[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 22nd 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16520 4497 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 5 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
329/11:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 222
2
333/10:24:30
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 221
6
335/11:30:08
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 221
1
336/14:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 221
0
337/13:40:13
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 220
8
338/17:51:47
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 220
6
Coasting Arc #1 (Orbit 3949)
---------------------------------------
Vector Time (GMT): 2019/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5130032
95 A = 6798498
85 meter
Y = 3661206
42 meter E =
0001438
Z = -2548806
55 I = 51
33750
XDOT = -1270
265174 Wp = 292
22012
YDOT = -5432
846570 meter/sec RA = 305
60692 deg
ZDOT = -5244
348702 TA = 276
47452
MA = 276
49090
Ha = 226
746 n
mi
Hp = 223
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16830816
76 X = -5158211
54
Y = 12011832
08 feet Y = 3603681
31 meter
Z = -8362226
22 Z = -2573794
86
XDOT = -4167
536660 XDOT = -1183
944722
YDOT = -17824
299771 feet/sec YDOT = -5446
568721 meter/sec
ZDOT = -17205
868446 ZDOT = -5250
309785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1413011
89 X = -430686
02
Y = -20582528
67 feet Y = -6273554
74 meter
Z = -8476452
14 Z = -2583622
61
XDOT = 15796
179708 XDOT = 4814
675575
YDOT = 6016
299270 feet/sec YDOT = 1833
768018 meter/sec
ZDOT = -17232
534774 ZDOT = -5252
476599
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 19324
52705540
00016717 00000-0 10270-3 0 9004
2 25544 51
6400 306
1654 0006523 304
8724 55
1812 15
50014405 39501
Satellite: ISS
Catalog Number: 25544
Epoch time: 19324
52705540 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 306
1654 deg
Eccentricity:
0006523
Arg of perigee: 304
8724 deg
Mean anomaly: 55
1812 deg
Mean motion: 15
50014405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3950
Checksum: 269
Coasting Arc #2 (Orbit 3965)
---------------------------------------
Vector Time (GMT): 2019/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4880193
30 A = 6797708
75 meter
Y = -3769623
80 meter E =
0009813
Z = 2845563
79 I = 51
31624
XDOT = 1379
845246 Wp = 52
33420
YDOT = 5600
815423 meter/sec RA = 300
63291 deg
ZDOT = 5047
052175 TA = 340
12863
MA = 340
16683
Ha = 226
633 n
mi
Hp = 222
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16011132
89 X = 4908161
29
Y = -12367532
15 feet Y = -3714893
72 meter
Z = 9335839
22 Z = 2869338
08
XDOT = 4527
051331 XDOT = 1292
596667
YDOT = 18375
378684 feet/sec YDOT = 5615
757872 meter/sec
ZDOT = 16558
570128 ZDOT = 5053
543246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2494411
87 X = 760296
74
Y = 20026205
08 feet Y = 6103987
31 meter
Z = 9444529
69 Z = 2878692
65
XDOT = -16595
485092 XDOT = -5058
303856
YDOT = -5765
110411 feet/sec YDOT = -1757
205653 meter/sec
ZDOT = 16587
648703 ZDOT = 5055
915325
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 19325
55861839
00016717 00000-0 10270-3 0 9013
2 25544 51
6395 301
0555 0006604 306
4326 53
6215 15
50051855 39661
Satellite: ISS
Catalog Number: 25544
Epoch time: 19325
55861839 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 301
0555 deg
Eccentricity:
0006604
Arg of perigee: 306
4326 deg
Mean anomaly: 53
6215 deg
Mean motion: 15
50051855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3966
Checksum: 308
Coasting Arc #3 (Orbit 3980)
---------------------------------------
Vector Time (GMT): 2019/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4640398
47 A = 6797043
67 meter
Y = 3851319
74 meter E =
0003531
Z = -3139596
31 I = 51
29825
XDOT = -1515
845815 Wp = 351
66608
YDOT = -5755
483434 meter/sec RA = 295
65556 deg
ZDOT = -4815
640185 TA = 224
61355
MA = 224
64197
Ha = 227
056 n
mi
Hp = 222
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15224404
43 X = -4667869
50
Y = 12635563
44 feet Y = 3799273
98 meter
Z = -10300512
83 Z = -3162204
65
XDOT = -4973
247426 XDOT = -1427
981574
YDOT = -18882
819666 feet/sec YDOT = -5771
943323 meter/sec
ZDOT = -15799
344439 ZDOT = -4822
790415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3464367
75 X = -1055939
29
Y = -19424156
21 feet Y = -5920482
81 meter
Z = -10403885
33 Z = -3171104
25
XDOT = 17397
116458 XDOT = 5302
641096
YDOT = 5383
878642 feet/sec YDOT = 1641
006210 meter/sec
ZDOT = -15831
424347 ZDOT = -4825
418141
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 19326
52570907
00016717 00000-0 10270-3 0 9025
2 25544 51
6400 296
2635 0006641 312
1084 47
9501 15
50025519 39817
Satellite: ISS
Catalog Number: 25544
Epoch time: 19326
52570907 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 296
2635 deg
Eccentricity:
0006641
Arg of perigee: 312
1084 deg
Mean anomaly: 47
9501 deg
Mean motion: 15
50025519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3981
Checksum: 296
Coasting Arc #4 (Orbit 3996)
---------------------------------------
Vector Time (GMT): 2019/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4393719
34 A = 6796185
82 meter
Y = -3893418
20 meter E =
0008843
Z = 3412800
10 I = 51
28278
XDOT = 1686
063669 Wp = 58
56521
YDOT = 5915
282258 meter/sec RA = 290
67794 deg
ZDOT = 4573
374134 TA = 341
53604
MA = 341
56812
Ha = 226
986 n
mi
Hp = 222
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14415089
70 X = 4420352
29
Y = -12773681
75 feet Y = -3844135
70 meter
Z = 11196850
74 Z = 3434208
17
XDOT = 5531
704952 XDOT = 1597
576578
YDOT = 19407
094023 feet/sec YDOT = 5933
642131 meter/sec
ZDOT = 15004
508313 ZDOT = 4581
349801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4310869
39 X = 1313952
99
Y = 18712998
35 feet Y = 5703721
90 meter
Z = 11294747
49 Z = 3442639
04
XDOT = -18265
125148 XDOT = -5567
210145
YDOT = -4878
700673 feet/sec YDOT = -1487
027965 meter/sec
ZDOT = 15040
345697 ZDOT = 4584
297368
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 19327
55726656
00016717 00000-0 10270-3 0 9034
2 25544 51
6406 291
1531 0006693 314
7253 45
3352 15
50057287 39975
Satellite: ISS
Catalog Number: 25544
Epoch time: 19327
55726656 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 291
1531 deg
Eccentricity:
0006693
Arg of perigee: 314
7253 deg
Mean anomaly: 45
3352 deg
Mean motion: 15
50057287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3997
Checksum: 323
Coasting Arc #5 (Orbit 4011)
---------------------------------------
Vector Time (GMT): 2019/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4166069
96 A = 6795461
45 meter
Y = 3915552
00 meter E =
0006400
Z = -3679708
67 I = 51
26908
XDOT = -1882
061099 Wp = 11
05014
YDOT = -6047
261522 meter/sec RA = 285
69797 deg
ZDOT = -4299
110840 TA = 212
87906
MA = 212
91889
Ha = 227
396 n
mi
Hp = 222
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13668208
54 X = -4191670
77
Y = 12846299
22 feet Y = 3868821
08 meter
Z = -12072535
02 Z = -3700008
37
XDOT = -6174
741139 XDOT = -1793
415792
YDOT = -19840
096858 feet/sec YDOT = -6067
812221 meter/sec
ZDOT = -14104
694358 ZDOT = -4308
038366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5046683
51 X = -1538229
13
Y = -18003556
38 feet Y = -5487483
99 meter
Z = -12165375
99 Z = -3708006
60
XDOT = 19077
758234 XDOT = 5814
900710
YDOT = 4220
997766 feet/sec YDOT = 1286
560119 meter/sec
ZDOT = -14144
866935 ZDOT = -4311
355442
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 19328
52435260
00016717 00000-0 10270-3 0 9041
2 25544 51
6402 286
3613 0006781 320
3009 39
7644 15
50035530 40125
Satellite: ISS
Catalog Number: 25544
Epoch time: 19328
52435260 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 286
3613 deg
Eccentricity:
0006781
Arg of perigee: 320
3009 deg
Mean anomaly: 39
7644 deg
Mean motion: 15
50035530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4012
Checksum: 280
Coasting Arc #6 (Orbit 4026)
---------------------------------------
Vector Time (GMT): 2019/329/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3427316
24 A = 6790959
29 meter
Y = -3175516
33 meter E =
0008003
Z = -4934200
21 I = 51
24568
XDOT = 3052
316852 Wp = 75
23966
YDOT = -6674
528045 meter/sec RA = 280
77882 deg
ZDOT = 2180
373215 TA = 216
15178
MA = 216
20591
Ha = 227
457 n
mi
Hp = 222
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11244475
85 X = -3367583
77
Y = -10418360
65 feet Y = -3213508
68 meter
Z = -16188320
90 Z = -4950704
38
XDOT = 10014
162900 XDOT = 3116
135207
YDOT = -21898
057892 feet/sec YDOT = -6640
038201 meter/sec
ZDOT = 7153
455431 ZDOT = 2195
355146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14880487
63 X = 4535572
63
Y = -3334568
07 feet Y = -1016376
35 meter
Z = -16263270
06 Z = -4957044
71
XDOT = 12241
125276 XDOT = 3731
094984
YDOT = 19480
925136 feet/sec YDOT = 5937
785981 meter/sec
ZDOT = 7222
288142 ZDOT = 2201
353426
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 19329
49143633
00016717 00000-0 10270-3 0 9059
2 25544 51
6399 281
5704 0006818 323
0080 37
0599 15
50013826 40278
Satellite: ISS
Catalog Number: 25544
Epoch time: 19329
49143633 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 281
5704 deg
Eccentricity:
0006818
Arg of perigee: 323
0080 deg
Mean anomaly: 37
0599 deg
Mean motion: 15
50013826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4027
Checksum: 311
Coasting Arc #7 (Orbit 4042)
---------------------------------------
Vector Time (GMT): 2019/330/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3526816
55 A = 6791486
92 meter
Y = 3287741
69 meter E =
0009658
Z = 4784488
18 I = 51
24394
XDOT = -2741
995150 Wp = 15
85174
YDOT = 6679
090197 meter/sec RA = 275
79571 deg
ZDOT = -2558
069141 TA = 99
55965
MA = 99
45051
Ha = 227
596 n
mi
Hp = 222
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11570920
43 X = 3466549
01
Y = 10786554
10 feet Y = 3326843
61 meter
Z = 15697139
70 Z = 4801474
47
XDOT = -8996
047080 XDOT = -2804
052920
YDOT = 21913
025581 feet/sec YDOT = 6648
080525 meter/sec
ZDOT = -8392
615293 ZDOT = -2571
539140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15309664
52 X = -4666385
75
Y = 3663642
43 feet Y = 1116678
21 meter
Z = 15774284
14 Z = 4808001
81
XDOT = -13144
819311 XDOT = -4006
540926
YDOT = -18381
934634 feet/sec YDOT = -5602
813677 meter/sec
ZDOT = -8454
551770 ZDOT = -2576
947380
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 19330
52298923
00016717 00000-0 10270-3 0 9069
2 25544 51
6413 276
4597 0006872 326
6388 33
4329 15
50041190 40432
Satellite: ISS
Catalog Number: 25544
Epoch time: 19330
52298923 = yrday
fracday
Element set: 906
Inclination: 51
6413 deg
RA of node: 276
4597 deg
Eccentricity:
0006872
Arg of perigee: 326
6388 deg
Mean anomaly: 33
4329 deg
Mean motion: 15
50041190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4043
Checksum: 315
Coasting Arc #8 (Orbit 4057)
---------------------------------------
Vector Time (GMT): 2019/331/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3668877
50 A = 6792143
12 meter
Y = -3359025
29 meter E =
0006892
Z = -4629226
26 I = 51
24386
XDOT = 2429
504382 Wp = 68
39463
YDOT = -6653
741473 meter/sec RA = 270
81287 deg
ZDOT = 2908
543377 TA = 230
72408
MA = 230
78524
Ha = 227
745 n
mi
Hp = 221
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12036999
67 X = -3608556
57
Y = -11020424
17 feet Y = -3399715
45 meter
Z = -15187750
19 Z = -4646902
52
XDOT = 7970
814903 XDOT = 2489
599522
YDOT = -21829
860475 feet/sec YDOT = -6626
237363 meter/sec
ZDOT = 9542
465148 ZDOT = 2920
490427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15692914
20 X = 4783200
25
Y = -4198351
51 feet Y = -1279657
54 meter
Z = -15268043
56 Z = -4653699
68
XDOT = 13920
847453 XDOT = 4243
074304
YDOT = 17202
775188 feet/sec YDOT = 5243
405877 meter/sec
ZDOT = 9597
452233 ZDOT = 2925
303441
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 19331
49006713
00016717 00000-0 10270-3 0 9071
2 25544 51
6414 271
6686 0006942 330
6846 29
3914 15
50027995 40588
Satellite: ISS
Catalog Number: 25544
Epoch time: 19331
49006713 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 271
6686 deg
Eccentricity:
0006942
Arg of perigee: 330
6846 deg
Mean anomaly: 29
3914 deg
Mean motion: 15
50027995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4058
Checksum: 323
Coasting Arc #9 (Orbit 4073)
---------------------------------------
Vector Time (GMT): 2019/332/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3819415
86 A = 6792830
10 meter
Y = 3450486
84 meter E =
0011053
Z = 4433249
84 I = 51
24691
XDOT = -2147
265963 Wp = 30
34279
YDOT = 6588
153189 meter/sec RA = 265
83083 deg
ZDOT = -3264
780509 TA = 92
85045
MA = 92
72395
Ha = 227
906 n
mi
Hp = 221
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12530891
94 X = 3759013
06
Y = 11320494
87 feet Y = 3492859
94 meter
Z = 14544782
92 Z = 4451657
14
XDOT = -7044
835838 XDOT = -2204
918293
YDOT = 21614
675816 feet/sec YDOT = 6563
819009 meter/sec
ZDOT = -10711
222143 ZDOT = -3275
350465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16133638
91 X = -4917533
14
Y = 4737380
01 feet Y = 1443953
43 meter
Z = 14628413
91 Z = 4458740
56
XDOT = -14496
476675 XDOT = -4418
526091
YDOT = -16013
495930 feet/sec YDOT = -4880
913559 meter/sec
ZDOT = -10759
919459 ZDOT = -3279
623451
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 19332
52161494
00016717 00000-0 10270-3 0 9085
2 25544 51
6413 266
5586 0006968 334
7760 25
3049 15
50049259 40747
Satellite: ISS
Catalog Number: 25544
Epoch time: 19332
52161494 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 266
5586 deg
Eccentricity:
0006968
Arg of perigee: 334
7760 deg
Mean anomaly: 25
3049 deg
Mean motion: 15
50049259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4074
Checksum: 326
Coasting Arc #10 (Orbit 4088)
---------------------------------------
Vector Time (GMT): 2019/333/10:24:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2722377
46 A = 6793506
11 meter
Y = -4559785
31 meter E =
0007749
Z = 4228283
41 I = 51
25238
XDOT = 3796
906545 Wp = 63
22958
YDOT = 5604
178138 meter/sec RA = 261
12494 deg
ZDOT = 3597
223786 TA = 349
77183
MA = 349
78759
Ha = 227
839 n
mi
Hp = 221
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8931684
59 X = 2752625
11
Y = -14959925
57 feet Y = -4529173
19 meter
Z = 13872320
90 Z = 4241580
71
XDOT = 12457
042469 XDOT = 3716
483305
YDOT = 18386
411215 feet/sec YDOT = 5646
187686 meter/sec
ZDOT = 11801
915308 ZDOT = 3615
473321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3813159
51 X = 1162251
02
Y = 16951076
69 feet Y = 5166688
18 meter
Z = 13933286
17 Z = 4246865
62
XDOT = -20377
706688 XDOT = -6211
124998
YDOT = -5189
414481 feet/sec YDOT = -1581
733534 meter/sec
ZDOT = 11884
676324 ZDOT = 3622
449343
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 19333
48868800
00016717 00000-0 10270-3 0 9097
2 25544 51
6409 261
7679 0006843 336
9361 23
1481 15
50078624 40895
Satellite: ISS
Catalog Number: 25544
Epoch time: 19333
48868800 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 261
7679 deg
Eccentricity:
0006843
Arg of perigee: 336
9361 deg
Mean anomaly: 23
1481 deg
Mean motion: 15
50078624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4089
Checksum: 336
Coasting Arc #11 (Orbit 4103)
---------------------------------------
Vector Time (GMT): 2019/334/10:24:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2570575
70 A = 6792805
17 meter
Y = 4461264
12 meter E =
0011808
Z = -4442003
80 I = 51
25657
XDOT = -4074
108159 Wp = 33
33043
YDOT = -5597
745400 meter/sec RA = 256
14279 deg
ZDOT = -3258
809172 TA = 203
54762
MA = 203
60173
Ha = 228
177 n
mi
Hp = 221
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8433647
31 X = -2598694
89
Y = 14636693
32 feet Y = 4432361
45 meter
Z = -14573503
28 Z = -4454558
52
XDOT = -13366
496584 XDOT = -3995
380163
YDOT = -18365
306431 feet/sec YDOT = -5642
864361 meter/sec
ZDOT = -10691
631143 ZDOT = -3278
409252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4238858
80 X = -1292004
16
Y = -16300614
96 feet Y = -4968427
44 meter
Z = -14631070
50 Z = -4459550
29
XDOT = 21148
587656 XDOT = 6446
089518
YDOT = 4193
089609 feet/sec YDOT = 1278
053713 meter/sec
ZDOT = -10780
571231 ZDOT = -3285
918111
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 19334
45576037
00016717 00000-0 10270-3 0 9105
2 25544 51
6413 256
9764 0006992 341
7301 18
3597 15
50062713 41048
Satellite: ISS
Catalog Number: 25544
Epoch time: 19334
45576037 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 256
9764 deg
Eccentricity:
0006992
Arg of perigee: 341
7301 deg
Mean anomaly: 18
3597 deg
Mean motion: 15
50062713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4104
Checksum: 307
Coasting Arc #12 (Orbit 4119)
---------------------------------------
Vector Time (GMT): 2019/335/10:24:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2444160
32 A = 6791990
87 meter
Y = -4325517
92 meter E =
0006480
Z = 4624645
83 I = 51
26302
XDOT = 4372
361841 Wp = 60
27399
YDOT = 5583
050269 meter/sec RA = 251
16161 deg
ZDOT = 2911
180474 TA =
59171
MA =
59095
Ha = 228
123 n
mi
Hp = 221
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8018898
68 X = 2469883
83
Y = -14191331
74 feet Y = -4298042
26 meter
Z = 15172722
54 Z = 4636580
70
XDOT = 14345
019165 XDOT = 4295
464640
YDOT = 18317
094057 feet/sec YDOT = 5631
514834 meter/sec
ZDOT = 9551
117041 ZDOT = 2932
233676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4497431
63 X = 1370817
16
Y = 15614291
25 feet Y = 4759235
97 meter
Z = 15227447
56 Z = 4641326
02
XDOT = -21922
492972 XDOT = -6681
975858
YDOT = -3093
067649 feet/sec YDOT = -942
767019 meter/sec
ZDOT = 9646
706551 ZDOT = 2940
316157
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 19335
48729845
00016717 00000-0 10270-3 0 9117
2 25544 51
6411 251
8662 0006990 344
6828 15
4109 15
50089350 41202
Satellite: ISS
Catalog Number: 25544
Epoch time: 19335
48729845 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 251
8662 deg
Eccentricity:
0006990
Arg of perigee: 344
6828 deg
Mean anomaly: 15
4109 deg
Mean motion: 15
50089350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4120
Checksum: 313
Coasting Arc #13 (Orbit 4119)
---------------------------------------
Vector Time (GMT): 2019/335/11:30:08
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4407351
47 A = 6795230
93 meter
Y = -3579898
49 meter E =
0006874
Z = -3731525
49 I = 51
27435
XDOT = 1453
568857 Wp = 35
80747
YDOT = -6206
608471 meter/sec RA = 250
88746 deg
ZDOT = 4247
036684 TA = 279
44629
MA = 279
52398
Ha = 228
245 n
mi
Hp = 221
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14459814
54 X = -4348866
70
Y = -11745073
78 feet Y = -3628857
20 meter
Z = -12242537
70 Z = -3752793
16
XDOT = 4768
926696 XDOT = 1502
235117
YDOT = -20362
888686 feet/sec YDOT = -6190
081982 meter/sec
ZDOT = 13933
847387 ZDOT = 4254
215137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17160688
32 X = 5230577
80
Y = -7082826
11 feet Y = -2158845
40 meter
Z = -12339249
35 Z = -3761003
20
XDOT = 15189
985984 XDOT = 4629
907728
YDOT = 12524
363500 feet/sec YDOT = 3817
425995 meter/sec
ZDOT = 13967
020087 ZDOT = 4257
147723
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 19335
48730006
00016717 00000-0 10270-3 0 9129
2 25544 51
6413 251
8665 0007070 345
7393 14
3557 15
50053107 41202
Satellite: ISS
Catalog Number: 25544
Epoch time: 19335
48730006 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 251
8665 deg
Eccentricity:
0007070
Arg of perigee: 345
7393 deg
Mean anomaly: 14
3557 deg
Mean motion: 15
50053107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4120
Checksum: 285
Coasting Arc #14 (Orbit 4135)
---------------------------------------
Vector Time (GMT): 2019/336/11:30:08
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4630041
40 A = 6796081
73 meter
Y = 3583028
84 meter E =
0013091
Z = 3448964
15 I = 51
28906
XDOT = -1280
874672 Wp = 56
94863
YDOT = 6038
933412 meter/sec RA = 245
90913 deg
ZDOT = -4534
588876 TA = 82
47317
MA = 82
32447
Ha = 228
416 n
mi
Hp = 220
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15190424
56 X = 4572877
63
Y = 11755343
96 feet Y = 3634485
30 meter
Z = 11315499
19 Z = 3471316
70
XDOT = -4202
344725 XDOT = -1326
282026
YDOT = 19812
773661 feet/sec YDOT = 6024
356292 meter/sec
ZDOT = -14877
260092 ZDOT = -4540
920634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17383776
06 X = -5298574
94
Y = 8026833
70 feet Y = 2446578
91 meter
Z = 11417175
77 Z = 3479955
17
XDOT = -15130
179130 XDOT = -4611
678599
YDOT = -11474
267377 feet/sec YDOT = -3497
356697 meter/sec
ZDOT = -14906
546846 ZDOT = -4543
515479
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 19336
51883781
00016717 00000-0 10270-3 0 9134
2 25544 51
6412 246
7564 0007065 349
4584 10
6417 15
50058778 41369
Satellite: ISS
Catalog Number: 25544
Epoch time: 19336
51883781 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 246
7564 deg
Eccentricity:
0007065
Arg of perigee: 349
4584 deg
Mean anomaly: 10
6417 deg
Mean motion: 15
50058778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4136
Checksum: 327
Coasting Arc #15 (Orbit 4137)
---------------------------------------
Vector Time (GMT): 2019/336/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4726174
07 A = 6791497
02 meter
Y = 1207102
14 meter E =
0011850
Z = 4725519
47 I = 51
27708
XDOT = 892
838379 Wp = 26
86830
YDOT = 7114
674109 meter/sec RA = 245
29255 deg
ZDOT = -2697
310751 TA = 90
02566
MA = 89
88987
Ha = 228
288 n
mi
Hp = 220
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15505820
44 X = 4689370
64
Y = 3960308
87 feet Y = 1259747
36 meter
Z = 15503672
82 Z = 4748388
23
XDOT = 2929
259775 XDOT = 826
315729
YDOT = 23342
106656 feet/sec YDOT = 7124
286748 meter/sec
ZDOT = -8849
444722 ZDOT = -2693
134602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 922965
79 X = 281319
97
Y = 15875168
35 feet Y = 4838751
31 meter
Z = 15607868
16 Z = 4757278
22
XDOT = -20161
185671 XDOT = -6145
129393
YDOT = 9896
151387 feet/sec YDOT = 3016
346943 meter/sec
ZDOT = -8830
889057 ZDOT = -2691
654984
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 19336
64777731
00016717 00000-0 10270-3 0 9146
2 25544 51
6423 246
1182 0007176 348
4566 11
6419 15
50106716 41384
Satellite: ISS
Catalog Number: 25544
Epoch time: 19336
64777731 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 246
1182 deg
Eccentricity:
0007176
Arg of perigee: 348
4566 deg
Mean anomaly: 11
6419 deg
Mean motion: 15
50106716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4138
Checksum: 314
Coasting Arc #16 (Orbit 4152)
---------------------------------------
Vector Time (GMT): 2019/337/13:40:13
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4540782
91 A = 6790168
40 meter
Y = -186237
12 meter E =
0010679
Z = 5044910
42 I = 51
28764
XDOT = 2324
768689 Wp = 18
81717
YDOT = 7070
106925 meter/sec RA = 240
49224 deg
ZDOT = -1820
449670 TA = 88
97187
MA = 88
84951
Ha = 228
343 n
mi
Hp = 220
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14897581
73 X = 4518022
55
Y = -611014
16 feet Y = -135586
52 meter
Z = 16551543
37 Z = 5066912
61
XDOT = 7627
193861 XDOT = 2254
378670
YDOT = 23195
888863 feet/sec YDOT = 7095
710694 meter/sec
ZDOT = -5972
603903 ZDOT = -1809
327209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2217959
65 X = 676034
10
Y = 14630791
59 feet Y = 4459465
28 meter
Z = 16651890
59 Z = 5075496
25
XDOT = -21154
678329 XDOT = -6447
945955
YDOT = 9988
280491 feet/sec YDOT = 3044
427894 meter/sec
ZDOT = -5922
349293 ZDOT = -1805
132064
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 19337
61484194
00016717 00000-0 10270-3 0 9153
2 25544 51
6429 241
3270 0007129 351
4734 8
6295 15
50107597 41537
Satellite: ISS
Catalog Number: 25544
Epoch time: 19337
61484194 = yrday
fracday
Element set: 915
Inclination: 51
6429 deg
RA of node: 241
3270 deg
Eccentricity:
0007129
Arg of perigee: 351
4734 deg
Mean anomaly: 8
6295 deg
Mean motion: 15
50107597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4153
Checksum: 314
Coasting Arc #17 (Orbit 4167)
---------------------------------------
Vector Time (GMT): 2019/338/13:40:13
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4670965
11 A = 6790725
02 meter
Y = 180528
05 meter E =
0011941
Z = -4934393
60 I = 51
30677
XDOT = -2578
932863 Wp = 71
90785
YDOT = -6863
460074 meter/sec RA = 235
51196 deg
ZDOT = 2198
188552 TA = 219
63713
MA = 219
72449
Ha = 228
558 n
mi
Hp = 220
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15324688
68 X = -4648668
02
Y = 592283
62 feet Y = 128419
01 meter
Z = -16188955
37 Z = -4957029
34
XDOT = -8461
065822 XDOT = -2512
669608
YDOT = -22517
913630 feet/sec YDOT = -6891
929166 meter/sec
ZDOT = 7211
904697 ZDOT = 2185
821498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2504901
50 X = -763493
98
Y = -15018950
03 feet Y = -4577775
97 meter
Z = -16292199
60 Z = -4965862
44
XDOT = 20169
661485 XDOT = 6147
712821
YDOT = -11098
113954 feet/sec YDOT = -3382
705133 meter/sec
ZDOT = 7155
939749 ZDOT = 2181
130435
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 19338
58190459
00016717 00000-0 10270-3 0 9169
2 25544 51
6429 236
5354 0007190 355
4814 4
6270 15
50083356 41688
Satellite: ISS
Catalog Number: 25544
Epoch time: 19338
58190459 = yrday
fracday
Element set: 916
Inclination: 51
6429 deg
RA of node: 236
5354 deg
Eccentricity:
0007190
Arg of perigee: 355
4814 deg
Mean anomaly: 4
6270 deg
Mean motion: 15
50083356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4168
Checksum: 321
Coasting Arc #18 (Orbit 4170)
---------------------------------------
Vector Time (GMT): 2019/338/17:51:47
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3465164
44 A = 6800830
76 meter
Y = 5813255
51 meter E =
0006677
Z = -669654
69 I = 51
34036
XDOT = -4426
032405 Wp = 98
65105
YDOT = 1961
024578 meter/sec RA = 234
66147 deg
ZDOT = -5931
034826 TA = 88
59327
MA = 88
51678
Ha = 228
618 n
mi
Hp = 220
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11368649
74 X = 3403154
21
Y = 19072360
58 feet Y = 5851658
74 meter
Z = -2197029
82 Z = -652972
38
XDOT = -14521
103690 XDOT = -4418
822384
YDOT = 6433
807671 feet/sec YDOT = 1911
570247 meter/sec
ZDOT = -19458
775677 ZDOT = -5952
517307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4290543
70 X = 1307757
72
Y = 21792644
05 feet Y = 6642397
91 meter
Z = -2121314
56 Z = -646576
68
XDOT = -14126
161929 XDOT = -4305
654156
YDOT = 894
646004 feet/sec YDOT = 272
688102 meter/sec
ZDOT = -19556
874080 ZDOT = -5960
935219
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 19338
77531605
00016717 00000-0 10270-3 0 9173
2 25544 51
6392 235
5723 0007121 357
4805 2
6308 15
50117399 41711
Satellite: ISS
Catalog Number: 25544
Epoch time: 19338
77531605 = yrday
fracday
Element set: 917
Inclination: 51
6392 deg
RA of node: 235
5723 deg
Eccentricity:
0007121
Arg of perigee: 357
4805 deg
Mean anomaly: 2
6308 deg
Mean motion: 15
50117399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4171
Checksum: 308
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