[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 11th 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 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
172/07:16:41
523 1
2 1
3 1
3
N/A 0
2 -0
1 220
4
000/00:03:23
046 0
5 -0
0 216
0
Coasting Arc #1 (Orbit 3762)
---------------------------------------
Vector Time (GMT): 2018/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5235482
67 A = 6781574
12 meter
Y = -665192
03 meter E =
0009747
Z = 4250276
47 I = 51
91515
XDOT = -2152
294462 Wp = 90
73607
YDOT = -6398
954566 meter/sec RA = 46
37436 deg
ZDOT = -3645
589415 TA = 36
42974
MA = 36
36345
Ha = 221
318 n
mi
Hp = 214
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17176780
42 X = -5248301
08
Y = -2182388
54 feet Y = -723811
04 meter
Z = 13944476
59 Z = 4224812
73
XDOT = -7061
333538 XDOT = -2062
871047
YDOT = -20993
945428 feet/sec YDOT = -6422
522525 meter/sec
ZDOT = -11960
595194 ZDOT = -3655
828311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5463843
50 X = -1665379
50
Y = 16526147
09 feet Y = 5037169
63 meter
Z = 13830614
93 Z = 4215571
43
XDOT = -20741
023339 XDOT = -6321
863914
YDOT = 3209
459166 feet/sec YDOT = 978
243154 meter/sec
ZDOT = -12005
396634 ZDOT = -3659
244894
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 18162
54155594
00016717 00000-0 10270-3 0 9003
2 25544 51
6429 46
8646 0002915 180
1668 179
9484 15
54199826 37631
Satellite: ISS
Catalog Number: 25544
Epoch time: 18162
54155594 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 46
8646 deg
Eccentricity:
0002915
Arg of perigee: 180
1668 deg
Mean anomaly: 179
9484 deg
Mean motion: 15
54199826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3763
Checksum: 348
Coasting Arc #2 (Orbit 3777)
---------------------------------------
Vector Time (GMT): 2018/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5767058
05 A = 6785477
24 meter
Y = 1943957
90 meter E =
0004173
Z = -3005696
47 I = 51
90402
XDOT = 647
005525 Wp = 105
76881
YDOT = 5781
955166 meter/sec RA = 41
40804 deg
ZDOT = 4985
582573 TA = 219
98969
MA = 220
02043
Ha = 221
155 n
mi
Hp = 214
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18920794
13 X = 5759491
82
Y = 6377814
64 feet Y = 2008407
28 meter
Z = -9861208
89 Z = -2977699
83
XDOT = 2122
721539 XDOT = 558
084408
YDOT = 18969
669180 feet/sec YDOT = 5788
692460 meter/sec
ZDOT = 16356
898204 ZDOT = 4988
510467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9610759
49 X = 2929359
49
Y = -17571445
88 feet Y = -5355776
70 meter
Z = -9736221
16 Z = -2967600
21
XDOT = 17748
686384 XDOT = 5409
799610
YDOT = 646
259360 feet/sec YDOT = 196
979853 meter/sec
ZDOT = 16369
063653 ZDOT = 4989
290601
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 18163
50606284
00016717 00000-0 10270-3 0 9018
2 25544 51
6425 42
0561 0002885 183
9960 176
1170 15
54168949 37782
Satellite: ISS
Catalog Number: 25544
Epoch time: 18163
50606284 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 42
0561 deg
Eccentricity:
0002885
Arg of perigee: 183
9960 deg
Mean anomaly: 176
1170 deg
Mean motion: 15
54168949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3778
Checksum: 324
Coasting Arc #3 (Orbit 3793)
---------------------------------------
Vector Time (GMT): 2018/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5917967
24 A = 6788477
36 meter
Y = -2989714
40 meter E =
0015350
Z = 1416573
31 I = 51
88769
XDOT = 1067
756103 Wp = 129
68856
YDOT = -4885
723852 meter/sec RA = 36
45080 deg
ZDOT = -5818
499757 TA = 34
91173
MA = 34
81116
Ha = 221
231 n
mi
Hp = 214
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19415903
03 X = -5890976
62
Y = -9808774
27 feet Y = -3055742
52 meter
Z = 4647550
23 Z = 1387890
66
XDOT = 3503
136821 XDOT = 1150
573681
YDOT = -16029
277731 feet/sec YDOT = -4873
319385 meter/sec
ZDOT = -19089
566131 ZDOT = -5813
112631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12768083
58 X = -3891711
87
Y = 17644764
46 feet Y = 5378124
21 meter
Z = 4519667
60 Z = 1377594
68
XDOT = -13965
729028 XDOT = -4256
754208
YDOT = -5194
652409 feet/sec YDOT = -1583
330054 meter/sec
ZDOT = -19064
652578 ZDOT = -5810
906106
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 18164
53486844
00016717 00000-0 10270-3 0 9021
2 25544 51
6418 36
9279 0003041 185
1091 175
0032 15
54146166 37946
Satellite: ISS
Catalog Number: 25544
Epoch time: 18164
53486844 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 36
9279 deg
Eccentricity:
0003041
Arg of perigee: 185
1091 deg
Mean anomaly: 175
0032 deg
Mean motion: 15
54146166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3794
Checksum: 311
Coasting Arc #4 (Orbit 3809)
---------------------------------------
Vector Time (GMT): 2018/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5656792
76 A = 6789064
44 meter
Y = 3735110
07 meter E =
0010407
Z = 292360
97 I = 51
86317
XDOT = -2833
424994 Wp = 57
77773
YDOT = 3808
095285 meter/sec RA = 31
49573 deg
ZDOT = 6021
056631 TA = 305
36272
MA = 305
45993
Ha = 220
947 n
mi
Hp = 214
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18559031
37 X = 5613185
17
Y = 12254298
14 feet Y = 3798124
35 meter
Z = 959189
54 Z = 319734
56
XDOT = -9296
013761 XDOT = -2905
044759
YDOT = 12493
750936 feet/sec YDOT = 3776
008409 meter/sec
ZDOT = 19754
122806 ZDOT = 6007
119551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14757458
08 X = 4498073
22
Y = -16630520
02 feet Y = -5068982
50 meter
Z = 1081086
41 Z = 329515
14
XDOT = 9822
216227 XDOT = 2993
811506
YDOT = 10024
560486 feet/sec YDOT = 3055
486036 meter/sec
ZDOT = 19691
113739 ZDOT = 6001
851468
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 18165
56366722
00016717 00000-0 10270-3 0 9038
2 25544 51
6418 31
7984 0002978 193
6487 166
4586 15
54203710 38109
Satellite: ISS
Catalog Number: 25544
Epoch time: 18165
56366722 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 31
7984 deg
Eccentricity:
0002978
Arg of perigee: 193
6487 deg
Mean anomaly: 166
4586 deg
Mean motion: 15
54203710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3810
Checksum: 331
Coasting Arc #5 (Orbit 3824)
---------------------------------------
Vector Time (GMT): 2018/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4920487
90 A = 6787480
52 meter
Y = -4217771
18 meter E =
0008547
Z = -2003499
78 I = 51
82835
XDOT = 4535
987569 Wp = 156
43156
YDOT = -2644
883855 meter/sec RA = 26
53758 deg
ZDOT = -5587
982536 TA = 45
63532
MA = 45
56532
Ha = 220
871 n
mi
Hp = 214
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16143333
00 X = -4863226
02
Y = -13837831
94 feet Y = -4272474
92 meter
Z = -6573162
00 Z = -2027263
41
XDOT = 14881
848981 XDOT = 4592
369634
YDOT = -8677
440470 feet/sec YDOT = -2593
843050 meter/sec
ZDOT = -18333
276038 ZDOT = -5565
811894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15735429
48 X = -4796158
90
Y = 14250925
92 feet Y = 4343682
22 meter
Z = -6678818
85 Z = -2035703
99
XDOT = -5703
943689 XDOT = -1738
562036
YDOT = -14819
461194 feet/sec YDOT = -4516
971772 meter/sec
ZDOT = -18233
606167 ZDOT = -5557
603160
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 18166
52816606
00016717 00000-0 10270-3 0 9047
2 25544 51
6413 26
9895 0002971 198
6714 161
4330 15
54158998 38257
Satellite: ISS
Catalog Number: 25544
Epoch time: 18166
52816606 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 26
9895 deg
Eccentricity:
0002971
Arg of perigee: 198
6714 deg
Mean anomaly: 161
4330 deg
Mean motion: 15
54158998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3825
Checksum: 338
Coasting Arc #6 (Orbit 3840)
---------------------------------------
Vector Time (GMT): 2018/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3780083
34 A = 6784017
21 meter
Y = 4432207
56 meter E =
0011573
Z = 3470133
78 I = 51
78576
XDOT = -5973
436774 Wp = 104
17565
YDOT = 1505
928131 meter/sec RA = 21
56991 deg
ZDOT = 4568
024687 TA = 296
46905
MA = 296
58772
Ha = 220
772 n
mi
Hp = 214
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12401848
21 X = 3713384
29
Y = 14541363
40 feet Y = 4474105
55 meter
Z = 11384953
36 Z = 3488334
71
XDOT = -19597
889677 XDOT = -6012
021389
YDOT = 4940
709091 feet/sec YDOT = 1438
912547 meter/sec
ZDOT = 14986
957633 ZDOT = 4538
914569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15782415
20 X = 4810480
15
Y = -10692422
79 feet Y = -3259050
47 meter
Z = 11465675
60 Z = 3494737
92
XDOT = 2017
420943 XDOT = 614
909903
YDOT = 18962
797478 feet/sec YDOT = 5779
860671 meter/sec
ZDOT = 14856
418918 ZDOT = 4528
236486
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 18167
55696172
00016717 00000-0 10270-3 0 9056
2 25544 51
6401 21
8599 0002801 201
9312 158
1721 15
54174726 38415
Satellite: ISS
Catalog Number: 25544
Epoch time: 18167
55696172 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 21
8599 deg
Eccentricity:
0002801
Arg of perigee: 201
9312 deg
Mean anomaly: 158
1721 deg
Mean motion: 15
54174726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3841
Checksum: 305
Coasting Arc #7 (Orbit 3855)
---------------------------------------
Vector Time (GMT): 2018/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2258673
04 A = 6780148
71 meter
Y = -4453223
05 meter E =
0008305
Z = -4594290
49 I = 51
74143
XDOT = 7016
638404 Wp = 83
35797
YDOT = -417
863600 meter/sec RA = 16
58978 deg
ZDOT = -3048
321879 TA = 156
21722
MA = 156
17882
Ha = 220
676 n
mi
Hp = 214
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7410344
62 X = -2186391
61
Y = -14610311
84 feet Y = -4478076
28 meter
Z = -15073131
53 Z = -4605087
31
XDOT = 23020
467206 XDOT = 7035
596565
YDOT = -1370
943568 feet/sec YDOT = -339
292277 meter/sec
ZDOT = -10001
056032 ZDOT = -3014
191846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15212081
58 X = -4636642
47
Y = 5960736
56 feet Y = 1816832
50 meter
Z = -15120711
20 Z = -4608792
77
XDOT = 1153
690407 XDOT = 351
644836
YDOT = -22006
464912 feet/sec YDOT = -6707
570505 meter/sec
ZDOT = -9848
235397 ZDOT = -3001
742149
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 18168
52145458
00016717 00000-0 10270-3 0 9061
2 25544 51
6396 17
0510 0002922 207
3867 152
7132 15
54191907 38569
Satellite: ISS
Catalog Number: 25544
Epoch time: 18168
52145458 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 17
0510 deg
Eccentricity:
0002922
Arg of perigee: 207
3867 deg
Mean anomaly: 152
7132 deg
Mean motion: 15
54191907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 314
Coasting Arc #8 (Orbit 3871)
---------------------------------------
Vector Time (GMT): 2018/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 523125
76 A = 6777690
93 meter
Y = 4305457
01 meter E =
0005073
Z = 5207454
33 I = 51
70154
XDOT = -7550
606339 Wp = 157
29652
YDOT = -565
362047 meter/sec RA = 11
59824 deg
ZDOT = 1220
975338 TA = 280
97110
MA = 281
02817
Ha = 220
673 n
mi
Hp = 215
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1716291
87 X = 449647
27
Y = 14125515
13 feet Y = 4310895
50 meter
Z = 17084823
91 Z = 5209817
51
XDOT = -24772
330508 XDOT = -7549
653925
YDOT = -1854
862360 feet/sec YDOT = -649
792952 meter/sec
ZDOT = 4005
824599 ZDOT = 1184
299725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14206321
34 X = 4330086
75
Y = -565028
82 feet Y = -172220
78 meter
Z = 17094683
96 Z = 5210459
67
XDOT = -3705
427843 XDOT = -1129
414406
YDOT = 23560
189777 feet/sec YDOT = 7181
145844 meter/sec
ZDOT = 3841
782455 ZDOT = 1170
975292
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 18169
55024550
00016717 00000-0 10270-3 0 9075
2 25544 51
6402 11
9213 0002841 209
1738 150
9257 15
54167124 38727
Satellite: ISS
Catalog Number: 25544
Epoch time: 18169
55024550 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 11
9213 deg
Eccentricity:
0002841
Arg of perigee: 209
1738 deg
Mean anomaly: 150
9257 deg
Mean motion: 15
54167124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3872
Checksum: 296
Coasting Arc #9 (Orbit 3886)
---------------------------------------
Vector Time (GMT): 2018/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1319262
57 A = 6777346
15 meter
Y = -4051688
97 meter E =
0013559
Z = -5281920
33 I = 51
66623
XDOT = 7481
192274 Wp = 106
72219
YDOT = 1459
811984 meter/sec RA = 6
59974 deg
ZDOT = 746
550488 TA = 170
42919
MA = 170
40334
Ha = 220
592 n
mi
Hp = 215
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4328289
28 X = 1390128
20
Y = -13292942
82 feet Y = -4036539
30 meter
Z = -17329134
94 Z = -5275340
15
XDOT = 24544
594076 XDOT = 7460
685922
YDOT = 4789
409396 feet/sec YDOT = 1543
357100 meter/sec
ZDOT = 2449
312626 ZDOT = 782
841581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13024607
60 X = -3969900
40
Y = -5180635
33 feet Y = -1579057
65 meter
Z = -17299015
84 Z = -5272740
03
XDOT = 5778
126135 XDOT = 1761
172846
YDOT = -23271
289956 feet/sec YDOT = -7093
089178 meter/sec
ZDOT = 2611
475277 ZDOT = 795
977664
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 18170
51473273
00016717 00000-0 10270-3 0 9084
2 25544 51
6383 7
1118 0002878 211
6859 148
4120 15
54204665 38877
Satellite: ISS
Catalog Number: 25544
Epoch time: 18170
51473273 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 7
1118 deg
Eccentricity:
0002878
Arg of perigee: 211
6859 deg
Mean anomaly: 148
4120 deg
Mean motion: 15
54204665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3887
Checksum: 315
Coasting Arc #10 (Orbit 3902)
---------------------------------------
Vector Time (GMT): 2018/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3073393
54 A = 6779525
61 meter
Y = 3696114
66 meter E =
0005010
Z = 4777019
73 I = 51
64099
XDOT = -6835
587777 Wp = 75
50945
YDOT = -2276
113295 meter/sec RA = 1
60327 deg
ZDOT = -2633
185117 TA = 40
47138
MA = 40
43413
Ha = 220
552 n
mi
Hp = 215
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10083312
12 X = -3137700
22
Y = 12126360
43 feet Y = 3661385
86 meter
Z = 15672636
92 Z = 4761934
47
XDOT = -22426
469084 XDOT = -6796
837056
YDOT = -7467
563305 feet/sec YDOT = -2352
336641 meter/sec
ZDOT = -8639
058784 ZDOT = -2666
295973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11722932
61 X = 3573149
86
Y = 10650121
74 feet Y = 3246157
11 meter
Z = 15604521
99 Z = 4756258
30
XDOT = -7554
535922 XDOT = -2302
622549
YDOT = 21207
053750 feet/sec YDOT = 6463
909983 meter/sec
ZDOT = -8786
843772 ZDOT = -2678
229982
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 18171
54351793
00016717 00000-0 10270-3 0 9091
2 25544 51
6388 1
9832 0003008 218
3228 141
7711 15
54196375 39036
Satellite: ISS
Catalog Number: 25544
Epoch time: 18171
54351793 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 1
9832 deg
Eccentricity:
0003008
Arg of perigee: 218
3228 deg
Mean anomaly: 141
7711 deg
Mean motion: 15
54196375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3903
Checksum: 311
Coasting Arc #11 (Orbit 3914)
---------------------------------------
Vector Time (GMT): 2018/172/07:18:23
046
Vector Time (MET): N/A
Weight (LBS) : 922898
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3221048
09 A = 6780867
65 meter
Y = -3793281
12 meter E =
0008432
Z = -4614431
30 I = 51
62040
XDOT = 6738
455145 Wp = 127
14486
YDOT = 2085
498127 meter/sec RA = 357
59336 deg
ZDOT = 2988
111188 TA = 172
70145
MA = 172
68917
Ha = 220
388 n
mi
Hp = 216
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10567743
08 X = 3285640
64
Y = -12445148
04 feet Y = -3756899
56 meter
Z = -15139210
30 Z = -4598628
05
XDOT = 22107
792469 XDOT = 6700
119075
YDOT = 6842
185455 feet/sec YDOT = 2160
637556 meter/sec
ZDOT = 9803
514395 ZDOT = 3020
751293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6256295
06 X = 1906918
74
Y = -15151654
05 feet Y = -4618224
15 meter
Z = -15067871
25 Z = -4592687
16
XDOT = 21972
289891 XDOT = 6697
153959
YDOT = -825
544582 feet/sec YDOT = -251
625988 meter/sec
ZDOT = 9949
215667 ZDOT = 3032
520935
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 18172
31510611
00016717 00000-0 10270-3 0 9105
2 25544 51
6425 358
1389 0003279 239
2473 120
8356 15
53968047 39154
Satellite: ISS
Catalog Number: 25544
Epoch time: 18172
31510611 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 358
1389 deg
Eccentricity:
0003279
Arg of perigee: 239
2473 deg
Mean anomaly: 120
8356 deg
Mean motion: 15
53968047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3915
Checksum: 313
Coasting Arc #12 (Orbit 3930)
---------------------------------------
Vector Time (GMT): 2018/173/07:18:23
046
Vector Time (MET): N/A
Weight (LBS) : 922898
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4625182
60 A = 6784502
28 meter
Y = 3447344
83 meter E =
0009444
Z = 3562128
68 I = 51
59926
XDOT = -5557
951327 Wp = 95
49030
YDOT = -2841
370029 meter/sec RA = 352
60517 deg
ZDOT = -4457
519164 TA = 42
40950
MA = 42
33655
Ha = 220
447 n
mi
Hp = 215
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15174483
59 X = -4680690
97
Y = 11310186
46 feet Y = 3395312
13 meter
Z = 11686773
87 Z = 3539526
63
XDOT = -18234
748447 XDOT = -5504
112963
YDOT = -9322
080146 feet/sec YDOT = -2903
221404 meter/sec
ZDOT = -14624
406706 ZDOT = -4484
387322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10697269
96 X = -3260527
88
Y = 15688222
31 feet Y = 4781770
16 meter
Z = 11585078
75 Z = 3531132
00
XDOT = -19048
172736 XDOT = -5805
883050
YDOT = -2077
675900 feet/sec YDOT = -633
275614 meter/sec
ZDOT = -14744
147703 ZDOT = -4494
016220
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 18173
34404652
00016717 00000-0 10270-3 0 9117
2 25544 51
6422 353
0114 0003105 242
5086 117
5751 15
53969592 39312
Satellite: ISS
Catalog Number: 25544
Epoch time: 18173
34404652 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 353
0114 deg
Eccentricity:
0003105
Arg of perigee: 242
5086 deg
Mean anomaly: 117
5751 deg
Mean motion: 15
53969592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3931
Checksum: 293
Coasting Arc #13 (Orbit 3945)
---------------------------------------
Vector Time (GMT): 2018/174/07:18:23
046
Vector Time (MET): N/A
Weight (LBS) : 922898
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5676289
76 A = 6787798
79 meter
Y = -3014271
29 meter E =
0003672
Z = -2177927
04 I = 51
57759
XDOT = 3996
892373 Wp = 18
81956
YDOT = 3572
330555 meter/sec RA = 347
62347 deg
ZDOT = 5478
865773 TA = 316
99721
MA = 317
02590
Ha = 220
241 n
mi
Hp = 216
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18622997
90 X = 5720153
55
Y = -9889341
49 feet Y = -2950549
60 meter
Z = -7145429
94 Z = -2150247
30
XDOT = 13113
163952 XDOT = 3930
035009
YDOT = 11720
244602 feet/sec YDOT = 3616
652122 meter/sec
ZDOT = 17975
281407 ZDOT = 5498
119373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14124493
79 X = 4305145
71
Y = -15712261
98 feet Y = -4789097
45 meter
Z = -7021096
33 Z = -2140030
16
XDOT = 15088
886377 XDOT = 4599
092568
YDOT = 5502
470892 feet/sec YDOT = 1677
153128 meter/sec
ZDOT = 18060
827290 ZDOT = 5504
940158
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 18174
30867509
00016717 00000-0 10270-3 0 9129
2 25544 51
6419 348
2037 0003244 247
4858 112
5951 15
53985954 39466
Satellite: ISS
Catalog Number: 25544
Epoch time: 18174
30867509 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 348
2037 deg
Eccentricity:
0003244
Arg of perigee: 247
4858 deg
Mean anomaly: 112
5951 deg
Mean motion: 15
53985954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3946
Checksum: 339
Coasting Arc #14 (Orbit 3961)
---------------------------------------
Vector Time (GMT): 2018/175/07:18:23
046
Vector Time (MET): N/A
Weight (LBS) : 922898
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6305672
28 A = 6789762
41 meter
Y = 2435865
34 meter E =
0011711
Z = 559680
69 I = 51
55199
XDOT = -2189
998378 Wp = 143
10748
YDOT = -4284
020421 meter/sec RA = 342
64769 deg
ZDOT = -5972
889678 TA = 30
84476
MA = 30
77601
Ha = 220
247 n
mi
Hp = 216
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20687901
17 X = -6335160
79
Y = 7991684
19 feet Y = 2365186
01 meter
Z = 1836222
74 Z = 528978
50
XDOT = -7185
034049 XDOT = -2112
917269
YDOT = -14055
185108 feet/sec YDOT = -4308
078731 meter/sec
ZDOT = -19596
094745 ZDOT = -5983
341310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16429408
38 X = -5007683
67
Y = 14913675
73 feet Y = 4545688
36 meter
Z = 1698470
35 Z = 517693
76
XDOT = -10558
676607 XDOT = -3218
284630
YDOT = -9372
292765 feet/sec YDOT = -2856
674835 meter/sec
ZDOT = -19642
142073 ZDOT = -5986
924904
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 18175
33761170
00016717 00000-0 10270-3 0 9131
2 25544 51
6421 343
0762 0003289 249
1016 110
9784 15
53941040 39623
Satellite: ISS
Catalog Number: 25544
Epoch time: 18175
33761170 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 343
0762 deg
Eccentricity:
0003289
Arg of perigee: 249
1016 deg
Mean anomaly: 110
9784 deg
Mean motion: 15
53941040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3962
Checksum: 298
Coasting Arc #15 (Orbit 3977)
---------------------------------------
Vector Time (GMT): 2018/176/07:18:23
046
Vector Time (MET): N/A
Weight (LBS) : 922898
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6470589
72 A = 6789170
34 meter
Y = -1718817
05 meter E =
0010599
Z = 1092643
54 I = 51
51931
XDOT = 309
792867 Wp = 50
72511
YDOT = 4920
341607 meter/sec RA = 337
66990 deg
ZDOT = 5873
888453 TA = 321
14885
MA = 321
22499
Ha = 220
041 n
mi
Hp = 216
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21228968
89 X = 6484021
60
Y = -5639163
56 feet Y = -1646383
52 meter
Z = 3584788
53 Z = 1124107
88
XDOT = 1016
380798 XDOT = 226
216910
YDOT = 16142
853040 feet/sec YDOT = 4923
337761 meter/sec
ZDOT = 19271
287575 ZDOT = 5875
191053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17523918
43 X = 5341290
34
Y = -13204184
92 feet Y = -4024635
56 meter
Z = 3725825
82 Z = 1135631
71
XDOT = 5935
991311 XDOT = 1809
290152
YDOT = 13345
310759 feet/sec YDOT = 4067
650719 meter/sec
ZDOT = 19276
301518 ZDOT = 5875
416703
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 18176
36654154
00016717 00000-0 10270-3 0 9149
2 25544 51
6419 337
9470 0003334 257
7784 102
2995 15
53995877 39788
Satellite: ISS
Catalog Number: 25544
Epoch time: 18176
36654154 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 337
9470 deg
Eccentricity:
0003334
Arg of perigee: 257
7784 deg
Mean anomaly: 102
2995 deg
Mean motion: 15
53995877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3978
Checksum: 361
Coasting Arc #16 (Orbit 3992)
---------------------------------------
Vector Time (GMT): 2018/177/07:18:23
046
Vector Time (MET): N/A
Weight (LBS) : 922898
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6189152
72 A = 6786725
93 meter
Y = 814405
32 meter E =
0003361
Z = -2658565
24 I = 51
47958
XDOT = 1513
362940 Wp = 167
50282
YDOT = -5432
875278 meter/sec RA = 332
68724 deg
ZDOT = -5191
829086 TA = 42
55081
MA = 42
52477
Ha = 220
006 n
mi
Hp = 216
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20305619
16 X = -6184885
72
Y = 2671933
47 feet Y = 745218
23 meter
Z = -8722326
92 Z = -2688619
53
XDOT = 4965
101510 XDOT = 1599
221541
YDOT = -17824
393957 feet/sec YDOT = -5415
470915 meter/sec
ZDOT = -17033
559995 ZDOT = -5184
270023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17577451
80 X = -5357607
31
Y = 10398309
64 feet Y = 3169404
78 meter
Z = -8856902
93 Z = -2699584
01
XDOT = -1562
072710 XDOT = -476
119762
YDOT = -17107
319799 feet/sec YDOT = -5214
311075 meter/sec
ZDOT = -16998
851120 ZDOT = -5181
249821
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 18177
33116380
00016717 00000-0 10270-3 0 9152
2 25544 51
6407 333
1396 0003392 260
6863 99
3906 15
53960695 39930
Satellite: ISS
Catalog Number: 25544
Epoch time: 18177
33116380 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 333
1396 deg
Eccentricity:
0003392
Arg of perigee: 260
6863 deg
Mean anomaly: 99
3906 deg
Mean motion: 15
53960695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3993
Checksum: 336
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