[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 29th 2018
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) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
030/15:25:11
379 1
1 1
1 1
1
N/A -0
5 -0
1 222
1
000/00:00:22
759 0
0 -0
0 213
8
037/00:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
6
040/08:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
5
043/19:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
6
Coasting Arc #1 (Orbit 1697)
---------------------------------------
Vector Time (GMT): 2018/029/16:59:17
652
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2801840
72 A = 6778075
74 meter
Y = 3527647
01 meter E =
0007566
Z = 5058061
41 I = 51
55432
XDOT = -6883
973219 Wp = 95
98805
YDOT = 2867
558363 meter/sec RA = 348
49681 deg
ZDOT = 1810
253016 TA = 336
46514
MA = 336
49974
Ha = 222
019 n
mi
Hp = 213
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9192390
83 X = 2737616
51
Y = 11573645
05 feet Y = 3558619
76 meter
Z = 16594689
66 Z = 5071515
68
XDOT = -22585
213974 XDOT = -6924
320473
YDOT = 9407
999879 feet/sec YDOT = 2790
351370 meter/sec
ZDOT = 5939
150315 ZDOT = 1776
715920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12864360
03 X = 3921056
94
Y = 7140480
79 feet Y = 2176418
55 meter
Z = 16653972
76 Z = 5076130
90
XDOT = -16675
409747 XDOT = -5082
664891
YDOT = 16516
238158 feet/sec YDOT = 5034
149391 meter/sec
ZDOT = 5789
350587 ZDOT = 1764
594059
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 18029
75913906
00016717 00000-0 10270-3 0 9007
2 25544 51
6426 348
8048 0003829 55
3745 304
7768 15
54230964 16980
Satellite: ISS
Catalog Number: 25544
Epoch time: 18029
75913906 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 348
8048 deg
Eccentricity:
0003829
Arg of perigee: 55
3745 deg
Mean anomaly: 304
7768 deg
Mean motion: 15
54230964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1698
Checksum: 341
Coasting Arc #2 (Orbit 1711)
---------------------------------------
Vector Time (GMT): 2018/030/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1598995
86 A = 6777641
09 meter
Y = -3925437
88 meter E =
0017368
Z = -5303723
03 I = 51
52142
XDOT = 7250
685679 Wp = 80
56063
YDOT = -2425
805135 meter/sec RA = 343
81858 deg
ZDOT = -388
872719 TA = 185
70911
MA = 185
72894
Ha = 222
091 n
mi
Hp = 213
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5246049
41 X = -1529219
69
Y = -12878733
22 feet Y = -3942928
62 meter
Z = -17400666
10 Z = -5311320
87
XDOT = 23788
338843 XDOT = 7279
161697
YDOT = -7958
678264 feet/sec YDOT = -2344
563765 meter/sec
ZDOT = -1275
829129 ZDOT = -353
583240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5196085
63 X = -1583766
90
Y = -12854137
70 feet Y = -3917941
17 meter
Z = -17433812
63 Z = -5313826
09
XDOT = 22818
467372 XDOT = 6955
068855
YDOT = -7699
735982 feet/sec YDOT = -2346
879527 meter/sec
ZDOT = -1118
310385 ZDOT = -340
861005
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 18030
65930659
00016717 00000-0 10270-3 0 9013
2 25544 51
6430 344
3160 0003105 49
4097 310
7326 15
54044848 17120
Satellite: ISS
Catalog Number: 25544
Epoch time: 18030
65930659 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 344
3160 deg
Eccentricity:
0003105
Arg of perigee: 49
4097 deg
Mean anomaly: 310
7326 deg
Mean motion: 15
54044848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1712
Checksum: 287
Coasting Arc #3 (Orbit 1727)
---------------------------------------
Vector Time (GMT): 2018/031/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -114722
35 A = 6778301
10 meter
Y = 4422841
59 meter E =
0007908
Z = 5130840
85 I = 51
49243
XDOT = -7357
888655 Wp = 52
96968
YDOT = 1565
619384 meter/sec RA = 338
81101 deg
ZDOT = -1507
822729 TA = 51
61126
MA = 51
54026
Ha = 222
058 n
mi
Hp = 213
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -376385
66 X = -189093
43
Y = 14510635
13 feet Y = 4421142
80 meter
Z = 16833467
35 Z = 5130103
00
XDOT = -24140
054642 XDOT = -7367
524992
YDOT = 5136
546536 feet/sec YDOT = 1483
284564 meter/sec
ZDOT = -4946
924964 ZDOT = -1543
587153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -164469
36 X = -50130
26
Y = 14519267
81 feet Y = 4425472
83 meter
Z = 16829427
59 Z = 5129609
53
XDOT = -22927
950352 XDOT = -6988
439267
YDOT = 5683
034960 feet/sec YDOT = 1732
189056 meter/sec
ZDOT = -5106
402363 ZDOT = -1556
431440
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 18031
68820380
00016717 00000-0 10270-3 0 9027
2 25544 51
6428 339
1881 0003077 51
2986 308
8442 15
54076250 17281
Satellite: ISS
Catalog Number: 25544
Epoch time: 18031
68820380 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 339
1881 deg
Eccentricity:
0003077
Arg of perigee: 51
2986 deg
Mean anomaly: 308
8442 deg
Mean motion: 15
54076250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1728
Checksum: 312
Coasting Arc #4 (Orbit 1742)
---------------------------------------
Vector Time (GMT): 2018/032/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1719875
00 A = 6781182
24 meter
Y = -4811504
96 meter E =
0011290
Z = -4468736
65 I = 51
47126
XDOT = 6920
077440 Wp = 97
17383
YDOT = -529
647039 meter/sec RA = 333
80666 deg
ZDOT = 3239
256891 TA = 205
52483
MA = 205
58062
Ha = 222
127 n
mi
Hp = 213
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5642634
51 X = 1795256
86
Y = -15785777
42 feet Y = -4791850
74 meter
Z = -14661209
47 Z = -4460199
15
XDOT = 22703
666141 XDOT = 6909
751645
YDOT = -1737
687137 feet/sec YDOT = -452
319656 meter/sec
ZDOT = 10627
483238 ZDOT = 3272
846177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5112146
27 X = 1558182
18
Y = -16001022
42 feet Y = -4877111
64 meter
Z = -14622393
72 Z = -4456905
60
XDOT = 21380
187946 XDOT = 6516
681286
YDOT = -3000
791165 feet/sec YDOT = -914
641147 meter/sec
ZDOT = 10777
093220 ZDOT = 3284
858013
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 18032
65279447
00016717 00000-0 10270-3 0 9038
2 25544 51
6427 334
3811 0003043 54
4738 305
6699 15
54039170 17439
Satellite: ISS
Catalog Number: 25544
Epoch time: 18032
65279447 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 334
3811 deg
Eccentricity:
0003043
Arg of perigee: 54
4738 deg
Mean anomaly: 305
6699 deg
Mean motion: 15
54039170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1743
Checksum: 311
Coasting Arc #5 (Orbit 1758)
---------------------------------------
Vector Time (GMT): 2018/033/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3146428
02 A = 6784920
25 meter
Y = 5000699
95 meter E =
0015349
Z = 3324070
66 I = 51
45520
XDOT = -6047
394500 Wp = 84
95569
YDOT = -687
815943 meter/sec RA = 328
80918 deg
ZDOT = -4669
528581 TA = 56
21992
MA = 56
07382
Ha = 222
198 n
mi
Hp = 213
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10322926
58 X = -3218259
50
Y = 16406495
90 feet Y = 4965112
95 meter
Z = 10905743
63 Z = 3308612
12
XDOT = -19840
533138 XDOT = -6016
572207
YDOT = -2256
613986 feet/sec YDOT = -755
269937 meter/sec
ZDOT = -15319
975661 ZDOT = -4698
829044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9448987
62 X = -2880051
43
Y = 16969581
53 feet Y = 5172328
45 meter
Z = 10836101
73 Z = 3302843
81
XDOT = -18597
816754 XDOT = -5668
614547
YDOT = -447
635834 feet/sec YDOT = -136
439402 meter/sec
ZDOT = -15450
282764 ZDOT = -4709
246187
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 18033
68168631
00016717 00000-0 10270-3 0 9045
2 25544 51
6431 329
2533 0003140 58
4666 301
6793 15
54054109 17597
Satellite: ISS
Catalog Number: 25544
Epoch time: 18033
68168631 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 329
2533 deg
Eccentricity:
0003140
Arg of perigee: 58
4666 deg
Mean anomaly: 301
6793 deg
Mean motion: 15
54054109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1759
Checksum: 306
Coasting Arc #6 (Orbit 1773)
---------------------------------------
Vector Time (GMT): 2018/034/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4236078
70 A = 6788068
14 meter
Y = -4955642
54 meter E =
0010145
Z = -1880566
07 I = 51
43804
XDOT = 4826
788784 Wp = 44
91327
YDOT = 2007
811843 meter/sec RA = 323
81840 deg
ZDOT = 5607
208011 TA = 294
32704
MA = 294
43294
Ha = 222
172 n
mi
Hp = 213
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13897896
00 X = 4300313
79
Y = -16258669
76 feet Y = -4907912
76 meter
Z = -6169836
19 Z = -1859832
82
XDOT = 15835
921207 XDOT = 4776
741923
YDOT = 6587
309196 feet/sec YDOT = 2061
508830 meter/sec
ZDOT = 18396
351742 ZDOT = 5630
532655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12700631
95 X = 3871152
62
Y = -17243257
47 feet Y = -5255744
88 meter
Z = -6076738
79 Z = -1852189
98
XDOT = 14900
186636 XDOT = 4541
576887
YDOT = 4485
259648 feet/sec YDOT = 1367
107141 meter/sec
ZDOT = 18499
836644 ZDOT = 5638
750209
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 18034
64626725
00016717 00000-0 10270-3 0 9056
2 25544 51
6428 324
4452 0003098 60
4200 299
7261 15
54060220 17744
Satellite: ISS
Catalog Number: 25544
Epoch time: 18034
64626725 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 324
4452 deg
Eccentricity:
0003098
Arg of perigee: 60
4200 deg
Mean anomaly: 299
7261 deg
Mean motion: 15
54060220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1774
Checksum: 294
Coasting Arc #7 (Orbit 1789)
---------------------------------------
Vector Time (GMT): 2018/035/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4997564
47 A = 6789641
80 meter
Y = 4583887
01 meter E =
0013980
Z = 201939
26 I = 51
41592
XDOT = -3371
996588 Wp = 121
07702
YDOT = -3399
192676 meter/sec RA = 318
83357 deg
ZDOT = -5989
369323 TA = 56
74076
MA = 56
60688
Ha = 222
224 n
mi
Hp = 213
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16396208
90 X = -5049432
21
Y = 15038999
38 feet Y = 4527710
82 meter
Z = 662530
40 Z = 177537
02
XDOT = -11062
980931 XDOT = -3304
642641
YDOT = -11152
206942 feet/sec YDOT = -3436
524456 meter/sec
ZDOT = -19650
161821 ZDOT = -6005
585184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14964832
99 X = -4561281
09
Y = 16467965
32 feet Y = 5019435
83 meter
Z = 553178
93 Z = 168608
94
XDOT = -10701
194364 XDOT = -3261
724042
YDOT = -9022
233622 feet/sec YDOT = -2749
976808 meter/sec
ZDOT = -19721
778529 ZDOT = -6011
198096
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 18035
67515227
00016717 00000-0 10270-3 0 9065
2 25544 51
6417 319
3173 0003052 67
7960 292
3516 15
54016756 17903
Satellite: ISS
Catalog Number: 25544
Epoch time: 18035
67515227 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 319
3173 deg
Eccentricity:
0003052
Arg of perigee: 67
7960 deg
Mean anomaly: 292
3516 deg
Mean motion: 15
54016756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1790
Checksum: 312
Coasting Arc #8 (Orbit 1805)
---------------------------------------
Vector Time (GMT): 2018/036/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5353643
51 A = 6788539
04 meter
Y = -3899651
83 meter E =
0016811
Z = 1452053
15 I = 51
38856
XDOT = 1856
646979 Wp = 62
25733
YDOT = 4711
002042 meter/sec RA = 313
84654 deg
ZDOT = 5763
039209 TA = 313
64846
MA = 313
78773
Ha = 222
065 n
mi
Hp = 213
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17564447
21 X = 5389799
38
Y = -12794133
31 feet Y = -3839581
47 meter
Z = 4763953
89 Z = 1478146
92
XDOT = 6091
361480 XDOT = 1775
835929
YDOT = 15456
043444 feet/sec YDOT = 4731
312848 meter/sec
ZDOT = 18907
608954 ZDOT = 5771
861455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16047739
73 X = 4891351
07
Y = -14613132
25 feet Y = -4454082
71 meter
Z = 4880709
47 Z = 1487640
25
XDOT = 6536
106392 XDOT = 1992
205228
YDOT = 13552
228291 feet/sec YDOT = 4130
719183 meter/sec
ZDOT = 18946
111171 ZDOT = 5774
774685
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 18036
70403054
00016717 00000-0 10270-3 0 9075
2 25544 51
6414 314
1886 0002941 67
2741 292
8723 15
54079394 18062
Satellite: ISS
Catalog Number: 25544
Epoch time: 18036
70403054 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 314
1886 deg
Eccentricity:
0002941
Arg of perigee: 67
2741 deg
Mean anomaly: 292
8723 deg
Mean motion: 15
54079394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1806
Checksum: 311
Coasting Arc #9 (Orbit 1810)
---------------------------------------
Vector Time (GMT): 2018/037/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4178787
22 A = 6778294
17 meter
Y = -1499848
61 meter E =
0016544
Z = -5136676
67 I = 51
34603
XDOT = 4083
742779 Wp = 78
35066
YDOT = -6303
728845 meter/sec RA = 312
01894 deg
ZDOT = -1482
381421 TA = 177
29787
MA = 177
28892
Ha = 222
121 n
mi
Hp = 213
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13709931
81 X = -4136754
03
Y = -4920763
16 feet Y = -1546343
94 meter
Z = -16852613
74 Z = -5156873
29
XDOT = 13398
106231 XDOT = 4161
129789
YDOT = -20681
525083 feet/sec YDOT = -6257
629018 meter/sec
ZDOT = -4863
456106 ZDOT = -1462
356001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6748965
19 X = 2057084
59
Y = 12790553
29 feet Y = 3898560
64 meter
Z = -16942253
26 Z = -5163998
79
XDOT = -22917
809936 XDOT = -6985
348468
YDOT = 5773
350350 feet/sec YDOT = 1759
717187 meter/sec
ZDOT = -4773
324184 ZDOT = -1454
909211
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 18037
02555552
00016717 00000-0 10270-3 0 9083
2 25544 51
6417 312
5828 0002772 77
4962 282
6500 15
54047954 18116
Satellite: ISS
Catalog Number: 25544
Epoch time: 18037
02555552 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 312
5828 deg
Eccentricity:
0002772
Arg of perigee: 77
4962 deg
Mean anomaly: 282
6500 deg
Mean motion: 15
54047954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1811
Checksum: 313
Coasting Arc #10 (Orbit 1826)
---------------------------------------
Vector Time (GMT): 2018/038/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3086091
49 A = 6777479
87 meter
Y = 2921391
85 meter E =
0005523
Z = 5275217
76 I = 51
32289
XDOT = -4874
549741 Wp = 74
54552
YDOT = 5910
695048 meter/sec RA = 306
99842 deg
ZDOT = -419
808433 TA = 19
48382
MA = 19
46272
Ha = 221
954 n
mi
Hp = 213
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10124972
09 X = 3027570
45
Y = 9584618
92 feet Y = 2955575
66 meter
Z = 17307144
89 Z = 5290066
46
XDOT = -15992
617261 XDOT = -4938
243266
YDOT = 19392
044120 feet/sec YDOT = 5855
828337 meter/sec
ZDOT = -1377
324256 ZDOT = -443
641942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1194406
15 X = -364054
99
Y = -13808617
51 feet Y = -4208866
62 meter
Z = 17372757
99 Z = 5295216
63
XDOT = 23799
188627 XDOT = 7253
992693
YDOT = -3933
467817 feet/sec YDOT = -1198
920990 meter/sec
ZDOT = -1484
327152 ZDOT = -452
422916
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 18038
05442888
00016717 00000-0 10270-3 0 9095
2 25544 51
6420 307
4541 0002844 79
2164 280
9309 15
54104680 18274
Satellite: ISS
Catalog Number: 25544
Epoch time: 18038
05442888 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 307
4541 deg
Eccentricity:
0002844
Arg of perigee: 79
2164 deg
Mean anomaly: 280
9309 deg
Mean motion: 15
54104680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1827
Checksum: 313
Coasting Arc #11 (Orbit 1841)
---------------------------------------
Vector Time (GMT): 2018/039/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1961453
58 A = 6779243
49 meter
Y = -4269564
68 meter E =
0014890
Z = -4900641
19 I = 51
30831
XDOT = 5295
347149 Wp = 101
76917
YDOT = -5040
706549 meter/sec RA = 301
97904 deg
ZDOT = 2275
068161 TA = 190
59131
MA = 190
62271
Ha = 222
150 n
mi
Hp = 213
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6435215
16 X = -1889759
96
Y = -14007758
15 feet Y = -4291098
29 meter
Z = -16078219
13 Z = -4909994
86
XDOT = 17373
186186 XDOT = 5340
269200
YDOT = -16537
751146 feet/sec YDOT = -4981
239099 meter/sec
ZDOT = 7464
134387 ZDOT = 2300
900041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4237048
81 X = -1291452
48
Y = 14776948
20 feet Y = 4504013
81 meter
Z = -16119169
71 Z = -4913122
93
XDOT = -22830
943150 XDOT = -6958
871472
YDOT = 1711
599213 feet/sec YDOT = 521
695440 meter/sec
ZDOT = 7579
881394 ZDOT = 2310
347849
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 18039
01899811
00016717 00000-0 10270-3 0 9106
2 25544 51
6407 302
6472 0003002 82
6302 277
5192 15
54087227 18424
Satellite: ISS
Catalog Number: 25544
Epoch time: 18039
01899811 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 302
6472 deg
Eccentricity:
0003002
Arg of perigee: 82
6302 deg
Mean anomaly: 277
5192 deg
Mean motion: 15
54087227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1842
Checksum: 294
Coasting Arc #12 (Orbit 1857)
---------------------------------------
Vector Time (GMT): 2018/040/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 840643
19 A = 6782600
09 meter
Y = 5407907
94 meter E =
0013727
Z = 3996536
02 I = 51
30378
XDOT = -5428
245345 Wp = 79
72405
YDOT = 3749
204161 meter/sec RA = 296
96434 deg
ZDOT = -3917
532786 TA = 51
19620
MA = 51
07370
Ha = 222
053 n
mi
Hp = 213
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2758015
72 X = 760695
24
Y = 17742480
11 feet Y = 5416861
65 meter
Z = 13111994
82 Z = 4000425
22
XDOT = -17809
203887 XDOT = -5450
737489
YDOT = 12300
538587 feet/sec YDOT = 3688
375953 meter/sec
ZDOT = -12852
797855 ZDOT = -3943
955648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9178218
72 X = 2797521
07
Y = -15418513
40 feet Y = -4699562
88 meter
Z = 13128457
82 Z = 4001553
94
XDOT = 20380
721482 XDOT = 6212
043908
YDOT = 1048
855138 feet/sec YDOT = 319
691046 meter/sec
ZDOT = -12970
964065 ZDOT = -3953
549847
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 18040
04786703
00016717 00000-0 10270-3 0 9117
2 25544 51
6413 297
5184 0002872 84
4053 275
7427 15
54105009 18587
Satellite: ISS
Catalog Number: 25544
Epoch time: 18040
04786703 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 297
5184 deg
Eccentricity:
0002872
Arg of perigee: 84
4053 deg
Mean anomaly: 275
7427 deg
Mean motion: 15
54105009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1858
Checksum: 308
Coasting Arc #13 (Orbit 1862)
---------------------------------------
Vector Time (GMT): 2018/040/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4450229
33 A = 6778259
46 meter
Y = -196057
67 meter E =
0016771
Z = -5124039
49 I = 51
28240
XDOT = 2062
964483 Wp = 78
72132
YDOT = -7214
786521 meter/sec RA = 295
28162 deg
ZDOT = -1516
648446 TA = 176
57560
MA = 176
56410
Ha = 222
192 n
mi
Hp = 213
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14600489
94 X = -4422816
71
Y = -643233
82 feet Y = -245670
01 meter
Z = -16811153
19 Z = -5145590
26
XDOT = 6768
256177 XDOT = 2150
855822
YDOT = -23670
559452 feet/sec YDOT = -7191
225635 meter/sec
ZDOT = -4975
880729 ZDOT = -1506
413825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1964580
17 X = 598804
04
Y = -14369965
66 feet Y = -4379965
53 meter
Z = -16907023
38 Z = -5153260
73
XDOT = 21903
426491 XDOT = 6676
164394
YDOT = 8790
087465 feet/sec YDOT = 2679
218659 meter/sec
ZDOT = -4929
215342 ZDOT = -1502
424836
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 18040
36938985
00016717 00000-0 10270-3 0 9124
2 25544 51
6397 295
9167 0003073 80
5428 279
6072 15
54076097 18637
Satellite: ISS
Catalog Number: 25544
Epoch time: 18040
36938985 = yrday
fracday
Element set: 912
Inclination: 51
6397 deg
RA of node: 295
9167 deg
Eccentricity:
0003073
Arg of perigee: 80
5428 deg
Mean anomaly: 279
6072 deg
Mean motion: 15
54076097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1863
Checksum: 345
Coasting Arc #14 (Orbit 1878)
---------------------------------------
Vector Time (GMT): 2018/041/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3815129
65 A = 6777504
22 meter
Y = 1877843
71 meter E =
0005707
Z = 5272841
88 I = 51
26697
XDOT = -2943
491117 Wp = 76
98440
YDOT = 7075
421633 meter/sec RA = 290
25797 deg
ZDOT = -388
442243 TA = 16
74592
MA = 16
72709
Ha = 222
038 n
mi
Hp = 213
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12516829
55 X = 3768235
30
Y = 6160904
57 feet Y = 1920244
98 meter
Z = 17299349
99 Z = 5291260
21
XDOT = -9657
123088 XDOT = -3020
504815
YDOT = 23213
325567 feet/sec YDOT = 7042
074880 meter/sec
ZDOT = -1274
416809 ZDOT = -402
927609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7064905
43 X = -2153383
18
Y = 11911439
24 feet Y = 3630606
68 meter
Z = 17381024
25 Z = 5297736
19
XDOT = -21565
364595 XDOT = -6573
123129
YDOT = -10827
859326 feet/sec YDOT = -3300
331523 meter/sec
ZDOT = -1339
963346 ZDOT = -408
420828
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 18041
39825469
00016717 00000-0 10270-3 0 9131
2 25544 51
6397 290
7890 0003083 81
7533 278
3969 15
54092171 18793
Satellite: ISS
Catalog Number: 25544
Epoch time: 18041
39825469 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 290
7890 deg
Eccentricity:
0003083
Arg of perigee: 81
7533 deg
Mean anomaly: 278
3969 deg
Mean motion: 15
54092171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1879
Checksum: 348
Coasting Arc #15 (Orbit 1893)
---------------------------------------
Vector Time (GMT): 2018/042/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3125777
52 A = 6779203
71 meter
Y = -3500816
75 meter E =
0015132
Z = -4905970
51 I = 51
26165
XDOT = 3605
369355 Wp = 102
29548
YDOT = -6368
698264 meter/sec RA = 285
23392 deg
ZDOT = 2250
218383 TA = 189
82426
MA = 189
85388
Ha = 222
198 n
mi
Hp = 213
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10255175
58 X = -3062567
98
Y = -11485619
25 feet Y = -3535417
98 meter
Z = -16095703
76 Z = -4921000
58
XDOT = 11828
639616 XDOT = 3665
387745
YDOT = -20894
679343 feet/sec YDOT = -6328
044934 meter/sec
ZDOT = 7382
606244 ZDOT = 2267
877538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12046523
12 X = 3671780
25
Y = -9477807
91 feet Y = -2888835
85 meter
Z = -16162060
30 Z = -4926195
98
XDOT = 19497
819241 XDOT = 5942
935305
YDOT = 12072
602596 feet/sec YDOT = 3679
729271 meter/sec
ZDOT = 7462
155680 ZDOT = 2274
465051
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 18042
36281459
00016717 00000-0 10270-3 0 9145
2 25544 51
6393 285
9811 0003106 86
0746 274
0762 15
54082477 18947
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
36281459 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 285
9811 deg
Eccentricity:
0003106
Arg of perigee: 86
0746 deg
Mean anomaly: 274
0762 deg
Mean motion: 15
54082477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1894
Checksum: 326
Coasting Arc #16 (Orbit 1909)
---------------------------------------
Vector Time (GMT): 2018/043/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2378073
46 A = 6782573
06 meter
Y = 4921293
24 meter E =
0013764
Z = 4005945
68 I = 51
26589
XDOT = -4111
294913 Wp = 80
64960
YDOT = 5172
706179 meter/sec RA = 280
21697 deg
ZDOT = -3900
353821 TA = 50
07773
MA = 49
95684
Ha = 222
093 n
mi
Hp = 213
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7802078
29 X = 2303407
15
Y = 16145975
19 feet Y = 4947469
08 meter
Z = 13142866
41 Z = 4017315
84
XDOT = -13488
500372 XDOT = -4149
886513
YDOT = 16970
820796 feet/sec YDOT = 5126
515001 meter/sec
ZDOT = -12796
436419 ZDOT = -3920
418456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16441285
69 X = -5011303
88
Y = 7066523
65 feet Y = 2153876
41 meter
Z = 13192734
60 Z = 4021145
51
XDOT = -15907
620168 XDOT = -4848
642627
YDOT = -12869
594647 feet/sec YDOT = -3922
652449 meter/sec
ZDOT = -12886
499791 ZDOT = -3927
805136
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 18043
39167553
00016717 00000-0 10270-3 0 9158
2 25544 51
6398 280
8532 0003004 89
2968 270
8528 15
54091202 19103
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
39167553 = yrday
fracday
Element set: 915
Inclination: 51
6398 deg
RA of node: 280
8532 deg
Eccentricity:
0003004
Arg of perigee: 89
2968 deg
Mean anomaly: 270
8528 deg
Mean motion: 15
54091202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1910
Checksum: 315
Coasting Arc #17 (Orbit 1916)
---------------------------------------
Vector Time (GMT): 2018/043/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3601305
93 A = 6779013
90 meter
Y = 2906934
97 meter E =
0008798
Z = 4946986
50 I = 51
25165
XDOT = -2665
571784 Wp = 71
36027
YDOT = 6882
745845 meter/sec RA = 277
98353 deg
ZDOT = -2098
099758 TA = 39
19518
MA = 39
13150
Ha = 222
133 n
mi
Hp = 213
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11815308
17 X = 3544502
85
Y = 9537188
22 feet Y = 2946889
76 meter
Z = 16230270
68 Z = 4964341
96
XDOT = -8745
314251 XDOT = -2732
147175
YDOT = 22581
187156 feet/sec YDOT = 6852
565296 meter/sec
ZDOT = -6883
529389 ZDOT = -2111
209743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13112600
70 X = 3996720
69
Y = -7491328
72 feet Y = -2283356
99 meter
Z = 16307079
74 Z = 4970397
90
XDOT = 17391
182545 XDOT = 5300
832440
YDOT = 15286
269599 feet/sec YDOT = 4659
254974 meter/sec
ZDOT = -6942
889827 ZDOT = -2116
192819
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 18043
84180186
00016717 00000-0 10270-3 0 9166
2 25544 51
6402 278
6049 0003196 100
3519 259
7994 15
54065196 19179
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
84180186 = yrday
fracday
Element set: 916
Inclination: 51
6402 deg
RA of node: 278
6049 deg
Eccentricity:
0003196
Arg of perigee: 100
3519 deg
Mean anomaly: 259
7994 deg
Mean motion: 15
54065196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1917
Checksum: 329
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