[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 3rd 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) : 74 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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
092/20:30:41
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
2
094/03:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
2
094/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
1
101/03:32:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 214
8
105/08:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 214
6
Coasting Arc #1 (Orbit 2674)
---------------------------------------
Vector Time (GMT): 2018/092/13:19:31
516
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3754663
80 A = 6786425
34 meter
Y = -5060641
17 meter E =
0003362
Z = -2517733
24 I = 51
87363
XDOT = 5356
846188 Wp = 135
01519
YDOT = -1332
207337 meter/sec RA = 35
15156 deg
ZDOT = -5317
508141 TA = 73
12691
MA = 73
09004
Ha = 220
324 n
mi
Hp = 215
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12318450
79 X = -3685565
34
Y = -16603153
45 feet Y = -5102242
34 meter
Z = -8260279
67 Z = -2535803
86
XDOT = 17574
954685 XDOT = 5397
175049
YDOT = -4370
758981 feet/sec YDOT = -1272
078507 meter/sec
ZDOT = -17445
892850 ZDOT = -5291
388103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18900448
11 X = -5760856
58
Y = -8297940
82 feet Y = -2529212
36 meter
Z = -8340167
51 Z = -2542083
06
XDOT = 12562
304940 XDOT = 3828
990546
YDOT = -11217
924426 feet/sec YDOT = -3419
223365 meter/sec
ZDOT = -17329
105349 ZDOT = -5281
911311
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 18092
58230647
00016717 00000-0 10270-3 0 9002
2 25544 51
6418 35
6273 0001906 298
9621 61
1340 15
54184119 26750
Satellite: ISS
Catalog Number: 25544
Epoch time: 18092
58230647 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 35
6273 deg
Eccentricity:
0001906
Arg of perigee: 298
9621 deg
Mean anomaly: 61
1340 deg
Mean motion: 15
54184119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2675
Checksum: 306
Coasting Arc #2 (Orbit 2679)
---------------------------------------
Vector Time (GMT): 2018/092/20:30:41
000
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1762651
79 A = 6777411
48 meter
Y = 3833765
82 meter E =
0001079
Z = 5302800
38 I = 51
83154
XDOT = -6609
344511 Wp = 110
34238
YDOT = -3847
092533 meter/sec RA = 33
64317 deg
ZDOT = 583
923597 TA = 334
09781
MA = 334
10321
Ha = 220
495 n
mi
Hp = 215
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5782978
33 X = -1831149
46
Y = 12577971
85 feet Y = 3813672
21 meter
Z = 17397639
05 Z = 5294071
17
XDOT = -21684
201150 XDOT = -6568
670475
YDOT = -12621
694661 feet/sec YDOT = -3920
775287 meter/sec
ZDOT = 1915
759832 ZDOT = 551
916594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12806509
74 X = 3903424
17
Y = -5386648
08 feet Y = -1641850
33 meter
Z = 17358092
91 Z = 5290746
72
XDOT = 7256
829501 XDOT = 2211
881632
YDOT = 22972
614647 feet/sec YDOT = 7002
052944 meter/sec
ZDOT = 1773
488374 ZDOT = 540
559256
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 18092
90380634
00016717 00000-0 10270-3 0 9011
2 25544 51
6385 34
0208 0001734 293
7468 66
3503 15
54139593 26805
Satellite: ISS
Catalog Number: 25544
Epoch time: 18092
90380634 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 34
0208 deg
Eccentricity:
0001734
Arg of perigee: 293
7468 deg
Mean anomaly: 66
3503 deg
Mean motion: 15
54139593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2680
Checksum: 310
Coasting Arc #3 (Orbit 2694)
---------------------------------------
Vector Time (GMT): 2018/093/20:30:41
000
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3316541
58 A = 6777831
42 meter
Y = -2843411
79 meter E =
0012326
Z = -5193021
37 I = 51
80642
XDOT = 6026
239934 Wp = 98
33324
YDOT = 4523
858266 meter/sec RA = 28
65527 deg
ZDOT = 1372
707259 TA = 184
84234
MA = 184
85427
Ha = 220
405 n
mi
Hp = 215
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10881041
92 X = 3373316
11
Y = -9328778
82 feet Y = -2806006
93 meter
Z = -17037471
68 Z = -5176772
46
XDOT = 19771
128392 XDOT = 5968
537080
YDOT = 14842
054679 feet/sec YDOT = 4590
925309 meter/sec
ZDOT = 4503
632740 ZDOT = 1401
840399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14417601
73 X = -4394485
01
Y = -191541
34 feet Y = -58381
80 meter
Z = -16964513
00 Z = -5170783
56
XDOT = -5140
332340 XDOT = -1566
773297
YDOT = -23109
009787 feet/sec YDOT = -7043
626183 meter/sec
ZDOT = 4632
958160 ZDOT = 1412
125647
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 18093
86830135
00016717 00000-0 10270-3 0 9024
2 25544 51
6396 29
2124 0001581 296
5493 63
5497 15
54191800 26955
Satellite: ISS
Catalog Number: 25544
Epoch time: 18093
86830135 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 29
2124 deg
Eccentricity:
0001581
Arg of perigee: 296
5493 deg
Mean anomaly: 63
5497 deg
Mean motion: 15
54191800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2695
Checksum: 323
Coasting Arc #4 (Orbit 2699)
---------------------------------------
Vector Time (GMT): 2018/094/03:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 906820
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1317632
60 A = 6777213
32 meter
Y = 4012583
89 meter E =
0000914
Z = 5299605
70 I = 51
79892
XDOT = -6998
790758 Wp = 105
80332
YDOT = -3080
763412 meter/sec RA = 27
25221 deg
ZDOT = 592
166730 TA = 338
55643
MA = 338
56026
Ha = 220
335 n
mi
Hp = 215
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4322941
62 X = -1388147
43
Y = 13164645
31 feet Y = 3997455
36 meter
Z = 17387157
80 Z = 5293033
44
XDOT = -22961
911935 XDOT = -6966
697120
YDOT = -10107
491510 feet/sec YDOT = -3158
849213 meter/sec
ZDOT = 1942
804233 ZDOT = 558
246890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9568531
03 X = -2916488
26
Y = -10073709
18 feet Y = -3070466
56 meter
Z = 17357204
96 Z = 5290476
07
XDOT = 18933
741121 XDOT = 5771
004294
YDOT = -14894
918850 feet/sec YDOT = -4539
971265 meter/sec
ZDOT = 1791
896597 ZDOT = 546
170083
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 18094
18979741
00016717 00000-0 10270-3 0 9038
2 25544 51
6421 27
6124 0001913 295
9259 64
1696 15
54207953 27000
Satellite: ISS
Catalog Number: 25544
Epoch time: 18094
18979741 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 27
6124 deg
Eccentricity:
0001913
Arg of perigee: 295
9259 deg
Mean anomaly: 64
1696 deg
Mean motion: 15
54207953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2700
Checksum: 322
Coasting Arc #5 (Orbit 2704)
---------------------------------------
Vector Time (GMT): 2018/094/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1143057
06 A = 6779445
90 meter
Y = 4697619
96 meter E =
0005651
Z = 4749207
16 I = 51
79585
XDOT = -7095
317723 Wp = 115
49740
YDOT = -1033
258344 meter/sec RA = 25
68889 deg
ZDOT = 2724
863957 TA = 307
60047
MA = 307
65176
Ha = 220
293 n
mi
Hp = 215
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3750187
21 X = 1067372
67
Y = 15412138
99 feet Y = 4709979
59 meter
Z = 15581388
32 Z = 4754575
62
XDOT = -23278
601452 XDOT = -7096
472290
YDOT = -3389
955197 feet/sec YDOT = -1112
609325 meter/sec
ZDOT = 8939
842380 ZDOT = 2690
394302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2792430
15 X = 851132
71
Y = 15590889
00 feet Y = 4752102
97 meter
Z = 15604618
17 Z = 4756287
62
XDOT = -21978
044295 XDOT = -6698
907901
YDOT = -4873
554625 feet/sec YDOT = -1485
459450 meter/sec
ZDOT = 8786
167195 ZDOT = 2678
023761
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 18094
51129578
00016717 00000-0 10270-3 0 9041
2 25544 51
6406 26
0107 0001978 304
2459 55
8506 15
54224204 27054
Satellite: ISS
Catalog Number: 25544
Epoch time: 18094
51129578 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 26
0107 deg
Eccentricity:
0001978
Arg of perigee: 304
2459 deg
Mean anomaly: 55
8506 deg
Mean motion: 15
54224204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2705
Checksum: 299
Coasting Arc #6 (Orbit 2719)
---------------------------------------
Vector Time (GMT): 2018/095/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 576460
28 A = 6777383
55 meter
Y = -4227976
81 meter E =
0013282
Z = -5276980
43 I = 51
75832
XDOT = 7328
875117 Wp = 77
21157
YDOT = 2056
594104 meter/sec RA = 20
70042 deg
ZDOT = -846
083648 TA = 184
69643
MA = 184
70891
Ha = 220
425 n
mi
Hp = 215
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1891273
90 X = 649328
83
Y = -13871315
01 feet Y = -4221123
31 meter
Z = -17312927
93 Z = -5274002
93
XDOT = 24044
865868 XDOT = 7309
442887
YDOT = 6747
355983 feet/sec YDOT = 2138
441926 meter/sec
ZDOT = -2775
864986 ZDOT = -810
529541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2530100
01 X = 771174
48
Y = -13786649
98 feet Y = -4202170
91 meter
Z = -17298978
20 Z = -5272728
55
XDOT = 22784
228042 XDOT = 6944
632707
YDOT = 7470
104314 feet/sec YDOT = 2276
887795 meter/sec
ZDOT = -2617
519643 ZDOT = -797
819987
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 18095
47578956
00016717 00000-0 10270-3 0 9056
2 25544 51
6405 21
2023 0001958 310
6961 49
4022 15
54191736 27206
Satellite: ISS
Catalog Number: 25544
Epoch time: 18095
47578956 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 21
2023 deg
Eccentricity:
0001958
Arg of perigee: 310
6961 deg
Mean anomaly: 49
4022 deg
Mean motion: 15
54191736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2720
Checksum: 306
Coasting Arc #7 (Orbit 2735)
---------------------------------------
Vector Time (GMT): 2018/096/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2334226
15 A = 6777575
03 meter
Y = 3627236
68 meter E =
0004075
Z = 5226888
73 I = 51
72849
XDOT = -7014
437373 Wp = 25
75202
YDOT = -2891
991998 meter/sec RA = 15
70794 deg
ZDOT = -1121
677814 TA = 75
00650
MA = 74
96139
Ha = 220
511 n
mi
Hp = 215
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7658222
28 X = -2400003
04
Y = 11900382
82 feet Y = 3600766
24 meter
Z = 17148585
07 Z = 5215389
86
XDOT = -23013
245974 XDOT = -6976
128451
YDOT = -9488
162723 feet/sec YDOT = -2970
218121 meter/sec
ZDOT = -3680
045320 ZDOT = -1155
658533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8016245
24 X = -2443351
55
Y = 11738147
96 feet Y = 3577787
50 meter
Z = 17096699
81 Z = 5211074
10
XDOT = -21930
952096 XDOT = -6684
554199
YDOT = -9378
167528 feet/sec YDOT = -2858
465462 meter/sec
ZDOT = -3831
228179 ZDOT = -1167
758349
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 18096
50457732
00016717 00000-0 10270-3 0 9060
2 25544 51
6411 16
0742 0002079 314
4310 45
6672 15
54205661 27367
Satellite: ISS
Catalog Number: 25544
Epoch time: 18096
50457732 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 16
0742 deg
Eccentricity:
0002079
Arg of perigee: 314
4310 deg
Mean anomaly: 45
6672 deg
Mean motion: 15
54205661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2736
Checksum: 291
Coasting Arc #8 (Orbit 2750)
---------------------------------------
Vector Time (GMT): 2018/097/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3964475
26 A = 6780106
42 meter
Y = -2974385
09 meter E =
0008528
Z = -4634740
95 I = 51
70486
XDOT = 6115
197661 Wp = 102
52604
YDOT = 3538
291891 meter/sec RA = 10
71577 deg
ZDOT = 2962
898430 TA = 196
98256
MA = 197
01112
Ha = 220
533 n
mi
Hp = 215
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13006808
60 X = 4019954
22
Y = -9758481
27 feet Y = -2929741
62 meter
Z = -15205843
02 Z = -4615347
94
XDOT = 20062
984451 XDOT = 6060
784768
YDOT = 11608
569195 feet/sec YDOT = 3606
372141 meter/sec
ZDOT = 9720
795374 ZDOT = 2992
471723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13141220
33 X = 4005443
96
Y = -9713487
26 feet Y = -2960670
92 meter
Z = -15118835
34 Z = -4608221
01
XDOT = 19249
050630 XDOT = 5867
110632
YDOT = 10721
352739 feet/sec YDOT = 3267
868315 meter/sec
ZDOT = 9852
199828 ZDOT = 3002
950507
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 18097
46906248
00016717 00000-0 10270-3 0 9078
2 25544 51
6411 11
2652 0002028 320
7817 39
3189 15
54207546 27514
Satellite: ISS
Catalog Number: 25544
Epoch time: 18097
46906248 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 11
2652 deg
Eccentricity:
0002028
Arg of perigee: 320
7817 deg
Mean anomaly: 39
3189 deg
Mean motion: 15
54207546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2751
Checksum: 306
Coasting Arc #9 (Orbit 2766)
---------------------------------------
Vector Time (GMT): 2018/098/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5330279
69 A = 6783933
92 meter
Y = 2264631
66 meter E =
0011181
Z = 3525387
21 I = 51
68513
XDOT = -4707
434637 Wp = 79
42418
YDOT = -4048
372169 meter/sec RA = 5
73196 deg
ZDOT = -4502
775377 TA = 59
06953
MA = 58
95967
Ha = 220
615 n
mi
Hp = 215
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17487794
25 X = -5372331
76
Y = 7429893
88 feet Y = 2204789
85 meter
Z = 11566231
01 Z = 3499392
26
XDOT = -15444
339361 XDOT = -4639
942620
YDOT = -13282
060923 feet/sec YDOT = -4100
636801 meter/sec
ZDOT = -14772
885094 ZDOT = -4525
478371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17460491
31 X = -5321957
75
Y = 7670425
97 feet Y = 2337945
84 meter
Z = 11449881
19 Z = 3489923
79
XDOT = -14967
406136 XDOT = -4562
065390
YDOT = -11798
746365 feet/sec YDOT = -3596
257892 meter/sec
ZDOT = -14873
545622 ZDOT = -4533
456705
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 18098
49784419
00016717 00000-0 10270-3 0 9087
2 25544 51
6411 6
1371 0002068 323
4210 36
6801 15
54207696 27670
Satellite: ISS
Catalog Number: 25544
Epoch time: 18098
49784419 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 6
1371 deg
Eccentricity:
0002068
Arg of perigee: 323
4210 deg
Mean anomaly: 36
6801 deg
Mean motion: 15
54207696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2767
Checksum: 311
Coasting Arc #10 (Orbit 2781)
---------------------------------------
Vector Time (GMT): 2018/099/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6274624
00 A = 6787349
03 meter
Y = -1548187
46 meter E =
0007511
Z = -2062261
12 I = 51
66429
XDOT = 2909
582002 Wp = 23
98750
YDOT = 4423
842640 meter/sec RA =
75528 deg
ZDOT = 5545
395694 TA = 313
20996
MA = 313
27267
Ha = 220
608 n
mi
Hp = 214
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20586036
73 X = 6301487
29
Y = -5079355
19 feet Y = -1477870
21 meter
Z = -6765948
56 Z = -2031715
83
XDOT = 9545
872710 XDOT = 2832
960521
YDOT = 14513
919423 feet/sec YDOT = 4455
951491 meter/sec
ZDOT = 18193
555425 ZDOT = 5559
343084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20463570
75 X = 6237296
36
Y = -5714536
87 feet Y = -1741790
84 meter
Z = -6629416
11 Z = -2020646
03
XDOT = 9452
525092 XDOT = 2881
129648
YDOT = 12725
122787 feet/sec YDOT = 3878
617426 meter/sec
ZDOT = 18255
085579 ZDOT = 5564
150084
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 18099
46232399
00016717 00000-0 10270-3 0 9091
2 25544 51
6416 1
3285 0002123 325
2693 34
8321 15
54212778 27824
Satellite: ISS
Catalog Number: 25544
Epoch time: 18099
46232399 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 1
3285 deg
Eccentricity:
0002123
Arg of perigee: 325
2693 deg
Mean anomaly: 34
8321 deg
Mean motion: 15
54212778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2782
Checksum: 309
Coasting Arc #11 (Orbit 2797)
---------------------------------------
Vector Time (GMT): 2018/100/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6731365
40 A = 6789069
72 meter
Y = 771273
20 meter E =
0010705
Z = 346641
52 I = 51
63803
XDOT = -853
496971 Wp = 127
56063
YDOT = -4698
455617 meter/sec RA = 355
78444 deg
ZDOT = -5999
272350 TA = 48
70315
MA = 48
61103
Ha = 220
627 n
mi
Hp = 214
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22084532
14 X = -6741173
50
Y = 2530423
88 feet Y = 695943
62 meter
Z = 1137275
31 Z = 313919
01
XDOT = -2800
186912 XDOT = -771
752829
YDOT = -15414
880632 feet/sec YDOT = -4707
543358 meter/sec
ZDOT = -19682
652067 ZDOT = -6003
219478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21944384
40 X = -6688648
37
Y = 3589511
51 feet Y = 1094083
11 meter
Z = 991161
07 Z = 302105
89
XDOT = -3146
325537 XDOT = -959
000024
YDOT = -13670
032174 feet/sec YDOT = -4166
625807 meter/sec
ZDOT = -19699
520474 ZDOT = -6004
413841
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 18100
49109861
00016717 00000-0 10270-3 0 9106
2 25544 51
6425 356
1995 0002074 330
3831 29
7204 15
54204256 27981
Satellite: ISS
Catalog Number: 25544
Epoch time: 18100
49109861 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 356
1995 deg
Eccentricity:
0002074
Arg of perigee: 330
3831 deg
Mean anomaly: 29
7204 deg
Mean motion: 15
54204256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2798
Checksum: 301
Coasting Arc #12 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2018/101/03:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2262570
54 A = 6777795
78 meter
Y = 3803319
31 meter E =
0003230
Z = 5131144
76 I = 51
57650
XDOT = -7186
758642 Wp = 106
25889
YDOT = 2196
048425 meter/sec RA = 352
36129 deg
ZDOT = 1539
540035 TA = 328
88817
MA = 328
90729
Ha = 220
634 n
mi
Hp = 214
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7423131
68 X = 2194948
23
Y = 12478081
73 feet Y = 3828243
23 meter
Z = 16834464
44 Z = 5141971
01
XDOT = -23578
604468 XDOT = -7218
259594
YDOT = 7204
883285 feet/sec YDOT = 2115
505129 meter/sec
ZDOT = 5050
984367 ZDOT = 1504
552579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14151460
17 X = -4313365
06
Y = 2988858
63 feet Y = 911004
11 meter
Z = 16882165
13 Z = 5145683
93
XDOT = 851
394727 XDOT = 259
505113
YDOT = -23646
299007 feet/sec YDOT = -7207
391937 meter/sec
ZDOT = 4894
548543 ZDOT = 1491
858396
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 18101
19837775
00016717 00000-0 10270-3 0 9117
2 25544 51
6409 352
6723 0001911 337
5221 22
5848 15
54227069 28099
Satellite: ISS
Catalog Number: 25544
Epoch time: 18101
19837775 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 352
6723 deg
Eccentricity:
0001911
Arg of perigee: 337
5221 deg
Mean anomaly: 22
5848 deg
Mean motion: 15
54227069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2809
Checksum: 310
Coasting Arc #13 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2018/102/03:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -453478
11 A = 6777196
53 meter
Y = -4213201
83 meter E =
0013927
Z = -5300983
99 I = 51
54174
XDOT = 7527
911193 Wp = 85
97641
YDOT = -1342
697831 meter/sec RA = 347
35620 deg
ZDOT = 425
109539 TA = 188
07724
MA = 188
09968
Ha = 220
692 n
mi
Hp = 214
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1487789
09 X = -380581
82
Y = -13822840
64 feet Y = -4217865
82 meter
Z = -17391679
75 Z = -5303009
40
XDOT = 24697
871368 XDOT = 7540
301156
YDOT = -4405
176611 feet/sec YDOT = -1258
446231 meter/sec
ZDOT = 1394
716335 ZDOT = 461
707779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13599435
51 X = 4145107
94
Y = 2836969
09 feet Y = 864708
18 meter
Z = -17400055
30 Z = -5303536
85
XDOT = -2996
194069 XDOT = -913
239952
YDOT = 23880
950190 feet/sec YDOT = 7278
913618 meter/sec
ZDOT = 1558
190365 ZDOT = 474
936423
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 18102
16285001
00016717 00000-0 10270-3 0 9125
2 25544 51
6410 347
8649 0001991 335
4048 24
7010 15
54208946 28241
Satellite: ISS
Catalog Number: 25544
Epoch time: 18102
16285001 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 347
8649 deg
Eccentricity:
0001991
Arg of perigee: 335
4048 deg
Mean anomaly: 24
7010 deg
Mean motion: 15
54208946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 290
Coasting Arc #14 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2018/103/03:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1356452
77 A = 6778923
31 meter
Y = 4502855
65 meter E =
0007606
Z = 4879943
82 I = 51
51523
XDOT = -7292
181903 Wp = 43
37251
YDOT = 359
158960 meter/sec RA = 342
34900 deg
ZDOT = -2350
777653 TA = 69
71849
MA = 69
63674
Ha = 220
759 n
mi
Hp = 214
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4450304
35 X = -1430408
40
Y = 14773148
45 feet Y = 4487273
82 meter
Z = 16010314
38 Z = 4873174
55
XDOT = -23924
481309 XDOT = -7284
237261
YDOT = 1178
343044 feet/sec YDOT = 277
656952 meter/sec
ZDOT = -7712
525109 ZDOT = -2386
181422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12876609
52 X = -3924790
58
Y = -8557593
89 feet Y = -2608354
62 meter
Z = 15979418
15 Z = 4870526
65
XDOT = 5014
552681 XDOT = 1528
435657
YDOT = -22288
461640 feet/sec YDOT = -6793
523108 meter/sec
ZDOT = -7870
502963 ZDOT = -2398
929303
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 18103
19161677
00016717 00000-0 10270-3 0 9132
2 25544 51
6403 342
7354 0002072 341
2740 18
8336 15
54243610 28405
Satellite: ISS
Catalog Number: 25544
Epoch time: 18103
19161677 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 342
7354 deg
Eccentricity:
0002072
Arg of perigee: 341
2740 deg
Mean anomaly: 18
8336 deg
Mean motion: 15
54243610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 281
Coasting Arc #15 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2018/104/03:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2973071
61 A = 6782527
96 meter
Y = -4646686
10 meter E =
0005903
Z = -3950987
19 I = 51
49538
XDOT = 6488
047902 Wp = 87
01626
YDOT = 747
791746 meter/sec RA = 337
34875 deg
ZDOT = 4008
201783 TA = 224
90413
MA = 224
95190
Ha = 220
885 n
mi
Hp = 214
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9754171
95 X = 3044003
12
Y = -15245033
14 feet Y = -4613042
96 meter
Z = -12962556
38 Z = -3936372
18
XDOT = 21286
246398 XDOT = 6459
733801
YDOT = 2453
384993 feet/sec YDOT = 820
187650 meter/sec
ZDOT = 13150
268316 ZDOT = 4039
649867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12065907
12 X = 3677688
49
Y = 13552603
49 feet Y = 4130833
54 meter
Z = -12896650
64 Z = -3930899
11
XDOT = -7036
375762 XDOT = -2144
687332
YDOT = 18894
436248 feet/sec YDOT = 5759
024168 meter/sec
ZDOT = 13290
417289 ZDOT = 4050
919190
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 18104
15608405
00016717 00000-0 10270-3 0 9145
2 25544 51
6397 337
9279 0002175 348
1926 11
9176 15
54215209 28550
Satellite: ISS
Catalog Number: 25544
Epoch time: 18104
15608405 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 337
9279 deg
Eccentricity:
0002175
Arg of perigee: 348
1926 deg
Mean anomaly: 11
9176 deg
Mean motion: 15
54215209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 319
Coasting Arc #16 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2018/105/03:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4309606
89 A = 6786217
11 meter
Y = 4563778
00 meter E =
0012844
Z = 2566541
84 I = 51
47670
XDOT = -5231
526847 Wp = 94
24787
YDOT = -1976
441627 meter/sec RA = 332
35570 deg
ZDOT = -5248
272662 TA = 56
82140
MA = 56
69828
Ha = 220
843 n
mi
Hp = 214
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14139130
21 X = -4372787
06
Y = 14973024
94 feet Y = 4515231
99 meter
Z = 8420412
88 Z = 2545453
14
XDOT = -17163
801992 XDOT = -5183
543268
YDOT = -6484
388539 feet/sec YDOT = -2034
676358 meter/sec
ZDOT = -17218
742330 ZDOT = -5273
569181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10943335
59 X = -3335528
69
Y = -17491045
38 feet Y = -5331270
63 meter
Z = 8325657
30 Z = 2537660
34
XDOT = 9272
051952 XDOT = 2826
121435
YDOT = -14085
074006 feet/sec YDOT = -4293
130557 meter/sec
ZDOT = -17331
255312 ZDOT = -5282
566619
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 18105
18484634
00016717 00000-0 10270-3 0 9156
2 25544 51
6383 332
7982 0002326 348
7103 11
3997 15
54260468 28710
Satellite: ISS
Catalog Number: 25544
Epoch time: 18105
18484634 = yrday
fracday
Element set: 915
Inclination: 51
6383 deg
RA of node: 332
7982 deg
Eccentricity:
0002326
Arg of perigee: 348
7103 deg
Mean anomaly: 11
3997 deg
Mean motion: 15
54260468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 320
Coasting Arc #17 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2018/105/08:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1787562
27 A = 6781099
44 meter
Y = -4912124
68 meter E =
0007570
Z = -4326543
61 I = 51
45600
XDOT = 6805
348341 Wp = 94
93004
YDOT = -577
888761 meter/sec RA = 331
25179 deg
ZDOT = 3472
427817 TA = 210
46008
MA = 210
50408
Ha = 220
842 n
mi
Hp = 214
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5864705
62 X = 1863374
48
Y = -16115894
62 feet Y = -4891711
43 meter
Z = -14194696
89 Z = -4317675
56
XDOT = 22327
258338 XDOT = 6794
437218
YDOT = -1895
960502 feet/sec YDOT = -501
847363 meter/sec
ZDOT = 11392
479715 ZDOT = 3505
459816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12191518
05 X = 3715974
70
Y = -12108937
09 feet Y = -3690804
02 meter
Z = -14154390
88 Z = -4314258
34
XDOT = 20097
232525 XDOT = 6125
636474
YDOT = 6762
828253 feet/sec YDOT = 2061
310052 meter/sec
ZDOT = 11539
882712 ZDOT = 3517
356251
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 18105
37774104
00016717 00000-0 10270-3 0 9162
2 25544 51
6412 331
8372 0002306 348
8440 11
2661 15
54246975 28746
Satellite: ISS
Catalog Number: 25544
Epoch time: 18105
37774104 = yrday
fracday
Element set: 916
Inclination: 51
6412 deg
RA of node: 331
8372 deg
Eccentricity:
0002306
Arg of perigee: 348
8440 deg
Mean anomaly: 11
2661 deg
Mean motion: 15
54246975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2874
Checksum: 302
Coasting Arc #18 (Orbit 2889)
---------------------------------------
Vector Time (GMT): 2018/106/08:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3231816
05 A = 6785083
15 meter
Y = 5106735
95 meter E =
0012695
Z = 3074680
76 I = 51
44069
XDOT = -5865
755477 Wp = 85
56591
YDOT = -761
556255 meter/sec RA = 326
25330 deg
ZDOT = -4882
272394 TA = 58
99152
MA = 58
86690
Ha = 220
936 n
mi
Hp = 214
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10603071
04 X = -3303616
20
Y = 16754383
05 feet Y = 5070194
34 meter
Z = 10087535
31 Z = 3058806
68
XDOT = -19244
604582 XDOT = -5833
087687
YDOT = -2498
544144 feet/sec YDOT = -826
968886 meter/sec
ZDOT = -16017
954048 ZDOT = -4910
687271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16546677
19 X = -5043427
21
Y = 10990032
21 feet Y = 3349761
82 meter
Z = 10015962
33 Z = 3052865
32
XDOT = -15679
629744 XDOT = -4779
151146
YDOT = -8838
363313 feet/sec YDOT = -2693
933138 meter/sec
ZDOT = -16144
550295 ZDOT = -4920
858930
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 18106
40650096
00016717 00000-0 10270-3 0 9171
2 25544 51
6411 326
7084 0002296 351
8917 8
2199 15
54230112 28905
Satellite: ISS
Catalog Number: 25544
Epoch time: 18106
40650096 = yrday
fracday
Element set: 917
Inclination: 51
6411 deg
RA of node: 326
7084 deg
Eccentricity:
0002296
Arg of perigee: 351
8917 deg
Mean anomaly: 8
2199 deg
Mean motion: 15
54230112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2890
Checksum: 300
Coasting Arc #19 (Orbit 2904)
---------------------------------------
Vector Time (GMT): 2018/107/08:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 928606
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4312681
55 A = 6788019
77 meter
Y = -5010972
96 meter E =
0010227
Z = -1516957
48 I = 51
42456
XDOT = 4574
742071 Wp = 28
10583
YDOT = 2205
271586 meter/sec RA = 321
26177 deg
ZDOT = 5745
882152 TA = 315
27194
MA = 315
35437
Ha = 220
950 n
mi
Hp = 214
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14149217
67 X = 4375763
80
Y = -16440200
01 feet Y = -4962392
96 meter
Z = -4976894
61 Z = -1495854
07
XDOT = 15008
996297 XDOT = 4521
831119
YDOT = 7235
142998 feet/sec YDOT = 2256
133980 meter/sec
ZDOT = 18851
319397 ZDOT = 5767
976447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19467263
77 X = 5933622
00
Y = -9614650
01 feet Y = -2930545
32 meter
Z = -4882024
53 Z = -1488041
08
XDOT = 10186
494274 XDOT = 3104
843455
YDOT = 11045
009860 feet/sec YDOT = 3366
519005 meter/sec
ZDOT = 18949
503104 ZDOT = 5775
808546
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 18107
37095978
00016717 00000-0 10270-3 0 9181
2 25544 51
6417 321
8991 0002406 355
1553 4
9576 15
54254835 29057
Satellite: ISS
Catalog Number: 25544
Epoch time: 18107
37095978 = yrday
fracday
Element set: 918
Inclination: 51
6417 deg
RA of node: 321
8991 deg
Eccentricity:
0002406
Arg of perigee: 355
1553 deg
Mean anomaly: 4
9576 deg
Mean motion: 15
54254835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2905
Checksum: 332
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