[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 26th 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) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
029/16:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
3
030/15:25:11
379 1
1 1
1 1
1
N/A -0
5 -0
1 222
1
000/00:00:22
759 0
0 -0
0 213
8
037/00:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
6
040/08:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
5
Coasting Arc #1 (Orbit 1647)
---------------------------------------
Vector Time (GMT): 2018/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2842202
12 A = 6778846
85 meter
Y = 3684912
12 meter E =
0010345
Z = 4924114
20 I = 51
65727
XDOT = -6951
644222 Wp = 53
18604
YDOT = -2333
085039 meter/sec RA = 4
46056 deg
ZDOT = -2257
207408 TA = 58
89576
MA = 58
79430
Ha = 222
082 n
mi
Hp = 213
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9324810
11 X = -2907115
13
Y = 12089606
70 feet Y = 3652765
60 meter
Z = 16155230
30 Z = 4910150
30
XDOT = -22807
231700 XDOT = -6914
074142
YDOT = -7654
478474 feet/sec YDOT = -2410
612965 meter/sec
ZDOT = -7405
536114 ZDOT = -2290
884625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15311804
62 X = -4667038
05
Y = -827562
35 feet Y = -252241
00 meter
Z = 16092418
09 Z = 4904969
03
XDOT = -6787
169942 XDOT = -2068
729398
YDOT = -21932
820076 feet/sec YDOT = -6685
123559 meter/sec
ZDOT = -7555
065139 ZDOT = -2302
783854
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 18026
54423545
00016717 00000-0 10270-3 0 9006
2 25544 51
6383 4
8323 0003746 45
2346 314
9111 15
54218410 16482
Satellite: ISS
Catalog Number: 25544
Epoch time: 18026
54423545 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 4
8323 deg
Eccentricity:
0003746
Arg of perigee: 45
2346 deg
Mean anomaly: 314
9111 deg
Mean motion: 15
54218410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1648
Checksum: 282
Coasting Arc #2 (Orbit 1662)
---------------------------------------
Vector Time (GMT): 2018/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4405701
50 A = 6782340
23 meter
Y = -3229279
88 meter E =
0009496
Z = -4027939
36 I = 51
63674
XDOT = 5823
882570 Wp = 86
60512
YDOT = 3055
875563 meter/sec RA = 359
46889 deg
ZDOT = 3928
673429 TA = 224
20280
MA = 224
27871
Ha = 222
124 n
mi
Hp = 213
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14454401
25 X = 4461050
15
Y = -10594750
28 feet Y = -3179702
67 meter
Z = -13215024
14 Z = -4006403
91
XDOT = 19107
226278 XDOT = 5770
194876
YDOT = 10025
838462 feet/sec YDOT = 3120
701858 meter/sec
ZDOT = 12889
348519 ZDOT = 3956
833273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17104430
62 X = 5213430
45
Y = 5581802
30 feet Y = 1701333
34 meter
Z = -13118584
08 Z = -3998544
43
XDOT = 3418
867141 XDOT = 1042
070705
YDOT = 20043
539052 feet/sec YDOT = 6109
270703 meter/sec
ZDOT = 13014
181897 ZDOT = 3966
722642
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 18027
50870908
00016717 00000-0 10270-3 0 9013
2 25544 51
6391
0238 0003865 48
4319 311
7165 15
54202593 16637
Satellite: ISS
Catalog Number: 25544
Epoch time: 18027
50870908 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node:
0238 deg
Eccentricity:
0003865
Arg of perigee: 48
4319 deg
Mean anomaly: 311
7165 deg
Mean motion: 15
54202593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1663
Checksum: 294
Coasting Arc #3 (Orbit 1678)
---------------------------------------
Vector Time (GMT): 2018/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5640966
24 A = 6786119
34 meter
Y = 2660931
06 meter E =
0016293
Z = 2659289
18 I = 51
61655
XDOT = -4225
351048 Wp = 91
47370
YDOT = -3731
662798 meter/sec RA = 354
48495 deg
ZDOT = -5201
831388 TA = 58
50351
MA = 58
34441
Ha = 222
132 n
mi
Hp = 213
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18507107
09 X = -5683219
48
Y = 8730088
77 feet Y = 2597613
51 meter
Z = 8724702
04 Z = 2631785
24
XDOT = -13862
700288 XDOT = -4158
041167
YDOT = -12242
988181 feet/sec YDOT = -3778
536941 meter/sec
ZDOT = -17066
375944 ZDOT = -5222
193097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18116849
02 X = -5522015
58
Y = -9624803
17 feet Y = -2933640
01 meter
Z = 8601792
48 Z = 2621826
35
XDOT = 855
794786 XDOT = 260
846251
YDOT = -17024
443745 feet/sec YDOT = -5189
050454 meter/sec
ZDOT = -17156
372403 ZDOT = -5229
262309
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 18028
53747723
00016717 00000-0 10270-3 0 9026
2 25544 51
6389 354
8941 0003899 50
9879 309
1620 15
54231034 16797
Satellite: ISS
Catalog Number: 25544
Epoch time: 18028
53747723 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 354
8941 deg
Eccentricity:
0003899
Arg of perigee: 50
9879 deg
Mean anomaly: 309
1620 deg
Mean motion: 15
54231034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1679
Checksum: 337
Coasting Arc #4 (Orbit 1693)
---------------------------------------
Vector Time (GMT): 2018/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6388587
64 A = 6788582
82 meter
Y = -2026101
34 meter E =
0013446
Z = -1045595
54 I = 51
59228
XDOT = 2325
953873 Wp = 42
92767
YDOT = 4320
841611 meter/sec RA = 349
50872 deg
ZDOT = 5893
132146 TA = 305
72769
MA = 305
85270
Ha = 222
126 n
mi
Hp = 213
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20959933
20 X = 6415848
09
Y = -6647314
10 feet Y = -1954507
30 meter
Z = -3430431
56 Z = -1014496
51
XDOT = 7631
082259 XDOT = 2248
839033
YDOT = 14175
989536 feet/sec YDOT = 4346
420534 meter/sec
ZDOT = 19334
423050 ZDOT = 5904
243531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18116591
04 X = 5521936
95
Y = 12499109
50 feet Y = 3809728
58 meter
Z = -3291631
16 Z = -1003289
18
XDOT = -5687
570756 XDOT = -1733
571566
YDOT = 13299
414346 feet/sec YDOT = 4053
661493 meter/sec
ZDOT = 19383
137244 ZDOT = 5907
980232
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18029
50194468
00016717 00000-0 10270-3 0 9037
2 25544 51
6388 350
0859 0003829 55
6272 304
5243 15
54237383 16944
Satellite: ISS
Catalog Number: 25544
Epoch time: 18029
50194468 = yrday
fracday
Element set: 903
Inclination: 51
6388 deg
RA of node: 350
0859 deg
Eccentricity:
0003829
Arg of perigee: 55
6272 deg
Mean anomaly: 304
5243 deg
Mean motion: 15
54237383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1694
Checksum: 325
Coasting Arc #5 (Orbit 1697)
---------------------------------------
Vector Time (GMT): 2018/029/16:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3123452
11 A = 6778467
06 meter
Y = 3386983
52 meter E =
0008284
Z = 4965174
14 I = 51
55555
XDOT = -6704
538913 Wp = 97
62137
YDOT = 3076
904898 meter/sec RA = 348
50195 deg
ZDOT = 2114
632511 TA = 331
75676
MA = 331
80166
Ha = 222
004 n
mi
Hp = 213
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10247546
28 X = 3061228
12
Y = 11112150
67 feet Y = 3421563
94 meter
Z = 16289941
40 Z = 4980195
51
XDOT = -21996
518743 XDOT = -6748
718955
YDOT = 10094
832341 feet/sec YDOT = 3001
683016 meter/sec
ZDOT = 6937
770705 ZDOT = 2081
957727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13637389
38 X = 4156676
28
Y = 6352148
48 feet Y = 1936134
86 meter
Z = 16356225
38 Z = 4985377
50
XDOT = -15991
727095 XDOT = -4874
278418
YDOT = 16809
818664 feet/sec YDOT = 5123
632729 meter/sec
ZDOT = 6791
773454 ZDOT = 2070
132549
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18029
75913524
00016717 00000-0 10270-3 0 9047
2 25544 51
6425 348
8049 0003801 55
4405 304
7106 15
54230138 16983
Satellite: ISS
Catalog Number: 25544
Epoch time: 18029
75913524 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 348
8049 deg
Eccentricity:
0003801
Arg of perigee: 55
4405 deg
Mean anomaly: 304
7106 deg
Mean motion: 15
54230138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1698
Checksum: 304
Coasting Arc #6 (Orbit 1711)
---------------------------------------
Vector Time (GMT): 2018/030/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1595115
91 A = 6777627
57 meter
Y = -3926720
88 meter E =
0017328
Z = -5303891
26 I = 51
52131
XDOT = 7251
803215 Wp = 80
66386
YDOT = -2423
149973 meter/sec RA = 343
81873 deg
ZDOT = -385
295604 TA = 185
64031
MA = 185
65985
Ha = 222
068 n
mi
Hp = 213
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5233319
91 X = -1525324
87
Y = -12882942
53 feet Y = -3944168
15 meter
Z = -17401218
04 Z = -5311470
21
XDOT = 23792
005299 XDOT = 7280
232084
YDOT = -7949
967102 feet/sec YDOT = -2341
896370 meter/sec
ZDOT = -1264
093188 ZDOT = -350
000811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5183374
15 X = -1579892
44
Y = -12858411
19 feet Y = -3919243
73 meter
Z = -17434280
28 Z = -5313968
63
XDOT = 22821
788623 XDOT = 6956
081172
YDOT = -7691
968991 feet/sec YDOT = -2344
512148 meter/sec
ZDOT = -1106
551245 ZDOT = -337
276820
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18030
65930037
00016717 00000-0 10270-3 0 9057
2 25544 51
6429 344
3161 0003058 49
3897 310
7521 15
54049216 17124
Satellite: ISS
Catalog Number: 25544
Epoch time: 18030
65930037 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 344
3161 deg
Eccentricity:
0003058
Arg of perigee: 49
3897 deg
Mean anomaly: 310
7521 deg
Mean motion: 15
54049216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1712
Checksum: 295
Coasting Arc #7 (Orbit 1727)
---------------------------------------
Vector Time (GMT): 2018/031/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -120612
39 A = 6778290
20 meter
Y = 4424101
73 meter E =
0007872
Z = 5129629
23 I = 51
49234
XDOT = -7357
760845 Wp = 52
97665
YDOT = 1561
053584 meter/sec RA = 338
81110 deg
ZDOT = -1513
096026 TA = 51
65620
MA = 51
58548
Ha = 222
033 n
mi
Hp = 213
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -395709
95 X = -194991
24
Y = 14514769
47 feet Y = 4422337
04 meter
Z = 16829492
22 Z = 5128862
75
XDOT = -24139
635318 XDOT = -7367
320521
YDOT = 5121
566875 feet/sec YDOT = 1478
720621 meter/sec
ZDOT = -4964
225808 ZDOT = -1548
859643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -183670
30 X = -55982
71
Y = 14523830
00 feet Y = 4426863
39 meter
Z = 16825324
80 Z = 5128359
00
XDOT = -22927
417628 XDOT = -6988
276893
YDOT = 5669
445875 feet/sec YDOT = 1728
047103 meter/sec
ZDOT = -5123
698836 ZDOT = -1561
703405
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18031
68819423
00016717 00000-0 10270-3 0 9067
2 25544 51
6427 339
1881 0003029 51
2703 308
8720 15
54081884 17282
Satellite: ISS
Catalog Number: 25544
Epoch time: 18031
68819423 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 339
1881 deg
Eccentricity:
0003029
Arg of perigee: 51
2703 deg
Mean anomaly: 308
8720 deg
Mean motion: 15
54081884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1728
Checksum: 313
Coasting Arc #8 (Orbit 1742)
---------------------------------------
Vector Time (GMT): 2018/032/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1727920
59 A = 6781176
70 meter
Y = -4812096
87 meter E =
0011232
Z = -4464937
83 I = 51
47120
XDOT = 6917
562930 Wp = 97
32360
YDOT = -522
532865 meter/sec RA = 333
80670 deg
ZDOT = 3245
867620 TA = 205
45030
MA = 205
50565
Ha = 222
099 n
mi
Hp = 213
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5669030
82 X = 1803290
02
Y = -15787719
37 feet Y = -4792352
75 meter
Z = -14648746
15 Z = -4456361
28
XDOT = 22695
416437 XDOT = 6907
125659
YDOT = -1714
346671 feet/sec YDOT = -445
234224 meter/sec
ZDOT = 10649
171980 ZDOT = 3279
444420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5138362
82 X = 1566172
99
Y = -16003999
53 feet Y = -4878019
06 meter
Z = -14609756
46 Z = -4453053
77
XDOT = 21372
505368 XDOT = 6514
339636
YDOT = -2979
047861 feet/sec YDOT = -908
013788 meter/sec
ZDOT = 10798
725185 ZDOT = 3291
451436
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18032
65278098
00016717 00000-0 10270-3 0 9073
2 25544 51
6426 334
3811 0002993 54
4604 305
6827 15
54046025 17433
Satellite: ISS
Catalog Number: 25544
Epoch time: 18032
65278098 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 334
3811 deg
Eccentricity:
0002993
Arg of perigee: 54
4604 deg
Mean anomaly: 305
6827 deg
Mean motion: 15
54046025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1743
Checksum: 310
Coasting Arc #9 (Orbit 1758)
---------------------------------------
Vector Time (GMT): 2018/033/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3155881
47 A = 6784917
90 meter
Y = 4999601
03 meter E =
0015315
Z = 3316743
87 I = 51
45517
XDOT = -6041
080563 Wp = 85
15910
YDOT = -697
870634 meter/sec RA = 328
80920 deg
ZDOT = -4676
211660 TA = 56
11800
MA = 55
97240
Ha = 222
168 n
mi
Hp = 213
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10353941
84 X = -3227664
37
Y = 16402890
52 feet Y = 4963908
59 meter
Z = 10881705
60 Z = 3301239
52
XDOT = -19819
818121 XDOT = -6010
113843
YDOT = -2289
601819 feet/sec YDOT = -765
253214 meter/sec
ZDOT = -15341
901772 ZDOT = -4705
481101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9479998
45 X = -2889503
53
Y = 16967726
96 feet Y = 5171763
18 meter
Z = 10811860
01 Z = 3295454
93
XDOT = -18578
994109 XDOT = -5662
877405
YDOT = -479
492180 feet/sec YDOT = -146
149216 meter/sec
ZDOT = -15472
069119 ZDOT = -4715
886667
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18033
68166780
00016717 00000-0 10270-3 0 9082
2 25544 51
6429 329
2533 0003089 58
5019 301
6435 15
54062024 17597
Satellite: ISS
Catalog Number: 25544
Epoch time: 18033
68166780 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 329
2533 deg
Eccentricity:
0003089
Arg of perigee: 58
5019 deg
Mean anomaly: 301
6435 deg
Mean motion: 15
54062024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1759
Checksum: 313
Coasting Arc #10 (Orbit 1773)
---------------------------------------
Vector Time (GMT): 2018/034/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4246056
59 A = 6788058
63 meter
Y = -4951453
03 meter E =
0010129
Z = -1868934
24 I = 51
43800
XDOT = 4815
600489 Wp = 44
76525
YDOT = 2020
905283 meter/sec RA = 323
81842 deg
ZDOT = 5612
169923 TA = 294
60921
MA = 294
71471
Ha = 222
139 n
mi
Hp = 213
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13930631
85 X = 4310187
59
Y = -16244924
64 feet Y = -4903612
25 meter
Z = -6131674
01 Z = -1848152
77
XDOT = 15799
214202 XDOT = 4765
383943
YDOT = 6630
266676 feet/sec YDOT = 2074
476206 meter/sec
ZDOT = 18412
630981 ZDOT = 5635
439807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12734041
29 X = 3881335
79
Y = -17231943
44 feet Y = -5252296
36 meter
Z = -6038362
70 Z = -1840492
95
XDOT = 14867
468098 XDOT = 4531
604276
YDOT = 4528
381314 feet/sec YDOT = 1380
250625 meter/sec
ZDOT = 18515
869994 ZDOT = 5643
637174
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18034
64624326
00016717 00000-0 10270-3 0 9095
2 25544 51
6427 324
4451 0003045 60
4455 299
7001 15
54069793 17742
Satellite: ISS
Catalog Number: 25544
Epoch time: 18034
64624326 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 324
4451 deg
Eccentricity:
0003045
Arg of perigee: 60
4455 deg
Mean anomaly: 299
7001 deg
Mean motion: 15
54069793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1774
Checksum: 311
Coasting Arc #11 (Orbit 1789)
---------------------------------------
Vector Time (GMT): 2018/035/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5006318
78 A = 6789613
07 meter
Y = 4574953
51 meter E =
0013918
Z = 186285
11 I = 51
41582
XDOT = -3355
283517 Wp = 121
37784
YDOT = -3414
539270 meter/sec RA = 318
83356 deg
ZDOT = -5990
039379 TA = 56
60917
MA = 56
47609
Ha = 222
188 n
mi
Hp = 213
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16424930
39 X = -5058009
93
Y = 15009690
00 feet Y = 4518680
41 meter
Z = 611171
61 Z = 161840
76
XDOT = -11008
148022 XDOT = -3287
755948
YDOT = -11202
556659 feet/sec YDOT = -3451
683182 meter/sec
ZDOT = -19652
360167 ZDOT = -6006
173632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14995763
01 X = -4570708
57
Y = 16441353
89 feet Y = 5011324
67 meter
Z = 501634
25 Z = 152898
12
XDOT = -10653
094033 XDOT = -3247
063061
YDOT = -9075
106453 feet/sec YDOT = -2766
092447 meter/sec
ZDOT = -19723
611173 ZDOT = -6011
756686
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18035
67512160
00016717 00000-0 10270-3 0 9103
2 25544 51
6416 319
3172 0002997 67
8887 292
2583 15
54027363 17906
Satellite: ISS
Catalog Number: 25544
Epoch time: 18035
67512160 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 319
3172 deg
Eccentricity:
0002997
Arg of perigee: 67
8887 deg
Mean anomaly: 292
2583 deg
Mean motion: 15
54027363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1790
Checksum: 323
Coasting Arc #12 (Orbit 1805)
---------------------------------------
Vector Time (GMT): 2018/036/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5359645
13 A = 6788481
14 meter
Y = -3884276
53 meter E =
0016765
Z = 1470814
32 I = 51
38837
XDOT = 1834
346707 Wp = 62
43924
YDOT = 4727
213575 meter/sec RA = 313
84643 deg
ZDOT = 5756
919434 TA = 313
67776
MA = 313
81658
Ha = 222
027 n
mi
Hp = 213
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17584137
57 X = 5395537
50
Y = -12743689
41 feet Y = -3824140
53 meter
Z = 4825506
29 Z = 1496936
61
XDOT = 6018
197859 XDOT = 1753
385759
YDOT = 15509
230888 feet/sec YDOT = 4747
274166 meter/sec
ZDOT = 18887
530951 ZDOT = 5765
632989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16072361
56 X = 4898855
80
Y = -14565062
19 feet Y = -4439430
95 meter
Z = 4942386
28 Z = 1506439
34
XDOT = 6472
755956 XDOT = 1972
896015
YDOT = 13611
197644 feet/sec YDOT = 4148
693042 meter/sec
ZDOT = 18925
546843 ZDOT = 5768
506678
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18036
70399236
00016717 00000-0 10270-3 0 9116
2 25544 51
6413 314
1884 0002886 67
2910 292
8547 15
54091088 18063
Satellite: ISS
Catalog Number: 25544
Epoch time: 18036
70399236 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 314
1884 deg
Eccentricity:
0002886
Arg of perigee: 67
2910 deg
Mean anomaly: 292
8547 deg
Mean motion: 15
54091088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1806
Checksum: 323
Coasting Arc #13 (Orbit 1810)
---------------------------------------
Vector Time (GMT): 2018/037/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4164431
81 A = 6778235
90 meter
Y = -1521874
89 meter E =
0016525
Z = -5141760
08 I = 51
34585
XDOT = 4102
297505 Wp = 78
52915
YDOT = -6297
075905 meter/sec RA = 312
01846 deg
ZDOT = -1459
492640 TA = 177
34566
MA = 177
33688
Ha = 222
082 n
mi
Hp = 213
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13662834
02 X = -4122128
70
Y = -4993027
85 feet Y = -1568208
18 meter
Z = -16869291
61 Z = -5161886
31
XDOT = 13458
981316 XDOT = 4179
497561
YDOT = -20659
697850 feet/sec YDOT = -6250
769629 meter/sec
ZDOT = -4788
361679 ZDOT = -1439
377543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6665420
04 X = 2031620
03
Y = 12812257
24 feet Y = 3905176
01 meter
Z = -16958614
34 Z = -5168985
65
XDOT = -22946
207647 XDOT = -6994
004091
YDOT = 5722
667172 feet/sec YDOT = 1744
268954 meter/sec
ZDOT = -4697
831742 ZDOT = -1431
899115
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18037
02551479
00016717 00000-0 10270-3 0 9122
2 25544 51
6416 312
5825 0002718 77
7067 282
4389 15
54060418 18114
Satellite: ISS
Catalog Number: 25544
Epoch time: 18037
02551479 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 312
5825 deg
Eccentricity:
0002718
Arg of perigee: 77
7067 deg
Mean anomaly: 282
4389 deg
Mean motion: 15
54060418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1811
Checksum: 310
Coasting Arc #14 (Orbit 1826)
---------------------------------------
Vector Time (GMT): 2018/038/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3065554
62 A = 6777449
39 meter
Y = 2946231
54 meter E =
0005498
Z = 5273379
49 I = 51
32281
XDOT = -4891
083373 Wp = 74
07991
YDOT = 5894
899399 meter/sec RA = 306
99777 deg
ZDOT = -448
286129 TA = 20
22289
MA = 20
20112
Ha = 221
914 n
mi
Hp = 213
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10057593
91 X = 3006766
28
Y = 9666113
98 feet Y = 2980184
20 meter
Z = 17301113
83 Z = 5288127
78
XDOT = -16046
861461 XDOT = -4954
460711
YDOT = 19340
221124 feet/sec YDOT = 5839
849564 meter/sec
ZDOT = -1470
755018 ZDOT = -472
199183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1090032
48 X = -332241
90
Y = -13825403
31 feet Y = -4213982
93 meter
Z = 17366276
14 Z = 5293240
97
XDOT = 23804
047390 XDOT = 7255
473644
YDOT = -3866
746794 feet/sec YDOT = -1178
584423 meter/sec
ZDOT = -1578
109380 ZDOT = -481
007739
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18038
05437959
00016717 00000-0 10270-3 0 9133
2 25544 51
6418 307
4538 0002788 79
3970 280
7497 15
54118220 18271
Satellite: ISS
Catalog Number: 25544
Epoch time: 18038
05437959 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 307
4538 deg
Eccentricity:
0002788
Arg of perigee: 79
3970 deg
Mean anomaly: 280
7497 deg
Mean motion: 15
54118220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1827
Checksum: 338
Coasting Arc #15 (Orbit 1841)
---------------------------------------
Vector Time (GMT): 2018/039/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1934996
91 A = 6779248
38 meter
Y = -4294608
77 meter E =
0014764
Z = -4889149
06 I = 51
30836
XDOT = 5307
719410 Wp = 102
00894
YDOT = -5013
619309 meter/sec RA = 301
97832 deg
ZDOT = 2306
198699 TA = 190
67438
MA = 190
70575
Ha = 222
106 n
mi
Hp = 213
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6348415
05 X = -1863081
03
Y = -14089923
79 feet Y = -4315845
28 meter
Z = -16040515
30 Z = -4898373
68
XDOT = 17413
777593 XDOT = 5352
186431
YDOT = -16448
882248 feet/sec YDOT = -4954
016047 meter/sec
ZDOT = 7566
268696 ZDOT = 2332
089572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4356200
72 X = -1327769
98
Y = 14783606
64 feet Y = 4506043
30 meter
Z = -16080887
63 Z = -4901454
55
XDOT = -22803
396586 XDOT = -6950
475280
YDOT = 1626
691828 feet/sec YDOT = 495
815669 meter/sec
ZDOT = 7682
273950 ZDOT = 2341
557100
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18039
01894019
00016717 00000-0 10270-3 0 9145
2 25544 51
6406 302
6468 0002947 82
8677 277
2811 15
54102038 18425
Satellite: ISS
Catalog Number: 25544
Epoch time: 18039
01894019 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 302
6468 deg
Eccentricity:
0002947
Arg of perigee: 82
8677 deg
Mean anomaly: 277
2811 deg
Mean motion: 15
54102038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1842
Checksum: 314
Coasting Arc #16 (Orbit 1857)
---------------------------------------
Vector Time (GMT): 2018/040/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 809159
65 A = 6782634
36 meter
Y = 5429528
13 meter E =
0013745
Z = 3973698
09 I = 51
30393
XDOT = -5434
361829 Wp = 80
10859
YDOT = 3708
971827 meter/sec RA = 296
96366 deg
ZDOT = -3947
219371 TA = 51
18832
MA = 51
06567
Ha = 222
010 n
mi
Hp = 213
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2654723
26 X = 729083
21
Y = 17813412
49 feet Y = 5438129
06 meter
Z = 13037067
21 Z = 3977434
04
XDOT = -17829
271091 XDOT = -5456
259430
YDOT = 12168
542739 feet/sec YDOT = 3648
078543 meter/sec
ZDOT = -12950
194786 ZDOT = -3973
670499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9302685
08 X = 2835458
41
Y = -15408232
61 feet Y = -4696429
30 meter
Z = 13052844
90 Z = 3978507
12
XDOT = 20312
841256 XDOT = 6191
354015
YDOT = 1154
200228 feet/sec YDOT = 351
800230 meter/sec
ZDOT = -13068
480501 ZDOT = -3983
272857
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18040
04779926
00016717 00000-0 10270-3 0 9150
2 25544 51
6412 297
5180 0002816 84
5861 275
5613 15
54120107 18589
Satellite: ISS
Catalog Number: 25544
Epoch time: 18040
04779926 = yrday
fracday
Element set: 915
Inclination: 51
6412 deg
RA of node: 297
5180 deg
Eccentricity:
0002816
Arg of perigee: 84
5861 deg
Mean anomaly: 275
5613 deg
Mean motion: 15
54120107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1858
Checksum: 313
Coasting Arc #17 (Orbit 1862)
---------------------------------------
Vector Time (GMT): 2018/040/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4437477
47 A = 6778175
38 meter
Y = -240096
93 meter E =
0016773
Z = -5133109
13 I = 51
28216
XDOT = 2097
414884 Wp = 78
96514
YDOT = -7213
175264 meter/sec RA = 295
28061 deg
ZDOT = -1476
757298 TA = 176
72680
MA = 176
71581
Ha = 222
147 n
mi
Hp = 213
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14558653
12 X = -4409529
28
Y = -787719
60 feet Y = -289563
68 meter
Z = -16840909
22 Z = -5154596
65
XDOT = 6881
282428 XDOT = 2185
091878
YDOT = -23665
273177 feet/sec YDOT = -7189
230328 meter/sec
ZDOT = -4845
004257 ZDOT = -1466
355851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2104628
14 X = 641490
66
Y = -14314919
31 feet Y = -4363187
41 meter
Z = -16936491
12 Z = -5162242
49
XDOT = 21891
927032 XDOT = 6672
659359
YDOT = 8891
083853 feet/sec YDOT = 2710
002359 meter/sec
ZDOT = -4797
596754 ZDOT = -1462
307491
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18040
36931885
00016717 00000-0 10270-3 0 9160
2 25544 51
6396 295
9162 0003013 80
6176 279
5317 15
54091464 18632
Satellite: ISS
Catalog Number: 25544
Epoch time: 18040
36931885 = yrday
fracday
Element set: 916
Inclination: 51
6396 deg
RA of node: 295
9162 deg
Eccentricity:
0003013
Arg of perigee: 80
6176 deg
Mean anomaly: 279
5317 deg
Mean motion: 15
54091464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1863
Checksum: 326
Coasting Arc #18 (Orbit 1878)
---------------------------------------
Vector Time (GMT): 2018/041/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3794419
65 A = 6777472
62 meter
Y = 1927297
64 meter E =
0005699
Z = 5269941
07 I = 51
26690
XDOT = -2977
504925 Wp = 76
11094
YDOT = 7058
392238 meter/sec RA = 290
25674 deg
ZDOT = -435
779987 TA = 18
07432
MA = 18
05407
Ha = 221
994 n
mi
Hp = 213
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12448883
38 X = 3746987
93
Y = 6323154
97 feet Y = 1969464
31 meter
Z = 17289832
91 Z = 5288257
50
XDOT = -9768
716947 XDOT = -3054
095731
YDOT = 23157
454850 feet/sec YDOT = 7024
667484 meter/sec
ZDOT = -1429
724368 ZDOT = -450
429550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7221675
51 X = -2201166
70
Y = 11831714
54 feet Y = 3606306
59 meter
Z = 17371046
08 Z = 5294694
85
XDOT = -21507
250905 XDOT = -6555
410076
YDOT = -10922
546966 feet/sec YDOT = -3329
192315 meter/sec
ZDOT = -1495
998972 ZDOT = -455
980487
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18041
39817303
00016717 00000-0 10270-3 0 9173
2 25544 51
6396 290
7885 0003027 81
7994 278
3502 15
54107745 18792
Satellite: ISS
Catalog Number: 25544
Epoch time: 18041
39817303 = yrday
fracday
Element set: 917
Inclination: 51
6396 deg
RA of node: 290
7885 deg
Eccentricity:
0003027
Arg of perigee: 81
7994 deg
Mean anomaly: 278
3502 deg
Mean motion: 15
54107745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1879
Checksum: 339
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