[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 16th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24007 8258 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
319/09:49:38
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
5
320/05:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
5
320/18:14:08
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
3
322/09:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 213
1
322/19:30:01
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
2
325/21:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
1
331/13:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
9
Coasting Arc #1 (Orbit 2188)
---------------------------------------
Vector Time (GMT): 2018/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6653409
74 A = 6789165
94 meter
Y = -250016
80 meter E =
0018939
Z = 1277317
72 I = 51
58923
XDOT = -945
993776 Wp = 55
38890
YDOT = 4893
241323 meter/sec RA = 349
09863 deg
ZDOT = 5834
347714 TA = 318
52399
MA = 318
66758
Ha = 222
936 n
mi
Hp = 213
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21828772
11 X = 6649506
39
Y = -820265
08 feet Y = -175635
62 meter
Z = 4190674
94 Z = 1309628
61
XDOT = -3103
654120 XDOT = -1028
981608
YDOT = 16053
941347 feet/sec YDOT = 4882
198323 meter/sec
ZDOT = 19141
560742 ZDOT = 5829
550969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12571047
44 X = -3831655
26
Y = 17829686
92 feet Y = 5434488
57 meter
Z = 4336002
03 Z = 1321613
42
XDOT = -9504
838048 XDOT = -2897
074637
YDOT = -11390
463387 feet/sec YDOT = -3471
813240 meter/sec
ZDOT = 19119
280440 ZDOT = 5827
556678
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 18318
56174389
00016717 00000-0 10270-3 0 9001
2 25544 51
6407 349
3636 0005250 46
1974 313
9612 15
53932334 21895
Satellite: ISS
Catalog Number: 25544
Epoch time: 18318
56174389 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 349
3636 deg
Eccentricity:
0005250
Arg of perigee: 46
1974 deg
Mean anomaly: 313
9612 deg
Mean motion: 15
53932334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2189
Checksum: 320
Coasting Arc #2 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2018/319/09:49:38
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3754994
83 A = 6779792
62 meter
Y = 2932559
55 meter E =
0009762
Z = 4815099
47 I = 51
52960
XDOT = -6185
776680 Wp = 91
41150
YDOT = 3781
673884 meter/sec RA = 344
56743 deg
ZDOT = 2516
084069 TA = 333
80775
MA = 333
85710
Ha = 222
672 n
mi
Hp = 213
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12319536
85 X = 3698533
55
Y = 9621258
35 feet Y = 2974234
67 meter
Z = 15797570
44 Z = 4833203
11
XDOT = -20294
542914 XDOT = -6239
826633
YDOT = 12407
066549 feet/sec YDOT = 3712
197949 meter/sec
ZDOT = 8254
868992 ZDOT = 2485
904165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14848325
70 X = -4525769
67
Y = -4615382
59 feet Y = -1406768
61 meter
Z = 15878548
42 Z = 4839781
56
XDOT = 14226
106562 XDOT = 4336
117280
YDOT = -17784
235469 feet/sec YDOT = -5420
634971 meter/sec
ZDOT = 8118
620620 ZDOT = 2474
555565
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 18319
46206342
00016717 00000-0 10270-3 0 9017
2 25544 51
6412 344
8759 0004853 48
4502 311
7066 15
53983942 22034
Satellite: ISS
Catalog Number: 25544
Epoch time: 18319
46206342 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 344
8759 deg
Eccentricity:
0004853
Arg of perigee: 48
4502 deg
Mean anomaly: 311
7066 deg
Mean motion: 15
53983942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 305
Coasting Arc #3 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2018/320/05:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4514259
13 A = 6786178
60 meter
Y = -4107286
99 meter E =
0009357
Z = -2967872
84 I = 51
52412
XDOT = 5353
339572 Wp = 59
01419
YDOT = 2297
551651 meter/sec RA = 340
43795 deg
ZDOT = 4979
411560 TA = 267
02601
MA = 267
13310
Ha = 222
907 n
mi
Hp = 213
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14810561
45 X = 4574268
99
Y = -13475351
01 feet Y = -4056469
82 meter
Z = -9737115
63 Z = -2945798
17
XDOT = 17563
450041 XDOT = 5303
062172
YDOT = 7537
899119 feet/sec YDOT = 2357
135207 meter/sec
ZDOT = 16336
652099 ZDOT = 5005
294483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20065139
86 X = -6115854
63
Y = -512214
24 feet Y = -156122
90 meter
Z = -9637273
21 Z = -2937440
87
XDOT = -7466
733386 XDOT = -2275
860336
YDOT = -16038
082525 feet/sec YDOT = -4888
407554 meter/sec
ZDOT = 16452
696886 ZDOT = 5014
782011
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 18320
23376777
00016717 00000-0 10270-3 0 9025
2 25544 51
6410 341
0279 0004853 53
0215 307
1381 15
53952722 22155
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
23376777 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 341
0279 deg
Eccentricity:
0004853
Arg of perigee: 53
0215 deg
Mean anomaly: 307
1381 deg
Mean motion: 15
53952722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 284
Coasting Arc #4 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2018/320/18:14:08
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4137892
71 A = 6779855
28 meter
Y = 2424560
94 meter E =
0010294
Z = 4783491
43 I = 51
48646
XDOT = -5639
982255 Wp = 91
90338
YDOT = 4518
393593 meter/sec RA = 337
82922 deg
ZDOT = 2583
448982 TA = 332
58854
MA = 332
64281
Ha = 222
730 n
mi
Hp = 213
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13575763
48 X = 4087237
06
Y = 7954596
24 feet Y = 2470550
44 meter
Z = 15693869
52 Z = 4803469
14
XDOT = -18503
878788 XDOT = -5702
638219
YDOT = 14824
125961 feet/sec YDOT = 4454
973034 meter/sec
ZDOT = 8475
882487 ZDOT = 2555
899402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7309795
70 X = 2228025
73
Y = 13832116
69 feet Y = 4216029
17 meter
Z = 15783343
46 Z = 4810763
09
XDOT = -22566
245023 XDOT = -6878
191483
YDOT = 2376
868698 feet/sec YDOT = 724
469579 meter/sec
ZDOT = 8351
371465 ZDOT = 2545
498023
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 18320
81254295
00016717 00000-0 10270-3 0 9030
2 25544 51
6402 338
1475 0005049 51
6763 308
4843 15
54003120 22248
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
81254295 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 338
1475 deg
Eccentricity:
0005049
Arg of perigee: 51
6763 deg
Mean anomaly: 308
4843 deg
Mean motion: 15
54003120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2224
Checksum: 282
Coasting Arc #5 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2018/321/18:14:08
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2698846
73 A = 6777937
81 meter
Y = -3331554
89 meter E =
0019268
Z = -5266264
26 I = 51
45020
XDOT = 6470
187764 Wp = 76
25027
YDOT = -4015
207837 meter/sec RA = 332
82104 deg
ZDOT = -773
627713 TA = 186
31184
MA = 186
33615
Ha = 222
939 n
mi
Hp = 213
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8854484
04 X = -2635810
64
Y = -10930298
20 feet Y = -3361382
81 meter
Z = -17277769
88 Z = -5279221
42
XDOT = 21227
650144 XDOT = 6518
363994
YDOT = -13173
254059 feet/sec YDOT = -3942
584331 meter/sec
ZDOT = -2538
148665 ZDOT = -742
080282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1959052
65 X = -597119
25
Y = -13857687
03 feet Y = -4223823
01 meter
Z = -17335549
06 Z = -5283875
35
XDOT = 23980
922806 XDOT = 7309
385271
YDOT = -384
589051 feet/sec YDOT = -117
222743 meter/sec
ZDOT = -2395
749329 ZDOT = -730
224395
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 18321
77716846
00016717 00000-0 10270-3 0 9042
2 25544 51
6410 333
3398 0005182 54
7190 305
4446 15
53991360 22397
Satellite: ISS
Catalog Number: 25544
Epoch time: 18321
77716846 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 333
3398 deg
Eccentricity:
0005182
Arg of perigee: 54
7190 deg
Mean anomaly: 305
4446 deg
Mean motion: 15
53991360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2239
Checksum: 313
Coasting Arc #6 (Orbit 2248)
---------------------------------------
Vector Time (GMT): 2018/322/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 917504
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4600962
10 A = 6780270
14 meter
Y = -1657978
09 meter E =
0016021
Z = -4711824
57 I = 51
43916
XDOT = 4747
919316 Wp = 67
01570
YDOT = -5332
297596 meter/sec RA = 329
63916 deg
ZDOT = -2761
282686 TA = 175
52056
MA = 175
50621
Ha = 222
974 n
mi
Hp = 213
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15095020
02 X = -4559192
21
Y = -5439560
67 feet Y = -1709195
71 meter
Z = -15458742
03 Z = -4734073
38
XDOT = 15577
163109 XDOT = 4820
606770
YDOT = -17494
414686 feet/sec YDOT = -5278
796651 meter/sec
ZDOT = -9059
326399 ZDOT = -2738
041973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15948230
97 X = 4861020
80
Y = -85305
03 feet Y = -26000
97 meter
Z = -15558528
43 Z = -4742239
46
XDOT = -8620
372087 XDOT = -2627
489412
YDOT = 20663
501196 feet/sec YDOT = 6298
235164 meter/sec
ZDOT = -8954
093389 ZDOT = -2729
207665
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 18322
42024845
00016717 00000-0 10270-3 0 9057
2 25544 51
6409 330
1335 0005088 59
7315 300
4340 15
53976072 22492
Satellite: ISS
Catalog Number: 25544
Epoch time: 18322
42024845 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 330
1335 deg
Eccentricity:
0005088
Arg of perigee: 59
7315 deg
Mean anomaly: 300
4340 deg
Mean motion: 15
53976072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2249
Checksum: 293
Coasting Arc #7 (Orbit 2255)
---------------------------------------
Vector Time (GMT): 2018/322/19:30:01
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5970593
78 A = 6785636
20 meter
Y = -882982
31 meter E =
0017770
Z = 3081284
98 I = 51
44645
XDOT = -1688
291634 Wp = 76
89826
YDOT = 5678
498726 meter/sec RA = 327
57929 deg
ZDOT = 4878
856716 TA = 318
65320
MA = 318
78759
Ha = 222
912 n
mi
Hp = 213
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19588562
28 X = 5965056
25
Y = -2896923
60 feet Y = -816245
94 meter
Z = 10109202
69 Z = 3110275
15
XDOT = -5539
014548 XDOT = -1775
364075
YDOT = 18630
245164 feet/sec YDOT = 5659
132240 meter/sec
ZDOT = 16006
747757 ZDOT = 4870
443919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19720626
79 X = 6010847
05
Y = 739164
49 feet Y = 225297
34 meter
Z = 10239650
01 Z = 3121045
32
XDOT = -8918
179791 XDOT = -2718
261200
YDOT = 15839
197786 feet/sec YDOT = 4827
787485 meter/sec
ZDOT = 15968
128971 ZDOT = 4867
085710
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 18322
87040472
00016717 00000-0 10270-3 0 9061
2 25544 51
6420 327
8915 0005238 57
9730 302
1931 15
53977839 22565
Satellite: ISS
Catalog Number: 25544
Epoch time: 18322
87040472 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 327
8915 deg
Eccentricity:
0005238
Arg of perigee: 57
9730 deg
Mean anomaly: 302
1931 deg
Mean motion: 15
53977839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2256
Checksum: 320
Coasting Arc #8 (Orbit 2270)
---------------------------------------
Vector Time (GMT): 2018/323/19:30:01
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5261558
45 A = 6781817
31 meter
Y = -279667
81 meter E =
0013620
Z = -4284091
63 I = 51
40586
XDOT = 3193
243621 Wp = 65
84752
YDOT = -5994
407024 meter/sec RA = 322
58125 deg
ZDOT = -3533
951484 TA = 167
97169
MA = 167
93913
Ha = 222
958 n
mi
Hp = 213
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17262330
89 X = -5237229
76
Y = -917545
31 feet Y = -338370
17 meter
Z = -14055418
75 Z = -4309591
94
XDOT = 10476
521066 XDOT = 3277
203880
YDOT = -19666
689710 feet/sec YDOT = -5958
228491 meter/sec
ZDOT = -11594
329016 ZDOT = -3518
235559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16774724
44 X = -5112936
01
Y = -3768857
21 feet Y = -1148747
68 meter
Z = -14170006
66 Z = -4319018
03
XDOT = 13410
804350 XDOT = 4087
613166
YDOT = -16408
900342 feet/sec YDOT = -5001
432824 meter/sec
ZDOT = -11522
845701 ZDOT = -3512
163370
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 18323
83502115
00016717 00000-0 10270-3 0 9076
2 25544 51
6414 323
0846 0005135 60
7492 299
4174 15
53999467 22717
Satellite: ISS
Catalog Number: 25544
Epoch time: 18323
83502115 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 323
0846 deg
Eccentricity:
0005135
Arg of perigee: 60
7492 deg
Mean anomaly: 299
4174 deg
Mean motion: 15
53999467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2271
Checksum: 317
Coasting Arc #9 (Orbit 2286)
---------------------------------------
Vector Time (GMT): 2018/324/19:30:01
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4267930
72 A = 6778847
60 meter
Y = 1542538
07 meter E =
0009253
Z = 5027953
41 I = 51
37027
XDOT = -4378
050487 Wp = 95
62846
YDOT = 6021
140691 meter/sec RA = 317
57109 deg
ZDOT = 1865
172998 TA = 336
22465
MA = 336
26737
Ha = 222
872 n
mi
Hp = 213
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14002397
37 X = 4225940
66
Y = 5060820
44 feet Y = 1590030
16 meter
Z = 16495910
15 Z = 5048584
11
XDOT = -14363
682699 XDOT = -4454
115433
YDOT = 19754
398593 feet/sec YDOT = 5971
756946 meter/sec
ZDOT = 6119
333983 ZDOT = 1843
720774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12977293
97 X = 3955479
20
Y = 7085759
16 feet Y = 2159739
39 meter
Z = 16588428
07 Z = 5056152
88
XDOT = -16683
861275 XDOT = -5085
240917
YDOT = 16428
178551 feet/sec YDOT = 5007
308822 meter/sec
ZDOT = 6022
072139 ZDOT = 1835
527588
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 18324
86394391
00016717 00000-0 10270-3 0 9086
2 25544 51
6414 317
9562 0005143 65
5009 294
6680 15
53994862 22870
Satellite: ISS
Catalog Number: 25544
Epoch time: 18324
86394391 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 317
9562 deg
Eccentricity:
0005143
Arg of perigee: 65
5009 deg
Mean anomaly: 294
6680 deg
Mean motion: 15
53994862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2287
Checksum: 340
Coasting Arc #10 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2018/325/19:30:01
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3124700
68 A = 6777673
34 meter
Y = -2868973
09 meter E =
0019657
Z = -5303008
86 I = 51
34272
XDOT = 5176
932095 Wp = 84
08159
YDOT = -5637
435805 meter/sec RA = 312
55281 deg
ZDOT = 1
480060 TA = 185
92096
MA = 185
94423
Ha = 222
957 n
mi
Hp = 212
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10251642
64 X = -3066626
86
Y = -9412641
36 feet Y = -2903590
72 meter
Z = -17398323
02 Z = -5318047
05
XDOT = 16984
685350 XDOT = 5239
579524
YDOT = -18495
524294 feet/sec YDOT = -5579
193470 meter/sec
ZDOT = 4
855840 ZDOT = 26
780410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8796094
89 X = -2681049
72
Y = -10676142
46 feet Y = -3254088
22 meter
Z = -17465518
46 Z = -5323490
03
XDOT = 18510
776473 XDOT = 5642
084669
YDOT = -15435
671238 feet/sec YDOT = -4704
792593 meter/sec
ZDOT = 119
352309 ZDOT = 36
378584
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 18325
82855421
00016717 00000-0 10270-3 0 9090
2 25544 51
6415 313
1480 0005093 67
1279 293
0411 15
54021372 23020
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
82855421 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 313
1480 deg
Eccentricity:
0005093
Arg of perigee: 67
1279 deg
Mean anomaly: 293
0411 deg
Mean motion: 15
54021372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 284
Coasting Arc #11 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2018/325/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4222118
90 A = 6778582
91 meter
Y = 1416279
16 meter E =
0008719
Z = 5103138
62 I = 51
34112
XDOT = -4030
866212 Wp = 95
27644
YDOT = 6338
596831 meter/sec RA = 312
09505 deg
ZDOT = 1572
700472 TA = 339
49197
MA = 339
52695
Ha = 222
910 n
mi
Hp = 213
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13852096
13 X = 4181178
84
Y = 4646585
16 feet Y = 1463264
68 meter
Z = 16742580
78 Z = 5123549
40
XDOT = -13224
626680 XDOT = -4109
086147
YDOT = 20795
921361 feet/sec YDOT = 6293
083458 meter/sec
ZDOT = 5159
778453 ZDOT = 1552
929684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14380310
08 X = 4383118
51
Y = -1898486
46 feet Y = -578658
67 meter
Z = 16834124
96 Z = 5131041
29
XDOT = -2849
170761 XDOT = -868
427248
YDOT = 23465
266235 feet/sec YDOT = 7152
213149 meter/sec
ZDOT = 5070
039369 ZDOT = 1545
348000
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 18325
95716927
00016717 00000-0 10270-3 0 9103
2 25544 51
6393 312
5051 0005119 68
2419 291
9278 15
53974234 23042
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
95716927 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 312
5051 deg
Eccentricity:
0005119
Arg of perigee: 68
2419 deg
Mean anomaly: 291
9278 deg
Mean motion: 15
53974234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 319
Coasting Arc #12 (Orbit 2318)
---------------------------------------
Vector Time (GMT): 2018/326/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3172781
99 A = 6777739
14 meter
Y = -2832635
82 meter E =
0019702
Z = -5294116
41 I = 51
31527
XDOT = 4803
917200 Wp = 87
22626
YDOT = -5950
496590 meter/sec RA = 307
07388 deg
ZDOT = 306
757285 TA = 185
70561
MA = 185
72808
Ha = 223
012 n
mi
Hp = 212
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10409389
73 X = -3115154
13
Y = -9293424
62 feet Y = -2867793
49 meter
Z = -17369148
34 Z = -5309389
34
XDOT = 15760
883202 XDOT = 4868
610170
YDOT = -19522
626606 feet/sec YDOT = -5896
414151 meter/sec
ZDOT = 1006
421538 ZDOT = 330
250402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13403473
34 X = -4085378
67
Y = -3562901
16 feet Y = -1085972
27 meter
Z = -17437404
84 Z = -5314920
99
XDOT = 4830
288312 XDOT = 1472
271877
YDOT = -23586
881628 feet/sec YDOT = -7189
281520 meter/sec
ZDOT = 1112
831277 ZDOT = 339
190973
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 18326
92177594
00016717 00000-0 10270-3 0 9113
2 25544 51
6375 307
6961 0005122 72
6732 287
4980 15
54012078 23194
Satellite: ISS
Catalog Number: 25544
Epoch time: 18326
92177594 = yrday
fracday
Element set: 911
Inclination: 51
6375 deg
RA of node: 307
6961 deg
Eccentricity:
0005122
Arg of perigee: 72
6732 deg
Mean anomaly: 287
4980 deg
Mean motion: 15
54012078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2319
Checksum: 321
Coasting Arc #13 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2018/327/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2045298
49 A = 6779317
60 meter
Y = 4173029
34 meter E =
0011203
Z = 4928460
01 I = 51
30190
XDOT = -5266
316989 Wp = 65
55959
YDOT = 5145
544670 meter/sec RA = 302
05354 deg
ZDOT = -2162
886868 TA = 45
65631
MA = 45
56455
Ha = 222
919 n
mi
Hp = 213
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6710296
88 X = 1974542
05
Y = 13691041
14 feet Y = 4195505
21 meter
Z = 16169488
22 Z = 4938224
13
XDOT = -17277
942878 XDOT = -5312
958078
YDOT = 16881
708234 feet/sec YDOT = 5086
392468 meter/sec
ZDOT = -7096
085525 ZDOT = -2188
582260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12286026
71 X = 3744780
94
Y = 8951175
72 feet Y = 2728318
36 meter
Z = 16212804
88 Z = 4941662
93
XDOT = -6562
923157 XDOT = -2000
378978
YDOT = 22121
282236 feet/sec YDOT = 6742
566825 meter/sec
ZDOT = -7212
278931 ZDOT = -2198
302618
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 18327
95068785
00016717 00000-0 10270-3 0 9129
2 25544 51
6380 302
5679 0004954 76
5539 283
6166 15
54002088 23352
Satellite: ISS
Catalog Number: 25544
Epoch time: 18327
95068785 = yrday
fracday
Element set: 912
Inclination: 51
6380 deg
RA of node: 302
5679 deg
Eccentricity:
0004954
Arg of perigee: 76
5539 deg
Mean anomaly: 283
6166 deg
Mean motion: 15
54002088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 335
Coasting Arc #14 (Orbit 2349)
---------------------------------------
Vector Time (GMT): 2018/328/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -975856
88 A = 6782494
80 meter
Y = -5320586
51 meter E =
0012164
Z = -4103218
17 I = 51
29581
XDOT = 5395
141744 Wp = 97
42598
YDOT = -3901
469779 meter/sec RA = 297
03733 deg
ZDOT = 3784
006210 TA = 211
82132
MA = 211
89487
Ha = 223
008 n
mi
Hp = 212
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3201630
18 X = -896356
39
Y = -17455992
50 feet Y = -5331054
27 meter
Z = -13462001
87 Z = -4107766
12
XDOT = 17700
596274 XDOT = 5419
987011
YDOT = -12800
097701 feet/sec YDOT = -3840
999046 meter/sec
ZDOT = 12414
718538 ZDOT = 3810
274401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11224931
40 X = -3421359
09
Y = -13727039
97 feet Y = -4184001
78 meter
Z = -13481724
41 Z = -4109229
60
XDOT = 8145
136501 XDOT = 2482
637605
YDOT = -18943
630991 feet/sec YDOT = -5774
018726 meter/sec
ZDOT = 12533
315039 ZDOT = 3820
154424
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 18328
91528938
00016717 00000-0 10270-3 0 9138
2 25544 51
6379 297
7588 0005085 81
0202 279
1526 15
54021174 23502
Satellite: ISS
Catalog Number: 25544
Epoch time: 18328
91528938 = yrday
fracday
Element set: 913
Inclination: 51
6379 deg
RA of node: 297
7588 deg
Eccentricity:
0005085
Arg of perigee: 81
0202 deg
Mean anomaly: 279
1526 deg
Mean motion: 15
54021174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2350
Checksum: 324
Coasting Arc #15 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2018/329/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -51283
28 A = 6786200
56 meter
Y = 6161736
41 meter E =
0018188
Z = 2825077
05 I = 51
29424
XDOT = -5297
181325 Wp = 95
09865
YDOT = 2286
848007 meter/sec RA = 292
03101 deg
ZDOT = -5057
393588 TA = 52
62158
MA = 52
45610
Ha = 222
930 n
mi
Hp = 212
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -168252
23 X = -133904
66
Y = 20215670
64 feet Y = 6160700
64 meter
Z = 9268625
48 Z = 2824627
95
XDOT = -17379
203821 XDOT = -5297
793288
YDOT = 7502
782176 feet/sec YDOT = 2227
608399 meter/sec
ZDOT = -16592
498649 ZDOT = -5083
127069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9955697
92 X = 3034496
73
Y = 17596544
79 feet Y = 5363426
85 meter
Z = 9265784
20 Z = 2824211
02
XDOT = -9880
677442 XDOT = -3011
630484
YDOT = 14434
331818 feet/sec YDOT = 4399
584338 meter/sec
ZDOT = -16708
474512 ZDOT = -5092
743031
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 18329
94419204
00016717 00000-0 10270-3 0 9148
2 25544 51
6379 292
6303 0004958 83
4271 276
7446 15
54042169 23669
Satellite: ISS
Catalog Number: 25544
Epoch time: 18329
94419204 = yrday
fracday
Element set: 914
Inclination: 51
6379 deg
RA of node: 292
6303 deg
Eccentricity:
0004958
Arg of perigee: 83
4271 deg
Mean anomaly: 276
7446 deg
Mean motion: 15
54042169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 331
Coasting Arc #16 (Orbit 2380)
---------------------------------------
Vector Time (GMT): 2018/330/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 921447
08 A = 6788904
77 meter
Y = -6594137
10 meter E =
0012751
Z = -1310847
89 I = 51
29100
XDOT = 4995
548404 Wp = 56
25105
YDOT = -444
920846 meter/sec RA = 287
03286 deg
ZDOT = 5797
417366 TA = 289
41654
MA = 289
55430
Ha = 223
057 n
mi
Hp = 212
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3023120
35 X = 1001483
55
Y = -21634308
06 feet Y = -6583385
18 meter
Z = -4300682
05 Z = -1306178
09
XDOT = 16389
594501 XDOT = 4971
991295
YDOT = -1459
714061 feet/sec YDOT = -389
189496 meter/sec
ZDOT = 19020
398181 ZDOT = 5821
626974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8575103
56 X = -2613691
56
Y = -20095712
68 feet Y = -6125173
23 meter
Z = -4278824
48 Z = -1304185
70
XDOT = 11700
067461 XDOT = 3566
180562
YDOT = -9032
128992 feet/sec YDOT = -2752
992917 meter/sec
ZDOT = 19129
282832 ZDOT = 5830
605407
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 18330
90878851
00016717 00000-0 10270-3 0 9154
2 25544 51
6371 287
8227 0005188 89
5941 270
5806 15
54024502 23819
Satellite: ISS
Catalog Number: 25544
Epoch time: 18330
90878851 = yrday
fracday
Element set: 915
Inclination: 51
6371 deg
RA of node: 287
8227 deg
Eccentricity:
0005188
Arg of perigee: 89
5941 deg
Mean anomaly: 270
5806 deg
Mean motion: 15
54024502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2381
Checksum: 327
Coasting Arc #17 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2018/331/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1705585
34 A = 6789598
89 meter
Y = -6564661
57 meter E =
0016538
Z = 110708
72 I = 51
28953
XDOT = 4615
314476 Wp = 58
46300
YDOT = 1311
028328 meter/sec RA = 283
81464 deg
ZDOT = 5982
720291 TA = 302
73542
MA = 302
89473
Ha = 223
018 n
mi
Hp = 212
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5595752
41 X = 1778328
69
Y = -21537603
59 feet Y = -6545181
81 meter
Z = 363217
58 Z = 119169
95
XDOT = 15142
107862 XDOT = 4571
250081
YDOT = 4301
274043 feet/sec YDOT = 1362
393011 meter/sec
ZDOT = 19628
347412 ZDOT = 6005
033144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20872080
83 X = 6361810
24
Y = 7714097
09 feet Y = 2351256
79 meter
Z = 402105
03 Z = 122561
61
XDOT = -5216
402026 XDOT = -1589
959338
YDOT = 12984
793249 feet/sec YDOT = 3957
764982 meter/sec
ZDOT = 19728
480481 ZDOT = 6013
240850
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 18331
61615638
00016717 00000-0 10270-3 0 9166
2 25544 51
6392 284
3007 0005135 88
4995 271
6746 15
54034247 23923
Satellite: ISS
Catalog Number: 25544
Epoch time: 18331
61615638 = yrday
fracday
Element set: 916
Inclination: 51
6392 deg
RA of node: 284
3007 deg
Eccentricity:
0005135
Arg of perigee: 88
4995 deg
Mean anomaly: 271
6746 deg
Mean motion: 15
54034247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 323
Coasting Arc #18 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2018/332/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2399006
34 A = 6788196
73 meter
Y = 6090384
85 meter E =
0011322
Z = -1792174
57 I = 51
27900
XDOT = -4063
348907 Wp = 120
60741
YDOT = -3247
517686 meter/sec RA = 278
81922 deg
ZDOT = -5629
174851 TA = 79
17589
MA = 79
04849
Ha = 223
005 n
mi
Hp = 212
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7870755
70 X = -2458226
95
Y = 19981577
60 feet Y = 6063226
51 meter
Z = -5879837
83 Z = -1803971
52
XDOT = -13331
197201 XDOT = -3999
388587
YDOT = -10654
585584 feet/sec YDOT = -3292
598812 meter/sec
ZDOT = -18468
421427 ZDOT = -5648
758179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19265607
38 X = -5872157
13
Y = -9455842
94 feet Y = -2882140
93 meter
Z = -5933644
60 Z = -1808574
88
XDOT = 11021
479194 XDOT = 3359
346858
YDOT = -10877
189956 feet/sec YDOT = -3315
367498 meter/sec
ZDOT = -18556
045931 ZDOT = -5655
882800
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 18332
58074454
00016717 00000-0 10270-3 0 9179
2 25544 51
6401 279
4925 0005161 90
5998 269
5746 15
54039239 24073
Satellite: ISS
Catalog Number: 25544
Epoch time: 18332
58074454 = yrday
fracday
Element set: 917
Inclination: 51
6401 deg
RA of node: 279
4925 deg
Eccentricity:
0005161
Arg of perigee: 90
5998 deg
Mean anomaly: 269
5746 deg
Mean motion: 15
54039239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 336
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