[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 16th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13923 1181 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
268/13:57:43
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
3
268/17:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
271/11:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
272/00:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
4
Coasting Arc #1 (Orbit 2941)
---------------------------------------
Vector Time (GMT): 2019/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3951644
92 A = 6791341
20 meter
Y = 2783081
27 meter E =
0014757
Z = 4763438
80 I = 51
24177
XDOT = -1776
528038 Wp = 57
16530
YDOT = 6991
478586 meter/sec RA = 267
45542 deg
ZDOT = -2597
309082 TA = 58
65578
MA = 58
51144
Ha = 229
710 n
mi
Hp = 218
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12964714
32 X = 3897091
77
Y = 9130844
06 feet Y = 2826966
82 meter
Z = 15628080
07 Z = 4782501
70
XDOT = -5828
504062 XDOT = -1841
960396
YDOT = 22937
921871 feet/sec YDOT = 6971
246069 meter/sec
ZDOT = -8521
355255 ZDOT = -2606
098483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11880792
81 X = -3621265
65
Y = -10372677
50 feet Y = -3161592
10 meter
Z = 15714558
25 Z = 4789797
35
XDOT = 7280
791532 XDOT = 2219
185259
YDOT = -21378
466391 feet/sec YDOT = -6516
156556 meter/sec
ZDOT = -8561
811537 ZDOT = -2609
640157
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 19259
54378625
00016717 00000-0 10270-3 0 9003
2 25544 51
6402 268
1623 0007360 53
0142 307
1681 15
50108694 29421
Satellite: ISS
Catalog Number: 25544
Epoch time: 19259
54378625 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 268
1623 deg
Eccentricity:
0007360
Arg of perigee: 53
0142 deg
Mean anomaly: 307
1681 deg
Mean motion: 15
50108694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2942
Checksum: 298
Coasting Arc #2 (Orbit 2956)
---------------------------------------
Vector Time (GMT): 2019/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4109311
84 A = 6792124
14 meter
Y = -2848666
57 meter E =
0015791
Z = -4610361
71 I = 51
24596
XDOT = 1479
920744 Wp = 87
81628
YDOT = -6900
222415 meter/sec RA = 262
47291 deg
ZDOT = 2953
856747 TA = 211
81284
MA = 211
90832
Ha = 229
886 n
mi
Hp = 218
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13481994
21 X = -4054757
05
Y = -9346018
92 feet Y = -2894315
20 meter
Z = -15125858
63 Z = -4630190
59
XDOT = 4855
383019 XDOT = 1542
622722
YDOT = -22638
524983 feet/sec YDOT = -6883
322024 meter/sec
ZDOT = 9691
131059 ZDOT = 2961
198661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12558474
79 X = 3827823
12
Y = 10424361
82 feet Y = 3177345
48 meter
Z = -15215821
65 Z = -4637782
44
XDOT = -5890
753225 XDOT = -1795
501583
YDOT = 21246
929701 feet/sec YDOT = 6476
064173 meter/sec
ZDOT = 9724
985701 ZDOT = 2964
175642
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 19260
51083497
00016717 00000-0 10270-3 0 9013
2 25544 51
6396 263
3717 0007352 56
0021 304
1827 15
50062270 29578
Satellite: ISS
Catalog Number: 25544
Epoch time: 19260
51083497 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 263
3717 deg
Eccentricity:
0007352
Arg of perigee: 56
0021 deg
Mean anomaly: 304
1827 deg
Mean motion: 15
50062270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2957
Checksum: 295
Coasting Arc #3 (Orbit 2972)
---------------------------------------
Vector Time (GMT): 2019/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4261297
05 A = 6792787
84 meter
Y = 2935647
18 meter E =
0016509
Z = 4391559
37 I = 51
25322
XDOT = -1230
669092 Wp = 65
32505
YDOT = 6794
786892 meter/sec RA = 257
48937 deg
ZDOT = -3331
295622 TA = 58
61207
MA = 58
45069
Ha = 229
751 n
mi
Hp = 218
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13980633
37 X = 4206821
10
Y = 9631388
38 feet Y = 2982995
77 meter
Z = 14408003
19 Z = 4412126
83
XDOT = -4037
628253 XDOT = -1290
377138
YDOT = 22292
607915 feet/sec YDOT = 6780
690563 meter/sec
ZDOT = -10929
447578 ZDOT = -3337
419390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13219535
15 X = -4029314
31
Y = -10524624
99 feet Y = -3207905
70 meter
Z = 14501326
38 Z = 4420004
28
XDOT = 4654
176789 XDOT = 1418
593085
YDOT = -21018
946867 feet/sec YDOT = -6406
575005 meter/sec
ZDOT = -10957
744603 ZDOT = -3339
920555
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 19261
54235133
00016717 00000-0 10270-3 0 9024
2 25544 51
6387 258
2599 0007275 59
2253 300
9613 15
50107562 29734
Satellite: ISS
Catalog Number: 25544
Epoch time: 19261
54235133 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 258
2599 deg
Eccentricity:
0007275
Arg of perigee: 59
2253 deg
Mean anomaly: 300
9613 deg
Mean motion: 15
50107562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2973
Checksum: 312
Coasting Arc #4 (Orbit 2987)
---------------------------------------
Vector Time (GMT): 2019/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4460887
65 A = 6793633
61 meter
Y = -2958237
42 meter E =
0014138
Z = -4195496
40 I = 51
26484
XDOT = 980
445679 Wp = 87
37371
YDOT = -6649
087495 meter/sec RA = 252
50814 deg
ZDOT = 3657
164281 TA = 220
36138
MA = 220
46639
Ha = 229
965 n
mi
Hp = 218
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14635458
18 X = -4407096
61
Y = -9705503
36 feet Y = -3007821
72 meter
Z = -13764751
96 Z = -4217035
14
XDOT = 3216
685297 XDOT = 1036
960144
YDOT = -21814
591519 feet/sec YDOT = -6637
807237 meter/sec
ZDOT = 11998
570476 ZDOT = 3662
064659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14053380
29 X = 4283470
31
Y = 10401703
37 feet Y = 3170439
19 meter
Z = -13862499
70 Z = -4225289
91
XDOT = -3433
812068 XDOT = -1046
625918
YDOT = 20610
884520 feet/sec YDOT = 6282
197602 meter/sec
ZDOT = 12021
284908 ZDOT = 3664
087640
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 19262
50939719
00016717 00000-0 10270-3 0 9033
2 25544 51
6395 253
4689 0007440 62
8760 297
3148 15
50070352 29881
Satellite: ISS
Catalog Number: 25544
Epoch time: 19262
50939719 = yrday
fracday
Element set: 903
Inclination: 51
6395 deg
RA of node: 253
4689 deg
Eccentricity:
0007440
Arg of perigee: 62
8760 deg
Mean anomaly: 297
3148 deg
Mean motion: 15
50070352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2988
Checksum: 338
Coasting Arc #5 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2019/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4650825
14 A = 6794407
78 meter
Y = 3000078
52 meter E =
0018219
Z = 3929864
18 I = 51
27824
XDOT = -787
821849 Wp = 74
16567
YDOT = 6491
327631 meter/sec RA = 247
52699 deg
ZDOT = -4002
735582 TA = 57
92621
MA = 57
74943
Ha = 229
840 n
mi
Hp = 218
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15258612
66 X = 4597842
42
Y = 9842777
31 feet Y = 3051791
26 meter
Z = 12893255
17 Z = 3952327
57
XDOT = -2584
717354 XDOT = -840
907916
YDOT = 21297
006665 feet/sec YDOT = 6482
220650 meter/sec
ZDOT = -13132
334585 ZDOT = -4006
691795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14854613
61 X = -4527686
23
Y = -10315345
39 feet Y = -3144117
27 meter
Z = 12995216
76 Z = 3960942
07
XDOT = 2411
780981 XDOT = 735
110843
YDOT = -20124
066038 feet/sec YDOT = -6133
815328 meter/sec
ZDOT = -13150
736018 ZDOT = -4008
344338
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 19263
54090895
00016717 00000-0 10270-3 0 9042
2 25544 51
6388 248
3574 0007369 65
4656 294
7262 15
50110812 30046
Satellite: ISS
Catalog Number: 25544
Epoch time: 19263
54090895 = yrday
fracday
Element set: 904
Inclination: 51
6388 deg
RA of node: 248
3574 deg
Eccentricity:
0007369
Arg of perigee: 65
4656 deg
Mean anomaly: 294
7262 deg
Mean motion: 15
50110812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 322
Coasting Arc #6 (Orbit 3018)
---------------------------------------
Vector Time (GMT): 2019/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4877693
84 A = 6795282
08 meter
Y = -2967379
52 meter E =
0012698
Z = -3694576
90 I = 51
29424
XDOT = 597
981061 Wp = 83
35122
YDOT = -6308
290080 meter/sec RA = 242
54858 deg
ZDOT = 4291
374125 TA = 232
52725
MA = 232
64280
Ha = 230
006 n
mi
Hp = 218
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16002932
55 X = -4826202
87
Y = -9735497
10 feet Y = -3021637
54 meter
Z = -12121315
29 Z = -3718145
96
XDOT = 1961
880121 XDOT = 647
632446
YDOT = -20696
489763 feet/sec YDOT = -6301
325286 meter/sec
ZDOT = 14079
311434 ZDOT = 4294
399704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15780806
20 X = 4809989
73
Y = 9961643
71 feet Y = 3036309
00 meter
Z = -12228321
60 Z = -3727192
42
XDOT = -1434
625060 XDOT = -437
273718
YDOT = 19516
247553 feet/sec YDOT = 5948
552254 meter/sec
ZDOT = 14093
459624 ZDOT = 4295
686494
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 19264
50795171
00016717 00000-0 10270-3 0 9059
2 25544 51
6384 243
5667 0007458 69
1814 291
0135 15
50075173 30193
Satellite: ISS
Catalog Number: 25544
Epoch time: 19264
50795171 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 243
5667 deg
Eccentricity:
0007458
Arg of perigee: 69
1814 deg
Mean anomaly: 291
0135 deg
Mean motion: 15
50075173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3019
Checksum: 316
Coasting Arc #7 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2019/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5089156
20 A = 6796098
89 meter
Y = 2951823
28 meter E =
0019499
Z = 3387474
30 I = 51
31360
XDOT = -472
952921 Wp = 83
61145
YDOT = 6118
197350 meter/sec RA = 237
57045 deg
ZDOT = -4595
818570 TA = 56
65310
MA = 56
46659
Ha = 229
889 n
mi
Hp = 218
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16696706
70 X = 5039315
27
Y = 9684459
56 feet Y = 3008455
21 meter
Z = 11113760
83 Z = 3412074
52
XDOT = -1551
682811 XDOT = -519
009170
YDOT = 20072
825953 feet/sec YDOT = 6112
650835 meter/sec
ZDOT = -15078
144915 ZDOT = -4598
228014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16650215
24 X = -5074985
61
Y = -9635532
82 feet Y = -2936910
40 meter
Z = 11225475
10 Z = 3421524
81
XDOT = 687
521447 XDOT = 209
556537
YDOT = -18861
999938 feet/sec YDOT = -5749
137581 meter/sec
ZDOT = -15089
468887 ZDOT = -4599
270117
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 19265
53946146
00016717 00000-0 10270-3 0 9064
2 25544 51
6383 238
4552 0007339 72
4297 287
7655 15
50108886 30353
Satellite: ISS
Catalog Number: 25544
Epoch time: 19265
53946146 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 238
4552 deg
Eccentricity:
0007339
Arg of perigee: 72
4297 deg
Mean anomaly: 287
7655 deg
Mean motion: 15
50108886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 341
Coasting Arc #8 (Orbit 3049)
---------------------------------------
Vector Time (GMT): 2019/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5325088
09 A = 6796910
35 meter
Y = -2857995
13 meter E =
0011959
Z = -3116936
40 I = 51
33569
XDOT = 352
392966 Wp = 76
45263
YDOT = -5917
594220 meter/sec RA = 232
59480 deg
ZDOT = 4842
417123 TA = 247
60008
MA = 247
72681
Ha = 230
011 n
mi
Hp = 218
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17470761
45 X = -5277593
02
Y = -9376624
45 feet Y = -2917278
54 meter
Z = -10226169
30 Z = -3142688
29
XDOT = 1156
144902 XDOT = 395
017218
YDOT = -19414
679201 feet/sec YDOT = -5913
415064 meter/sec
ZDOT = 15887
195286 ZDOT = 4844
232595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17587139
34 X = 5360560
07
Y = 9024132
52 feet Y = 2750555
59 meter
Z = -10343147
13 Z = -3152591
24
XDOT = 1
059609 XDOT =
322969
YDOT = 18148
467572 feet/sec YDOT = 5531
652916 meter/sec
ZDOT = 15895
794069 ZDOT = 4845
038032
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 19266
50649942
00016717 00000-0 10270-3 0 9077
2 25544 51
6390 233
6641 0007429 75
6946 284
5029 15
50086410 30508
Satellite: ISS
Catalog Number: 25544
Epoch time: 19266
50649942 = yrday
fracday
Element set: 907
Inclination: 51
6390 deg
RA of node: 233
6641 deg
Eccentricity:
0007429
Arg of perigee: 75
6946 deg
Mean anomaly: 284
5029 deg
Mean motion: 15
50086410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3050
Checksum: 319
Coasting Arc #9 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2019/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5538747
88 A = 6797712
31 meter
Y = 2781768
40 meter E =
0020443
Z = 2772433
65 I = 51
35957
XDOT = -302
642179 Wp = 92
73580
YDOT = 5716
436275 meter/sec RA = 227
62024 deg
ZDOT = -5099
378703 TA = 55
74649
MA = 55
55303
Ha = 229
956 n
mi
Hp = 218
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18171745
00 X = 5493762
77
Y = 9126536
73 feet Y = 2843455
16 meter
Z = 9095910
94 Z = 2799229
40
XDOT = -992
920536 XDOT = -341
772627
YDOT = 18754
712188 feet/sec YDOT = 5712
832930 meter/sec
ZDOT = -16730
245088 ZDOT = -5100
944081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18438502
70 X = -5620055
62
Y = -8443808
20 feet Y = -2573672
74 meter
Z = 9217662
74 Z = 2809543
60
XDOT = -437
199019 XDOT = -133
258261
YDOT = -17428
944406 feet/sec YDOT = -5312
342255 meter/sec
ZDOT = -16737
681969 ZDOT = -5101
645464
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 19267
53800420
00016717 00000-0 10270-3 0 9082
2 25544 51
6388 228
5524 0007403 78
7472 281
4510 15
50108696 30667
Satellite: ISS
Catalog Number: 25544
Epoch time: 19267
53800420 = yrday
fracday
Element set: 908
Inclination: 51
6388 deg
RA of node: 228
5524 deg
Eccentricity:
0007403
Arg of perigee: 78
7472 deg
Mean anomaly: 281
4510 deg
Mean motion: 15
50108696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 313
Coasting Arc #10 (Orbit 3080)
---------------------------------------
Vector Time (GMT): 2019/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5764452
81 A = 6798421
37 meter
Y = -2624759
15 meter E =
0012172
Z = -2472499
55 I = 51
38480
XDOT = 252
324282 Wp = 68
96658
YDOT = -5520
961666 meter/sec RA = 222
64857 deg
ZDOT = 5298
130078 TA = 263
29783
MA = 263
43638
Ha = 230
000 n
mi
Hp = 218
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18912246
75 X = -5722663
59
Y = -8611414
52 feet Y = -2688987
81 meter
Z = -8111875
17 Z = -2500399
34
XDOT = 827
835571 XDOT = 288
307245
YDOT = -18113
391293 feet/sec YDOT = -5517
938487 meter/sec
ZDOT = 17382
316530 ZDOT = 5299
443497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19298914
09 X = 5882309
02
Y = 7570213
25 feet Y = 2307401
00 meter
Z = -8238679
65 Z = -2511149
56
XDOT = 830
687664 XDOT = 253
193600
YDOT = 16716
848078 feet/sec YDOT = 5095
295294 meter/sec
ZDOT = 17388
583160 ZDOT = 5300
040147
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 19268
50503878
00016717 00000-0 10270-3 0 9098
2 25544 51
6385 223
7614 0007366 82
1634 278
0352 15
50092403 30819
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
50503878 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 223
7614 deg
Eccentricity:
0007366
Arg of perigee: 82
1634 deg
Mean anomaly: 278
0352 deg
Mean motion: 15
50092403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3081
Checksum: 311
Coasting Arc #11 (Orbit 3082)
---------------------------------------
Vector Time (GMT): 2019/268/13:57:43
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 845977
59 A = 6790586
13 meter
Y = -4569501
28 meter E =
0012832
Z = 4941337
96 I = 51
36261
XDOT = 6454
194258 Wp = 101
86061
YDOT = 3536
944882 meter/sec RA = 222
28123 deg
ZDOT = 2158
450275 TA = 326
98172
MA = 327
06178
Ha = 229
879 n
mi
Hp = 218
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2775517
01 X = 873010
01
Y = -14991802
10 feet Y = -4559889
51 meter
Z = 16211738
73 Z = 4945513
33
XDOT = 21175
178011 XDOT = 6403
678917
YDOT = 11604
149874 feet/sec YDOT = 3608
837918 meter/sec
ZDOT = 7081
529772 ZDOT = 2189
679294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5839695
24 X = 1779939
11
Y = 14061702
03 feet Y = 4286006
78 meter
Z = 16230976
35 Z = 4947201
59
XDOT = -23024
213005 XDOT = -7017
780124
YDOT = 1196
144448 feet/sec YDOT = 364
584828 meter/sec
ZDOT = 7223
436012 ZDOT = 2201
703296
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 19268
63397568
00016717 00000-0 10270-3 0 9101
2 25544 51
6402 223
1232 0007214 83
3648 276
8324 15
50141077 30838
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
63397568 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 223
1232 deg
Eccentricity:
0007214
Arg of perigee: 83
3648 deg
Mean anomaly: 276
8324 deg
Mean motion: 15
50141077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3083
Checksum: 303
Coasting Arc #12 (Orbit 3084)
---------------------------------------
Vector Time (GMT): 2019/268/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1033340
32 A = 6790369
93 meter
Y = -4446644
79 meter E =
0012351
Z = 5017001
64 I = 51
36632
XDOT = 6450
266929 Wp = 101
47848
YDOT = 3676
842395 meter/sec RA = 221
63689 deg
ZDOT = 1923
850618 TA = 329
75606
MA = 329
82729
Ha = 229
977 n
mi
Hp = 218
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3390224
14 X = 1058617
48
Y = -14588729
64 feet Y = -4434947
59 meter
Z = 16459979
15 Z = 5022082
89
XDOT = 21162
293075 XDOT = 6399
327057
YDOT = 12063
131218 feet/sec YDOT = 3748
689132 meter/sec
ZDOT = 6311
845858 ZDOT = 1955
059505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13728970
76 X = 4184590
29
Y = 5922054
47 feet Y = 1805042
20 meter
Z = 16483330
93 Z = 5024119
27
XDOT = -15331
511062 XDOT = -4673
044572
YDOT = 17520
967103 feet/sec YDOT = 5340
390773 meter/sec
ZDOT = 6453
656367 ZDOT = 1967
074461
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 19268
76291422
00016717 00000-0 10270-3 0 9118
2 25544 51
6418 222
4849 0007335 83
5061 276
6924 15
50103655 30852
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
76291422 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 222
4849 deg
Eccentricity:
0007335
Arg of perigee: 83
5061 deg
Mean anomaly: 276
6924 deg
Mean motion: 15
50103655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3085
Checksum: 314
Coasting Arc #13 (Orbit 3099)
---------------------------------------
Vector Time (GMT): 2019/269/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 932083
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1082714
06 A = 6789813
45 meter
Y = 4317004
20 meter E =
0020715
Z = -5146159
76 I = 51
39082
XDOT = -6652
813179 Wp = 81
31672
YDOT = -3456
589791 meter/sec RA = 216
66150 deg
ZDOT = -1502
101267 TA = 174
13492
MA = 174
11063
Ha = 229
913 n
mi
Hp = 218
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3552211
49 X = -1105910
47
Y = 14163399
61 feet Y = 4304766
36 meter
Z = -16883726
25 Z = -5151475
90
XDOT = -21826
814893 XDOT = -6606
369790
YDOT = -11340
517686 feet/sec YDOT = -3530
726697 meter/sec
ZDOT = -4928
153764 ZDOT = -1534
304919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13382757
87 X = -4079064
60
Y = -5770370
02 feet Y = -1758808
78 meter
Z = -16908132
02 Z = -5153598
64
XDOT = 14422
511092 XDOT = 4395
981381
YDOT = -18600
368144 feet/sec YDOT = -5669
392210 meter/sec
ZDOT = -5074
525386 ZDOT = -1546
715338
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 19269
72994529
00016717 00000-0 10270-3 0 9124
2 25544 51
6422 217
6929 0007162 86
0362 274
1607 15
50132777 31008
Satellite: ISS
Catalog Number: 25544
Epoch time: 19269
72994529 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 217
6929 deg
Eccentricity:
0007162
Arg of perigee: 86
0362 deg
Mean anomaly: 274
1607 deg
Mean motion: 15
50132777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3100
Checksum: 316
Coasting Arc #14 (Orbit 3115)
---------------------------------------
Vector Time (GMT): 2019/270/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 932083
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1134869
14 A = 6789482
12 meter
Y = -4187534
32 meter E =
0010672
Z = 5213696
44 I = 51
41771
XDOT = 6874
009711 Wp = 101
71949
YDOT = 3223
053715 meter/sec RA = 211
68800 deg
ZDOT = 1088
400285 TA = 337
79822
MA = 337
84440
Ha = 229
927 n
mi
Hp = 218
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3723323
93 X = 1156285
75
Y = -13738629
66 feet Y = -4174723
08 meter
Z = 17105303
28 Z = 5219261
70
XDOT = 22552
525297 XDOT = 6832
170853
YDOT = 10574
323212 feet/sec YDOT = 3299
689929 meter/sec
ZDOT = 3570
867078 ZDOT = 1121
689684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13034500
57 X = 3972915
77
Y = 5642778
65 feet Y = 1719918
93 meter
Z = 17130829
83 Z = 5221476
93
XDOT = -13446
473526 XDOT = -4098
485131
YDOT = 19720
409622 feet/sec YDOT = 6010
780853 meter/sec
ZDOT = 3722
211480 ZDOT = 1134
530059
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 19270
76144317
00016717 00000-0 10270-3 0 9133
2 25544 51
6428 212
5816 0007224 89
7705 270
4273 15
50113868 31168
Satellite: ISS
Catalog Number: 25544
Epoch time: 19270
76144317 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 212
5816 deg
Eccentricity:
0007224
Arg of perigee: 89
7705 deg
Mean anomaly: 270
4273 deg
Mean motion: 15
50113868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3116
Checksum: 305
Coasting Arc #15 (Orbit 3126)
---------------------------------------
Vector Time (GMT): 2019/271/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6257540
91 A = 6800616
17 meter
Y = -2493556
52 meter E =
0015413
Z = -910528
47 I = 51
47415
XDOT = 1051
135424 Wp = 61
95827
YDOT = -4763
580209 meter/sec RA = 207
90486 deg
ZDOT = 5905
294964 TA = 288
18269
MA = 288
35044
Ha = 229
973 n
mi
Hp = 218
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20529989
86 X = -6224769
30
Y = -8180959
71 feet Y = -2563349
63 meter
Z = -2987298
12 Z = -940845
50
XDOT = 3448
607035 XDOT = 1075
640251
YDOT = -15628
543992 feet/sec YDOT = -4751
687945 meter/sec
ZDOT = 19374
327310 ZDOT = 5910
461101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19684143
47 X = 5999726
93
Y = 10005018
39 feet Y = 3049529
61 meter
Z = -3125162
15 Z = -952549
42
XDOT = -3990
036449 XDOT = -1216
163110
YDOT = 13827
287305 feet/sec YDOT = 4214
557171 meter/sec
ZDOT = 19398
060473 ZDOT = 5912
528832
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 19271
47059738
00016717 00000-0 10270-3 0 9145
2 25544 51
6401 209
0670 0007360 92
4877 267
7117 15
50120658 31273
Satellite: ISS
Catalog Number: 25544
Epoch time: 19271
47059738 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 209
0670 deg
Eccentricity:
0007360
Arg of perigee: 92
4877 deg
Mean anomaly: 267
7117 deg
Mean motion: 15
50120658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3127
Checksum: 312
Coasting Arc #16 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2019/272/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 251173
21 A = 6790347
44 meter
Y = 4557219
42 meter E =
0019698
Z = -5045272
62 I = 51
45902
XDOT = -7207
030717 Wp = 84
25847
YDOT = -1705
711641 meter/sec RA = 205
13291 deg
ZDOT = -1904
011254 TA = 167
20434
MA = 167
15428
Ha = 229
960 n
mi
Hp = 218
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 824059
10 X = 224701
73
Y = 14951507
28 feet Y = 4559879
59 meter
Z = -16552731
68 Z = -5044117
35
XDOT = -23645
113901 XDOT = -7178
172608
YDOT = -5596
166802 feet/sec YDOT = -1786
144619 meter/sec
ZDOT = -6246
756084 ZDOT = -1938
950291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5475302
99 X = 1668872
35
Y = 13943272
46 feet Y = 4249909
45 meter
Z = -16547682
00 Z = -5043733
47
XDOT = -23164
748313 XDOT = -7060
615286
YDOT = 1511
789123 feet/sec YDOT = 460
793325 meter/sec
ZDOT = -6405
701145 ZDOT = -1952
457709
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 19272
05081307
00016717 00000-0 10270-3 0 9158
2 25544 51
6427 206
1897 0007218 98
8582 261
3386 15
50109808 31367
Satellite: ISS
Catalog Number: 25544
Epoch time: 19272
05081307 = yrday
fracday
Element set: 915
Inclination: 51
6427 deg
RA of node: 206
1897 deg
Eccentricity:
0007218
Arg of perigee: 98
8582 deg
Mean anomaly: 261
3386 deg
Mean motion: 15
50109808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 319
Coasting Arc #17 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2019/273/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -186609
15 A = 6789729
32 meter
Y = -4424409
49 meter E =
0011818
Z = 5138340
12 I = 51
48864
XDOT = 7382
157046 Wp = 111
91963
YDOT = 1439
193665 meter/sec RA = 200
16488 deg
ZDOT = 1500
227746 TA = 323
56317
MA = 323
64354
Ha = 229
886 n
mi
Hp = 218
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -612234
74 X = -162079
80
Y = -14515779
16 feet Y = -4426358
57 meter
Z = 16858071
24 Z = 5137493
69
XDOT = 24219
675348 XDOT = 7358
227534
YDOT = 4721
763993 feet/sec YDOT = 1521
612522 meter/sec
ZDOT = 4922
007041 ZDOT = 1536
029699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5375076
50 X = -1638323
32
Y = -13502384
72 feet Y = -4115526
86 meter
Z = 16854417
87 Z = 5137226
57
XDOT = 23430
208297 XDOT = 7141
527489
YDOT = -2950
837140 feet/sec YDOT = -899
415160 meter/sec
ZDOT = 5084
907686 ZDOT = 1549
879863
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 19273
08230513
00016717 00000-0 10270-3 0 9168
2 25544 51
6432 201
0788 0007225 102
6400 257
5559 15
50156662 31524
Satellite: ISS
Catalog Number: 25544
Epoch time: 19273
08230513 = yrday
fracday
Element set: 916
Inclination: 51
6432 deg
RA of node: 201
0788 deg
Eccentricity:
0007225
Arg of perigee: 102
6400 deg
Mean anomaly: 257
5559 deg
Mean motion: 15
50156662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 286
Coasting Arc #18 (Orbit 3166)
---------------------------------------
Vector Time (GMT): 2019/274/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 73421
50 A = 6789474
24 meter
Y = 4337176
68 meter E =
0020922
Z = -5241235
89 I = 51
51907
XDOT = -7483
139428 Wp = 89
86278
YDOT = -1155
797914 meter/sec RA = 195
19888 deg
ZDOT = -1064
907196 TA = 169
91032
MA = 169
86825
Ha = 229
893 n
mi
Hp = 218
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 240884
18 X = 50375
92
Y = 14229582
29 feet Y = 4337868
41 meter
Z = -17195655
79 Z = -5240935
59
XDOT = -24550
982376 XDOT = -7464
485981
YDOT = -3791
987907 feet/sec YDOT = -1239
375456 meter/sec
ZDOT = -3493
790012 ZDOT = -1101
212682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5162267
11 X = 1573459
02
Y = 13263873
67 feet Y = 4042828
70 meter
Z = -17194483
68 Z = -5240878
63
XDOT = -23391
775083 XDOT = -7129
813045
YDOT = 4376
203606 feet/sec YDOT = 1333
866859 meter/sec
ZDOT = -3659
013190 ZDOT = -1115
267220
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 19274
04932723
00016717 00000-0 10270-3 0 9178
2 25544 51
6432 196
2879 0007139 105
4210 254
7730 15
50118276 31679
Satellite: ISS
Catalog Number: 25544
Epoch time: 19274
04932723 = yrday
fracday
Element set: 917
Inclination: 51
6432 deg
RA of node: 196
2879 deg
Eccentricity:
0007139
Arg of perigee: 105
4210 deg
Mean anomaly: 254
7730 deg
Mean motion: 15
50118276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3167
Checksum: 311
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