[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 2nd 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) : 73 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 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
187/05:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 216
2
191/20:25:31
000 0
0 0
2 0
2
N/A -0
2 0
0 220
1
000/00:00:58
000 0
0 -0
0 216
0
193/18:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
9
197/12:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 215
7
Coasting Arc #1 (Orbit 88)
---------------------------------------
Vector Time (GMT): 2018/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1685218
15 A = 6787623
40 meter
Y = -6173869
32 meter E =
0003508
Z = -2255673
19 I = 51
33241
XDOT = 5401
217275 Wp = 7
66374
YDOT = -502
866809 meter/sec RA = 301
65007 deg
ZDOT = 5416
015155 TA = 327
13806
MA = 327
15986
Ha = 219
961 n
mi
Hp = 216
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5528930
95 X = 1765087
53
Y = -20255476
78 feet Y = -6154577
21 meter
Z = -7400502
59 Z = -2247293
84
XDOT = 17720
529118 XDOT = 5380
131253
YDOT = -1649
825488 feet/sec YDOT = -442
585215 meter/sec
ZDOT = 17769
078594 ZDOT = 5442
200774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20902692
37 X = -6371140
63
Y = -2120893
61 feet Y = -646448
37 meter
Z = -7362072
92 Z = -2243959
83
XDOT = -4716
132402 XDOT = -1437
477156
YDOT = -15556
529589 feet/sec YDOT = -4741
630219 meter/sec
ZDOT = 17886
285393 ZDOT = 5451
739788
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 18183
50446117
00016717 00000-0 10270-3 0 9006
2 25544 51
6408 302
3636 0003757 256
3328 103
7407 15
53979983 898
Satellite: ISS
Catalog Number: 25544
Epoch time: 18183
50446117 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 302
3636 deg
Eccentricity:
0003757
Arg of perigee: 256
3328 deg
Mean anomaly: 103
7407 deg
Mean motion: 15
53979983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 89
Checksum: 318
Coasting Arc #2 (Orbit 104)
---------------------------------------
Vector Time (GMT): 2018/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2562192
66 A = 6789552
79 meter
Y = 6247646
23 meter E =
0011110
Z = 641055
33 I = 51
32179
XDOT = -4670
212639 Wp = 143
57420
YDOT = -1300
943383 meter/sec RA = 296
65733 deg
ZDOT = -5942
921206 TA = 29
47239
MA = 29
40980
Ha = 219
874 n
mi
Hp = 216
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8406143
90 X = -2634979
00
Y = 20497527
02 feet Y = 6218586
99 meter
Z = 2103199
90 Z = 628433
10
XDOT = -15322
219943 XDOT = -4626
450814
YDOT = -4268
186952 feet/sec YDOT = -1352
923619 meter/sec
ZDOT = -19497
772987 ZDOT = -5965
501051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21695792
82 X = 6612877
65
Y = 4510277
98 feet Y = 1374732
73 meter
Z = 2045796
97 Z = 623558
92
XDOT = -1076
645481 XDOT = -328
161543
YDOT = 14136
418853 feet/sec YDOT = 4308
780466 meter/sec
ZDOT = -19598
575892 ZDOT = -5973
645932
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 18184
53337937
00016717 00000-0 10270-3 0 9010
2 25544 51
6400 297
2359 0003824 257
6302 102
4423 15
53995443 1057
Satellite: ISS
Catalog Number: 25544
Epoch time: 18184
53337937 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 297
2359 deg
Eccentricity:
0003824
Arg of perigee: 257
6302 deg
Mean anomaly: 102
4423 deg
Mean motion: 15
53995443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 105
Checksum: 301
Coasting Arc #3 (Orbit 120)
---------------------------------------
Vector Time (GMT): 2018/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3216329
52 A = 6789217
83 meter
Y = -5884824
85 meter E =
0010417
Z = 1019493
94 I = 51
30811
XDOT = 3824
618546 Wp = 46
60895
YDOT = 3113
109189 meter/sec RA = 291
66531 deg
ZDOT = 5872
935789 TA = 324
49286
MA = 324
56214
Ha = 219
828 n
mi
Hp = 216
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10552262
22 X = 3276944
10
Y = -19307168
14 feet Y = -5848518
81 meter
Z = 3344796
39 Z = 1035264
28
XDOT = 12547
961108 XDOT = 3760
995314
YDOT = 10213
612826 feet/sec YDOT = 3155
522432 meter/sec
ZDOT = 19268
162038 ZDOT = 5891
360035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21026887
55 X = -6408995
32
Y = -6442371
48 feet Y = -1963634
83 meter
Z = 3416210
24 Z = 1041260
88
XDOT = 7045
954550 XDOT = 2147
606947
YDOT = -12683
522703 feet/sec YDOT = -3865
937720 meter/sec
ZDOT = 19350
109931 ZDOT = 5897
913507
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 18185
56229313
00016717 00000-0 10270-3 0 9023
2 25544 51
6412 292
1078 0003733 263
9719 96
1008 15
54009489 1216
Satellite: ISS
Catalog Number: 25544
Epoch time: 18185
56229313 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 292
1078 deg
Eccentricity:
0003733
Arg of perigee: 263
9719 deg
Mean anomaly: 96
1008 deg
Mean motion: 15
54009489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 121
Checksum: 303
Coasting Arc #4 (Orbit 135)
---------------------------------------
Vector Time (GMT): 2018/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3691106
00 A = 6786751
16 meter
Y = 5065242
88 meter E =
0003190
Z = -2599008
21 I = 51
28821
XDOT = -2922
550240 Wp = 174
83463
YDOT = -4802
022298 meter/sec RA = 286
66896 deg
ZDOT = -5211
748554 TA = 34
56544
MA = 34
54470
Ha = 219
779 n
mi
Hp = 216
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12109927
81 X = -3734848
08
Y = 16618250
92 feet Y = 5023722
03 meter
Z = -8526929
82 Z = -2617044
00
XDOT = -9588
419423 XDOT = -2843
319751
YDOT = -15754
666333 feet/sec YDOT = -4834
260814 meter/sec
ZDOT = -17098
912579 ZDOT = -5225
753174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18840841
52 X = 5742688
49
Y = 8151336
26 feet Y = 2484527
29 meter
Z = -8608342
21 Z = -2623822
71
XDOT = -12724
369369 XDOT = -3878
387784
YDOT = 11300
311569 feet/sec YDOT = 3444
334966 meter/sec
ZDOT = -17160
851661 ZDOT = -5230
627586
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 18186
52689592
00016717 00000-0 10270-3 0 9030
2 25544 51
6407 287
3005 0003757 267
5989 92
4734 15
54010783 1361
Satellite: ISS
Catalog Number: 25544
Epoch time: 18186
52689592 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 287
3005 deg
Eccentricity:
0003757
Arg of perigee: 267
5989 deg
Mean anomaly: 92
4734 deg
Mean motion: 15
54010783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 136
Checksum: 335
Coasting Arc #5 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2018/187/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2058942
54 A = 6783026
07 meter
Y = -5127529
78 meter E =
0003028
Z = -3937744
74 I = 51
26581
XDOT = 4403
568959 Wp = 119
32429
YDOT = -4835
349041 meter/sec RA = 282
98703 deg
ZDOT = 3994
707213 TA = 192
60296
MA = 192
61053
Ha = 219
778 n
mi
Hp = 216
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6755060
84 X = -1982324
68
Y = -16822604
26 feet Y = -5150125
55 meter
Z = -12919110
05 Z = -3947560
69
XDOT = 14447
404720 XDOT = 4437
907791
YDOT = -15864
006040 feet/sec YDOT = -4785
913645 meter/sec
ZDOT = 13105
994792 ZDOT = 4016
181103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7975544
76 X = -2430946
04
Y = -16245134
54 feet Y = -4951517
01 meter
Z = -12962274
30 Z = -3950901
21
XDOT = 11879
560439 XDOT = 3620
890022
YDOT = -16364
688032 feet/sec YDOT = -4987
956912 meter/sec
ZDOT = 13202
743588 ZDOT = 4024
196246
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 18187
23426875
00016717 00000-0 10270-3 0 9043
2 25544 51
6371 283
7759 0003806 276
7347 83
3372 15
54021328 1478
Satellite: ISS
Catalog Number: 25544
Epoch time: 18187
23426875 = yrday
fracday
Element set: 904
Inclination: 51
6371 deg
RA of node: 283
7759 deg
Eccentricity:
0003806
Arg of perigee: 276
7347 deg
Mean anomaly: 83
3372 deg
Mean motion: 15
54021328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 147
Checksum: 325
Coasting Arc #6 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2018/188/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1268047
10 A = 6786591
17 meter
Y = 6123316
56 meter E =
0009510
Z = 2625964
01 I = 51
27251
XDOT = -4652
139428 Wp = 102
72201
YDOT = 3195
782386 meter/sec RA = 277
98011 deg
ZDOT = -5191
692918 TA = 47
52212
MA = 47
44178
Ha = 219
699 n
mi
Hp = 216
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4160259
51 X = 1186724
72
Y = 20089621
25 feet Y = 6137041
78 meter
Z = 8615367
49 Z = 2631926
80
XDOT = -15262
924634 XDOT = -4662
311335
YDOT = 10484
850349 feet/sec YDOT = 3143
702577 meter/sec
ZDOT = -17033
113249 ZDOT = -5214
315756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6013100
65 X = 1832793
08
Y = 19603522
00 feet Y = 5975153
51 meter
Z = 8641165
65 Z = 2633827
29
XDOT = -12643
567615 XDOT = -3853
759409
YDOT = 11451
194490 feet/sec YDOT = 3490
324081 meter/sec
ZDOT = -17134
758152 ZDOT = -5222
674285
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 18188
26317242
00016717 00000-0 10270-3 0 9055
2 25544 51
6379 278
6473 0004075 282
4477 77
6220 15
54059046 1633
Satellite: ISS
Catalog Number: 25544
Epoch time: 18188
26317242 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 278
6473 deg
Eccentricity:
0004075
Arg of perigee: 282
4477 deg
Mean anomaly: 77
6220 deg
Mean motion: 15
54059046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 163
Checksum: 322
Coasting Arc #7 (Orbit 177)
---------------------------------------
Vector Time (GMT): 2018/189/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -508733
37 A = 6789141
95 meter
Y = -6680104
26 meter E =
0008704
Z = -1066781
71 I = 51
27644
XDOT = 4772
795630 Wp = 14
82172
YDOT = -1296
324579 meter/sec RA = 272
98041 deg
ZDOT = 5860
294155 TA = 333
54998
MA = 333
59438
Ha = 219
852 n
mi
Hp = 216
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1669072
75 X = -428814
94
Y = -21916352
55 feet Y = -6685346
29 meter
Z = -3499940
00 Z = -1069059
59
XDOT = 15658
778315 XDOT = 4758
470554
YDOT = -4253
033397 feet/sec YDOT = -1243
032632 meter/sec
ZDOT = 19226
686860 ZDOT = 5883
443804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4114573
53 X = -1254122
01
Y = -21589760
78 feet Y = -6580559
09 meter
Z = -3509188
92 Z = -1069600
78
XDOT = 13375
969504 XDOT = 4076
995505
YDOT = -5681
099767 feet/sec YDOT = -1731
599209 meter/sec
ZDOT = 19330
417302 ZDOT = 5891
911194
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 18189
22776959
00016717 00000-0 10270-3 0 9067
2 25544 51
6372 273
8384 0003808 284
0531 76
0198 15
54025370 1782
Satellite: ISS
Catalog Number: 25544
Epoch time: 18189
22776959 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 273
8384 deg
Eccentricity:
0003808
Arg of perigee: 284
0531 deg
Mean anomaly: 76
0198 deg
Mean motion: 15
54025370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 178
Checksum: 333
Coasting Arc #8 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2018/190/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -260958
25 A = 6789325
77 meter
Y = 6751523
66 meter E =
0007576
Z = -621196
76 I = 51
27669
XDOT = -4791
866997 Wp = 152
72327
YDOT = -728
537317 meter/sec RA = 267
98586 deg
ZDOT = -5940
618185 TA = 34
01591
MA = 33
96737
Ha = 219
940 n
mi
Hp = 216
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -856162
24 X = -333418
80
Y = 22150668
19 feet Y = 6748200
38 meter
Z = -2038047
11 Z = -622639
52
XDOT = -15721
348416 XDOT = -4754
507761
YDOT = -2390
214294 feet/sec YDOT = -781
913618 meter/sec
ZDOT = -19490
217142 ZDOT = -5963
804776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2048506
65 X = 624384
83
Y = 22071668
45 feet Y = 6727444
54 meter
Z = -2045439
63 Z = -623450
00
XDOT = -14160
975354 XDOT = -4316
265288
YDOT = -490
764434 feet/sec YDOT = -149
584999 meter/sec
ZDOT = -19593
833643 ZDOT = -5972
200494
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 18190
25666785
00016717 00000-0 10270-3 0 9078
2 25544 51
6371 268
7101 0003792 291
8721 68
2028 15
54072341 1943
Satellite: ISS
Catalog Number: 25544
Epoch time: 18190
25666785 = yrday
fracday
Element set: 907
Inclination: 51
6371 deg
RA of node: 268
7101 deg
Eccentricity:
0003792
Arg of perigee: 291
8721 deg
Mean anomaly: 68
2028 deg
Mean motion: 15
54072341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 194
Checksum: 315
Coasting Arc #9 (Orbit 209)
---------------------------------------
Vector Time (GMT): 2018/191/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 944270
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1021804
58 A = 6787491
16 meter
Y = -6323062
01 meter E =
0011255
Z = 2227046
05 I = 51
27153
XDOT = 4713
733005 Wp = 59
74211
YDOT = 2678
151678 meter/sec RA = 262
98843 deg
ZDOT = 5426
106117 TA = 325
15429
MA = 325
22792
Ha = 219
969 n
mi
Hp = 216
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3352377
22 X = 1081617
06
Y = -20744954
11 feet Y = -6311301
39 meter
Z = 7306581
53 Z = 2232153
94
XDOT = 15465
003297 XDOT = 4657
077727
YDOT = 8786
586871 feet/sec YDOT = 2730
546300 meter/sec
ZDOT = 17802
185422 ZDOT = 5448
866560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 213568
31 X = 65095
62
Y = -21004732
18 feet Y = -6402242
37 meter
Z = 7330300
27 Z = 2234275
52
XDOT = 14941
579325 XDOT = 4554
193378
YDOT = 6417
114610 feet/sec YDOT = 1955
936533 meter/sec
ZDOT = 17903
636100 ZDOT = 5457
028283
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 18191
28556622
00016717 00000-0 10270-3 0 9081
2 25544 51
6362 263
5813 0003669 290
7729 69
3030 15
54033579 2109
Satellite: ISS
Catalog Number: 25544
Epoch time: 18191
28556622 = yrday
fracday
Element set: 908
Inclination: 51
6362 deg
RA of node: 263
5813 deg
Eccentricity:
0003669
Arg of perigee: 290
7729 deg
Mean anomaly: 69
3030 deg
Mean motion: 15
54033579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 210
Checksum: 314
Coasting Arc #10 (Orbit 218)
---------------------------------------
Vector Time (GMT): 2018/191/20:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 944252
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4346853
14 A = 6778834
67 meter
Y = -1319129
83 meter E =
0009302
Z = -5040003
46 I = 51
24767
XDOT = 148
925558 Wp = 97
89233
YDOT = -7440
198346 meter/sec RA = 259
82248 deg
ZDOT = 1820
534601 TA = 189
83938
MA = 189
85761
Ha = 220
102 n
mi
Hp = 216
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14261329
20 X = -4307297
62
Y = -4327853
76 feet Y = -1367517
36 meter
Z = -16535444
43 Z = -5061023
03
XDOT = 488
600912 XDOT = 223
269671
YDOT = -24410
099560 feet/sec YDOT = -7438
117565 meter/sec
ZDOT = 5972
882550 ZDOT = 1821
437407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11768338
44 X = 3586989
56
Y = -8972698
33 feet Y = -2734878
45 meter
Z = -16629300
83 Z = -5068610
89
XDOT = 18914
858391 XDOT = 5765
248838
YDOT = 13739
077612 feet/sec YDOT = 4187
670856 meter/sec
ZDOT = 5977
935098 ZDOT = 1822
074618
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 18191
86432034
00016717 00000-0 10270-3 0 9096
2 25544 51
6388 260
7002 0004009 297
3016 62
7728 15
53997091 2194
Satellite: ISS
Catalog Number: 25544
Epoch time: 18191
86432034 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 260
7002 deg
Eccentricity:
0004009
Arg of perigee: 297
3016 deg
Mean anomaly: 62
7728 deg
Mean motion: 15
53997091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 219
Checksum: 314
Coasting Arc #11 (Orbit 234)
---------------------------------------
Vector Time (GMT): 2018/192/20:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 944252
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4357359
93 A = 6781812
95 meter
Y = 2945341
49 meter E =
0007811
Z = 4279619
24 I = 51
26483
XDOT = -1090
794076 Wp = 48
99710
YDOT = 6728
878733 meter/sec RA = 254
80358 deg
ZDOT = -3511
130326 TA = 76
99240
MA = 76
90520
Ha = 220
178 n
mi
Hp = 216
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14295800
28 X = 4303312
52
Y = 9663193
88 feet Y = 2993765
58 meter
Z = 14040745
55 Z = 4300654
82
XDOT = -3578
720723 XDOT = -1148
902118
YDOT = 22076
373796 feet/sec YDOT = 6716
356408 meter/sec
ZDOT = -11519
456450 ZDOT = -3516
568982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16028537
92 X = -4885498
36
Y = 6180011
72 feet Y = 1883667
57 meter
Z = 14134467
96 Z = 4308185
83
XDOT = -15709
906834 XDOT = -4788
379603
YDOT = -14272
286391 feet/sec YDOT = -4350
192892 meter/sec
ZDOT = -11544
693023 ZDOT = -3518
822433
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 18192
89323748
00016717 00000-0 10270-3 0 9103
2 25544 51
6390 255
5724 0004067 302
5638 57
5121 15
54006738 2350
Satellite: ISS
Catalog Number: 25544
Epoch time: 18192
89323748 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 255
5724 deg
Eccentricity:
0004067
Arg of perigee: 302
5638 deg
Mean anomaly: 57
5121 deg
Mean motion: 15
54006738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 235
Checksum: 307
Coasting Arc #12 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2018/193/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 944252
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3345782
39 A = 6778413
67 meter
Y = 2894729
75 meter E =
0011448
Z = -5145496
18 I = 51
26019
XDOT = -3577
489155 Wp = 64
44730
YDOT = -6626
899016 meter/sec RA = 250
21240 deg
ZDOT = -1399
515833 TA = 191
99204
MA = 192
01933
Ha = 220
366 n
mi
Hp = 215
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10976976
35 X = -3352909
66
Y = 9497144
85 feet Y = 2857275
89 meter
Z = -16881549
15 Z = -5161765
43
XDOT = -11737
169144 XDOT = -3496
321456
YDOT = -21741
794671 feet/sec YDOT = -6666
450902 meter/sec
ZDOT = -4591
587378 ZDOT = -1416
697723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4962964
21 X = 1512711
49
Y = -13549263
88 feet Y = -4129815
63 meter
Z = -16954731
09 Z = -5167802
04
XDOT = 19728
224705 XDOT = 6013
162890
YDOT = 13076
839986 feet/sec YDOT = 3985
820828 meter/sec
ZDOT = -4667
596613 ZDOT = -1422
683448
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 18193
79353846
00016717 00000-0 10270-3 0 9116
2 25544 51
6371 251
0847 0004027 306
0901 53
9878 15
53996166 2490
Satellite: ISS
Catalog Number: 25544
Epoch time: 18193
79353846 = yrday
fracday
Element set: 911
Inclination: 51
6371 deg
RA of node: 251
0847 deg
Eccentricity:
0004027
Arg of perigee: 306
0901 deg
Mean anomaly: 53
9878 deg
Mean motion: 15
53996166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 330
Coasting Arc #13 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2018/194/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 944252
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4068075
52 A = 6777785
82 meter
Y = -1273056
27 meter E =
0003588
Z = 5270328
57 I = 51
27051
XDOT = 2854
369622 Wp = 350
79298
YDOT = 7100
523599 meter/sec RA = 245
18876 deg
ZDOT = -484
660436 TA = 103
87420
MA = 103
83428
Ha = 220
318 n
mi
Hp = 215
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13346704
47 X = 4056408
89
Y = -4176693
80 feet Y = -1227630
24 meter
Z = 17291104
22 Z = 5290060
95
XDOT = 9364
729732 XDOT = 2777
111651
YDOT = 23295
681098 feet/sec YDOT = 7132
011223 meter/sec
ZDOT = -1590
093295 ZDOT = -470
981785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9422149
24 X = -2871871
09
Y = 10185039
69 feet Y = 3104400
10 meter
Z = 17379575
57 Z = 5297294
63
XDOT = -18946
822625 XDOT = -5774
991536
YDOT = -14898
096927 feet/sec YDOT = -4540
939943 meter/sec
ZDOT = -1529
795549 ZDOT = -466
281683
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 18194
82245283
00016717 00000-0 10270-3 0 9127
2 25544 51
6372 245
9572 0004080 309
8952 50
1841 15
54003444 2650
Satellite: ISS
Catalog Number: 25544
Epoch time: 18194
82245283 = yrday
fracday
Element set: 912
Inclination: 51
6372 deg
RA of node: 245
9572 deg
Eccentricity:
0004080
Arg of perigee: 309
8952 deg
Mean anomaly: 50
1841 deg
Mean motion: 15
54003444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 301
Coasting Arc #14 (Orbit 279)
---------------------------------------
Vector Time (GMT): 2018/195/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 944252
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4700487
09 A = 6779467
32 meter
Y = -332256
49 meter E =
0008608
Z = -4881739
39 I = 51
29114
XDOT = -1903
883290 Wp = 94
54518
YDOT = -7050
595346 meter/sec RA = 240
16623 deg
ZDOT = 2315
935705 TA = 198
23055
MA = 198
26142
Ha = 220
492 n
mi
Hp = 215
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15421545
59 X = -4672710
00
Y = -1090080
34 feet Y = -384664
69 meter
Z = -16016205
35 Z = -4904504
78
XDOT = -6246
336252 XDOT = -1836
149429
YDOT = -23131
874494 feet/sec YDOT = -7071
507433 meter/sec
ZDOT = 7598
214254 ZDOT = 2306
851187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13725734
26 X = 4183603
80
Y = -6880675
94 feet Y = -2097230
03 meter
Z = -16118054
94 Z = -4912783
14
XDOT = 16722
060715 XDOT = 5096
884106
YDOT = 15673
742124 feet/sec YDOT = 4777
356599 meter/sec
ZDOT = 7558
444295 ZDOT = 2303
813821
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 18195
78705660
00016717 00000-0 10270-3 0 9134
2 25544 51
6374 241
1489 0004147 313
2380 46
8426 15
54005332 2801
Satellite: ISS
Catalog Number: 25544
Epoch time: 18195
78705660 = yrday
fracday
Element set: 913
Inclination: 51
6374 deg
RA of node: 241
1489 deg
Eccentricity:
0004147
Arg of perigee: 313
2380 deg
Mean anomaly: 46
8426 deg
Mean motion: 15
54005332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 280
Checksum: 299
Coasting Arc #15 (Orbit 295)
---------------------------------------
Vector Time (GMT): 2018/196/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 929538
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5168146
63 A = 6782774
85 meter
Y = 1834268
50 meter E =
0009451
Z = 3988659
71 I = 51
31962
XDOT = 720
873331 Wp = 55
94876
YDOT = 6543
678057 meter/sec RA = 235
15243 deg
ZDOT = -3931
383911 TA = 75
15849
MA = 75
05383
Ha = 220
610 n
mi
Hp = 215
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16955861
63 X = 5127876
87
Y = 6017941
29 feet Y = 1891836
77 meter
Z = 13086153
90 Z = 4013666
56
XDOT = 2365
069983 XDOT = 666
742698
YDOT = 21468
760029 feet/sec YDOT = 6551
437050 meter/sec
ZDOT = -12898
241178 ZDOT = -3928
013122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17515774
00 X = -5338807
91
Y = 3738766
02 feet Y = 1139575
88 meter
Z = 13197862
51 Z = 4022708
49
XDOT = -13088
926249 XDOT = -3989
504721
YDOT = -15703
250945 feet/sec YDOT = -4786
350888 meter/sec
ZDOT = -12883
959443 ZDOT = -3927
030838
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 18196
81596519
00016717 00000-0 10270-3 0 9141
2 25544 51
6372 236
0205 0004211 318
8230 41
2604 15
54023277 2967
Satellite: ISS
Catalog Number: 25544
Epoch time: 18196
81596519 = yrday
fracday
Element set: 914
Inclination: 51
6372 deg
RA of node: 236
0205 deg
Eccentricity:
0004211
Arg of perigee: 318
8230 deg
Mean anomaly: 41
2604 deg
Mean motion: 15
54023277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 296
Checksum: 292
Coasting Arc #16 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2018/197/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929538
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -682317
50 A = 6783845
74 meter
Y = -5626087
83 meter E =
0009527
Z = 3718773
12 I = 51
33747
XDOT = 6027
684283 Wp = 78
43394
YDOT = 2089
862559 meter/sec RA = 231
41720 deg
ZDOT = 4260
278061 TA = 326
20179
MA = 326
26248
Ha = 220
798 n
mi
Hp = 215
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2238574
47 X = -637417
78
Y = -18458293
40 feet Y = -5633467
19 meter
Z = 12200699
23 Z = 3715567
38
XDOT = 19775
867069 XDOT = 5983
173132
YDOT = 6856
504459 feet/sec YDOT = 2157
019104 meter/sec
ZDOT = 13977
290226 ZDOT = 4289
449887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13858175
19 X = -4223971
80
Y = 12409840
31 feet Y = 3782519
33 meter
Z = 12187030
66 Z = 3714606
94
XDOT = -4655
602219 XDOT = -1419
027556
YDOT = -19077
167200 feet/sec YDOT = -5814
720563 meter/sec
ZDOT = 14107
623436 ZDOT = 4300
003623
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 18197
58764615
00016717 00000-0 10270-3 0 9151
2 25544 51
6372 232
1734 0003868 323
3031 36
7856 15
54000692 3086
Satellite: ISS
Catalog Number: 25544
Epoch time: 18197
58764615 = yrday
fracday
Element set: 915
Inclination: 51
6372 deg
RA of node: 232
1734 deg
Eccentricity:
0003868
Arg of perigee: 323
3031 deg
Mean anomaly: 36
7856 deg
Mean motion: 15
54000692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 308
Checksum: 311
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