[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 1st 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19998 2692 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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
306/13:59:45
869 0
0 0
0 0
0
N/A 0
0 0
0 227
1
000/00:00:00
000 0
0 0
0 222
1
308/07:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 222
3
308/09:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 222
2
311/22:41:23
984 1
1 1
5 1
5
N/A 0
7 -0
0 225
9
000/00:06:43
968 0
7 -0
0 223
8
312/03:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
9
000/00:00:00
000 0
0 0
0 223
6
317/14:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
2
000/00:00:00
000 0
0 0
0 223
7
Coasting Arc #1 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2019/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5512111
99 A = 6794238
19 meter
Y = 565318
23 meter E =
0007512
Z = -3939525
78 I = 51
89232
XDOT = 2292
724330 Wp = 160
72664
YDOT = 6061
614581 meter/sec RA = 39
74771 deg
ZDOT = 4073
088640 TA = 151
84646
MA = 151
80583
Ha = 227
198 n
mi
Hp = 222
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18084356
93 X = 5524517
16
Y = 1854718
59 feet Y = 627028
07 meter
Z = -12924953
34 Z = -3912719
33
XDOT = 7522
061450 XDOT = 2204
986013
YDOT = 19887
186947 feet/sec YDOT = 6086
762705 meter/sec
ZDOT = 13363
151707 ZDOT = 4084
013187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15183706
57 X = -4627993
76
Y = 10153018
41 feet Y = 3094640
01 meter
Z = -12802719
91 Z = -3902269
03
XDOT = -17662
080415 XDOT = -5383
402110
YDOT = -9481
111157 feet/sec YDOT = -2889
842681 meter/sec
ZDOT = 13412
406450 ZDOT = 4088
101486
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 19305
50844130
00016717 00000-0 10270-3 0 9000
2 25544 51
6444 40
3930 0006560 215
1480 144
9238 15
50241010 36552
Satellite: ISS
Catalog Number: 25544
Epoch time: 19305
50844130 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 40
3930 deg
Eccentricity:
0006560
Arg of perigee: 215
1480 deg
Mean anomaly: 144
9238 deg
Mean motion: 15
50241010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3655
Checksum: 266
Coasting Arc #2 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2019/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916487
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5711971
25 A = 6795208
30 meter
Y = -494561
87 meter E =
0009121
Z = 3636442
71 I = 51
86864
XDOT = -2308
747642 Wp = 118
75024
YDOT = -5825
872052 meter/sec RA = 34
80877 deg
ZDOT = -4414
708579 TA = 18
33397
MA = 18
30111
Ha = 227
229 n
mi
Hp = 222
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18740063
15 X = -5723680
48
Y = -1622578
32 feet Y = -558502
77 meter
Z = 11930586
32 Z = 3608667
21
XDOT = -7574
631371 XDOT = -2221
984926
YDOT = -19113
753453 feet/sec YDOT = -5851
204817 meter/sec
ZDOT = -14483
952031 ZDOT = -4425
713261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15348737
93 X = 4678295
32
Y = -11011136
86 feet Y = -3356194
52 meter
Z = 11803928
42 Z = 3597837
38
XDOT = 17310
001105 XDOT = 5276
088337
YDOT = 8534
329849 feet/sec YDOT = 2601
263738 meter/sec
ZDOT = -14533
585618 ZDOT = -4429
836896
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 19306
53985895
00016717 00000-0 10270-3 0 9019
2 25544 51
6440 35
2821 0006503 218
0790 141
9902 15
50233096 36711
Satellite: ISS
Catalog Number: 25544
Epoch time: 19306
53985895 = yrday
fracday
Element set: 901
Inclination: 51
6440 deg
RA of node: 35
2821 deg
Eccentricity:
0006503
Arg of perigee: 218
0790 deg
Mean anomaly: 141
9902 deg
Mean motion: 15
50233096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 304
Coasting Arc #3 (Orbit 3671)
---------------------------------------
Vector Time (GMT): 2019/306/13:59:45
869
Vector Time (MET): N/A
Weight (LBS) : 916487
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -576479
18 A = 6791365
63 meter
Y = -4872270
61 meter E =
0006219
Z = -4700459
15 I = 51
85244
XDOT = 6827
133860 Wp = 103
01816
YDOT = 1952
821886 meter/sec RA = 34
44522 deg
ZDOT = -2866
058743 TA = 138
58564
MA = 138
53848
Ha = 227
050 n
mi
Hp = 222
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1891335
90 X = -499120
63
Y = -15985139
79 feet Y = -4878284
50 meter
Z = -15421453
91 Z = -4703071
79
XDOT = 22398
733136 XDOT = 6818
711361
YDOT = 6406
895953 feet/sec YDOT = 2029
120725 meter/sec
ZDOT = -9403
079864 ZDOT = -2832
914971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15672325
66 X = 4776924
86
Y = 3623117
02 feet Y = 1104326
07 meter
Z = -15432897
25 Z = -4703947
08
XDOT = -13237
956216 XDOT = -4034
929055
YDOT = 17916
544725 feet/sec YDOT = 5460
962832 meter/sec
ZDOT = -9252
075450 ZDOT = -2820
032597
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 19306
60432216
00016717 00000-0 10270-3 0 9022
2 25544 51
6427 34
9636 0006448 219
3169 140
7514 15
50225985 36723
Satellite: ISS
Catalog Number: 25544
Epoch time: 19306
60432216 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 34
9636 deg
Eccentricity:
0006448
Arg of perigee: 219
3169 deg
Mean anomaly: 140
7514 deg
Mean motion: 15
50225985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3672
Checksum: 309
Coasting Arc #4 (Orbit 3687)
---------------------------------------
Vector Time (GMT): 2019/307/13:59:45
869
Vector Time (MET): N/A
Weight (LBS) : 916487
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 514996
60 A = 6790563
88 meter
Y = 4698039
04 meter E =
0008251
Z = 4877703
27 I = 51
82222
XDOT = -7039
444580 Wp = 168
98010
YDOT = -1774
833041 meter/sec RA = 29
50119 deg
ZDOT = 2444
119242 TA = 257
02678
MA = 257
11893
Ha = 226
777 n
mi
Hp = 222
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1689621
40 X = 438730
02
Y = 15413513
92 feet Y = 4703371
54 meter
Z = 16002963
49 Z = 4880019
85
XDOT = -23095
290617 XDOT = -7030
947015
YDOT = -5822
943047 feet/sec YDOT = -1853
505630 meter/sec
ZDOT = 8018
763918 ZDOT = 2409
944425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15125046
99 X = -4610114
32
Y = -3367591
50 feet Y = -1026441
89 meter
Z = 16013068
21 Z = 4880783
19
XDOT = 12589
791932 XDOT = 3837
368581
YDOT = -19022
315059 feet/sec YDOT = -5798
001630 meter/sec
ZDOT = 7863
045472 ZDOT = 2396
656260
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 19307
63573468
00016717 00000-0 10270-3 0 9032
2 25544 51
6431 29
8520 0006375 224
0999 135
9644 15
50254395 36880
Satellite: ISS
Catalog Number: 25544
Epoch time: 19307
63573468 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node: 29
8520 deg
Eccentricity:
0006375
Arg of perigee: 224
0999 deg
Mean anomaly: 135
9644 deg
Mean motion: 15
50254395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3688
Checksum: 336
Coasting Arc #5 (Orbit 3698)
---------------------------------------
Vector Time (GMT): 2019/308/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916487
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1169872
27 A = 6791065
09 meter
Y = 4721041
85 meter E =
0008382
Z = 4740935
76 I = 51
80146
XDOT = -7070
234778 Wp = 163
68633
YDOT = -1030
293639 meter/sec RA = 25
99729 deg
ZDOT = 2761
589884 TA = 258
96002
MA = 259
05431
Ha = 226
699 n
mi
Hp = 222
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3838163
62 X = 1093964
16
Y = 15488982
44 feet Y = 4733699
67 meter
Z = 15554251
19 Z = 4746434
34
XDOT = -23196
308326 XDOT = -7071
602683
YDOT = -3380
228473 feet/sec YDOT = -1109
365692 meter/sec
ZDOT = 9060
334265 ZDOT = 2727
241599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5214549
15 X = 1589394
58
Y = -15055969
90 feet Y = -4589059
63 meter
Z = 15578865
64 Z = 4748438
25
XDOT = 16659
807954 XDOT = 5077
909464
YDOT = 15013
621064 feet/sec YDOT = 4576
151700 meter/sec
ZDOT = 8903
756640 ZDOT = 2713
865024
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 19308
34482997
00016717 00000-0 10270-3 0 9048
2 25544 51
6414 26
3343 0006394 225
4729 134
5899 15
50267178 36995
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
34482997 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 26
3343 deg
Eccentricity:
0006394
Arg of perigee: 225
4729 deg
Mean anomaly: 134
5899 deg
Mean motion: 15
50267178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3699
Checksum: 347
Coasting Arc #6 (Orbit 3699)
---------------------------------------
Vector Time (GMT): 2019/308/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 931200
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4642918
96 A = 6798071
45 meter
Y = -4328225
74 meter E =
0008210
Z = -2419550
91 I = 51
82432
XDOT = 4951
903179 Wp = 182
95335
YDOT = -2313
387908 meter/sec RA = 25
55137 deg
ZDOT = -5371
154847 TA = 23
98890
MA = 23
95067
Ha = 226
713 n
mi
Hp = 222
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15232673
75 X = -4582421
44
Y = -14200215
67 feet Y = -4379807
83 meter
Z = -7938159
16 Z = -2441957
86
XDOT = 16246
401506 XDOT = 5003
494502
YDOT = -7589
855341 feet/sec YDOT = -2257
723677 meter/sec
ZDOT = -17621
899104 ZDOT = -5346
974814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15162823
58 X = 4621628
63
Y = 14217700
37 feet Y = 4333555
07 meter
Z = -8039939
22 Z = -2450573
48
XDOT = -15336
703952 XDOT = -4674
627365
YDOT = 6466
886074 feet/sec YDOT = 1971
106875 meter/sec
ZDOT = -17511
373233 ZDOT = -5337
466561
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 19308
40929352
00016717 00000-0 10270-3 0 9057
2 25544 51
6437 26
0153 0006425 224
9648 135
0983 15
50256530 37008
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
40929352 = yrday
fracday
Element set: 905
Inclination: 51
6437 deg
RA of node: 26
0153 deg
Eccentricity:
0006425
Arg of perigee: 224
9648 deg
Mean anomaly: 135
0983 deg
Mean motion: 15
50256530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3700
Checksum: 299
Coasting Arc #7 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2019/309/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 931200
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4658820
64 A = 6797207
66 meter
Y = 4090987
54 meter E =
0008614
Z = 2781303
58 I = 51
79122
XDOT = -5162
480897 Wp = 102
68104
YDOT = 2377
376363 meter/sec RA = 20
60870 deg
ZDOT = 5135
288933 TA = 288
71102
MA = 288
80450
Ha = 226
578 n
mi
Hp = 222
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15284844
62 X = 4599217
59
Y = 13421875
14 feet Y = 4142752
49 meter
Z = 9125011
74 Z = 2803789
89
XDOT = -16937
273284 XDOT = -5213
626390
YDOT = 7799
791218 feet/sec YDOT = 2319
359864 meter/sec
ZDOT = 16848
060804 ZDOT = 5110
087034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15436778
47 X = -4705130
08
Y = -13175897
05 feet Y = -4016013
42 meter
Z = 9227169
34 Z = 2812441
22
XDOT = 15962
165422 XDOT = 4865
268021
YDOT = -6948
319681 feet/sec YDOT = -2117
847839 meter/sec
ZDOT = 16732
872985 ZDOT = 5100
179686
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 19309
44070046
00016717 00000-0 10270-3 0 9060
2 25544 51
6439 20
9043 0006412 228
4115 131
6486 15
50279057 37161
Satellite: ISS
Catalog Number: 25544
Epoch time: 19309
44070046 = yrday
fracday
Element set: 906
Inclination: 51
6439 deg
RA of node: 20
9043 deg
Eccentricity:
0006412
Arg of perigee: 228
4115 deg
Mean anomaly: 131
6486 deg
Mean motion: 15
50279057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 295
Coasting Arc #8 (Orbit 3730)
---------------------------------------
Vector Time (GMT): 2019/310/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 931200
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4615789
79 A = 6796353
47 meter
Y = -3867853
16 meter E =
0004904
Z = -3144047
71 I = 51
75655
XDOT = 5380
347835 Wp = 187
00949
YDOT = -2471
462007 meter/sec RA = 15
66379 deg
ZDOT = -4862
428844 TA = 29
09582
MA = 29
06851
Ha = 226
391 n
mi
Hp = 222
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15143667
28 X = -4556923
04
Y = -12689806
94 feet Y = -3919141
06 meter
Z = -10315117
16 Z = -3166326
77
XDOT = 17652
059827 XDOT = 5431
203845
YDOT = -8108
471152 feet/sec YDOT = -2411
010842 meter/sec
ZDOT = -15952
850539 ZDOT = -4836
169255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15487651
22 X = 4720636
09
Y = 12181788
00 feet Y = 3713008
98 meter
Z = -10416343
00 Z = -3174901
35
XDOT = -16591
337227 XDOT = -5057
039587
YDOT = 7566
550931 feet/sec YDOT = 2306
284724 meter/sec
ZDOT = -15832
836908 ZDOT = -4825
848690
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 19310
40764473
00016717 00000-0 10270-3 0 9073
2 25544 51
6440 16
1131 0006432 232
3561 127
7007 15
50255962 37310
Satellite: ISS
Catalog Number: 25544
Epoch time: 19310
40764473 = yrday
fracday
Element set: 907
Inclination: 51
6440 deg
RA of node: 16
1131 deg
Eccentricity:
0006432
Arg of perigee: 232
3561 deg
Mean anomaly: 127
7007 deg
Mean motion: 15
50255962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3731
Checksum: 277
Coasting Arc #9 (Orbit 3746)
---------------------------------------
Vector Time (GMT): 2019/311/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 931200
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4559137
38 A = 6795339
13 meter
Y = 3650581
03 meter E =
0007905
Z = 3471214
91 I = 51
72189
XDOT = -5572
260825 Wp = 118
92967
YDOT = 2609
805672 meter/sec RA = 10
71533 deg
ZDOT = 4562
412466 TA = 281
67405
MA = 281
76274
Ha = 226
208 n
mi
Hp = 222
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14957799
81 X = 4501115
18
Y = 11976971
89 feet Y = 3701240
16 meter
Z = 11388500
35 Z = 3493220
84
XDOT = -18281
695620 XDOT = -5623
192296
YDOT = 8562
354568 feet/sec YDOT = 2547
208018 meter/sec
ZDOT = 14968
544837 ZDOT = 4535
220345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15466068
37 X = -4714057
64
Y = -11211459
85 feet Y = -3417252
96 meter
Z = 11488492
85 Z = 3501692
62
XDOT = 17109
210008 XDOT = 5214
887211
YDOT = -8352
194314 feet/sec YDOT = -2545
748827 meter/sec
ZDOT = 14844
273979 ZDOT = 4524
534709
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 19311
43904647
00016717 00000-0 10270-3 0 9087
2 25544 51
6449 11
0018 0006405 236
4219 123
6320 15
50290204 37470
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
43904647 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 11
0018 deg
Eccentricity:
0006405
Arg of perigee: 236
4219 deg
Mean anomaly: 123
6320 deg
Mean motion: 15
50290204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3747
Checksum: 281
Coasting Arc #10 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2019/311/22:44:45
968
Vector Time (MET): N/A
Weight (LBS) : 931051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5562676
58 A = 6796614
05 meter
Y = -1935432
34 meter E =
0002373
Z = -3392367
16 I = 51
70480
XDOT = 4324
257973 Wp = 221
41394
YDOT = 4294
041882 meter/sec RA = 7
86772 deg
ZDOT = 4637
299474 TA = 99
09597
MA = 99
06912
Ha = 225
907 n
mi
Hp = 223
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18250251
24 X = 5600384
23
Y = -6349843
65 feet Y = -1873015
80 meter
Z = -11129813
51 Z = -3365253
67
XDOT = 14187
198074 XDOT = 4253
393545
YDOT = 14088
063916 feet/sec YDOT = 4342
002655 meter/sec
ZDOT = 15214
237121 ZDOT = 4658
133254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13409951
91 X = 4087353
34
Y = -14010947
12 feet Y = -4270536
68 meter
Z = -11005974
92 Z = -3354621
16
XDOT = 17938
848002 XDOT = 5467
760871
YDOT = 5134
510964 feet/sec YDOT = 1564
998942 meter/sec
ZDOT = 15308
814021 ZDOT = 4666
126514
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 19311
95474772
00016717 00000-0 10270-3 0 9096
2 25544 51
6453 8
4501 0006638 252
4131 107
6288 15
49999110 37555
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
95474772 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 8
4501 deg
Eccentricity:
0006638
Arg of perigee: 252
4131 deg
Mean anomaly: 107
6288 deg
Mean motion: 15
49999110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 325
Coasting Arc #11 (Orbit 3757)
---------------------------------------
Vector Time (GMT): 2019/312/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 931051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1869143
85 A = 6790817
71 meter
Y = -4208881
50 meter E =
0006008
Z = -4996176
91 I = 51
67543
XDOT = 7324
660583 Wp = 77
07248
YDOT = -767
308962 meter/sec RA = 7
01196 deg
ZDOT = -2094
682009 TA = 172
52329
MA = 172
51433
Ha = 225
909 n
mi
Hp = 223
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6132361
71 X = -1797670
91
Y = -13808666
35 feet Y = -4229384
07 meter
Z = -16391656
52 Z = -5005082
99
XDOT = 24031
038659 XDOT = 7342
871453
YDOT = -2517
417854 feet/sec YDOT = -685
297654 meter/sec
ZDOT = -6872
316302 ZDOT = -2059
056671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13547868
92 X = -4129390
45
Y = 6589473
11 feet Y = 2008471
40 meter
Z = -16431847
80 Z = -5008427
21
XDOT = -3034
320363 XDOT = -924
860847
YDOT = -22963
727880 feet/sec YDOT = -6999
344258 meter/sec
ZDOT = -6709
781180 ZDOT = -2045
141304
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 19312
14816907
00016717 00000-0 10270-3 0 9100
2 25544 51
6411 7
4893 0006676 252
5534 107
4886 15
49988354 37585
Satellite: ISS
Catalog Number: 25544
Epoch time: 19312
14816907 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 7
4893 deg
Eccentricity:
0006676
Arg of perigee: 252
5534 deg
Mean anomaly: 107
4886 deg
Mean motion: 15
49988354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3758
Checksum: 339
Coasting Arc #12 (Orbit 3773)
---------------------------------------
Vector Time (GMT): 2019/313/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 931051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1819356
75 A = 6790500
35 meter
Y = 4103246
39 meter E =
0005001
Z = 5098568
98 I = 51
64014
XDOT = -7376
762263 Wp = 205
76457
YDOT = 1109
480645 meter/sec RA = 2
05805 deg
ZDOT = 1735
649095 TA = 227
41601
MA = 227
45821
Ha = 225
704 n
mi
Hp = 223
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5969018
20 X = 1748571
28
Y = 13462094
47 feet Y = 4123196
04 meter
Z = 16727588
51 Z = 5107234
91
XDOT = -24201
975930 XDOT = -7397
051540
YDOT = 3640
028364 feet/sec YDOT = 1026
875069 meter/sec
ZDOT = 5694
386795 ZDOT = 1699
765477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13096280
77 X = 3991746
38
Y = -6635880
33 feet Y = -2022616
32 meter
Z = 16766690
36 Z = 5110487
22
XDOT = 4572
585645 XDOT = 1393
724105
YDOT = 23029
485338 feet/sec YDOT = 7019
387131 meter/sec
ZDOT = 5530
654610 ZDOT = 1685
743525
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 19313
17975508
00016717 00000-0 10270-3 0 9118
2 25544 51
6406 2
3789 0006617 256
6690 103
3723 15
49946006 37741
Satellite: ISS
Catalog Number: 25544
Epoch time: 19313
17975508 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 2
3789 deg
Eccentricity:
0006617
Arg of perigee: 256
6690 deg
Mean anomaly: 103
3723 deg
Mean motion: 15
49946006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3774
Checksum: 323
Coasting Arc #13 (Orbit 3788)
---------------------------------------
Vector Time (GMT): 2019/314/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 931051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1749177
44 A = 6789992
14 meter
Y = -4026648
68 meter E =
0007359
Z = -5186347
68 I = 51
60475
XDOT = 7391
895180 Wp = 80
66552
YDOT = -1455
901558 meter/sec RA = 357
10147 deg
ZDOT = -1363
168722 TA = 176
20650
MA = 176
20091
Ha = 225
538 n
mi
Hp = 223
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5738771
13 X = -1678827
25
Y = -13210789
64 feet Y = -4045815
92 meter
Z = -17015576
37 Z = -5194673
82
XDOT = 24251
624606 XDOT = 7414
247793
YDOT = -4776
579914 feet/sec YDOT = -1373
115198 meter/sec
ZDOT = -4472
338327 ZDOT = -1327
206459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12747244
95 X = -3885360
26
Y = 6609594
92 feet Y = 2014604
53 meter
Z = -17053131
60 Z = -5197794
51
XDOT = -6122
663956 XDOT = -1866
187974
YDOT = -22919
495744 feet/sec YDOT = -6985
862303 meter/sec
ZDOT = -4308
227410 ZDOT = -1313
147715
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 19314
14686354
00016717 00000-0 10270-3 0 9125
2 25544 51
6399 357
5880 0006591 258
7249 101
3161 15
49992860 37892
Satellite: ISS
Catalog Number: 25544
Epoch time: 19314
14686354 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 357
5880 deg
Eccentricity:
0006591
Arg of perigee: 258
7249 deg
Mean anomaly: 101
3161 deg
Mean motion: 15
49992860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3789
Checksum: 351
Coasting Arc #14 (Orbit 3804)
---------------------------------------
Vector Time (GMT): 2019/315/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 931051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1679149
49 A = 6789832
96 meter
Y = 3971764
98 meter E =
0004409
Z = 5248195
87 I = 51
57068
XDOT = -7376
139696 Wp = 233
40340
YDOT = 1809
705375 meter/sec RA = 352
14188 deg
ZDOT = 988
428023 TA = 207
10280
MA = 207
12582
Ha = 225
290 n
mi
Hp = 223
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5509020
64 X = 1609117
73
Y = 13030724
99 feet Y = 3990150
81 meter
Z = 17218490
38 Z = 5256182
70
XDOT = -24199
933385 XDOT = -7400
629502
YDOT = 5937
353594 feet/sec YDOT = 1727
083235 meter/sec
ZDOT = 3242
874091 ZDOT = 952
537027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12473885
71 X = 3802040
36
Y = -6581028
89 feet Y = -2005897
60 meter
Z = 17254499
33 Z = 5259171
40
XDOT = 7684
098353 XDOT = 2342
113178
YDOT = 22654
636591 feet/sec YDOT = 6905
133233 meter/sec
ZDOT = 3079
065807 ZDOT = 938
499258
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 19315
17844581
00016717 00000-0 10270-3 0 9138
2 25544 51
6401 352
4770 0006597 263
3317 96
7083 15
49951589 38054
Satellite: ISS
Catalog Number: 25544
Epoch time: 19315
17844581 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 352
4770 deg
Eccentricity:
0006597
Arg of perigee: 263
3317 deg
Mean anomaly: 96
7083 deg
Mean motion: 15
49951589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3805
Checksum: 336
Coasting Arc #15 (Orbit 3819)
---------------------------------------
Vector Time (GMT): 2019/316/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 931051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1601261
63 A = 6789485
90 meter
Y = -3948095
33 meter E =
0008233
Z = -5293538
32 I = 51
53778
XDOT = 7320
359660 Wp = 84
96108
YDOT = -2158
390045 meter/sec RA = 347
18035 deg
ZDOT = -604
669689 TA = 179
25038
MA = 179
24915
Ha = 225
190 n
mi
Hp = 223
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5253483
04 X = -1531280
04
Y = -12953068
67 feet Y = -3965610
34 meter
Z = -17367251
71 Z = -5301147
01
XDOT = 24016
928019 XDOT = 7346
888573
YDOT = -7081
332170 feet/sec YDOT = -2076
380266 meter/sec
ZDOT = -1983
824440 ZDOT = -569
044696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12309910
18 X = -3752060
62
Y = 6531094
51 feet Y = 1990677
61 meter
Z = -17401534
99 Z = -5303987
86
XDOT = -9207
733386 XDOT = -2806
517136
YDOT = -22206
399619 feet/sec YDOT = -6768
510604 meter/sec
ZDOT = -1821
204851 ZDOT = -555
103238
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 19316
14554923
00016717 00000-0 10270-3 0 9145
2 25544 51
6408 347
6861 0006449 266
0884 93
9529 15
50005780 38209
Satellite: ISS
Catalog Number: 25544
Epoch time: 19316
14554923 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 347
6861 deg
Eccentricity:
0006449
Arg of perigee: 266
0884 deg
Mean anomaly: 93
9529 deg
Mean motion: 15
50005780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3820
Checksum: 328
Coasting Arc #16 (Orbit 3835)
---------------------------------------
Vector Time (GMT): 2019/317/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 931051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1527177
70 A = 6789535
96 meter
Y = 3947258
33 meter E =
0003974
Z = 5312368
22 I = 51
50373
XDOT = -7234
944439 Wp = 264
39128
YDOT = 2503
806300 meter/sec RA = 342
21570 deg
ZDOT = 219
225917 TA = 183
51144
MA = 183
51423
Ha = 225
162 n
mi
Hp = 223
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5010425
52 X = 1457119
51
Y = 12950322
60 feet Y = 3963944
33 meter
Z = 17429029
60 Z = 5319616
93
XDOT = -23736
694354 XDOT = -7263
469918
YDOT = 8214
587597 feet/sec YDOT = 2422
740536 meter/sec
ZDOT = 719
245136 ZDOT = 184
011064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12223993
64 X = 3725873
26
Y = -6500030
10 feet Y = -1981209
18 meter
Z = 17461668
89 Z = 5322316
68
XDOT = 10693
239459 XDOT = 3259
299387
YDOT = 21612
134866 feet/sec YDOT = 6587
378707 meter/sec
ZDOT = 558
469016 ZDOT = 170
221356
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 19317
17712716
00016717 00000-0 10270-3 0 9156
2 25544 51
6394 342
5749 0006393 270
0600 89
9818 15
49956432 38361
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
17712716 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 342
5749 deg
Eccentricity:
0006393
Arg of perigee: 270
0600 deg
Mean anomaly: 89
9818 deg
Mean motion: 15
49956432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3836
Checksum: 341
Coasting Arc #17 (Orbit 3842)
---------------------------------------
Vector Time (GMT): 2019/317/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 931051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2093624
21 A = 6792829
64 meter
Y = -4612105
53 meter E =
0003755
Z = -4530011
19 I = 51
49962
XDOT = 6984
180844 Wp = 137
99931
YDOT = 86
429104 meter/sec RA = 339
76585 deg
ZDOT = 3138
647433 TA = 163
59002
MA = 163
57786
Ha = 225
247 n
mi
Hp = 223
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6868845
84 X = 2167047
43
Y = -15131579
84 feet Y = -4588282
35 meter
Z = -14862241
43 Z = -4519662
79
XDOT = 22913
979148 XDOT = 6967
449039
YDOT = 283
560053 feet/sec YDOT = 164
437406 meter/sec
ZDOT = 10297
399715 ZDOT = 3172
534318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15585773
07 X = 4750543
63
Y = 5885852
90 feet Y = 1794007
96 meter
Z = -14814600
41 Z = -4515490
20
XDOT = 1754
744537 XDOT = 534
846135
YDOT = 21670
680445 feet/sec YDOT = 6605
223400 meter/sec
ZDOT = 10451
854597 ZDOT = 3185
725281
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 19317
62843935
00016717 00000-0 10270-3 0 9165
2 25544 51
6398 340
3433 0006530 274
7088 85
3316 15
49976491 38433
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
62843935 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 340
3433 deg
Eccentricity:
0006530
Arg of perigee: 274
7088 deg
Mean anomaly: 85
3316 deg
Mean motion: 15
49976491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3843
Checksum: 342
Coasting Arc #18 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2019/318/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 931051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2086298
42 A = 6793459
54 meter
Y = 4796570
72 meter E =
0004775
Z = 4335009
71 I = 51
47116
XDOT = -6829
747259 Wp = 34
08421
YDOT = 165
323680 meter/sec RA = 334
80032 deg
ZDOT = -3464
129117 TA = 91
26032
MA = 91
20561
Ha = 225
389 n
mi
Hp = 223
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6844811
09 X = -2160837
64
Y = 15736780
59 feet Y = 4772823
15 meter
Z = 14222472
81 Z = 4324694
31
XDOT = -22407
307279 XDOT = -6814
261090
YDOT = 542
400524 feet/sec YDOT = 89
035484 meter/sec
ZDOT = -11365
253010 ZDOT = -3497
268728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16285067
73 X = -4963688
64
Y = -5535643
88 feet Y = -1687264
26 meter
Z = 14174965
63 Z = 4320529
52
XDOT = -2899
037113 XDOT = -883
626512
YDOT = -21009
276648 feet/sec YDOT = -6403
627522 meter/sec
ZDOT = -11516
321961 ZDOT = -3510
174934
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 19318
66001340
00016717 00000-0 10270-3 0 9177
2 25544 51
6399 335
2325 0006645 278
5987 81
4411 15
50008359 38595
Satellite: ISS
Catalog Number: 25544
Epoch time: 19318
66001340 = yrday
fracday
Element set: 917
Inclination: 51
6399 deg
RA of node: 335
2325 deg
Eccentricity:
0006645
Arg of perigee: 278
5987 deg
Mean anomaly: 81
4411 deg
Mean motion: 15
50008359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 326
Coasting Arc #19 (Orbit 3873)
---------------------------------------
Vector Time (GMT): 2019/319/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 931051
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2045981
85 A = 6794255
52 meter
Y = -4994587
11 meter E =
0001106
Z = -4127919
04 I = 51
44477
XDOT = 6654
326507 Wp = 146
26135
YDOT = -391
260000 meter/sec RA = 329
83308 deg
ZDOT = 3771
175849 TA = 162
76636
MA = 162
76261
Ha = 225
685 n
mi
Hp = 223
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6712538
89 X = 2121732
31
Y = -16386440
65 feet Y = -4971283
57 meter
Z = -13543041
47 Z = -4117796
67
XDOT = 21831
779880 XDOT = 6639
888432
YDOT = -1283
661417 feet/sec YDOT = -316
927699 meter/sec
ZDOT = 12372
624178 ZDOT = 3803
465707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17009599
07 X = 5184525
80
Y = 5050582
11 feet Y = 1539417
43 meter
Z = -13496397
58 Z = -4113701
98
XDOT = 3921
261568 XDOT = 1195
200526
YDOT = 20253
506276 feet/sec YDOT = 6173
268713 meter/sec
ZDOT = 12519
839598 ZDOT = 3816
047109
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 19319
62711185
00016717 00000-0 10270-3 0 9180
2 25544 51
6408 330
4412 0006593 283
0605 76
9809 15
49987739 38743
Satellite: ISS
Catalog Number: 25544
Epoch time: 19319
62711185 = yrday
fracday
Element set: 918
Inclination: 51
6408 deg
RA of node: 330
4412 deg
Eccentricity:
0006593
Arg of perigee: 283
0605 deg
Mean anomaly: 76
9809 deg
Mean motion: 15
49987739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3874
Checksum: 347
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