[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 8th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
097/20:12:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 216
9
107/20:48:33
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
3
109/09:19:21
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 217
4
Coasting Arc #1 (Orbit 396)
---------------------------------------
Vector Time (GMT): 2019/095/13:24:28
701
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -159026
51 A = 6782055
38 meter
Y = 4204899
66 meter E =
0003400
Z = 5316104
75 I = 51
63798
XDOT = -7664
575438 Wp = 113
06650
YDOT = -250
902023 meter/sec RA = 1
68504 deg
ZDOT = -32
108371 TA = 337
23191
MA = 337
24698
Ha = 223
872 n
mi
Hp = 216
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -521740
52 X = -231857
93
Y = 13795602
57 feet Y = 4202714
65 meter
Z = 17441288
56 Z = 5315154
92
XDOT = -25146
244874 XDOT = -7661
044167
YDOT = -823
169368 feet/sec YDOT = -336
592930 meter/sec
ZDOT = -105
342423 ZDOT = -69
331646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7143266
52 X = 2177267
64
Y = 11820817
89 feet Y = 3602985
29 meter
Z = 17436496
73 Z = 5314644
20
XDOT = -20492
389359 XDOT = -6246
080277
YDOT = 12780
910074 feet/sec YDOT = 3895
621391 meter/sec
ZDOT = -273
668610 ZDOT = -83
414192
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 19095
60682076
00016717 00000-0 10270-3 0 9006
2 25544 51
6439 2
0299 0001680 155
3548 204
7684 15
52512470 3970
Satellite: ISS
Catalog Number: 25544
Epoch time: 19095
60682076 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 2
0299 deg
Eccentricity:
0001680
Arg of perigee: 155
3548 deg
Mean anomaly: 204
7684 deg
Mean motion: 15
52512470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 397
Checksum: 310
Coasting Arc #2 (Orbit 411)
---------------------------------------
Vector Time (GMT): 2019/096/13:24:28
701
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1286658
14 A = 6782716
38 meter
Y = -4191889
75 meter E =
0014798
Z = -5187867
85 I = 51
60640
XDOT = 7508
219414 Wp = 105
14544
YDOT = 636
572070 meter/sec RA = 356
70136 deg
ZDOT = 1347
212448 TA = 177
83460
MA = 177
82818
Ha = 223
841 n
mi
Hp = 216
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4221319
37 X = 1358637
46
Y = -13752919
14 feet Y = -4177099
46 meter
Z = -17020563
81 Z = -5181442
47
XDOT = 24633
265793 XDOT = 7493
998980
YDOT = 2088
491042 feet/sec YDOT = 720
454847 meter/sec
ZDOT = 4419
988345 ZDOT = 1383
650335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4284910
03 X = -1306040
58
Y = -13769787
74 feet Y = -4197031
30 meter
Z = -16991009
56 Z = -5178859
71
XDOT = 20395
174850 XDOT = 6216
449294
YDOT = -12006
105007 feet/sec YDOT = -3659
460806 meter/sec
ZDOT = 4584
700393 ZDOT = 1397
416680
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 19096
57237077
00016717 00000-0 10270-3 0 9011
2 25544 51
6435 357
2284 0001567 155
8576 204
2650 15
52511599 4122
Satellite: ISS
Catalog Number: 25544
Epoch time: 19096
57237077 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 357
2284 deg
Eccentricity:
0001567
Arg of perigee: 155
8576 deg
Mean anomaly: 204
2650 deg
Mean motion: 15
52511599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 412
Checksum: 317
Coasting Arc #3 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2019/097/13:24:28
701
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2365732
08 A = 6784284
76 meter
Y = 4180501
77 meter E =
0007423
Z = 4785747
81 I = 51
57794
XDOT = -7136
369449 Wp = 72
56338
YDOT = -1049
599737 meter/sec RA = 351
71813 deg
ZDOT = -2605
338239 TA = 43
16252
MA = 43
10435
Ha = 223
777 n
mi
Hp = 216
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7761588
20 X = -2435550
62
Y = 13715556
98 feet Y = 4153656
47 meter
Z = 15701272
34 Z = 4774085
93
XDOT = -23413
285595 XDOT = -7111
446688
YDOT = -3443
568692 feet/sec YDOT = -1129
264457 meter/sec
ZDOT = -8547
697633 ZDOT = -2639
943874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1633844
24 X = 497995
72
Y = 15727621
60 feet Y = 4793779
06 meter
Z = 15648040
75 Z = 4769522
82
XDOT = -19817
185008 XDOT = -6040
277990
YDOT = 10736
764884 feet/sec YDOT = 3272
565937 meter/sec
ZDOT = -8704
060371 ZDOT = -2652
997601
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 19097
60228355
00016717 00000-0 10270-3 0 9026
2 25544 51
6427 352
1074 0001480 162
2479 197
8725 15
52547866 4285
Satellite: ISS
Catalog Number: 25544
Epoch time: 19097
60228355 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 352
1074 deg
Eccentricity:
0001480
Arg of perigee: 162
2479 deg
Mean anomaly: 197
8725 deg
Mean motion: 15
52547866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 428
Checksum: 325
Coasting Arc #4 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2019/097/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2033406
22 A = 6782504
80 meter
Y = -3850637
59 meter E =
0014624
Z = -5212735
68 I = 51
56087
XDOT = 7233
677469 Wp = 88
93540
YDOT = -2198
420724 meter/sec RA = 350
33507 deg
ZDOT = -1200
429035 TA = 169
53087
MA = 169
50039
Ha = 223
890 n
mi
Hp = 216
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6671280
24 X = -1964875
26
Y = -12633325
42 feet Y = -3872993
74 meter
Z = -17102151
19 Z = -5222446
62
XDOT = 23732
537628 XDOT = 7263
554306
YDOT = -7212
666417 feet/sec YDOT = -2117
361710 meter/sec
ZDOT = -3938
415469 ZDOT = -1165
217363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3599690
09 X = -1097185
54
Y = 13771742
91 feet Y = 4197627
24 meter
Z = -17145605
71 Z = -5225980
62
XDOT = -21464
183735 XDOT = -6542
283202
YDOT = -10304
252857 feet/sec YDOT = -3140
736271 meter/sec
ZDOT = -3778
929845 ZDOT = -1151
817817
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 19097
85976356
00016717 00000-0 10270-3 0 9035
2 25544 51
6411 350
8225 0002120 163
1465 196
9758 15
52512526 4324
Satellite: ISS
Catalog Number: 25544
Epoch time: 19097
85976356 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 350
8225 deg
Eccentricity:
0002120
Arg of perigee: 163
1465 deg
Mean anomaly: 196
9758 deg
Mean motion: 15
52512526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 313
Coasting Arc #5 (Orbit 447)
---------------------------------------
Vector Time (GMT): 2019/098/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 935393
29 A = 6782020
80 meter
Y = 4114521
48 meter E =
0003265
Z = 5307097
34 I = 51
52738
XDOT = -7441
964182 Wp = 120
13070
YDOT = 1846
393136 meter/sec RA = 345
34528 deg
ZDOT = -121
362930 TA = 331
01852
MA = 331
03665
Ha = 223
745 n
mi
Hp = 217
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3068875
63 X = 863534
74
Y = 13499086
21 feet Y = 4124580
16 meter
Z = 17411736
69 Z = 5311466
47
XDOT = -24415
892987 XDOT = -7461
468450
YDOT = 6057
720261 feet/sec YDOT = 1763
062824 meter/sec
ZDOT = -398
172342 ZDOT = -157
561155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6647863
38 X = 2026268
76
Y = -12115196
25 feet Y = -3692711
82 meter
Z = 17431002
06 Z = 5312969
43
XDOT = 21497
288815 XDOT = 6552
373631
YDOT = 10994
636754 feet/sec YDOT = 3351
165283 meter/sec
ZDOT = -562
066368 ZDOT = -171
317829
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 19098
88967055
00016717 00000-0 10270-3 0 9046
2 25544 51
6417 345
7001 0002042 169
3379 190
7816 15
52527161 4485
Satellite: ISS
Catalog Number: 25544
Epoch time: 19098
88967055 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 345
7001 deg
Eccentricity:
0002042
Arg of perigee: 169
3379 deg
Mean anomaly: 190
7816 deg
Mean motion: 15
52527161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 448
Checksum: 325
Coasting Arc #6 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2019/099/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 162220
13 A = 6782723
62 meter
Y = -4415523
69 meter E =
0014609
Z = -5159098
58 I = 51
49836
XDOT = 7382
873600 Wp = 108
34678
YDOT = -1416
410892 meter/sec RA = 340
35492 deg
ZDOT = 1443
277560 TA = 175
60077
MA = 175
58791
Ha = 223
773 n
mi
Hp = 216
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 532218
27 X = 236644
05
Y = -14486626
27 feet Y = -4413293
64 meter
Z = -16926176
43 Z = -5158129
68
XDOT = 24222
026248 XDOT = 7391
152872
YDOT = -4647
017361 feet/sec YDOT = -1333
804103 meter/sec
ZDOT = 4735
162597 ZDOT = 1479
161375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9826458
30 X = -2995104
49
Y = 10665476
90 feet Y = 3250837
36 meter
Z = -16921269
61 Z = -5157602
98
XDOT = -20717
728852 XDOT = -6314
763754
YDOT = -11311
814653 feet/sec YDOT = -3447
841106 meter/sec
ZDOT = 4897
575157 ZDOT = 1492
780908
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 19099
85520390
00016717 00000-0 10270-3 0 9052
2 25544 51
6422 340
8996 0002054 168
9770 191
1427 15
52540675 4638
Satellite: ISS
Catalog Number: 25544
Epoch time: 19099
85520390 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 340
8996 deg
Eccentricity:
0002054
Arg of perigee: 168
9770 deg
Mean anomaly: 191
1427 deg
Mean motion: 15
52540675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 324
Coasting Arc #7 (Orbit 478)
---------------------------------------
Vector Time (GMT): 2019/100/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1205728
90 A = 6784569
80 meter
Y = 4700959
37 meter E =
0007450
Z = 4735450
74 I = 51
47281
XDOT = -7121
291045 Wp = 77
50387
YDOT = 899
739294 meter/sec RA = 335
36356 deg
ZDOT = -2701
214995 TA = 39
28065
MA = 39
22663
Ha = 223
829 n
mi
Hp = 217
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3955803
48 X = -1281209
15
Y = 15423095
06 feet Y = 4687054
09 meter
Z = 15536255
69 Z = 4729410
32
XDOT = -23363
815764 XDOT = -7117
701796
YDOT = 2951
900570 feet/sec YDOT = 820
124075 meter/sec
ZDOT = -8862
253921 ZDOT = -2735
799160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12881217
04 X = 3926194
95
Y = -9405299
15 feet Y = -2866735
18 meter
Z = 15508387
37 Z = 4726956
47
XDOT = 19256
412662 XDOT = 5869
354579
YDOT = 11473
991985 feet/sec YDOT = 3497
272757 meter/sec
ZDOT = -9018
722366 ZDOT = -2748
906577
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 19100
88510230
00016717 00000-0 10270-3 0 9061
2 25544 51
6418 335
7776 0002044 169
9947 190
1246 15
52508838 4798
Satellite: ISS
Catalog Number: 25544
Epoch time: 19100
88510230 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 335
7776 deg
Eccentricity:
0002044
Arg of perigee: 169
9947 deg
Mean anomaly: 190
1246 deg
Mean motion: 15
52508838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 479
Checksum: 323
Coasting Arc #8 (Orbit 493)
---------------------------------------
Vector Time (GMT): 2019/101/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2145527
32 A = 6786922
64 meter
Y = -4975125
51 meter E =
0008181
Z = -4096563
34 I = 51
45155
XDOT = 6634
617010 Wp = 121
58407
YDOT = -277
451265 meter/sec RA = 330
37526 deg
ZDOT = 3813
197000 TA = 187
95799
MA = 187
97098
Ha = 223
654 n
mi
Hp = 217
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7039131
63 X = 2220900
05
Y = -16322590
26 feet Y = -4950711
30 meter
Z = -13440168
42 Z = -4085958
03
XDOT = 21767
116173 XDOT = 6618
703967
YDOT = -910
273180 feet/sec YDOT = -203
347297 meter/sec
ZDOT = 12510
488845 ZDOT = 3845
386989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15687063
36 X = -4781416
91
Y = 8437691
05 feet Y = 2571808
23 meter
Z = -13391634
22 Z = -4081770
11
XDOT = -17001
590837 XDOT = -5182
084887
YDOT = -11529
605050 feet/sec YDOT = -3514
223619 meter/sec
ZDOT = 12656
054495 ZDOT = 3857
565410
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 19101
85062650
00016717 00000-0 10270-3 0 9078
2 25544 51
6422 330
9770 0002011 179
2114 180
9041 15
52536151 4944
Satellite: ISS
Catalog Number: 25544
Epoch time: 19101
85062650 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 330
9770 deg
Eccentricity:
0002011
Arg of perigee: 179
2114 deg
Mean anomaly: 180
9041 deg
Mean motion: 15
52536151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 494
Checksum: 276
Coasting Arc #9 (Orbit 509)
---------------------------------------
Vector Time (GMT): 2019/102/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2967694
00 A = 6789627
69 meter
Y = 5175169
32 meter E =
0013085
Z = 3227677
21 I = 51
43233
XDOT = -5999
645498 Wp = 101
86749
YDOT = -466
246770 meter/sec RA = 325
38889 deg
ZDOT = -4755
095369 TA = 40
64335
MA = 40
54576
Ha = 223
686 n
mi
Hp = 217
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9736528
88 X = -3041021
93
Y = 16978901
97 feet Y = 5141572
51 meter
Z = 10589492
16 Z = 3213083
11
XDOT = -19683
876305 XDOT = -5970
888256
YDOT = -1529
681004 feet/sec YDOT = -533
178248 meter/sec
ZDOT = -15600
706591 ZDOT = -4784
169573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18070606
58 X = 5507920
88
Y = -7611964
86 feet Y = -2320126
89 meter
Z = 10522909
29 Z = 3207382
75
XDOT = 14126
685062 XDOT = 4305
813607
YDOT = 11725
433791 feet/sec YDOT = 3573
912220 meter/sec
ZDOT = -15732
095300 ZDOT = -4795
142648
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 19102
88051573
00016717 00000-0 10270-3 0 9085
2 25544 51
6424 325
8553 0001997 179
8473 180
2680 15
52528935 5106
Satellite: ISS
Catalog Number: 25544
Epoch time: 19102
88051573 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 325
8553 deg
Eccentricity:
0001997
Arg of perigee: 179
8473 deg
Mean anomaly: 180
2680 deg
Mean motion: 15
52528935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 510
Checksum: 325
Coasting Arc #10 (Orbit 524)
---------------------------------------
Vector Time (GMT): 2019/103/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3622372
67 A = 6791964
76 meter
Y = -5297280
62 meter E =
0004844
Z = -2222425
88 I = 51
41362
XDOT = 5235
437552 Wp = 53
86573
YDOT = 1302
506088 meter/sec RA = 320
40591 deg
ZDOT = 5439
854022 TA = 281
38491
MA = 281
43933
Ha = 223
558 n
mi
Hp = 217
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11884424
78 X = 3692134
44
Y = -17379529
59 feet Y = -5256382
70 meter
Z = -7291423
48 Z = -2204660
23
XDOT = 17176
632388 XDOT = 5194
059713
YDOT = 4273
313936 feet/sec YDOT = 1360
821172 meter/sec
ZDOT = 17847
290099 ZDOT = 5465
185238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19889507
46 X = -6062321
87
Y = 6990611
19 feet Y = 2130738
29 meter
Z = -7210499
69 Z = -2197760
30
XDOT = -10738
828688 XDOT = -3273
194984
YDOT = -12065
242519 feet/sec YDOT = -3677
485920 meter/sec
ZDOT = 17961
658716 ZDOT = 5474
713577
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 19103
84603134
00016717 00000-0 10270-3 0 9099
2 25544 51
6427 321
0542 0001704 187
9974 172
1151 15
52518698 5251
Satellite: ISS
Catalog Number: 25544
Epoch time: 19103
84603134 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 321
0542 deg
Eccentricity:
0001704
Arg of perigee: 187
9974 deg
Mean anomaly: 172
1151 deg
Mean motion: 15
52518698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 525
Checksum: 304
Coasting Arc #11 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2019/104/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4132015
50 A = 6793493
24 meter
Y = 5274500
94 meter E =
0014511
Z = 1073561
05 I = 51
39281
XDOT = -4398
916927 Wp = 130
00542
YDOT = -2242
985686 meter/sec RA = 315
42551 deg
ZDOT = -5867
391374 TA = 38
31393
MA = 38
21093
Ha = 223
523 n
mi
Hp = 217
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13556481
31 X = -4195904
12
Y = 17304793
11 feet Y = 5227936
67 meter
Z = 3522181
92 Z = 1053333
93
XDOT = -14432
142150 XDOT = -4345
007839
YDOT = -7358
876923 feet/sec YDOT = -2291
876272 meter/sec
ZDOT = -19249
971700 ZDOT = -5888
628574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21069166
32 X = 6421881
89
Y = -6321719
33 feet Y = -1926860
05 meter
Z = 3430147
34 Z = 1045508
91
XDOT = 6989
872161 XDOT = 2130
513035
YDOT = 12719
446342 feet/sec YDOT = 3876
887245 meter/sec
ZDOT = -19345
725497 ZDOT = -5896
577131
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 19104
87591321
00016717 00000-0 10270-3 0 9109
2 25544 51
6415 315
9333 0001890 187
6229 172
4895 15
52539417 5412
Satellite: ISS
Catalog Number: 25544
Epoch time: 19104
87591321 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 315
9333 deg
Eccentricity:
0001890
Arg of perigee: 187
6229 deg
Mean anomaly: 172
4895 deg
Mean motion: 15
52539417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 315
Coasting Arc #12 (Orbit 556)
---------------------------------------
Vector Time (GMT): 2019/105/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4463159
15 A = 6793953
86 meter
Y = -5115023
03 meter E =
0010943
Z = 98199
45 I = 51
37171
XDOT = 3544
654102 Wp = 51
10600
YDOT = 3216
385433 meter/sec RA = 310
44429 deg
ZDOT = 5986
885544 TA = 309
95489
MA = 310
05096
Ha = 223
447 n
mi
Hp = 217
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14642910
61 X = 4519548
09
Y = -16781571
63 feet Y = -5064797
57 meter
Z = 322176
66 Z = 120017
04
XDOT = 11629
442593 XDOT = 3479
343196
YDOT = 10552
445645 feet/sec YDOT = 3255
659430 meter/sec
ZDOT = 19642
012940 ZDOT = 6003
945293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21540488
08 X = -6565540
77
Y = 5654166
46 feet Y = 1723389
94 meter
Z = 421367
19 Z = 128432
72
XDOT = -3167
601714 XDOT = -965
485003
YDOT = -13620
056804 feet/sec YDOT = -4151
393314 meter/sec
ZDOT = 19718
776093 ZDOT = 6010
282953
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 19105
90579037
00016717 00000-0 10270-3 0 9115
2 25544 51
6418 310
8116 0001685 195
1398 164
9703 15
52536585 5575
Satellite: ISS
Catalog Number: 25544
Epoch time: 19105
90579037 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 310
8116 deg
Eccentricity:
0001685
Arg of perigee: 195
1398 deg
Mean anomaly: 164
9703 deg
Mean motion: 15
52536585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 557
Checksum: 324
Coasting Arc #13 (Orbit 571)
---------------------------------------
Vector Time (GMT): 2019/106/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4665218
45 A = 6793139
32 meter
Y = 4756636
80 meter E =
0009849
Z = -1300629
88 I = 51
34772
XDOT = -2693
039589 Wp = 150
05461
YDOT = -4220
915333 meter/sec RA = 305
46178 deg
ZDOT = -5804
429751 TA = 44
14726
MA = 44
06870
Ha = 223
331 n
mi
Hp = 217
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15305834
80 X = -4711744
03
Y = 15605763
78 feet Y = 4704206
82 meter
Z = -4267158
41 Z = -1323405
18
XDOT = -8835
431723 XDOT = -2617
445204
YDOT = -13848
147417 feet/sec YDOT = -4250
608558 meter/sec
ZDOT = -19043
404696 ZDOT = -5817
327626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21328545
26 X = 6500940
60
Y = -4691257
50 feet Y = -1429895
29 meter
Z = -4370622
73 Z = -1332165
81
XDOT = -640
615241 XDOT = -195
259525
YDOT = 14801
361702 feet/sec YDOT = 4511
455047 meter/sec
ZDOT = -19101
249613 ZDOT = -5822
060882
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 19106
87129503
00016717 00000-0 10270-3 0 9122
2 25544 51
6410 306
0102 0001686 197
3819 162
7275 15
52559997 5721
Satellite: ISS
Catalog Number: 25544
Epoch time: 19106
87129503 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 306
0102 deg
Eccentricity:
0001686
Arg of perigee: 197
3819 deg
Mean anomaly: 162
7275 deg
Mean motion: 15
52559997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 572
Checksum: 317
Coasting Arc #14 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2019/107/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4725701
91 A = 6791354
39 meter
Y = -4235035
64 meter E =
0012863
Z = 2404807
00 I = 51
32310
XDOT = 1908
955131 Wp = 79
91487
YDOT = 5169
599819 meter/sec RA = 300
47477 deg
ZDOT = 5330
546566 TA = 307
08111
MA = 307
19863
Ha = 223
289 n
mi
Hp = 217
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15504271
35 X = 4761026
76
Y = -13894473
90 feet Y = -4181991
83 meter
Z = 7889786
74 Z = 2427848
99
XDOT = 6262
976153 XDOT = 1825
112301
YDOT = 16960
629328 feet/sec YDOT = 5190
478733 meter/sec
ZDOT = 17488
669837 ZDOT = 5339
615557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20479522
40 X = -6242158
43
Y = 3516606
23 feet Y = 1071861
58 meter
Z = 7994386
30 Z = 2436688
94
XDOT = 4100
426981 XDOT = 1249
810144
YDOT = -16133
161394 feet/sec YDOT = -4917
387593 meter/sec
ZDOT = 17529
112615 ZDOT = 5342
873525
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 19107
90116311
00016717 00000-0 10270-3 0 9131
2 25544 51
6406 300
8882 0001595 200
7643 159
3444 15
52569831 5881
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
90116311 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 300
8882 deg
Eccentricity:
0001595
Arg of perigee: 200
7643 deg
Mean anomaly: 159
3444 deg
Mean motion: 15
52569831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 306
Coasting Arc #15 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2019/107/20:48:33
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2675162
54 A = 6793411
28 meter
Y = 6156228
85 meter E =
0013932
Z = 997594
08 I = 51
32922
XDOT = -4793
668086 Wp = 129
89549
YDOT = -1122
975881 meter/sec RA = 300
31827 deg
ZDOT = -5878
868234 TA = 39
25160
MA = 39
15067
Ha = 223
291 n
mi
Hp = 217
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8776780
00 X = -2748650
21
Y = 20197601
21 feet Y = 6125902
49 meter
Z = 3272946
46 Z = 984420
06
XDOT = -15727
257499 XDOT = -4752
197892
YDOT = -3684
304071 feet/sec YDOT = -1176
350639 meter/sec
ZDOT = -19287
625441 ZDOT = -5902
053425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16005956
45 X = 4878615
53
Y = -15138519
03 feet Y = -4614220
60 meter
Z = 3212746
51 Z = 979245
14
XDOT = 11804
384177 XDOT = 3597
976297
YDOT = 8332
697239 feet/sec YDOT = 2539
806119 meter/sec
ZDOT = -19392
303075 ZDOT = -5910
773977
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 19107
90116332
00016717 00000-0 10270-3 0 9145
2 25544 51
6402 300
8887 0001436 200
6686 159
4408 15
52586903 5882
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
90116332 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 300
8887 deg
Eccentricity:
0001436
Arg of perigee: 200
6686 deg
Mean anomaly: 159
4408 deg
Mean motion: 15
52586903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 311
Coasting Arc #16 (Orbit 603)
---------------------------------------
Vector Time (GMT): 2019/108/20:48:33
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3034408
86 A = 6793959
79 meter
Y = -6070214
00 meter E =
0011228
Z = 181504
62 I = 51
31395
XDOT = 4212
835010 Wp = 49
65102
YDOT = 2291
847031 meter/sec RA = 295
33262 deg
ZDOT = 5979
811775 TA = 312
31180
MA = 312
40689
Ha = 223
345 n
mi
Hp = 217
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9955409
63 X = 3101180
53
Y = -19915400
26 feet Y = -6035907
76 meter
Z = 595487
59 Z = 196407
44
XDOT = 13821
637172 XDOT = 4157
846860
YDOT = 7519
183171 feet/sec YDOT = 2338
650886 meter/sec
ZDOT = 19618
805036 ZDOT = 6000
142666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16705269
72 X = -5091766
21
Y = 14716715
40 feet Y = 4485654
85 meter
Z = 663479
67 Z = 202228
60
XDOT = -8787
665795 XDOT = -2678
480534
YDOT = -10895
266921 feet/sec YDOT = -3320
877358 meter/sec
ZDOT = 19710
456745 ZDOT = 6007
747216
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 19108
93103040
00016717 00000-0 10270-3 0 9152
2 25544 51
6394 295
7666 0001337 207
0261 153
0821 15
52531182 6046
Satellite: ISS
Catalog Number: 25544
Epoch time: 19108
93103040 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 295
7666 deg
Eccentricity:
0001337
Arg of perigee: 207
0261 deg
Mean anomaly: 153
0821 deg
Mean motion: 15
52531182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 604
Checksum: 282
Coasting Arc #17 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2019/109/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4479124
47 A = 6789263
91 meter
Y = -3910528
44 meter E =
0011821
Z = 3267299
03 I = 51
29277
XDOT = 1644
490981 Wp = 92
13357
YDOT = 5827
062897 meter/sec RA = 292
75142 deg
ZDOT = 4704
584786 TA = 305
97341
MA = 306
08298
Ha = 223
113 n
mi
Hp = 217
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14695290
25 X = 4506649
26
Y = -12829817
73 feet Y = -3860285
62 meter
Z = 10719485
01 Z = 3289124
35
XDOT = 5395
311618 XDOT = 1556
356299
YDOT = 19117
660424 feet/sec YDOT = 5844
960262 meter/sec
ZDOT = 15434
989457 ZDOT = 4712
358774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17270152
01 X = 5263942
33
Y = -8953451
07 feet Y = -2729011
89 meter
Z = 10818535
06 Z = 3297489
49
XDOT = -94
074898 XDOT = -28
674029
YDOT = 18570
286949 feet/sec YDOT = 5660
223462 meter/sec
ZDOT = 15469
520774 ZDOT = 4715
109932
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 19109
44595935
00016717 00000-0 10270-3 0 9168
2 25544 51
6407 293
2071 0001232 221
9044 138
2014 15
52569508 6123
Satellite: ISS
Catalog Number: 25544
Epoch time: 19109
44595935 = yrday
fracday
Element set: 916
Inclination: 51
6407 deg
RA of node: 293
2071 deg
Eccentricity:
0001232
Arg of perigee: 221
9044 deg
Mean anomaly: 138
2014 deg
Mean motion: 15
52569508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 295
Coasting Arc #18 (Orbit 626)
---------------------------------------
Vector Time (GMT): 2019/110/09:19:21
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4452083
30 A = 6786494
12 meter
Y = 3033567
71 meter E =
0006526
Z = -4133777
01 I = 51
27139
XDOT = -1032
962810 Wp = 74
67286
YDOT = -6604
982230 meter/sec RA = 287
75201 deg
ZDOT = -3737
817206 TA = 156
61841
MA = 156
58872
Ha = 223
073 n
mi
Hp = 217
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14606572
50 X = -4465594
70
Y = 9952649
95 feet Y = 2983705
67 meter
Z = -13562260
52 Z = -4155436
86
XDOT = -3388
985596 XDOT = -940
870704
YDOT = -21669
889207 feet/sec YDOT = -6616
018781 meter/sec
ZDOT = -12263
179809 ZDOT = -3742
611080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16367555
61 X = -4988830
95
Y = 6468144
90 feet Y = 1971490
56 meter
Z = -13660466
20 Z = -4163710
10
XDOT = 2075
487703 XDOT = 632
608652
YDOT = -20669
254823 feet/sec YDOT = -6299
988870 meter/sec
ZDOT = -12284
169112 ZDOT = -3744
214745
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 19110
41145022
00016717 00000-0 10270-3 0 9176
2 25544 51
6403 288
4041 0001291 228
3379 131
7662 15
52583922 6278
Satellite: ISS
Catalog Number: 25544
Epoch time: 19110
41145022 = yrday
fracday
Element set: 917
Inclination: 51
6403 deg
RA of node: 288
4041 deg
Eccentricity:
0001291
Arg of perigee: 228
3379 deg
Mean anomaly: 131
7662 deg
Mean motion: 15
52583922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 627
Checksum: 288
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