[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 10th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14325 6884 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
253/21:33:29
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 218
7
254/16:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 218
5
257/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 218
1
260/17:57:24
933 -1
0 2
4 2
4
N/A -2
1 -0
2 229
7
000/00:00:49
866 -0
5 -0
0 219
0
264/20:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 219
0
Coasting Arc #1 (Orbit 2832)
---------------------------------------
Vector Time (GMT): 2019/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4140654
64 A = 6788497
33 meter
Y = -1302366
60 meter E =
0019605
Z = -5235727
51 I = 51
29923
XDOT = 3378
317125 Wp = 60
94457
YDOT = -6792
333745 meter/sec RA = 302
35845 deg
ZDOT = -975
613272 TA = 199
61083
MA = 199
68634
Ha = 229
060 n
mi
Hp = 218
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13584824
94 X = -4100351
48
Y = -4272856
30 feet Y = -1348445
12 meter
Z = -17177583
69 Z = -5255743
11
XDOT = 11083
717601 XDOT = 3458
758816
YDOT = -22284
559530 feet/sec YDOT = -6754
105272 meter/sec
ZDOT = -3200
830946 ZDOT = -959
007287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12206832
48 X = 3720642
54
Y = 7118070
66 feet Y = 2169587
94 meter
Z = -17268481
75 Z = -5263433
24
XDOT = -15194
004936 XDOT = -4631
132704
YDOT = 18423
888112 feet/sec YDOT = 5615
601096 meter/sec
ZDOT = -3124
712128 ZDOT = -952
412257
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 19252
51777156
00016717 00000-0 10270-3 0 9005
2 25544 51
6428 302
9886 0008146 21
1715 338
9772 15
50415467 28333
Satellite: ISS
Catalog Number: 25544
Epoch time: 19252
51777156 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 302
9886 deg
Eccentricity:
0008146
Arg of perigee: 21
1715 deg
Mean anomaly: 338
9772 deg
Mean motion: 15
50415467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2833
Checksum: 322
Coasting Arc #2 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2019/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3976593
79 A = 6788133
18 meter
Y = 1526041
41 meter E =
0008901
Z = 5279950
52 I = 51
28057
XDOT = -3217
124228 Wp = 41
74606
YDOT = 6947
516627 meter/sec RA = 297
37416 deg
ZDOT = 421
081400 TA = 44
25342
MA = 44
18227
Ha = 228
993 n
mi
Hp = 218
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13046567
56 X = 3933586
86
Y = 5006697
53 feet Y = 1570270
24 meter
Z = 17322672
30 Z = 5299162
56
XDOT = -10554
869514 XDOT = -3296
619618
YDOT = 22793
689721 feet/sec YDOT = 6911
096008 meter/sec
ZDOT = 1381
500657 ZDOT = 405
260634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11651090
88 X = -3551252
50
Y = -7516807
89 feet Y = -2291123
05 meter
Z = 17409899
52 Z = 5306537
37
XDOT = 14403
284380 XDOT = 4390
121079
YDOT = -19339
688543 feet/sec YDOT = -5894
737068 meter/sec
ZDOT = 1308
957967 ZDOT = 398
970388
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 19253
54905715
00016717 00000-0 10270-3 0 9014
2 25544 51
6419 297
8768 0008170 25
0978 335
0568 15
50447337 28494
Satellite: ISS
Catalog Number: 25544
Epoch time: 19253
54905715 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 297
8768 deg
Eccentricity:
0008170
Arg of perigee: 25
0978 deg
Mean anomaly: 335
0568 deg
Mean motion: 15
50447337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 342
Coasting Arc #3 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2019/253/21:33:29
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -639676
99 A = 6797255
89 meter
Y = 6238157
67 meter E =
0017463
Z = 2614918
47 I = 51
30572
XDOT = -5384
639833 Wp = 75
11347
YDOT = 1640
401194 meter/sec RA = 295
36698 deg
ZDOT = -5196
954112 TA = 75
34095
MA = 75
14742
Ha = 229
245 n
mi
Hp = 218
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2098677
79 X = -722087
99
Y = 20466396
57 feet Y = 6230543
70 meter
Z = 8579128
85 Z = 2611610
73
XDOT = -17666
141183 XDOT = -5377
339474
YDOT = 5381
893681 feet/sec YDOT = 1580
226916 meter/sec
ZDOT = -17050
374383 ZDOT = -5223
092696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16630247
93 X = -5068899
57
Y = 12123518
35 feet Y = 3695248
39 meter
Z = 8563553
33 Z = 2610171
05
XDOT = -14876
073631 XDOT = -4534
227243
YDOT = -8200
245576 feet/sec YDOT = -2499
434852 meter/sec
ZDOT = -17169
369959 ZDOT = -5233
223964
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 19253
93579122
00016717 00000-0 10270-3 0 9027
2 25544 51
6430 295
9616 0008338 26
1724 333
9846 15
50421513 28556
Satellite: ISS
Catalog Number: 25544
Epoch time: 19253
93579122 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 295
9616 deg
Eccentricity:
0008338
Arg of perigee: 26
1724 deg
Mean anomaly: 333
9846 deg
Mean motion: 15
50421513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 317
Coasting Arc #4 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2019/254/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2436534
71 A = 6790580
51 meter
Y = -4214744
77 meter E =
0015007
Z = -4744981
64 I = 51
26996
XDOT = 4490
532877 Wp = 75
04128
YDOT = -5591
473981 meter/sec RA = 291
38341 deg
ZDOT = 2671
680110 TA = 221
48589
MA = 221
59990
Ha = 229
282 n
mi
Hp = 218
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7993880
29 X = -2366174
92
Y = -13827902
77 feet Y = -4241598
71 meter
Z = -15567525
06 Z = -4756646
11
XDOT = 14732
719414 XDOT = 4539
747229
YDOT = -18344
730910 feet/sec YDOT = -5540
982331 meter/sec
ZDOT = 8765
354693 ZDOT = 2693
613060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15920183
32 X = 4852471
88
Y = -132579
48 feet Y = -40410
22 meter
Z = -15620212
53 Z = -4761040
78
XDOT = 8835
059355 XDOT = 2692
926091
YDOT = 20601
122597 feet/sec YDOT = 6279
222167 meter/sec
ZDOT = 8865
551413 ZDOT = 2702
220071
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 19254
70925353
00016717 00000-0 10270-3 0 9035
2 25544 51
6403 292
1260 0008424 28
6368 331
5244 15
50420587 28676
Satellite: ISS
Catalog Number: 25544
Epoch time: 19254
70925353 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 292
1260 deg
Eccentricity:
0008424
Arg of perigee: 28
6368 deg
Mean anomaly: 331
5244 deg
Mean motion: 15
50420587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 305
Coasting Arc #5 (Orbit 2882)
---------------------------------------
Vector Time (GMT): 2019/255/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2430877
18 A = 6791493
90 meter
Y = 4479670
77 meter E =
0016576
Z = 4483297
47 I = 51
26225
XDOT = -4275
838156 Wp = 50
27816
YDOT = 5513
880310 meter/sec RA = 286
39809 deg
ZDOT = -3172
756638 TA = 71
86245
MA = 71
68200
Ha = 229
315 n
mi
Hp = 218
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7975318
84 X = 2358826
40
Y = 14697082
58 feet Y = 4506452
05 meter
Z = 14708981
21 Z = 4494930
28
XDOT = -14028
340406 XDOT = -4321
766840
YDOT = 18090
158499 feet/sec YDOT = 5465
807813 meter/sec
ZDOT = -10409
306555 ZDOT = -3193
638839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16675176
00 X = -5082593
64
Y = -16090
80 feet Y = -4904
48 meter
Z = 14761514
89 Z = 4499309
74
XDOT = -9333
097930 XDOT = -2844
728249
YDOT = -19639
919920 feet/sec YDOT = -5986
247592 meter/sec
ZDOT = -10504
701087 ZDOT = -3201
832891
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 19255
74053616
00016717 00000-0 10270-3 0 9045
2 25544 51
6404 287
0133 0008500 31
7543 328
4118 15
50449424 28838
Satellite: ISS
Catalog Number: 25544
Epoch time: 19255
74053616 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 287
0133 deg
Eccentricity:
0008500
Arg of perigee: 31
7543 deg
Mean anomaly: 328
4118 deg
Mean motion: 15
50449424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2883
Checksum: 297
Coasting Arc #6 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2019/256/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2510810
08 A = 6792528
31 meter
Y = -4695667
81 meter E =
0013202
Z = -4225315
20 I = 51
25646
XDOT = 4046
799344 Wp = 71
31338
YDOT = -5401
478484 meter/sec RA = 281
41371 deg
ZDOT = 3611
492555 TA = 235
84579
MA = 235
97106
Ha = 229
433 n
mi
Hp = 218
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8237565
87 X = -2437591
07
Y = -15405734
27 feet Y = -4723336
46 meter
Z = -13862582
69 Z = -4237333
41
XDOT = 13276
900734 XDOT = 4089
356974
YDOT = -17721
386104 feet/sec YDOT = -5355
986024 meter/sec
ZDOT = 11848
728855 ZDOT = 3631
254119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17425619
58 X = 5311328
85
Y = -184444
92 feet Y = -56218
81 meter
Z = -13916863
90 Z = -4241860
12
XDOT = 9696
490546 XDOT = 2955
490318
YDOT = 18576
048846 feet/sec YDOT = 5661
979688 meter/sec
ZDOT = 11939
001598 ZDOT = 3639
007687
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 19256
70736374
00016717 00000-0 10270-3 0 9052
2 25544 51
6397 282
2208 0008534 35
2698 324
9016 15
50425372 28986
Satellite: ISS
Catalog Number: 25544
Epoch time: 19256
70736374 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 282
2208 deg
Eccentricity:
0008534
Arg of perigee: 35
2698 deg
Mean anomaly: 324
9016 deg
Mean motion: 15
50425372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 332
Coasting Arc #7 (Orbit 2909)
---------------------------------------
Vector Time (GMT): 2019/257/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3963097
04 A = 6792131
70 meter
Y = 3452017
55 meter E =
0016396
Z = -4319941
29 I = 51
25293
XDOT = -1923
245471 Wp = 54
87250
YDOT = -6542
097598 meter/sec RA = 277
67221 deg
ZDOT = -3463
467347 TA = 179
63233
MA = 179
63113
Ha = 229
470 n
mi
Hp = 218
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13002286
88 X = -3980420
17
Y = 11325516
88 feet Y = 3407602
10 meter
Z = -14173035
74 Z = -4339234
87
XDOT = -6309
860468 XDOT = -1833
123375
YDOT = -21463
574795 feet/sec YDOT = -6563
101134 meter/sec
ZDOT = -11363
081846 ZDOT = -3472
590154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16282219
89 X = 4962820
62
Y = -5451085
37 feet Y = -1661490
82 meter
Z = -14261021
09 Z = -4346759
23
XDOT = -2951
748715 XDOT = -899
693008
YDOT = 21017
232212 feet/sec YDOT = 6406
052378 meter/sec
ZDOT = -11404
067769 ZDOT = -3475
959856
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 19257
48082527
00016717 00000-0 10270-3 0 9063
2 25544 51
6418 278
3858 0008347 39
9196 320
2567 15
50438338 29104
Satellite: ISS
Catalog Number: 25544
Epoch time: 19257
48082527 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 278
3858 deg
Eccentricity:
0008347
Arg of perigee: 39
9196 deg
Mean anomaly: 320
2567 deg
Mean motion: 15
50438338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2910
Checksum: 341
Coasting Arc #8 (Orbit 2925)
---------------------------------------
Vector Time (GMT): 2019/258/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3824776
55 A = 6791091
80 meter
Y = -3237065
25 meter E =
0013863
Z = 4570615
52 I = 51
24568
XDOT = 2101
110669 Wp = 78
72223
YDOT = 6736
934474 meter/sec RA = 272
68607 deg
ZDOT = 3007
963406 TA = 341
06627
MA = 341
11776
Ha = 229
431 n
mi
Hp = 218
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12548479
51 X = 3838488
58
Y = -10620292
82 feet Y = -3194216
75 meter
Z = 14995457
75 Z = 4589228
50
XDOT = 6893
407707 XDOT = 2011
009144
YDOT = 22102
803391 feet/sec YDOT = 6759
927107 meter/sec
ZDOT = 9868
646345 ZDOT = 3017
950253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15497896
82 X = -4723758
95
Y = 5245737
89 feet Y = 1598900
91 meter
Z = 15080322
90 Z = 4596482
42
XDOT = 2240
216744 XDOT = 682
818064
YDOT = -21928
787478 feet/sec YDOT = -6683
894423 meter/sec
ZDOT = 9913
562921 ZDOT = 3021
653978
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 19258
51210542
00016717 00000-0 10270-3 0 9079
2 25544 51
6411 273
2730 0008510 43
7233 316
4590 15
50451640 29268
Satellite: ISS
Catalog Number: 25544
Epoch time: 19258
51210542 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 273
2730 deg
Eccentricity:
0008510
Arg of perigee: 43
7233 deg
Mean anomaly: 316
4590 deg
Mean motion: 15
50451640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2926
Checksum: 281
Coasting Arc #9 (Orbit 2940)
---------------------------------------
Vector Time (GMT): 2019/259/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3747400
18 A = 6790220
20 meter
Y = 3010100
63 meter E =
0019526
Z = -4814893
42 I = 51
24382
XDOT = -2286
791296 Wp = 61
30186
YDOT = -6853
932110 meter/sec RA = 267
69934 deg
ZDOT = -2503
615474 TA = 183
86547
MA = 183
88058
Ha = 229
606 n
mi
Hp = 217
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12294620
02 X = -3757393
30
Y = 9875658
24 feet Y = 2968138
18 meter
Z = -15796894
43 Z = -4833121
55
XDOT = -7502
596115 XDOT = -2197
817460
YDOT = -22486
653905 feet/sec YDOT = -6879
007402 meter/sec
ZDOT = -8213
961530 ZDOT = -2514
507073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14898739
71 X = 4541135
86
Y = -4907319
38 feet Y = -1495750
95 meter
Z = -15879985
90 Z = -4840219
70
XDOT = -1374
833237 XDOT = -419
049171
YDOT = 22579
920585 feet/sec YDOT = 6882
359794 meter/sec
ZDOT = -8262
998972 ZDOT = -2518
562087
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
47892948
00016717 00000-0 10270-3 0 9082
2 25544 51
6427 268
4803 0008468 46
6049 313
5806 15
50442491 29410
Satellite: ISS
Catalog Number: 25544
Epoch time: 19259
47892948 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 268
4803 deg
Eccentricity:
0008468
Arg of perigee: 46
6049 deg
Mean anomaly: 313
5806 deg
Mean motion: 15
50442491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2941
Checksum: 346
Coasting Arc #10 (Orbit 2956)
---------------------------------------
Vector Time (GMT): 2019/260/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3682689
27 A = 6789404
78 meter
Y = -2752350
53 meter E =
0011807
Z = 4985062
93 I = 51
24185
XDOT = 2506
219357 Wp = 79
22900
YDOT = 6970
281830 meter/sec RA = 262
71172 deg
ZDOT = 1995
105956 TA = 351
27803
MA = 351
29853
Ha = 229
568 n
mi
Hp = 217
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12082313
87 X = 3688978
28
Y = -9030021
44 feet Y = -2711132
46 meter
Z = 16355193
35 Z = 5002967
74
XDOT = 8222
504452 XDOT = 2418
398187
YDOT = 22868
378707 feet/sec YDOT = 6997
817296 meter/sec
ZDOT = 6545
623215 ZDOT = 2007
066349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14322392
69 X = -4365465
29
Y = 4440370
80 feet Y = 1353425
02 meter
Z = 16436791
65 Z = 5009934
09
XDOT = 374
881056 XDOT = 114
263746
YDOT = -23242
651730 feet/sec YDOT = -7084
360247 meter/sec
ZDOT = 6599
526908 ZDOT = 2011
535801
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
51020793
00016717 00000-0 10270-3 0 9091
2 25544 51
6408 263
3675 0008635 50
6982 309
4933 15
50452074 29577
Satellite: ISS
Catalog Number: 25544
Epoch time: 19260
51020793 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 263
3675 deg
Eccentricity:
0008635
Arg of perigee: 50
6982 deg
Mean anomaly: 309
4933 deg
Mean motion: 15
50452074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2957
Checksum: 322
Coasting Arc #11 (Orbit 2960)
---------------------------------------
Vector Time (GMT): 2019/260/17:57:49
866
Vector Time (MET): N/A
Weight (LBS) : 951554
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3649670
80 A = 6790597
38 meter
Y = 2785739
16 meter E =
0019108
Z = -5020666
14 I = 51
24405
XDOT = -2627
470705 Wp = 64
81264
YDOT = -6918
211153 meter/sec RA = 261
26569 deg
ZDOT = -1926
427751 TA = 186
32785
MA = 186
35202
Ha = 229
681 n
mi
Hp = 219
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11973985
58 X = -3656162
67
Y = 9139564
17 feet Y = 2744889
20 meter
Z = -16472001
76 Z = -5038411
05
XDOT = -8620
310713 XDOT = -2540
556388
YDOT = -22697
543152 feet/sec YDOT = -6947
107594 meter/sec
ZDOT = -6320
301020 ZDOT = -1938
979387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8057889
21 X = -2456044
63
Y = -12621710
68 feet Y = -3847097
42 meter
Z = -16552874
27 Z = -5045316
08
XDOT = 22444
981168 XDOT = 6841
230260
YDOT = -5956
797072 feet/sec YDOT = -1815
631748 meter/sec
ZDOT = -6376
900718 ZDOT = -1943
679339
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
76803073
00016717 00000-0 10270-3 0 9100
2 25544 51
6420 262
0900 0006899 44
3962 315
7740 15
50022642 29611
Satellite: ISS
Catalog Number: 25544
Epoch time: 19260
76803073 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 262
0900 deg
Eccentricity:
0006899
Arg of perigee: 44
3962 deg
Mean anomaly: 315
7740 deg
Mean motion: 15
50022642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2961
Checksum: 295
Coasting Arc #12 (Orbit 2976)
---------------------------------------
Vector Time (GMT): 2019/261/17:57:49
866
Vector Time (MET): N/A
Weight (LBS) : 951554
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3564379
88 A = 6790113
24 meter
Y = -2687486
72 meter E =
0009088
Z = 5108298
79 I = 51
24894
XDOT = 2969
217259 Wp = 79
14603
YDOT = 6897
225973 meter/sec RA = 256
28281 deg
ZDOT = 1556
153972 TA = 355
76829
MA = 355
77597
Ha = 229
499 n
mi
Hp = 219
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11694159
72 X = 3569353
67
Y = -8817213
65 feet Y = -2647599
11 meter
Z = 16759510
47 Z = 5125625
69
XDOT = 9741
526440 XDOT = 2884
310787
YDOT = 22628
694138 feet/sec YDOT = 6929
955232 meter/sec
ZDOT = 5105
492034 ZDOT = 1570
370720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7972242
99 X = 2429939
66
Y = 12177313
94 feet Y = 3711645
29 meter
Z = 16838473
39 Z = 5132366
69
XDOT = -22372
747645 XDOT = -6819
213482
YDOT = 7495
410557 feet/sec YDOT = 2284
601138 meter/sec
ZDOT = 5169
678604 ZDOT = 1575
718039
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
79960114
00016717 00000-0 10270-3 0 9115
2 25544 51
6422 256
9797 0006695 47
6624 312
5092 15
50033042 29772
Satellite: ISS
Catalog Number: 25544
Epoch time: 19261
79960114 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 256
9797 deg
Eccentricity:
0006695
Arg of perigee: 47
6624 deg
Mean anomaly: 312
5092 deg
Mean motion: 15
50033042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2977
Checksum: 321
Coasting Arc #13 (Orbit 2991)
---------------------------------------
Vector Time (GMT): 2019/262/17:57:49
866
Vector Time (MET): N/A
Weight (LBS) : 951554
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3525329
22 A = 6789794
01 meter
Y = 2605511
32 meter E =
0020307
Z = -5202932
46 I = 51
25810
XDOT = -3293
900260 Wp = 71
21238
YDOT = -6800
631459 meter/sec RA = 251
30011 deg
ZDOT = -1171
131333 TA = 187
44814
MA = 187
47836
Ha = 229
730 n
mi
Hp = 218
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11566040
73 X = -3528929
53
Y = 8548265
49 feet Y = 2566068
17 meter
Z = -17069988
38 Z = -5220066
29
XDOT = -10806
759384 XDOT = -3211
920049
YDOT = -22311
783002 feet/sec YDOT = -6837
007862 meter/sec
ZDOT = -3842
294398 ZDOT = -1186
932540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7918953
78 X = -2413697
11
Y = -11893888
71 feet Y = -3625257
28 meter
Z = -17148067
73 Z = -5226731
04
XDOT = 21992
269261 XDOT = 6703
243671
YDOT = -8987
434464 feet/sec YDOT = -2739
370025 meter/sec
ZDOT = -3913
707060 ZDOT = -1192
897912
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
76669780
00016717 00000-0 10270-3 0 9129
2 25544 51
6434 252
1887 0006848 50
6545 309
5212 15
50030373 29920
Satellite: ISS
Catalog Number: 25544
Epoch time: 19262
76669780 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 252
1887 deg
Eccentricity:
0006848
Arg of perigee: 50
6545 deg
Mean anomaly: 309
5212 deg
Mean motion: 15
50030373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2992
Checksum: 323
Coasting Arc #14 (Orbit 3007)
---------------------------------------
Vector Time (GMT): 2019/263/17:57:49
866
Vector Time (MET): N/A
Weight (LBS) : 951554
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3496792
20 A = 6789492
03 meter
Y = -2503304
50 meter E =
0008698
Z = 5246313
20 I = 51
26867
XDOT = 3629
405846 Wp = 74
15101
YDOT = 6709
891180 meter/sec RA = 246
31792 deg
ZDOT = 783
820987 TA = 8
32746
MA = 8
31303
Ha = 229
613 n
mi
Hp = 218
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11472415
34 X = 3499041
03
Y = -8212941
29 feet Y = -2464188
12 meter
Z = 17212313
66 Z = 5263305
05
XDOT = 11907
499495 XDOT = 3550
296749
YDOT = 22014
078676 feet/sec YDOT = 6750
035460 meter/sec
ZDOT = 2571
591164 ZDOT = 801
259051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7790725
08 X = 2374613
00
Y = 11649114
57 feet Y = 3550650
12 meter
Z = 17289742
40 Z = 5269913
48
XDOT = -21585
230756 XDOT = -6579
178334
YDOT = 10508
020564 feet/sec YDOT = 3202
844668 meter/sec
ZDOT = 2650
469863 ZDOT = 807
863214
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
79826511
00016717 00000-0 10270-3 0 9131
2 25544 51
6431 247
0781 0006809 54
4516 305
7269 15
50038007 30081
Satellite: ISS
Catalog Number: 25544
Epoch time: 19263
79826511 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 247
0781 deg
Eccentricity:
0006809
Arg of perigee: 54
4516 deg
Mean anomaly: 305
7269 deg
Mean motion: 15
50038007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3008
Checksum: 306
Coasting Arc #15 (Orbit 3022)
---------------------------------------
Vector Time (GMT): 2019/264/17:57:49
866
Vector Time (MET): N/A
Weight (LBS) : 951554
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3509528
55 A = 6789379
07 meter
Y = 2432243
53 meter E =
0020955
Z = -5296635
08 I = 51
28226
XDOT = -3936
400934 Wp = 77
74025
YDOT = -6543
430612 meter/sec RA = 241
33728 deg
ZDOT = -393
501525 TA = 188
46020
MA = 188
49558
Ha = 229
790 n
mi
Hp = 218
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11514201
29 X = -3510737
45
Y = 7979801
60 feet Y = 2392990
60 meter
Z = -17377411
66 Z = -5313686
19
XDOT = -12914
701228 XDOT = -3861
026412
YDOT = -21467
948203 feet/sec YDOT = -6587
028788 meter/sec
ZDOT = -1291
015501 ZDOT = -412
439983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7756056
47 X = -2364046
01
Y = -11549514
19 feet Y = -3520291
93 meter
Z = -17455108
45 Z = -5320317
06
XDOT = 20872
261437 XDOT = 6361
865286
YDOT = -11921
035941 feet/sec YDOT = -3633
531755 meter/sec
ZDOT = -1376
747358 ZDOT = -419
632595
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
76536055
00016717 00000-0 10270-3 0 9141
2 25544 51
6427 242
2878 0006822 57
3029 302
8778 15
50030806 30235
Satellite: ISS
Catalog Number: 25544
Epoch time: 19264
76536055 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 242
2878 deg
Eccentricity:
0006822
Arg of perigee: 57
3029 deg
Mean anomaly: 302
8778 deg
Mean motion: 15
50030806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3023
Checksum: 310
Coasting Arc #16 (Orbit 3024)
---------------------------------------
Vector Time (GMT): 2019/264/20:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 951554
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -544976
52 A = 6797372
68 meter
Y = -6031125
87 meter E =
0019292
Z = 3065198
32 I = 51
30870
XDOT = 5574
644020 Wp = 74
97381
YDOT = 1985
988898 meter/sec RA = 240
92113 deg
ZDOT = 4877
940740 TA = 320
37820
MA = 320
51902
Ha = 229
785 n
mi
Hp = 218
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1787980
71 X = -492383
37
Y = -19787158
38 feet Y = -6036926
04 meter
Z = 10056424
93 Z = 3062678
91
XDOT = 18289
514501 XDOT = 5528
327289
YDOT = 6515
711608 feet/sec YDOT = 2048
069655 meter/sec
ZDOT = 16003
742584 ZDOT = 4904
907928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16103467
52 X = 4908336
90
Y = -11646020
29 feet Y = -3549706
99 meter
Z = 10045334
21 Z = 3061817
87
XDOT = 2768
928065 XDOT = 843
969274
YDOT = 17797
614811 feet/sec YDOT = 5424
712994 meter/sec
ZDOT = 16126
268779 ZDOT = 4915
286724
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
89430587
00016717 00000-0 10270-3 0 9159
2 25544 51
6413 241
6483 0006774 56
8438 303
3361 15
50009691 30253
Satellite: ISS
Catalog Number: 25544
Epoch time: 19264
89430587 = yrday
fracday
Element set: 915
Inclination: 51
6413 deg
RA of node: 241
6483 deg
Eccentricity:
0006774
Arg of perigee: 56
8438 deg
Mean anomaly: 303
3361 deg
Mean motion: 15
50009691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3025
Checksum: 316
Coasting Arc #17 (Orbit 3039)
---------------------------------------
Vector Time (GMT): 2019/265/20:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 951554
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 712988
92 A = 6796564
83 meter
Y = 5867856
19 meter E =
0010943
Z = -3366965
24 I = 51
32292
XDOT = -5779
492102 Wp = 73
91250
YDOT = -1944
129990 meter/sec RA = 235
94481 deg
ZDOT = -4621
649546 TA = 145
43288
MA = 145
36168
Ha = 229
785 n
mi
Hp = 218
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2339202
48 X = 663674
77
Y = 19251496
67 feet Y = 5875553
52 meter
Z = -11046473
89 Z = -3363621
70
XDOT = -18961
588262 XDOT = -5734
873238
YDOT = -6378
379231 feet/sec YDOT = -2008
510969 meter/sec
ZDOT = -15162
892210 ZDOT = -4649
615847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15152478
52 X = -4618475
45
Y = 12117033
98 feet Y = 3693271
96 meter
Z = -11031611
86 Z = -3362435
29
XDOT = -3531
652647 XDOT = -1076
447727
YDOT = -18307
969995 feet/sec YDOT = -5580
269254 meter/sec
ZDOT = -15289
982813 ZDOT = -4660
386761
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
86139899
00016717 00000-0 10270-3 0 9160
2 25544 51
6410 236
8569 0006631 60
2114 299
9695 15
50009791 30401
Satellite: ISS
Catalog Number: 25544
Epoch time: 19265
86139899 = yrday
fracday
Element set: 916
Inclination: 51
6410 deg
RA of node: 236
8569 deg
Eccentricity:
0006631
Arg of perigee: 60
2114 deg
Mean anomaly: 299
9695 deg
Mean motion: 15
50009791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3040
Checksum: 335
Coasting Arc #18 (Orbit 3055)
---------------------------------------
Vector Time (GMT): 2019/266/20:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 951554
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -886054
51 A = 6795829
54 meter
Y = -5678247
69 meter E =
0018086
Z = 3609401
69 I = 51
33983
XDOT = 6015
573660 Wp = 82
97252
YDOT = 1856
112210 meter/sec RA = 230
96869 deg
ZDOT = 4379
982372 TA = 319
95817
MA = 320
09136
Ha = 229
828 n
mi
Hp = 218
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2907002
99 X = -840025
32
Y = -18629421
54 feet Y = -5687898
70 meter
Z = 11841869
07 Z = 3605209
53
XDOT = 19736
134054 XDOT = 5973
095460
YDOT = 6089
606987 feet/sec YDOT = 1923
145210 meter/sec
ZDOT = 14370
020904 ZDOT = 4409
100554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14109192
32 X = 4300481
82
Y = -12525189
71 feet Y = -3817677
82 meter
Z = 11823121
04 Z = 3603687
29
XDOT = 4497
668083 XDOT = 1370
889232
YDOT = 18807
919516 feet/sec YDOT = 5732
653868 meter/sec
ZDOT = 14502
375912 ZDOT = 4420
324178
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
89296345
00016717 00000-0 10270-3 0 9175
2 25544 51
6407 231
7454 0006712 63
4669 296
7169 15
50014281 30562
Satellite: ISS
Catalog Number: 25544
Epoch time: 19266
89296345 = yrday
fracday
Element set: 917
Inclination: 51
6407 deg
RA of node: 231
7454 deg
Eccentricity:
0006712
Arg of perigee: 63
4669 deg
Mean anomaly: 296
7169 deg
Mean motion: 15
50014281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3056
Checksum: 331
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