YDOT = 9508
793711 feet/sec YDOT = 2898
280323 meter/sec
ZDOT = 1449
009451 ZDOT = 441
658081
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 19066
90077801
00016717 00000-0 10270-3 0 9045
2 25544 51
6387 144
8126 0003775 81
8303 278
3277 15
52778490 39515
Satellite: ISS
Catalog Number: 25544
Epoch time: 19066
90077801 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 144
8126 deg
Eccentricity:
0003775
Arg of perigee: 81
8303 deg
Mean anomaly: 278
3277 deg
Mean motion: 15
52778490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 334
Coasting Arc #6 (Orbit 3952)
---------------------------------------
Vector Time (GMT): 2019/066/23:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 926995
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1281227
30 A = 6781649
79 meter
Y = -4146555
30 meter E =
0007598
Z = 5205518
02 I = 51
84759
XDOT = 6611
996927 Wp = 68
31945
YDOT = -3669
400228 meter/sec RA = 143
26221 deg
ZDOT = -1291
281182 TA = 34
06483
MA = 34
01609
Ha = 224
434 n
mi
Hp = 215
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4203501
65 X = -1260049
30
Y = -13604184
06 feet Y = -4160763
81 meter
Z = 17078471
19 Z = 5199346
35
XDOT = 21692
903303 XDOT = 6658
810026
YDOT = -12038
714658 feet/sec YDOT = -3595
198670 meter/sec
ZDOT = -4236
486818 ZDOT = -1259
048862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -965706
08 X = -294347
21
Y = 14239127
30 feet Y = 4340086
00 meter
Z = 17050867
84 Z = 5197104
52
XDOT = -23582
765074 XDOT = -7188
026794
YDOT = 3315
473955 feet/sec YDOT = 1010
556461 meter/sec
ZDOT = -4090
434508 ZDOT = -1246
764438
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 19067
02949219
00016717 00000-0 10270-3 0 9051
2 25544 51
6402 144
1737 0003669 81
9043 278
2525 15
52827655 39533
Satellite: ISS
Catalog Number: 25544
Epoch time: 19067
02949219 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 144
1737 deg
Eccentricity:
0003669
Arg of perigee: 81
9043 deg
Mean anomaly: 278
2525 deg
Mean motion: 15
52827655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3953
Checksum: 328
Coasting Arc #7 (Orbit 3967)
---------------------------------------
Vector Time (GMT): 2019/067/23:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 283260
34 A = 6783478
04 meter
Y = 4795697
78 meter E =
0014788
Z = -4803055
87 I = 51
88010
XDOT = -6514
535940 Wp = 103
06930
YDOT = 3027
935056 meter/sec RA = 138
29398 deg
ZDOT = 2642
692236 TA = 192
94177
MA = 192
97977
Ha = 224
433 n
mi
Hp = 215
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 929331
82 X = 252942
79
Y = 15733916
61 feet Y = 4798695
27 meter
Z = -15758057
33 Z = -4801754
16
XDOT = -21373
149408 XDOT = -6560
747604
YDOT = 9934
170132 feet/sec YDOT = 2954
826909 meter/sec
ZDOT = 8670
250117 ZDOT = 2610
934752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4541600
17 X = 1384279
73
Y = -15098600
19 feet Y = -4602053
34 meter
Z = -15752533
15 Z = -4801372
10
XDOT = 22451
865803 XDOT = 6843
328697
YDOT = -2129
934238 feet/sec YDOT = -649
203956 meter/sec
ZDOT = 8526
378806 ZDOT = 2598
840260
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 19067
99485671
00016717 00000-0 10270-3 0 9065
2 25544 51
6409 139
3709 0003660 84
9941 275
1628 15
52794793 39688
Satellite: ISS
Catalog Number: 25544
Epoch time: 19067
99485671 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 139
3709 deg
Eccentricity:
0003660
Arg of perigee: 84
9941 deg
Mean anomaly: 275
1628 deg
Mean motion: 15
52794793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3968
Checksum: 367
Coasting Arc #8 (Orbit 3983)
---------------------------------------
Vector Time (GMT): 2019/068/23:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 650935
23 A = 6786028
79 meter
Y = -5365191
43 meter E =
0014285
Z = 4093488
41 I = 51
91264
XDOT = 6247
098527 Wp = 79
84901
YDOT = -2203
971445 meter/sec RA = 133
33205 deg
ZDOT = -3868
162496 TA = 50
05508
MA = 49
92967
Ha = 224
449 n
mi
Hp = 215
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2135614
28 X = 690998
17
Y = -17602334
08 feet Y = -5357687
72 meter
Z = 13430080
10 Z = 4096748
34
XDOT = 20495
730076 XDOT = 6290
068941
YDOT = -7230
877443 feet/sec YDOT = -2133
872221 meter/sec
ZDOT = -12690
821836 ZDOT = -3837
711987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7808953
60 X = -2380169
06
Y = 15906470
19 feet Y = 4848292
11 meter
Z = 13445241
33 Z = 4098109
56
XDOT = -20653
800850 XDOT = -6295
278499
YDOT = 509
533906 feet/sec YDOT = 155
305935 meter/sec
ZDOT = -12552
911014 ZDOT = -3826
127277
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 19069
02457465
00016717 00000-0 10270-3 0 9072
2 25544 51
6406 134
2480 0003784 87
0284 273
1301 15
52815633 39847
Satellite: ISS
Catalog Number: 25544
Epoch time: 19069
02457465 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 134
2480 deg
Eccentricity:
0003784
Arg of perigee: 87
0284 deg
Mean anomaly: 273
1301 deg
Mean motion: 15
52815633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3984
Checksum: 313
Coasting Arc #9 (Orbit 3998)
---------------------------------------
Vector Time (GMT): 2019/069/23:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1432044
02 A = 6788872
89 meter
Y = 5825010
37 meter E =
0008200
Z = -3185342
03 I = 51
94349
XDOT = -5804
296994 Wp = 84
63146
YDOT = 1217
255586 meter/sec RA = 128
37706 deg
ZDOT = 4846
901840 TA = 238
81094
MA = 238
89134
Ha = 224
430 n
mi
Hp = 215
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4698307
14 X = -1481601
92
Y = 19110926
40 feet Y = 5808718
82 meter
Z = -10450597
20 Z = -3192419
33
XDOT = -19042
969140 XDOT = -5841
020794
YDOT = 3993
620688 feet/sec YDOT = 1152
143060 meter/sec
ZDOT = 15901
908923 ZDOT = 4818
617505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10462394
78 X = 3188937
93
Y = -16648123
30 feet Y = -5074347
98 meter
Z = -10483075
21 Z = -3195241
32
XDOT = 18211
617317 XDOT = 5550
900958
YDOT = 1535
998555 feet/sec YDOT = 468
172359 meter/sec
ZDOT = 15773
861123 ZDOT = 4807
872870
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 19069
98993365
00016717 00000-0 10270-3 0 9082
2 25544 51
6401 129
4451 0003681 90
5642 269
5931 15
52799686 39992
Satellite: ISS
Catalog Number: 25544
Epoch time: 19069
98993365 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 129
4451 deg
Eccentricity:
0003681
Arg of perigee: 90
5642 deg
Mean anomaly: 269
5931 deg
Mean motion: 15
52799686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3999
Checksum: 368
Coasting Arc #10 (Orbit 4014)
---------------------------------------
Vector Time (GMT): 2019/070/23:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2112203
72 A = 6791435
75 meter
Y = -6111466
02 meter E =
0017586
Z = 2051069
88 I = 51
97176
XDOT = 5266
298951 Wp = 107
84914
YDOT = -62
532164 meter/sec RA = 123
42949 deg
ZDOT = -5575
666404 TA = 49
57911
MA = 49
42583
Ha = 224
489 n
mi
Hp = 215
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6929802
23 X = 2170423
94
Y = -20050741
55 feet Y = -6087520
17 meter
Z = 6729231
87 Z = 2061472
11
XDOT = 17277
883696 XDOT = 5293
690253
YDOT = -205
158020 feet/sec YDOT = -3
488073 meter/sec
ZDOT = -18292
868779 ZDOT = -5550
018207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12609252
70 X = -3843300
22
Y = 17041678
57 feet Y = 5194303
63 meter
Z = 6776790
89 Z = 2065565
86
XDOT = -15409
790887 XDOT = -4696
904262
YDOT = -4129
666516 feet/sec YDOT = -1258
722354 meter/sec
ZDOT = -18176
828560 ZDOT = -5540
297345
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 19071
01964917
00016717 00000-0 10270-3 0 9091
2 25544 51
6402 124
3223 0003774 95
6956 264
4626 15
52784919 40159
Satellite: ISS
Catalog Number: 25544
Epoch time: 19071
01964917 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 124
3223 deg
Eccentricity:
0003774
Arg of perigee: 95
6956 deg
Mean anomaly: 264
4626 deg
Mean motion: 15
52784919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4015
Checksum: 324
Coasting Arc #11 (Orbit 4029)
---------------------------------------
Vector Time (GMT): 2019/071/23:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2617759
86 A = 6792805
01 meter
Y = 6206864
82 meter E =
0012398
Z = -843922
85 I = 51
99455
XDOT = -4669
523964 Wp = 53
85905
YDOT = -1167
628209 meter/sec RA = 118
48587 deg
ZDOT = 5964
763575 TA = 297
06399
MA = 297
19046
Ha = 224
357 n
mi
Hp = 215
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8588450
98 X = -2682872
92
Y = 20363729
72 feet Y = 6177227
07 meter
Z = -2768775
75 Z = -856797
51
XDOT = -15319
960511 XDOT = -4685
093621
YDOT = -3830
801210 feet/sec YDOT = -1219
932720 meter/sec
ZDOT = 19569
434301 ZDOT = 5942
043092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14018742
71 X = 4272912
78
Y = -17075975
10 feet Y = -5204757
21 meter
Z = -2827547
51 Z = -861836
48
XDOT = 12472
808357 XDOT = 3801
711987
YDOT = 7052
482908 feet/sec YDOT = 2149
596790 meter/sec
ZDOT = 19466
733694 ZDOT = 5933
460430
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 19071
98500248
00016717 00000-0 10270-3 0 9102
2 25544 51
6407 119
5188 0003603 97
5080 262
6481 15
52824014 40307
Satellite: ISS
Catalog Number: 25544
Epoch time: 19071
98500248 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 119
5188 deg
Eccentricity:
0003603
Arg of perigee: 97
5080 deg
Mean anomaly: 262
6481 deg
Mean motion: 15
52824014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4030
Checksum: 293
Coasting Arc #12 (Orbit 4045)
---------------------------------------
Vector Time (GMT): 2019/072/23:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3032923
74 A = 6793194
18 meter
Y = -6054676
46 meter E =
0014299
Z = -463008
90 I = 52
00944
XDOT = 4048
663262 Wp = 129
74551
YDOT = 2478
327317 meter/sec RA = 113
54624 deg
ZDOT = -6019
854323 TA = 55
21983
MA = 55
08533
Ha = 224
475 n
mi
Hp = 215
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9950537
20 X = 3102652
46
Y = -19864424
07 feet Y = -6020370
33 meter
Z = -1519058
08 Z = -448106
47
XDOT = 13283
015950 XDOT = 4049
889991
YDOT = 8130
995134 feet/sec YDOT = 2523
608824 meter/sec
ZDOT = -19750
178225 ZDOT = -6000
184674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14928619
28 X = -4550243
16
Y = 16460458
51 feet Y = 5017147
75 meter
Z = -1451104
27 Z = -442296
58
XDOT = -9538
969949 XDOT = -2907
478040
YDOT = -10344
614588 feet/sec YDOT = -3153
038526 meter/sec
ZDOT = -19661
388761 ZDOT = -5992
791294
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 19073
01471315
00016717 00000-0 10270-3 0 9111
2 25544 51
6399 114
3956 0003653 102
8742 257
2818 15
52771072 40469
Satellite: ISS
Catalog Number: 25544
Epoch time: 19073
01471315 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 114
3956 deg
Eccentricity:
0003653
Arg of perigee: 102
8742 deg
Mean anomaly: 257
2818 deg
Mean motion: 15
52771072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4046
Checksum: 304
Coasting Arc #13 (Orbit 4058)
---------------------------------------
Vector Time (GMT): 2019/073/19:14:09
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4229457
63 A = 6781364
48 meter
Y = -420784
13 meter E =
0006942
Z = 5278928
00 I = 51
97983
XDOT = 1866
315145 Wp = 112
86252
YDOT = -7385
794202 meter/sec RA = 109
49883 deg
ZDOT = 902
994026 TA = 328
52349
MA = 328
56501
Ha = 224
459 n
mi
Hp = 215
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13876173
31 X = -4250079
89
Y = -1380525
36 feet Y = -468195
94 meter
Z = 17319317
60 Z = 5258332
96
XDOT = 6123
081183 XDOT = 1944
380265
YDOT = -24231
608273 feet/sec YDOT = -7364
487230 meter/sec
ZDOT = 2962
578827 ZDOT = 912
249773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1014439
55 X = 309201
17
Y = 14022953
13 feet Y = 4274196
11 meter
Z = 17226157
32 Z = 5250532
75
XDOT = -23892
997030 XDOT = -7282
585495
YDOT = -1977
564407 feet/sec YDOT = -602
761631 meter/sec
ZDOT = 3005
113142 ZDOT = 915
958486
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 19073
85135086
00016717 00000-0 10270-3 0 9126
2 25544 51
6388 110
2331 0003568 104
8766 255
2781 15
52844253 40595
Satellite: ISS
Catalog Number: 25544
Epoch time: 19073
85135086 = yrday
fracday
Element set: 912
Inclination: 51
6388 deg
RA of node: 110
2331 deg
Eccentricity:
0003568
Arg of perigee: 104
8766 deg
Mean anomaly: 255
2781 deg
Mean motion: 15
52844253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4059
Checksum: 315
Coasting Arc #14 (Orbit 4062)
---------------------------------------
Vector Time (GMT): 2019/074/01:07:11
000
Vector Time (MET): N/A
Weight (LBS) : 916818
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2947187
31 A = 6792600
47 meter
Y = 5999208
62 meter E =
0016215
Z = 1173169
88 I = 52
01829
XDOT = -3839
245919 Wp = 67
32787
YDOT = -3050
280787 meter/sec RA = 108
28659 deg
ZDOT = 5894
740690 TA = 305
34166
MA = 305
49312
Ha = 224
353 n
mi
Hp = 215
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9669249
71 X = -3019751
68
Y = 19682442
99 feet Y = 5965845
43 meter
Z = 3848982
55 Z = 1158677
15
XDOT = -12595
951179 XDOT = -3833
484634
YDOT = -10007
482897 feet/sec YDOT = -3093
181439 meter/sec
ZDOT = 19339
700425 ZDOT = 5876
105347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6763623
15 X = 2061552
34
Y = -20872252
79 feet Y = -6361862
65 meter
Z = 3782867
14 Z = 1153017
90
XDOT = 12509
721232 XDOT = 3812
963032
YDOT = 7579
091301 feet/sec YDOT = 2310
107029 meter/sec
ZDOT = 19255
639141 ZDOT = 5869
118810
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 19074
10877724
00016717 00000-0 10270-3 0 9138
2 25544 51
6374 108
9505 0003554 107
1243 253
0298 15
52811868 40638
Satellite: ISS
Catalog Number: 25544
Epoch time: 19074
10877724 = yrday
fracday
Element set: 913
Inclination: 51
6374 deg
RA of node: 108
9505 deg
Eccentricity:
0003554
Arg of perigee: 107
1243 deg
Mean anomaly: 253
0298 deg
Mean motion: 15
52811868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4063
Checksum: 310
Coasting Arc #15 (Orbit 4070)
---------------------------------------
Vector Time (GMT): 2019/074/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 916818
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3868987
20 A = 6781342
21 meter
Y = 1652618
09 meter E =
0018489
Z = -5334463
02 I = 51
98600
XDOT = -2410
611537 Wp = 96
75135
YDOT = 7246
055174 meter/sec RA = 105
49206 deg
ZDOT = 495
818327 TA = 177
96954
MA = 177
96203
Ha = 224
473 n
mi
Hp = 215
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12693527
54 X = 3876131
21
Y = 5421975
36 feet Y = 1695923
52 meter
Z = -17501519
10 Z = -5315651
84
XDOT = -7908
830501 XDOT = -2493
868203
YDOT = 23773
146896 feet/sec YDOT = 7218
632535 meter/sec
ZDOT = 1626
700548 ZDOT = 483
906067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13771683
14 X = 4197609
02
Y = -1957458
76 feet Y = -596633
43 meter
Z = -17416536
05 Z = -5308560
19
XDOT = 5323
972132 XDOT = 1622
746706
YDOT = 23449
826196 feet/sec YDOT = 7147
507025 meter/sec
ZDOT = 1572
141622 ZDOT = 479
188766
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 19074
62363177
00016717 00000-0 10270-3 0 9148
2 25544 51
6373 106
3900 0003840 107
8572 252
2999 15
52788623 40718
Satellite: ISS
Catalog Number: 25544
Epoch time: 19074
62363177 = yrday
fracday
Element set: 914
Inclination: 51
6373 deg
RA of node: 106
3900 deg
Eccentricity:
0003840
Arg of perigee: 107
8572 deg
Mean anomaly: 252
2999 deg
Mean motion: 15
52788623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4071
Checksum: 320
Coasting Arc #16 (Orbit 4086)
---------------------------------------
Vector Time (GMT): 2019/075/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 916818
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3495490
97 A = 6782369
25 meter
Y = -2842590
62 meter E =
0008403
Z = 5063179
25 I = 51
99751
XDOT = 2804
725070 Wp = 77
13581
YDOT = -6877
506922 meter/sec RA = 100
53091 deg
ZDOT = -1920
392529 TA = 31
41163
MA = 31
36148
Ha = 224
519 n
mi
Hp = 215
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11468146
22 X = -3488038
30
Y = -9326084
71 feet Y = -2881637
72 meter
Z = 16611480
47 Z = 5046217
94
XDOT = 9201
853903 XDOT = 2890
750921
YDOT = -22563
999089 feet/sec YDOT = -6845
661621 meter/sec
ZDOT = -6300
500423 ZDOT = -1906
559136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14761444
29 X = -4499288
22
Y = -1769154
20 feet Y = -539238
20 meter
Z = 16534974
22 Z = 5039860
14
XDOT = -4251
854873 XDOT = -1295
965365
YDOT = -22956
954454 feet/sec YDOT = -6997
279717 meter/sec
ZDOT = -6237
263438 ZDOT = -1901
117896
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 19075
65333625
00016717 00000-0 10270-3 0 9158
2 25544 51
6373 101
2668 0003738 110
3996 249
7557 15
52815282 40878
Satellite: ISS
Catalog Number: 25544
Epoch time: 19075
65333625 = yrday
fracday
Element set: 915
Inclination: 51
6373 deg
RA of node: 101
2668 deg
Eccentricity:
0003738
Arg of perigee: 110
3996 deg
Mean anomaly: 249
7557 deg
Mean motion: 15
52815282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4087
Checksum: 330
Coasting Arc #17 (Orbit 4101)
---------------------------------------
Vector Time (GMT): 2019/076/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 916818
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3167080
54 A = 6784643
83 meter
Y = 3952639
78 meter E =
0013312
Z = -4527461
64 I = 52
00941
XDOT = -3132
929732 Wp = 111
02540
YDOT = 6197
016107 meter/sec RA = 95
57422 deg
ZDOT = 3221
637212 TA = 191
23659
MA = 191
26635
Ha = 224
419 n
mi
Hp = 215
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10390684
18 X = 3144637
14
Y = 12967978
27 feet Y = 3987930
50 meter
Z = -14853876
76 Z = -4512132
18
XDOT = -10278
640854 XDOT = -3217
642340
YDOT = 20331
417674 feet/sec YDOT = 6161
508052 meter/sec
ZDOT = 10569
675892 ZDOT = 3206
212712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15859599
35 X = 4834005
88
Y = 5162702
94 feet Y = 1573591
86 meter
Z = -14784858
46 Z = -4506424
86
XDOT = 2769
368037 XDOT = 844
103378
YDOT = 21532
132904 feet/sec YDOT = 6562
994109 meter/sec
ZDOT = 10499
286491 ZDOT = 3200
182522
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 19076
61868338
00016717 00000-0 10270-3 0 9160
2 25544 51
6368 96
4644 0003749 112
3961 247
7589 15
52791695 41029
Satellite: ISS
Catalog Number: 25544
Epoch time: 19076
61868338 = yrday
fracday
Element set: 916
Inclination: 51
6368 deg
RA of node: 96
4644 deg
Eccentricity:
0003749
Arg of perigee: 112
3961 deg
Mean anomaly: 247
7589 deg
Mean motion: 15
52791695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4102
Checksum: 353
Coasting Arc #18 (Orbit 4117)
---------------------------------------
Vector Time (GMT): 2019/077/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 916818
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2833754
12 A = 6787381
08 meter
Y = -4925761
36 meter E =
0015012
Z = 3698037
33 I = 52
02072
XDOT = 3462
296908 Wp = 92
35180
YDOT = -5276
990384 meter/sec RA = 90
62212 deg
ZDOT = -4361
191422 TA = 43
86223
MA = 43
74312
Ha = 224
377 n
mi
Hp = 215
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9297093
57 X = -2796424
94
Y = -16160634
38 feet Y = -4957241
32 meter
Z = 12132668
42 Z = 3684363
38
XDOT = 11359
241824 XDOT = 3542
232257
YDOT = -17312
960576 feet/sec YDOT = -5237
826009 meter/sec
ZDOT = -14308
370806 ZDOT = -4344
178558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16808768
02 X = -5123312
49
Y = -8158078
90 feet Y = -2486582
45 meter
Z = 12071236
95 Z = 3679313
02
XDOT = -773
939741 XDOT = -235
896833
YDOT = -19533
639866 feet/sec YDOT = -5953
853431 meter/sec
ZDOT = -14230
867669 ZDOT = -4337
568465
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 19077
64838529
00016717 00000-0 10270-3 0 9174
2 25544 51
6365 91
3408 0003634 116
5283 243
6242 15
52825870 41185
Satellite: ISS
Catalog Number: 25544
Epoch time: 19077
64838529 = yrday
fracday
Element set: 917
Inclination: 51
6365 deg
RA of node: 91
3408 deg
Eccentricity:
0003634
Arg of perigee: 116
5283 deg
Mean anomaly: 243
6242 deg
Mean motion: 15
52825870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4118
Checksum: 323
Coasting Arc #19 (Orbit 4132)
---------------------------------------
Vector Time (GMT): 2019/078/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 916818
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2536078
13 A = 6790128
85 meter
Y = 5697753
66 meter E =
0007368
Z = -2689825
32 I = 52
02981
XDOT = -3775
038456 Wp = 81
83135
YDOT = 4139
820514 meter/sec RA = 85
67600 deg
ZDOT = 5223
179269 TA = 248
01217
MA = 248
09048
Ha = 224
343 n
mi
Hp = 215
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8320466
30 X = 2485241
21
Y = 18693417
51 feet Y = 5725829
29 meter
Z = -8824886
23 Z = -2677630
35
XDOT = -12385
296772 XDOT = -3846
421435
YDOT = 13582
088300 feet/sec YDOT = 4097
206878 meter/sec
ZDOT = 17136
414923 ZDOT = 5204
667987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17579884
49 X = 5358348
79
Y = 10515863
98 feet Y = 3205235
34 meter
Z = -8770228
09 Z = -2673165
52
XDOT = -1691
518167 XDOT = -515
574737
YDOT = 17012
955733 feet/sec YDOT = 5185
548907 meter/sec
ZDOT = 17052
229667 ZDOT = 5197
519602
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 19078
61372846
00016717 00000-0 10270-3 0 9188
2 25544 51
6373 86
5378 0003714 118
9267 241
2258 15
52812705 41334
Satellite: ISS
Catalog Number: 25544
Epoch time: 19078
61372846 = yrday
fracday
Element set: 918
Inclination: 51
6373 deg
RA of node: 86
5378 deg
Eccentricity:
0003714
Arg of perigee: 118
9267 deg
Mean anomaly: 241
2258 deg
Mean motion: 15
52812705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4133
Checksum: 326
Coasting Arc #20 (Orbit 4148)
---------------------------------------
Vector Time (GMT): 2019/079/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 916818
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2191411
46 A = 6792209
08 meter
Y = -6246512
87 meter E =
0017457
Z = 1482722
41 I = 52
03343
XDOT = 4129
107491 Wp = 119
14056
YDOT = -2837
392000 meter/sec RA = 80
73420 deg
ZDOT = -5807
795597 TA = 44
76381
MA = 44
62308
Ha = 224
277 n
mi
Hp = 215
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7189670
14 X = -2128600
47
Y = -20493808
63 feet Y = -6270667
37 meter
Z = 4864574
84 Z = 1472230
89
XDOT = 13546
940588 XDOT = 4188
739847
YDOT = -9309
028872 feet/sec YDOT = -2790
884799 meter/sec
ZDOT = -19054
447497 ZDOT = -5787
592959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17878582
48 X = -5449391
94
Y = -12348999
73 feet Y = -3763975
12 meter
Z = 4817689
45 Z = 1468431
74
XDOT = 4702
273111 XDOT = 1433
252844
YDOT = -14261
409598 feet/sec YDOT = -4346
877645 meter/sec
ZDOT = -18962
726920 ZDOT = -5779
839165
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 19079
64342546
00016717 00000-0 10270-3 0 9197
2 25544 51
6375 81
4137 0003600 121
7454 238
4050 15
52826295 41491
Satellite: ISS
Catalog Number: 25544
Epoch time: 19079
64342546 = yrday
fracday
Element set: 919
Inclination: 51
6375 deg
RA of node: 81
4137 deg
Eccentricity:
0003600
Arg of perigee: 121
7454 deg
Mean anomaly: 238
4050 deg
Mean motion: 15
52826295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4149
Checksum: 312
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