[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 14th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
238/15:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
0
Coasting Arc #1 (Orbit 742)
---------------------------------------
Vector Time (GMT): 2018/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -424311
70 A = 6790111
37 meter
Y = 6765017
82 meter E =
0018095
Z = 211493
96 I = 52
04111
XDOT = -4699
244584 Wp = 48
56159
YDOT = -493
727047 meter/sec RA = 92
19418 deg
ZDOT = 6043
477368 TA = 313
70528
MA = 313
85504
Ha = 223
286 n
mi
Hp = 213
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1392098
76 X = -500955
77
Y = 22194940
35 feet Y = 6759844
34 meter
Z = 693877
83 Z = 209246
48
XDOT = -15417
469107 XDOT = -4722
729745
YDOT = -1619
839393 feet/sec YDOT = -546
408375 meter/sec
ZDOT = 19827
681653 ZDOT = 6020
593525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15053793
86 X = 4588396
37
Y = -16369228
92 feet Y = -4989340
98 meter
Z = 682947
68 Z = 208162
45
XDOT = 9871
145840 XDOT = 3008
725252
YDOT = 9945
547107 feet/sec YDOT = 3031
402758 meter/sec
ZDOT = 19724
984365 ZDOT = 6012
175234
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 18225
56391584
00016717 00000-0 10270-3 0 9006
2 25544 51
6410 92
7675 0005610 51
0745 309
0907 15
53854872 7439
Satellite: ISS
Catalog Number: 25544
Epoch time: 18225
56391584 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 92
7675 deg
Eccentricity:
0005610
Arg of perigee: 51
0745 deg
Mean anomaly: 309
0907 deg
Mean motion: 15
53854872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 743
Checksum: 309
Coasting Arc #2 (Orbit 757)
---------------------------------------
Vector Time (GMT): 2018/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1121636
98 A = 6788840
92 meter
Y = -6440686
25 meter E =
0009410
Z = -1831744
86 I = 52
03592
XDOT = 4550
623470 Wp = 105
03946
YDOT = 2399
702413 meter/sec RA = 87
25081 deg
ZDOT = -5677
840649 TA = 94
97197
MA = 94
86453
Ha = 223
370 n
mi
Hp = 213
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3679911
34 X = 1202472
65
Y = -21130860
41 feet Y = -6427691
43 meter
Z = -6009661
61 Z = -1826099
82
XDOT = 14929
867029 XDOT = 4551
030627
YDOT = 7873
039412 feet/sec YDOT = 2450
592674 meter/sec
ZDOT = -18628
086120 ZDOT = -5655
734776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15945069
95 X = -4860057
32
Y = 14357000
01 feet Y = 4376013
60 meter
Z = -5983505
40 Z = -1823772
45
XDOT = -5964
453217 XDOT = -1817
965340
YDOT = -14309
935045 feet/sec YDOT = -4361
668202 meter/sec
ZDOT = -18529
121384 ZDOT = -5647
676198
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 18226
52863097
00016717 00000-0 10270-3 0 9017
2 25544 51
6403 87
9598 0005574 54
5024 305
6648 15
53809585 7589
Satellite: ISS
Catalog Number: 25544
Epoch time: 18226
52863097 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 87
9598 deg
Eccentricity:
0005574
Arg of perigee: 54
5024 deg
Mean anomaly: 305
6648 deg
Mean motion: 15
53809585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 758
Checksum: 340
Coasting Arc #3 (Orbit 773)
---------------------------------------
Vector Time (GMT): 2018/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1779195
27 A = 6785795
40 meter
Y = 5683169
19 meter E =
0017939
Z = 3233771
97 I = 52
02233
XDOT = -4345
073958 Wp = 77
68961
YDOT = -4108
289110 meter/sec RA = 82
30157 deg
ZDOT = 4810
772608 TA = 319
56761
MA = 319
70080
Ha = 223
453 n
mi
Hp = 213
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5837254
83 X = -1858321
57
Y = 18645568
19 feet Y = 5662830
70 meter
Z = 10609488
09 Z = 3224936
95
XDOT = -14255
491989 XDOT = -4322
178912
YDOT = -13478
638812 feet/sec YDOT = -4156
750526 meter/sec
ZDOT = 15783
374697 ZDOT = 4789
721778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15945779
25 X = 4860273
51
Y = -11327771
83 feet Y = -3452704
86 meter
Z = 10569091
93 Z = 3221459
22
XDOT = 2520
953835 XDOT = 768
386729
YDOT = 18244
662937 feet/sec YDOT = 5560
973263 meter/sec
ZDOT = 15689
369807 ZDOT = 4782
119917
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 18227
55765815
00016717 00000-0 10270-3 0 9021
2 25544 51
6393 82
8318 0005683 57
3161 302
8539 15
53830083 7748
Satellite: ISS
Catalog Number: 25544
Epoch time: 18227
55765815 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 82
8318 deg
Eccentricity:
0005683
Arg of perigee: 57
3161 deg
Mean anomaly: 302
8539 deg
Mean motion: 15
53830083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 774
Checksum: 323
Coasting Arc #4 (Orbit 788)
---------------------------------------
Vector Time (GMT): 2018/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2482400
29 A = 6782125
71 meter
Y = -4559003
32 meter E =
0014261
Z = -4379414
25 I = 52
00452
XDOT = 4016
711081 Wp = 65
91370
YDOT = 5516
894534 meter/sec RA = 77
34301 deg
ZDOT = -3469
557323 TA = 168
99588
MA = 168
96465
Ha = 223
363 n
mi
Hp = 213
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8144357
92 X = 2554468
53
Y = -14957359
98 feet Y = -4530840
58 meter
Z = -14368157
00 Z = -4367180
54
XDOT = 13178
185961 XDOT = 3971
574240
YDOT = 18100
047685 feet/sec YDOT = 5561
559694 meter/sec
ZDOT = -11383
062082 ZDOT = -3450
155511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15464053
90 X = -4713443
63
Y = 7246288
52 feet Y = 2208668
74 meter
Z = -14312632
84 Z = -4362490
49
XDOT = 462
291250 XDOT = 140
906373
YDOT = -21305
168890 feet/sec YDOT = -6493
815478 meter/sec
ZDOT = -11296
653584 ZDOT = -3443
220012
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 18228
52236915
00016717 00000-0 10270-3 0 9034
2 25544 51
6392 78
0242 0005544 60
6071 299
5634 15
53839547 7891
Satellite: ISS
Catalog Number: 25544
Epoch time: 18228
52236915 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 78
0242 deg
Eccentricity:
0005544
Arg of perigee: 60
6071 deg
Mean anomaly: 299
5634 deg
Mean motion: 15
53839547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 789
Checksum: 329
Coasting Arc #5 (Orbit 804)
---------------------------------------
Vector Time (GMT): 2018/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3165527
05 A = 6779342
08 meter
Y = 3162533
76 meter E =
0009657
Z = 5084744
71 I = 51
98704
XDOT = -3580
012872 Wp = 93
64890
YDOT = -6536
470092 meter/sec RA = 72
37536 deg
ZDOT = 1833
120002 TA = 338
68360
MA = 338
72380
Ha = 223
623 n
mi
Hp = 213
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10385587
43 X = -3225354
94
Y = 10375766
94 feet Y = 3126800
23 meter
Z = 16682233
30 Z = 5069222
42
XDOT = -11745
449054 XDOT = -3515
558449
YDOT = -21445
111852 feet/sec YDOT = -6576
143853 meter/sec
ZDOT = 6014
173235 ZDOT = 1815
886336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14552525
36 X = 4435609
73
Y = -2464849
93 feet Y = -751286
26 meter
Z = 16612115
88 Z = 5063372
92
XDOT = -2851
423754 XDOT = -869
113960
YDOT = 23262
158245 feet/sec YDOT = 7090
305833 meter/sec
ZDOT = 5937
647722 ZDOT = 1809
795026
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 18229
55139361
00016717 00000-0 10270-3 0 9046
2 25544 51
6395 72
8960 0005713 64
8309 295
3436 15
53814412 8058
Satellite: ISS
Catalog Number: 25544
Epoch time: 18229
55139361 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 72
8960 deg
Eccentricity:
0005713
Arg of perigee: 64
8309 deg
Mean anomaly: 295
3436 deg
Mean motion: 15
53814412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 805
Checksum: 318
Coasting Arc #6 (Orbit 819)
---------------------------------------
Vector Time (GMT): 2018/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3855899
71 A = 6778173
97 meter
Y = -1624789
75 meter E =
0020266
Z = -5349877
93 I = 51
97060
XDOT = 2951
701005 Wp = 84
07985
YDOT = 7060
953619 meter/sec RA = 67
40164 deg
ZDOT = -15
046845 TA = 185
76545
MA = 185
78882
Ha = 223
450 n
mi
Hp = 213
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12650589
61 X = 3899768
69
Y = -5330675
03 feet Y = -1581425
16 meter
Z = -17552092
95 Z = -5331040
88
XDOT = 9684
058414 XDOT = 2872
597183
YDOT = 23165
858330 feet/sec YDOT = 7093
519285 meter/sec
ZDOT = -49
366291 ZDOT = -
900777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13562304
38 X = -4133790
37
Y = -2736268
23 feet Y = -834014
56 meter
Z = -17467289
92 Z = -5324029
97
XDOT = 4757
938437 XDOT = 1450
219636
YDOT = -23625
320460 feet/sec YDOT = -7200
997676 meter/sec
ZDOT = 13
209634 ZDOT = 4
026296
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 18230
51610087
00016717 00000-0 10270-3 0 9054
2 25544 51
6378 68
0883 0005671 69
0579 291
1180 15
53849937 8206
Satellite: ISS
Catalog Number: 25544
Epoch time: 18230
51610087 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 68
0883 deg
Eccentricity:
0005671
Arg of perigee: 69
0579 deg
Mean anomaly: 291
1180 deg
Mean motion: 15
53849937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 820
Checksum: 324
Coasting Arc #7 (Orbit 835)
---------------------------------------
Vector Time (GMT): 2018/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4470234
41 A = 6779302
32 meter
Y = 41631
94 meter E =
0010862
Z = 5089392
90 I = 51
96124
XDOT = -2134
679585 Wp = 63
83081
YDOT = -7145
655484 meter/sec RA = 62
42793 deg
ZDOT = -1808
880679 TA = 43
62694
MA = 43
54111
Ha = 223
591 n
mi
Hp = 213
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14666123
39 X = -4495089
10
Y = 136587
72 feet Y = -8496
31 meter
Z = 16697483
27 Z = 5067617
87
XDOT = -7003
541947 XDOT = -2045
829722
YDOT = -23443
751588 feet/sec YDOT = -7169
030150 meter/sec
ZDOT = -5934
647896 ZDOT = -1819
034356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12455587
66 X = 3796463
12
Y = 7951609
51 feet Y = 2423650
58 meter
Z = 16599699
43 Z = 5059588
39
XDOT = -6384
515029 XDOT = -1946
000181
YDOT = 22535
811201 feet/sec YDOT = 6868
915254 meter/sec
ZDOT = -5979
270081 ZDOT = -1822
481521
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 18231
54512200
00016717 00000-0 10270-3 0 9067
2 25544 51
6384 62
9609 0005513 72
7129 287
4626 15
53834942 8369
Satellite: ISS
Catalog Number: 25544
Epoch time: 18231
54512200 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 62
9609 deg
Eccentricity:
0005513
Arg of perigee: 72
7129 deg
Mean anomaly: 287
4626 deg
Mean motion: 15
53834942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 836
Checksum: 310
Coasting Arc #8 (Orbit 850)
---------------------------------------
Vector Time (GMT): 2018/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4981859
98 A = 6782100
52 meter
Y = 1420302
82 meter E =
0013801
Z = -4390122
60 I = 51
95394
XDOT = 1106
488540 Wp = 97
15623
YDOT = 6747
478245 meter/sec RA = 57
45708 deg
ZDOT = 3446
187953 TA = 207
66258
MA = 207
73607
Ha = 223
500 n
mi
Hp = 213
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16344684
98 X = 4986932
18
Y = 4659786
15 feet Y = 1476041
83 meter
Z = -14403289
38 Z = -4365910
37
XDOT = 3630
211744 XDOT = 1014
214548
YDOT = 22137
395816 feet/sec YDOT = 6759
335795 meter/sec
ZDOT = 11306
390921 ZDOT = 3451
338787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11450409
32 X = -3490084
76
Y = -12683254
80 feet Y = -3865856
06 meter
Z = -14294763
13 Z = -4357043
80
XDOT = 7828
834790 XDOT = 2386
228844
YDOT = -19807
522215 feet/sec YDOT = -6037
332771 meter/sec
ZDOT = 11328
590012 ZDOT = 3452
954236
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 18232
50982723
00016717 00000-0 10270-3 0 9076
2 25544 51
6379 58
1526 0005651 76
9672 283
2111 15
53853264 8518
Satellite: ISS
Catalog Number: 25544
Epoch time: 18232
50982723 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 58
1526 deg
Eccentricity:
0005651
Arg of perigee: 76
9672 deg
Mean anomaly: 283
2111 deg
Mean motion: 15
53853264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 851
Checksum: 318
Coasting Arc #9 (Orbit 866)
---------------------------------------
Vector Time (GMT): 2018/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5291605
22 A = 6785736
99 meter
Y = -2727200
16 meter E =
0018206
Z = 3241578
59 I = 51
94726
XDOT = 134
901917 Wp = 89
02567
YDOT = -5988
518730 meter/sec RA = 52
49477 deg
ZDOT = -4794
556701 TA = 53
57906
MA = 53
41132
Ha = 223
501 n
mi
Hp = 213
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17360909
51 X = -5276461
30
Y = -8947507
09 feet Y = -2786289
91 meter
Z = 10635100
37 Z = 3215910
90
XDOT = 442
591591 XDOT = 225
146286
YDOT = -19647
371163 feet/sec YDOT = -5986
505524 meter/sec
ZDOT = -15730
172905 ZDOT = -4793
682284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10299440
48 X = 3139269
46
Y = 16667658
72 feet Y = 5080302
38 meter
Z = 10520223
41 Z = 3206564
10
XDOT = -9407
117553 XDOT = -2867
289430
YDOT = 15787
587718 feet/sec YDOT = 4812
056737 meter/sec
ZDOT = -15725
411690 ZDOT = -4793
105483
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 18233
53884293
00016717 00000-0 10270-3 0 9084
2 25544 51
6377 53
0247 0005512 79
7050 280
4724 15
53864892 8672
Satellite: ISS
Catalog Number: 25544
Epoch time: 18233
53884293 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 53
0247 deg
Eccentricity:
0005512
Arg of perigee: 79
7050 deg
Mean anomaly: 280
4724 deg
Mean motion: 15
53864892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 867
Checksum: 330
Coasting Arc #10 (Orbit 881)
---------------------------------------
Vector Time (GMT): 2018/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5364764
08 A = 6788752
80 meter
Y = 3727961
85 meter E =
0011994
Z = -1840358
26 I = 51
93562
XDOT = -1498
081675 Wp = 58
52065
YDOT = 4937
302522 meter/sec RA = 47
53987 deg
ZDOT = 5667
583345 TA = 281
33409
MA = 281
46883
Ha = 223
560 n
mi
Hp = 213
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17600932
03 X = 5331617
61
Y = 12230845
97 feet Y = 3787769
03 meter
Z = -6037920
80 Z = -1814378
99
XDOT = -4914
966124 XDOT = -1580
710318
YDOT = 16198
499088 feet/sec YDOT = 4920
087897 meter/sec
ZDOT = 18594
433548 ZDOT = 5660
105639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9117428
64 X = -2778992
25
Y = -19433162
01 feet Y = -5923227
78 meter
Z = -5921790
13 Z = -1804961
63
XDOT = 11072
624240 XDOT = 3374
935868
YDOT = -10816
813644 feet/sec YDOT = -3296
964799 meter/sec
ZDOT = 18560
162179 ZDOT = 5657
137432
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 18234
50354676
00016717 00000-0 10270-3 0 9090
2 25544 51
6370 48
2175 0005702 85
3715 274
8089 15
53849609 8820
Satellite: ISS
Catalog Number: 25544
Epoch time: 18234
50354676 = yrday
fracday
Element set: 909
Inclination: 51
6370 deg
RA of node: 48
2175 deg
Eccentricity:
0005702
Arg of perigee: 85
3715 deg
Mean anomaly: 274
8089 deg
Mean motion: 15
53849609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 882
Checksum: 334
Coasting Arc #11 (Orbit 897)
---------------------------------------
Vector Time (GMT): 2018/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5102757
01 A = 6789963
04 meter
Y = -4465657
90 meter E =
0016797
Z = 211218
27 I = 51
91790
XDOT = 2966
686825 Wp = 118
22886
YDOT = -3692
034013 meter/sec RA = 42
58930 deg
ZDOT = -6030
957910 TA = 59
50427
MA = 59
33853
Ha = 223
405 n
mi
Hp = 212
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16741328
79 X = -5053467
52
Y = -14651108
61 feet Y = -4522444
87 meter
Z = 692973
31 Z = 186551
02
XDOT = 9733
224490 XDOT = 3037
046378
YDOT = -12112
972483 feet/sec YDOT = -3658
465092 meter/sec
ZDOT = -19786
607317 ZDOT = -6016
376123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7489650
61 X = 2282845
51
Y = 20951675
62 feet Y = 6386070
73 meter
Z = 582844
10 Z = 177650
88
XDOT = -12987
787982 XDOT = -3958
677777
YDOT = 5230
026011 feet/sec YDOT = 1594
111928 meter/sec
ZDOT = -19720
609814 ZDOT = -6010
841871
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 18235
53255891
00016717 00000-0 10270-3 0 9105
2 25544 51
6378 43
0891 0005637 85
9157 274
2640 15
53906072 8981
Satellite: ISS
Catalog Number: 25544
Epoch time: 18235
53255891 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 43
0891 deg
Eccentricity:
0005637
Arg of perigee: 85
9157 deg
Mean anomaly: 274
2640 deg
Mean motion: 15
53906072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 898
Checksum: 330
Coasting Arc #12 (Orbit 913)
---------------------------------------
Vector Time (GMT): 2018/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4527276
19 A = 6789250
92 meter
Y = 4857359
87 meter E =
0019017
Z = 1379224
76 I = 51
89019
XDOT = -4370
720922 Wp = 69
67207
YDOT = 2402
261317 meter/sec RA = 37
63768 deg
ZDOT = 5828
033405 TA = 305
30727
MA = 305
48496
Ha = 223
531 n
mi
Hp = 212
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14853268
34 X = 4465923
95
Y = 15936220
04 feet Y = 4907643
99 meter
Z = 4525015
62 Z = 1401067
18
XDOT = -14339
635570 XDOT = -4425
567816
YDOT = 7881
434768 feet/sec YDOT = 2353
078339 meter/sec
ZDOT = 19120
844503 ZDOT = 5806
669098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5547164
86 X = -1690775
85
Y = -21045684
71 feet Y = -6414724
70 meter
Z = 4622399
08 Z = 1408907
24
XDOT = 14939
526584 XDOT = 4553
567703
YDOT = 282
016250 feet/sec YDOT = 85
958553 meter/sec
ZDOT = 19024
576652 ZDOT = 5798
690963
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 18236
56157157
00016717 00000-0 10270-3 0 9116
2 25544 51
6378 37
9611 0005813 93
1046 267
0771 15
53867996 9142
Satellite: ISS
Catalog Number: 25544
Epoch time: 18236
56157157 = yrday
fracday
Element set: 911
Inclination: 51
6378 deg
RA of node: 37
9611 deg
Eccentricity:
0005813
Arg of perigee: 93
1046 deg
Mean anomaly: 267
0771 deg
Mean motion: 15
53867996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 914
Checksum: 332
Coasting Arc #13 (Orbit 928)
---------------------------------------
Vector Time (GMT): 2018/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3570817
96 A = 6786445
93 meter
Y = -4994203
76 meter E =
0010281
Z = -2897314
57 I = 51
85426
XDOT = 5641
625648 Wp = 103
45195
YDOT = -1106
048607 meter/sec RA = 32
68045 deg
ZDOT = -5063
942395 TA = 109
41386
MA = 109
30272
Ha = 223
509 n
mi
Hp = 212
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11715282
02 X = -3500632
64
Y = -16385182
93 feet Y = -5033742
79 meter
Z = -9505625
24 Z = -2914489
39
XDOT = 18509
270499 XDOT = 5678
171999
YDOT = -3628
768396 feet/sec YDOT = -1042
755890 meter/sec
ZDOT = -16613
984235 ZDOT = -5036
449042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2882164
47 X = 878483
73
Y = 19898665
01 feet Y = 6065113
09 meter
Z = -9582026
01 Z = -2920601
53
XDOT = -16770
801072 XDOT = -5111
740167
YDOT = -5484
392527 feet/sec YDOT = -1671
642842 meter/sec
ZDOT = -16490
386708 ZDOT = -5026
269869
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 18237
52626846
00016717 00000-0 10270-3 0 9120
2 25544 51
6379 33
1541 0005841 95
6251 264
5568 15
53875913 9299
Satellite: ISS
Catalog Number: 25544
Epoch time: 18237
52626846 = yrday
fracday
Element set: 912
Inclination: 51
6379 deg
RA of node: 33
1541 deg
Eccentricity:
0005841
Arg of perigee: 95
6251 deg
Mean anomaly: 264
5568 deg
Mean motion: 15
53875913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 929
Checksum: 333
Coasting Arc #14 (Orbit 944)
---------------------------------------
Vector Time (GMT): 2018/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2342377
29 A = 6782861
75 meter
Y = 4866187
49 meter E =
0016200
Z = 4092481
26 I = 51
81492
XDOT = -6635
124320 Wp = 102
00135
YDOT = -61
164415 meter/sec RA = 27
71210 deg
ZDOT = 3854
258306 TA = 308
20750
MA = 308
35326
Ha = 223
407 n
mi
Hp = 212
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7684964
87 X = 2267909
37
Y = 15965182
06 feet Y = 4891965
43 meter
Z = 13426775
78 Z = 4103678
38
XDOT = -21768
780576 XDOT = -6652
668862
YDOT = -200
670653 feet/sec YDOT = -135
460855 meter/sec
ZDOT = 12645
204416 ZDOT = 3821
985122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 230611
47 X = 70290
38
Y = -17679332
24 feet Y = -5388660
47 meter
Z = 13476351
92 Z = 4107592
06
XDOT = 18231
634410 XDOT = 5557
002168
YDOT = 9806
642777 feet/sec YDOT = 2989
064719 meter/sec
ZDOT = 12500
322024 ZDOT = 3810
098153
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 18238
55527603
00016717 00000-0 10270-3 0 9136
2 25544 51
6388 28
0260 0005695 100
8819 259
2975 15
53889436 9452
Satellite: ISS
Catalog Number: 25544
Epoch time: 18238
55527603 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 28
0260 deg
Eccentricity:
0005695
Arg of perigee: 100
8819 deg
Mean anomaly: 259
2975 deg
Mean motion: 15
53889436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 945
Checksum: 342
Coasting Arc #15 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2018/238/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1517974
03 A = 6778025
93 meter
Y = 3918190
38 meter E =
0008146
Z = 5311600
00 I = 51
79791
XDOT = -6959
105595 Wp = 101
93363
YDOT = -3213
551671 meter/sec RA = 27
01987 deg
ZDOT = 379
588237 TA = 344
44531
MA = 344
47033
Ha = 223
439 n
mi
Hp = 212
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4980229
75 X = -1587476
02
Y = 12854955
31 feet Y = 3900827
04 meter
Z = 17426509
20 Z = 5304057
31
XDOT = -22831
711271 XDOT = -6924
497368
YDOT = -10543
148528 feet/sec YDOT = -3291
179682 meter/sec
ZDOT = 1245
368233 ZDOT = 345
868132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -228520
23 X = -69652
97
Y = -13827466
94 feet Y = -4214611
92 meter
Z = 17392087
96 Z = 5301108
41
XDOT = 24128
456797 XDOT = 7354
353632
YDOT = 986
651036 feet/sec YDOT = 300
731236 meter/sec
ZDOT = 1094
440796 ZDOT = 333
585555
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 18238
68390078
00016717 00000-0 10270-3 0 9145
2 25544 51
6419 27
3863 0005584 101
2652 258
9128 15
53905846 9477
Satellite: ISS
Catalog Number: 25544
Epoch time: 18238
68390078 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 27
3863 deg
Eccentricity:
0005584
Arg of perigee: 101
2652 deg
Mean anomaly: 258
9128 deg
Mean motion: 15
53905846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 947
Checksum: 336
Coasting Arc #16 (Orbit 961)
---------------------------------------
Vector Time (GMT): 2018/239/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3053409
84 A = 6778801
51 meter
Y = -3163599
21 meter E =
0019402
Z = -5176753
68 I = 51
77039
XDOT = 6453
256678 Wp = 101
37695
YDOT = 3848
509308 meter/sec RA = 22
03385 deg
ZDOT = 1455
338277 TA = 182
62687
MA = 182
63708
Ha = 223
438 n
mi
Hp = 213
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10017748
82 X = 3113704
73
Y = -10379262
49 feet Y = -3129117
10 meter
Z = -16984100
00 Z = -5161774
81
XDOT = 21172
101962 XDOT = 6402
672799
YDOT = 12626
342873 feet/sec YDOT = 3920
391367 meter/sec
ZDOT = 4774
731880 ZDOT = 1486
562378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5138017
82 X = -1566067
83
Y = 13563922
13 feet Y = 4134283
47 meter
Z = -16916406
92 Z = -5156120
83
XDOT = -23435
349509 XDOT = -7143
094530
YDOT = -2752
001035 feet/sec YDOT = -838
809915 meter/sec
ZDOT = 4914
351331 ZDOT = 1497
894286
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 18239
64859395
00016717 00000-0 10270-3 0 9155
2 25544 51
6420 22
5802 0005699 102
9457 257
2332 15
53888884 9625
Satellite: ISS
Catalog Number: 25544
Epoch time: 18239
64859395 = yrday
fracday
Element set: 915
Inclination: 51
6420 deg
RA of node: 22
5802 deg
Eccentricity:
0005699
Arg of perigee: 102
9457 deg
Mean anomaly: 257
2332 deg
Mean motion: 15
53888884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 962
Checksum: 344
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