[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 20th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 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
082/14:09:43
720 0
7 2
2 2
2
N/A 2
0 -0
2 224
1
000/00:05:27
441 0
4 -0
1 217
1
082/22:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
1
000/00:00:00
000 0
0 0
0 217
0
087/06:36:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 217
1
090/20:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
6
000/00:00:00
000 0
0 0
0 217
3
094/11:01:35
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 217
4
Coasting Arc #1 (Orbit 147)
---------------------------------------
Vector Time (GMT): 2019/079/13:07:49
844
Vector Time (MET): N/A
Weight (LBS) : 915052
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -959115
17 A = 6793079
17 meter
Y = -6716999
96 meter E =
0015416
Z = -124831
17 I = 52
03626
XDOT = 4684
811620 Wp = 131
76758
YDOT = -565
701829 meter/sec RA = 81
05119 deg
ZDOT = -6043
805929 TA = 49
56934
MA = 49
43498
Ha = 224
285 n
mi
Hp = 215
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3146703
32 X = -883326
14
Y = -22037401
43 feet Y = -6727301
71 meter
Z = -409551
09 Z = -129305
15
XDOT = 15370
116863 XDOT = 4720
146376
YDOT = -1855
977128 feet/sec YDOT = -513
116239 meter/sec
ZDOT = -19828
759611 ZDOT = -6020
963253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8328205
20 X = -2538436
95
Y = -20643966
70 feet Y = -6292281
05 meter
Z = -429153
64 Z = -130806
03
XDOT = 13101
698447 XDOT = 3993
397687
YDOT = -4907
247342 feet/sec YDOT = -1495
728990 meter/sec
ZDOT = -19725
308598 ZDOT = -6012
274061
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 19079
57908208
00016717 00000-0 10270-3 0 9002
2 25544 51
6368 81
7335 0003680 119
9104 240
2414 15
52837218 1482
Satellite: ISS
Catalog Number: 25544
Epoch time: 19079
57908208 = yrday
fracday
Element set: 900
Inclination: 51
6368 deg
RA of node: 81
7335 deg
Eccentricity:
0003680
Arg of perigee: 119
9104 deg
Mean anomaly: 240
2414 deg
Mean motion: 15
52837218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 148
Checksum: 308
Coasting Arc #2 (Orbit 163)
---------------------------------------
Vector Time (GMT): 2019/080/13:07:49
844
Vector Time (MET): N/A
Weight (LBS) : 915052
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 529815
34 A = 6792150
93 meter
Y = 6624047
66 meter E =
0015608
Z = 1377828
59 I = 52
02691
XDOT = -4899
752920 Wp = 73
04402
YDOT = -832
814247 meter/sec RA = 76
11350 deg
ZDOT = 5837
924611 TA = 301
88050
MA = 302
03229
Ha = 224
164 n
mi
Hp = 215
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1738239
31 X = 449011
30
Y = 21732439
81 feet Y = 6629520
82 meter
Z = 4520435
00 Z = 1380205
01
XDOT = -16075
304857 XDOT = -4918
433210
YDOT = -2732
330207 feet/sec YDOT = -887
710325 meter/sec
ZDOT = 19153
295967 ZDOT = 5814
078358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7215981
07 X = 2199431
03
Y = 20570818
61 feet Y = 6269985
51 meter
Z = 4530539
45 Z = 1380908
42
XDOT = -14862
219175 XDOT = -4530
004405
YDOT = 982
832454 feet/sec YDOT = 299
567332 meter/sec
ZDOT = 19045
441692 ZDOT = 5805
050628
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 19080
60877178
00016717 00000-0 10270-3 0 9010
2 25544 51
6364 76
6109 0003736 128
5763 231
5724 15
52882187 1649
Satellite: ISS
Catalog Number: 25544
Epoch time: 19080
60877178 = yrday
fracday
Element set: 901
Inclination: 51
6364 deg
RA of node: 76
6109 deg
Eccentricity:
0003736
Arg of perigee: 128
5763 deg
Mean anomaly: 231
5724 deg
Mean motion: 15
52882187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 164
Checksum: 323
Coasting Arc #3 (Orbit 178)
---------------------------------------
Vector Time (GMT): 2019/081/13:07:49
844
Vector Time (MET): N/A
Weight (LBS) : 915052
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5796
80 A = 6790217
06 meter
Y = -6272113
38 meter E =
0008679
Z = -2599154
13 I = 52
01216
XDOT = 5103
272827 Wp = 127
64012
YDOT = 2186
250994 meter/sec RA = 71
17086 deg
ZDOT = -5281
514501 TA = 81
42062
MA = 81
32230
Ha = 224
186 n
mi
Hp = 215
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19018
36 X = 88558
15
Y = -20577799
81 feet Y = -6271586
16 meter
Z = -8527408
57 Z = -2598924
11
XDOT = 16743
021085 XDOT = 5104
100895
YDOT = 7172
739480 feet/sec YDOT = 2243
323274 meter/sec
ZDOT = -17327
803480 ZDOT = -5256
723039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5537566
30 X = -1687850
21
Y = -19819437
18 feet Y = -6040964
45 meter
Z = -8525735
90 Z = -2598644
30
XDOT = 16730
009713 XDOT = 5099
306961
YDOT = 2707
112540 feet/sec YDOT = 825
127902 meter/sec
ZDOT = -17215
812716 ZDOT = -5247
379716
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 19081
57410730
00016717 00000-0 10270-3 0 9025
2 25544 51
6375 71
8068 0003587 128
1084 232
0392 15
52839259 1793
Satellite: ISS
Catalog Number: 25544
Epoch time: 19081
57410730 = yrday
fracday
Element set: 902
Inclination: 51
6375 deg
RA of node: 71
8068 deg
Eccentricity:
0003587
Arg of perigee: 128
1084 deg
Mean anomaly: 232
0392 deg
Mean motion: 15
52839259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 179
Checksum: 312
Coasting Arc #4 (Orbit 194)
---------------------------------------
Vector Time (GMT): 2019/082/13:07:49
844
Vector Time (MET): N/A
Weight (LBS) : 915052
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -583778
58 A = 6787430
88 meter
Y = 5702339
19 meter E =
0014816
Z = 3625285
12 I = 51
99227
XDOT = -5271
695179 Wp = 102
39003
YDOT = -3370
498476 meter/sec RA = 66
22432 deg
ZDOT = 4434
341949 TA = 300
32753
MA = 300
47399
Ha = 224
073 n
mi
Hp = 215
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1915284
06 X = -665110
03
Y = 18708461
90 feet Y = 5695356
64 meter
Z = 11893980
04 Z = 3622251
13
XDOT = -17295
587858 XDOT = -5255
153124
YDOT = -11058
065865 feet/sec YDOT = -3429
357249 meter/sec
ZDOT = 14548
365975 ZDOT = 4408
774553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3500398
13 X = 1066921
35
Y = 18486820
34 feet Y = 5634782
84 meter
Z = 11879659
40 Z = 3620920
18
XDOT = -18498
804158 XDOT = -5638
435507
YDOT = -5810
698900 feet/sec YDOT = -1771
101025 meter/sec
ZDOT = 14432
994643 ZDOT = 4399
176767
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 19082
60379165
00016717 00000-0 10270-3 0 9037
2 25544 51
6384 66
6843 0003530 134
0022 226
1422 15
52872650 1950
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
60379165 = yrday
fracday
Element set: 903
Inclination: 51
6384 deg
RA of node: 66
6843 deg
Eccentricity:
0003530
Arg of perigee: 134
0022 deg
Mean anomaly: 226
1422 deg
Mean motion: 15
52872650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 195
Checksum: 291
Coasting Arc #5 (Orbit 194)
---------------------------------------
Vector Time (GMT): 2019/082/14:12:27
441
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4614655
20 A = 6784283
57 meter
Y = 951906
30 meter E =
0013260
Z = -4893616
19 I = 51
97720
XDOT = 1109
151727 Wp = 114
04895
YDOT = 7170
152310 meter/sec RA = 65
95677 deg
ZDOT = 2440
619557 TA = 179
82528
MA = 179
82482
Ha = 224
100 n
mi
Hp = 217
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15139944
87 X = 4627438
27
Y = 3123052
16 feet Y = 1003581
51 meter
Z = -16055171
23 Z = -4871168
94
XDOT = 3638
949237 XDOT = 1017
035415
YDOT = 23524
121753 feet/sec YDOT = 7182
040849 meter/sec
ZDOT = 8007
282011 ZDOT = 2445
782846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14486766
03 X = 4415566
29
Y = -5688044
66 feet Y = -1733716
01 meter
Z = -15953672
51 Z = -4862679
38
XDOT = 15407
248521 XDOT = 4696
129349
YDOT = 16717
938618 feet/sec YDOT = 5095
627691 meter/sec
ZDOT = 8029
910130 ZDOT = 2447
516608
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 19082
60379307
00016717 00000-0 10270-3 0 9046
2 25544 51
6388 66
6833 0002103 154
9377 205
1877 15
52433092 1956
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
60379307 = yrday
fracday
Element set: 904
Inclination: 51
6388 deg
RA of node: 66
6833 deg
Eccentricity:
0002103
Arg of perigee: 154
9377 deg
Mean anomaly: 205
1877 deg
Mean motion: 15
52433092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 195
Checksum: 316
Coasting Arc #6 (Orbit 200)
---------------------------------------
Vector Time (GMT): 2019/082/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1659087
86 A = 6785542
37 meter
Y = 4750981
91 meter E =
0010379
Z = 4547033
76 I = 51
97526
XDOT = -5063
660940 Wp = 121
18684
YDOT = -4809
259467 meter/sec RA = 64
29319 deg
ZDOT = 3166
819767 TA = 297
14114
MA = 297
24694
Ha = 224
114 n
mi
Hp = 217
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5443201
65 X = -1734178
41
Y = 15587211
00 feet Y = 4732009
46 meter
Z = 14918089
76 Z = 4538791
62
XDOT = -16613
060828 XDOT = -5024
888792
YDOT = -15778
410324 feet/sec YDOT = -4865
667736 meter/sec
ZDOT = 10389
828633 ZDOT = 3142
317024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11143325
85 X = 3396485
72
Y = -12228746
29 feet Y = -3727321
87 meter
Z = 14880290
52 Z = 4535512
55
XDOT = 8385
215723 XDOT = 2555
813752
YDOT = 20191
512250 feet/sec YDOT = 6154
372934 meter/sec
ZDOT = 10279
430665 ZDOT = 3133
170467
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 19082
99002321
00016717 00000-0 10270-3 0 9058
2 25544 51
6373 64
7606 0002153 159
6338 200
4900 15
52435450 2014
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
99002321 = yrday
fracday
Element set: 905
Inclination: 51
6373 deg
RA of node: 64
7606 deg
Eccentricity:
0002153
Arg of perigee: 159
6338 deg
Mean anomaly: 200
4900 deg
Mean motion: 15
52435450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 201
Checksum: 276
Coasting Arc #7 (Orbit 215)
---------------------------------------
Vector Time (GMT): 2019/083/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2272423
66 A = 6783486
37 meter
Y = -3925591
26 meter E =
0013377
Z = -5055760
17 I = 51
95277
XDOT = 5016
356555 Wp = 85
55043
YDOT = 5437
097633 meter/sec RA = 59
33678 deg
ZDOT = -1970
445886 TA = 165
39199
MA = 165
35329
Ha = 224
106 n
mi
Hp = 217
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7455458
20 X = 2340710
00
Y = -12879236
42 feet Y = -3899798
04 meter
Z = -16587139
67 Z = -5044555
37
XDOT = 16457
862712 XDOT = 4964
755925
YDOT = 17838
246826 feet/sec YDOT = 5492
905358 meter/sec
ZDOT = -6464
717474 ZDOT = -1946
204017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11805495
59 X = -3598315
06
Y = 9153277
57 feet Y = 2789919
00 meter
Z = -16536008
40 Z = -5040175
36
XDOT = -8036
484685 XDOT = -2449
520532
YDOT = -21826
232925 feet/sec YDOT = -6652
635796 meter/sec
ZDOT = -6355
582455 ZDOT = -1937
181532
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 19083
95559946
00016717 00000-0 10270-3 0 9066
2 25544 51
6370 59
9593 0002385 159
5285 200
5963 15
52451164 2165
Satellite: ISS
Catalog Number: 25544
Epoch time: 19083
95559946 = yrday
fracday
Element set: 906
Inclination: 51
6370 deg
RA of node: 59
9593 deg
Eccentricity:
0002385
Arg of perigee: 159
5285 deg
Mean anomaly: 200
5963 deg
Mean motion: 15
52451164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 216
Checksum: 335
Coasting Arc #8 (Orbit 231)
---------------------------------------
Vector Time (GMT): 2019/084/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2917785
96 A = 6782496
59 meter
Y = 3057632
41 meter E =
0004877
Z = 5302136
56 I = 51
93150
XDOT = -4880
623573 Wp = 136
33465
YDOT = -5873
386388 meter/sec RA = 54
37608 deg
ZDOT = 697
416980 TA = 307
00931
MA = 307
05392
Ha = 224
194 n
mi
Hp = 217
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9572788
59 X = -2977515
30
Y = 10031602
39 feet Y = 3024670
06 meter
Z = 17395461
16 Z = 5287817
76
XDOT = -16012
544532 XDOT = -4817
970635
YDOT = -19269
640382 feet/sec YDOT = -5927
614575 meter/sec
ZDOT = 2288
113450 ZDOT = 673
861252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12619746
96 X = 3846498
87
Y = -5939301
16 feet Y = -1810298
99 meter
Z = 17330322
71 Z = 5282282
36
XDOT = 7709
093977 XDOT = 2349
731844
YDOT = 22784
162136 feet/sec YDOT = 6944
612619 meter/sec
ZDOT = 2182
146727 ZDOT = 665
118323
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 19084
98554580
00016717 00000-0 10270-3 0 9070
2 25544 51
6373 54
8374 0002323 163
9443 196
1783 15
52411938 2329
Satellite: ISS
Catalog Number: 25544
Epoch time: 19084
98554580 = yrday
fracday
Element set: 907
Inclination: 51
6373 deg
RA of node: 54
8374 deg
Eccentricity:
0002323
Arg of perigee: 163
9443 deg
Mean anomaly: 196
1783 deg
Mean motion: 15
52411938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 232
Checksum: 323
Coasting Arc #9 (Orbit 246)
---------------------------------------
Vector Time (GMT): 2019/085/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3620704
66 A = 6782351
09 meter
Y = -2180043
14 meter E =
0015635
Z = -5317989
63 I = 51
91243
XDOT = 4584
628846 Wp = 103
12131
YDOT = 6097
982943 meter/sec RA = 49
41317 deg
ZDOT = 619
690521 TA = 172
79397
MA = 172
77147
Ha = 224
019 n
mi
Hp = 217
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11878952
31 X = 3670645
25
Y = -7152372
50 feet Y = -2139274
93 meter
Z = -17447472
55 Z = -5300280
21
XDOT = 15041
433222 XDOT = 4513
088623
YDOT = 20006
505719 feet/sec YDOT = 6148
851496 meter/sec
ZDOT = 2033
105383 ZDOT = 641
786828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13709940
68 X = -4178789
92
Y = 2665004
61 feet Y = 812293
41 meter
Z = -17367081
39 Z = -5293486
41
XDOT = -7163
744315 XDOT = -2183
509267
YDOT = -22915
729812 feet/sec YDOT = -6984
714447 meter/sec
ZDOT = 2132
427835 ZDOT = 649
964004
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 19085
95111496
00016717 00000-0 10270-3 0 9084
2 25544 51
6386 50
0361 0002429 165
1477 194
9747 15
52463827 2471
Satellite: ISS
Catalog Number: 25544
Epoch time: 19085
95111496 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 50
0361 deg
Eccentricity:
0002429
Arg of perigee: 165
1477 deg
Mean anomaly: 194
9747 deg
Mean motion: 15
52463827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 247
Checksum: 329
Coasting Arc #10 (Orbit 262)
---------------------------------------
Vector Time (GMT): 2019/086/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4311146
42 A = 6783547
39 meter
Y = 1331425
59 meter E =
0005321
Z = 5061057
92 I = 51
89230
XDOT = -4146
061129 Wp = 81
19038
YDOT = -6163
267493 meter/sec RA = 44
44953 deg
ZDOT = -1907
838188 TA = 27
25423
MA = 27
22631
Ha = 224
192 n
mi
Hp = 217
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14144181
17 X = -4350298
10
Y = 4368194
20 feet Y = 1282996
68 meter
Z = 16604520
72 Z = 5040020
90
XDOT = -13602
562758 XDOT = -4067
566397
YDOT = -20220
693876 feet/sec YDOT = -6209
192853 meter/sec
ZDOT = -6259
311642 ZDOT = -1927
787164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14902394
25 X = 4542249
77
Y = 463944
68 feet Y = 141410
34 meter
Z = 16509163
84 Z = 5031993
14
XDOT = 6344
336770 XDOT = 1933
753847
YDOT = 22428
278421 feet/sec YDOT = 6836
139263 meter/sec
ZDOT = -6348
895973 ZDOT = -1935
143493
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 19086
98105482
00016717 00000-0 10270-3 0 9097
2 25544 51
6373 44
9142 0002477 168
4401 191
6808 15
52426243 2633
Satellite: ISS
Catalog Number: 25544
Epoch time: 19086
98105482 = yrday
fracday
Element set: 909
Inclination: 51
6373 deg
RA of node: 44
9142 deg
Eccentricity:
0002477
Arg of perigee: 168
4401 deg
Mean anomaly: 191
6808 deg
Mean motion: 15
52426243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 263
Checksum: 314
Coasting Arc #11 (Orbit 267)
---------------------------------------
Vector Time (GMT): 2019/087/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3252508
26 A = 6791819
18 meter
Y = -5489854
59 meter E =
0007677
Z = -2319109
02 I = 51
91623
XDOT = 5331
355906 Wp = 143
66513
YDOT = -868
562255 meter/sec RA = 42
80776 deg
ZDOT = -5436
256824 TA = 62
05442
MA = 61
97673
Ha = 223
887 n
mi
Hp = 217
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10670958
86 X = -3179612
53
Y = -18011333
95 feet Y = -5525818
94 meter
Z = -7608625
38 Z = -2334731
08
XDOT = 17491
325152 XDOT = 5367
078373
YDOT = -2849
613698 feet/sec YDOT = -808
743845 meter/sec
ZDOT = -17835
488269 ZDOT = -5410
272414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15000648
86 X = 4572197
77
Y = -14566632
60 feet Y = -4439909
62 meter
Z = -7678700
56 Z = -2340467
93
XDOT = 5859
742840 XDOT = 1786
049618
YDOT = 15348
083757 feet/sec YDOT = 4678
095929 meter/sec
ZDOT = -17717
793916 ZDOT = -5400
383586
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 19087
30290861
00016717 00000-0 10270-3 0 9102
2 25544 51
6411 43
3174 0002223 169
0302 191
0899 15
52474839 2683
Satellite: ISS
Catalog Number: 25544
Epoch time: 19087
30290861 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 43
3174 deg
Eccentricity:
0002223
Arg of perigee: 169
0302 deg
Mean anomaly: 191
0899 deg
Mean motion: 15
52474839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 268
Checksum: 299
Coasting Arc #12 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2019/088/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2632183
07 A = 6789577
86 meter
Y = 5317108
71 meter E =
0013150
Z = 3291788
45 I = 51
88220
XDOT = -6022
959489 Wp = 97
11364
YDOT = 33
297614 meter/sec RA = 37
85700 deg
ZDOT = 4744
491659 TA = 300
95949
MA = 301
08864
Ha = 223
911 n
mi
Hp = 217
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8635771
24 X = 2556540
46
Y = 17444582
38 feet Y = 5346120
87 meter
Z = 10799830
87 Z = 3304390
49
XDOT = -19760
365779 XDOT = -6045
930138
YDOT = 109
244141 feet/sec YDOT = -34
183499 meter/sec
ZDOT = 15565
917516 ZDOT = 4715
178798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14718783
58 X = -4486285
24
Y = 12689585
99 feet Y = 3867785
81 meter
Z = 10856249
97 Z = 3308984
99
XDOT = -4195
558554 XDOT = -1278
806247
YDOT = -18119
727300 feet/sec YDOT = -5522
892881 meter/sec
ZDOT = 15433
258841 ZDOT = 4704
057295
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 19088
33284468
00016717 00000-0 10270-3 0 9113
2 25544 51
6399 38
1957 0002155 168
7644 191
3556 15
52451139 2847
Satellite: ISS
Catalog Number: 25544
Epoch time: 19088
33284468 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 38
1957 deg
Eccentricity:
0002155
Arg of perigee: 168
7644 deg
Mean anomaly: 191
3556 deg
Mean motion: 15
52451139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 334
Coasting Arc #13 (Orbit 298)
---------------------------------------
Vector Time (GMT): 2019/089/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1834525
18 A = 6786822
59 meter
Y = -5060514
94 meter E =
0007359
Z = -4140267
85 I = 51
84828
XDOT = 6608
006757 Wp = 86
38455
YDOT = 713
981125 meter/sec RA = 32
90023 deg
ZDOT = -3806
017981 TA = 144
44787
MA = 144
39882
Ha = 223
774 n
mi
Hp = 217
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6018783
41 X = -1757689
77
Y = -16602739
31 feet Y = -5080600
55 meter
Z = -13583555
93 Z = -4148992
25
XDOT = 21679
812195 XDOT = 6618
019064
YDOT = 2342
457760 feet/sec YDOT = 787
932208 meter/sec
ZDOT = -12486
935633 ZDOT = -3773
894768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14396750
07 X = 4388129
42
Y = -10176057
00 feet Y = -3101662
18 meter
Z = -13622450
19 Z = -4152122
82
XDOT = 2857
561263 XDOT = 870
984673
YDOT = 20540
711228 feet/sec YDOT = 6260
808782 meter/sec
ZDOT = -12341
651444 ZDOT = -3761
735360
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 19089
29840371
00016717 00000-0 10270-3 0 9121
2 25544 51
6418 33
3947 0002128 176
4045 183
7123 15
52485189 2999
Satellite: ISS
Catalog Number: 25544
Epoch time: 19089
29840371 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 33
3947 deg
Eccentricity:
0002128
Arg of perigee: 176
4045 deg
Mean anomaly: 183
7123 deg
Mean motion: 15
52485189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 299
Checksum: 324
Coasting Arc #14 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2019/090/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 938220
39 A = 6784504
22 meter
Y = 4737319
74 meter E =
0008823
Z = 4761702
50 I = 51
81014
XDOT = -7050
484974 Wp = 129
18077
YDOT = -1330
800368 meter/sec RA = 27
93636 deg
ZDOT = 2704
384311 TA = 294
11005
MA = 294
20230
Ha = 223
765 n
mi
Hp = 217
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3078150
90 X = 862047
11
Y = 15542387
60 feet Y = 4747386
04 meter
Z = 15622383
54 Z = 4766074
60
XDOT = -23131
512381 XDOT = -7048
215865
YDOT = -4366
142941 feet/sec YDOT = -1409
630923 meter/sec
ZDOT = 8872
651938 ZDOT = 2670
141618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14047108
89 X = -4281558
79
Y = 7288228
66 feet Y = 2221452
10 meter
Z = 15641615
89 Z = 4767564
52
XDOT = -1906
972569 XDOT = -581
245239
YDOT = -22447
076801 feet/sec YDOT = -6841
869009 meter/sec
ZDOT = 8717
857423 ZDOT = 2657
202943
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 19090
32833152
00016717 00000-0 10270-3 0 9137
2 25544 51
6400 28
2729 0002057 176
5458 183
5709 15
52477470 3152
Satellite: ISS
Catalog Number: 25544
Epoch time: 19090
32833152 = yrday
fracday
Element set: 913
Inclination: 51
6400 deg
RA of node: 28
2729 deg
Eccentricity:
0002057
Arg of perigee: 176
5458 deg
Mean anomaly: 183
5709 deg
Mean motion: 15
52477470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 303
Coasting Arc #15 (Orbit 323)
---------------------------------------
Vector Time (GMT): 2019/090/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3475120
78 A = 6788838
09 meter
Y = 4662876
44 meter E =
0012245
Z = 3495042
52 I = 51
80493
XDOT = -6073
527109 Wp = 102
35572
YDOT = 1106
634199 meter/sec RA = 25
08402 deg
ZDOT = 4546
509977 TA = 298
59803
MA = 298
72118
Ha = 223
625 n
mi
Hp = 217
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11401314
88 X = 3405744
06
Y = 15298151
06 feet Y = 4701350
07 meter
Z = 11466674
95 Z = 3511754
31
XDOT = -19926
270043 XDOT = -6107
534650
YDOT = 3630
689628 feet/sec YDOT = 1038
526014 meter/sec
ZDOT = 14916
371315 ZDOT = 4516
924615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3045409
21 X = 928240
73
Y = -18788867
55 feet Y = -5726846
83 meter
Z = 11541749
44 Z = 3517925
23
XDOT = 15212
081579 XDOT = 4636
642465
YDOT = 11578
298232 feet/sec YDOT = 3529
065301 meter/sec
ZDOT = 14782
372463 ZDOT = 4505
667127
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 19090
90766456
00016717 00000-0 10270-3 0 9144
2 25544 51
6372 25
3889 0002326 185
9508 174
1616 15
52497604 3248
Satellite: ISS
Catalog Number: 25544
Epoch time: 19090
90766456 = yrday
fracday
Element set: 914
Inclination: 51
6372 deg
RA of node: 25
3889 deg
Eccentricity:
0002326
Arg of perigee: 185
9508 deg
Mean anomaly: 174
1616 deg
Mean motion: 15
52497604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 324
Checksum: 326
Coasting Arc #16 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2019/091/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2604094
24 A = 6786169
01 meter
Y = -4563593
61 meter E =
0007783
Z = -4301918
72 I = 51
76745
XDOT = 6762
656914 Wp = 83
72486
YDOT = -508
505679 meter/sec RA = 20
12123 deg
ZDOT = -3558
927961 TA = 150
02894
MA = 149
98436
Ha = 223
615 n
mi
Hp = 217
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8543616
28 X = -2531973
11
Y = -14972419
97 feet Y = -4592311
58 meter
Z = -14113906
57 Z = -4314392
73
XDOT = 22187
194601 XDOT = 6785
127739
YDOT = -1668
325719 feet/sec YDOT = -432
755625 meter/sec
ZDOT = -11676
272838 ZDOT = -3526
023105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4535391
32 X = -1382387
28
Y = 16583599
24 feet Y = 5054681
05 meter
Z = -14169811
54 Z = -4318958
56
XDOT = -15783
002020 XDOT = -4810
659016
YDOT = -14152
804272 feet/sec YDOT = -4313
774742 meter/sec
ZDOT = -11527
334958 ZDOT = -3513
531695
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 19091
87321772
00016717 00000-0 10270-3 0 9150
2 25544 51
6391 20
5881 0002192 186
4176 173
6948 15
52504824 3397
Satellite: ISS
Catalog Number: 25544
Epoch time: 19091
87321772 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 20
5881 deg
Eccentricity:
0002192
Arg of perigee: 186
4176 deg
Mean anomaly: 173
6948 deg
Mean motion: 15
52504824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 321
Coasting Arc #17 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2019/092/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1627783
61 A = 6783925
83 meter
Y = 4425261
50 meter E =
0007818
Z = 4874877
76 I = 51
72833
XDOT = -7276
415869 Wp = 136
33444
YDOT = 5
365805 meter/sec RA = 15
15023 deg
ZDOT = 2416
980168 TA = 289
94988
MA = 290
03408
Ha = 223
491 n
mi
Hp = 217
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5340497
41 X = 1554498
74
Y = 14518574
48 feet Y = 4443055
28 meter
Z = 15993693
43 Z = 4882606
42
XDOT = -23872
755476 XDOT = -7287
675378
YDOT = 17
604346 feet/sec YDOT = -76
066866 meter/sec
ZDOT = 7929
724959 ZDOT = 2381
606861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6258810
05 X = 1907685
30
Y = -14107947
03 feet Y = -4300102
25 meter
Z = 16028140
08 Z = 4885377
10
XDOT = 16268
150648 XDOT = 4958
532318
YDOT = 16073
506761 feet/sec YDOT = 4899
204861 meter/sec
ZDOT = 7769
691794 ZDOT = 2368
202059
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 19092
90313489
00016717 00000-0 10270-3 0 9162
2 25544 51
6391 15
4656 0002246 193
2060 166
9033 15
52510679 3551
Satellite: ISS
Catalog Number: 25544
Epoch time: 19092
90313489 = yrday
fracday
Element set: 916
Inclination: 51
6391 deg
RA of node: 15
4656 deg
Eccentricity:
0002246
Arg of perigee: 193
2060 deg
Mean anomaly: 166
9033 deg
Mean motion: 15
52510679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 355
Checksum: 307
Coasting Arc #18 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2019/093/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -535897
21 A = 6782452
61 meter
Y = -4296084
74 meter E =
0013642
Z = -5232730
72 I = 51
69142
XDOT = 7557
675459 Wp = 89
93781
YDOT = 441
998404 meter/sec RA = 10
17573 deg
ZDOT = -1139
439016 TA = 169
14330
MA = 169
11383
Ha = 223
544 n
mi
Hp = 217
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1758192
96 X = -462399
65
Y = -14094766
19 feet Y = -4301667
15 meter
Z = -17167751
71 Z = -5235154
92
XDOT = 24795
523161 XDOT = 7557
705969
YDOT = 1450
125997 feet/sec YDOT = 526
513665 meter/sec
ZDOT = -3738
316982 ZDOT = -1102
726650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8363435
24 X = -2549175
06
Y = 11465047
16 feet Y = 3494546
37 meter
Z = -17178213
53 Z = -5235919
48
XDOT = -16402
891801 XDOT = -4999
601421
YDOT = -17305
307597 feet/sec YDOT = -5274
657756 meter/sec
ZDOT = -3572
294697 ZDOT = -1088
835424
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 19093
86867940
00016717 00000-0 10270-3 0 9175
2 25544 51
6396 10
6657 0002218 191
8760 168
2339 15
52514325 3707
Satellite: ISS
Catalog Number: 25544
Epoch time: 19093
86867940 = yrday
fracday
Element set: 917
Inclination: 51
6396 deg
RA of node: 10
6657 deg
Eccentricity:
0002218
Arg of perigee: 191
8760 deg
Mean anomaly: 168
2339 deg
Mean motion: 15
52514325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 326
Coasting Arc #19 (Orbit 379)
---------------------------------------
Vector Time (GMT): 2019/094/11:01:35
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2536087
26 A = 6784309
75 meter
Y = 4111251
98 meter E =
0007885
Z = 4760884
09 I = 51
67896
XDOT = -7073
495833 Wp = 131
92054
YDOT = 1247
562849 meter/sec RA = 7
16632 deg
ZDOT = 2682
659453 TA = 291
55218
MA = 291
63620
Ha = 223
280 n
mi
Hp = 217
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8320496
25 X = 2466799
80
Y = 13488359
53 feet Y = 4139225
41 meter
Z = 15619698
47 Z = 4773034
74
XDOT = -23207
007325 XDOT = -7099
951619
YDOT = 4093
053966 feet/sec YDOT = 1168
314442 meter/sec
ZDOT = 8801
376158 ZDOT = 2648
234594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7495320
52 X = 2284573
69
Y = 13902583
44 feet Y = 4237507
43 meter
Z = 15674177
01 Z = 4777489
15
XDOT = -22434
640440 XDOT = -6838
078406
YDOT = 2318
499256 feet/sec YDOT = 706
678573 meter/sec
ZDOT = 8645
512868 ZDOT = 2635
152322
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 19094
51237261
00016717 00000-0 10270-3 0 9186
2 25544 51
6406 7
4688 0001911 204
2553 155
8509 15
52530717 3800
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
51237261 = yrday
fracday
Element set: 918
Inclination: 51
6406 deg
RA of node: 7
4688 deg
Eccentricity:
0001911
Arg of perigee: 204
2553 deg
Mean anomaly: 155
8509 deg
Mean motion: 15
52530717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 380
Checksum: 300
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