[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 8th 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 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 626 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
249/18:14:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 219
3
250/16:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 219
0
253/21:33:27
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
257/11:11:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 218
1
260/17:57:24
923 -1
0 2
4 2
4
N/A -2
1 -0
2 229
6
000/00:00:49
846 -0
5 -0
0 219
0
Coasting Arc #1 (Orbit 2786)
---------------------------------------
Vector Time (GMT): 2019/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4722753
98 A = 6790184
76 meter
Y = 855869
79 meter E =
0008610
Z = 4794847
02 I = 51
37048
XDOT = -3715
093452 Wp = 60
41894
YDOT = 6203
681136 meter/sec RA = 317
30099 deg
ZDOT = 2552
601695 TA = 4
36395
MA = 4
35645
Ha = 228
501 n
mi
Hp = 219
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15494599
68 X = 4689541
74
Y = 2807971
77 feet Y = 908497
35 meter
Z = 15731125
38 Z = 4817707
65
XDOT = -12188
626811 XDOT = -3796
587786
YDOT = 20353
284567 feet/sec YDOT = 6161
680732 meter/sec
ZDOT = 8374
677476 ZDOT = 2534
357145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14066133
20 X = -4287357
40
Y = -6843414
40 feet Y = -2085872
71 meter
Z = 15834999
43 Z = 4826507
82
XDOT = 16767
924857 XDOT = 5110
863497
YDOT = -15285
739229 feet/sec YDOT = -4659
093317 meter/sec
ZDOT = 8291
119546 ZDOT = 2527
133238
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 19249
55281821
00016717 00000-0 10270-3 0 9004
2 25544 51
6433 317
6852 0007857 9
2804 350
8490 15
50450014 27874
Satellite: ISS
Catalog Number: 25544
Epoch time: 19249
55281821 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 317
6852 deg
Eccentricity:
0007857
Arg of perigee: 9
2804 deg
Mean anomaly: 350
8490 deg
Mean motion: 15
50450014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2787
Checksum: 312
Coasting Arc #2 (Orbit 2790)
---------------------------------------
Vector Time (GMT): 2019/249/18:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4075875
13 A = 6788854
25 meter
Y = 1764457
23 meter E =
0007604
Z = 5128607
65 I = 51
35644
XDOT = -4500
086095 Wp = 44
09412
YDOT = 6021
937463 meter/sec RA = 316
00280 deg
ZDOT = 1508
576331 TA = 31
33822
MA = 31
29293
Ha = 228
718 n
mi
Hp = 219
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13372293
73 X = 4030929
68
Y = 5788901
68 feet Y = 1809785
33 meter
Z = 16826140
58 Z = 5148297
47
XDOT = -14764
061993 XDOT = -4574
418488
YDOT = 19757
012674 feet/sec YDOT = 5971
198740 meter/sec
ZDOT = 4949
397412 ZDOT = 1486
536015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8387755
54 X = -2556587
89
Y = 11788118
58 feet Y = 3593018
54 meter
Z = 16915509
05 Z = 5155847
16
XDOT = -15440
338303 XDOT = -4706
215115
YDOT = -17925
253723 feet/sec YDOT = -5463
617335 meter/sec
ZDOT = 4848
598993 ZDOT = 1477
852973
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 19249
81064197
00016717 00000-0 10270-3 0 9019
2 25544 51
6403 316
4084 0008234 10
8642 349
2685 15
50429502 27914
Satellite: ISS
Catalog Number: 25544
Epoch time: 19249
81064197 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 316
4084 deg
Eccentricity:
0008234
Arg of perigee: 10
8642 deg
Mean anomaly: 349
2685 deg
Mean motion: 15
50429502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2791
Checksum: 307
Coasting Arc #3 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2019/250/16:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3072151
11 A = 6788204
07 meter
Y = -2937569
25 meter E =
0018526
Z = -5307170
90 I = 51
33272
XDOT = 5146
259759 Wp = 65
69136
YDOT = -5658
119009 meter/sec RA = 311
32405 deg
ZDOT = 160
734645 TA = 205
80436
MA = 205
89688
Ha = 228
920 n
mi
Hp = 219
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10079235
93 X = -3013294
90
Y = -9637694
40 feet Y = -2971595
21 meter
Z = -17411978
03 Z = -5321951
18
XDOT = 16884
054326 XDOT = 5208
367245
YDOT = -18563
382576 feet/sec YDOT = -5600
222640 meter/sec
ZDOT = 527
344635 ZDOT = 185
884035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13531605
91 X = 4124433
48
Y = -3006055
40 feet Y = -916245
69 meter
Z = -17478913
06 Z = -5327572
70
XDOT = 5978
135519 XDOT = 1822
135706
YDOT = 23326
405528 feet/sec YDOT = 7109
888405 meter/sec
ZDOT = 642
235503 ZDOT = 195
753381
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 19250
71301776
00016717 00000-0 10270-3 0 9028
2 25544 51
6408 311
9354 0008192 14
9709 345
1683 15
50415576 28056
Satellite: ISS
Catalog Number: 25544
Epoch time: 19250
71301776 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 311
9354 deg
Eccentricity:
0008192
Arg of perigee: 14
9709 deg
Mean anomaly: 345
1683 deg
Mean motion: 15
50415576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 308
Coasting Arc #4 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2019/251/16:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2900643
64 A = 6788303
80 meter
Y = 3161267
65 meter E =
0010774
Z = 5256974
57 I = 51
31204
XDOT = -4976
335118 Wp = 29
41658
YDOT = 5786
128098 meter/sec RA = 306
34112 deg
ZDOT = -723
826343 TA = 67
58826
MA = 67
47416
Ha = 228
937 n
mi
Hp = 218
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9516547
37 X = 2839542
62
Y = 10371613
04 feet Y = 3193363
16 meter
Z = 17247291
91 Z = 5270916
22
XDOT = -16326
558787 XDOT = -5037
151509
YDOT = 18983
359901 feet/sec YDOT = 5730
139152 meter/sec
ZDOT = -2374
758342 ZDOT = -748
147122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13796143
40 X = -4205064
51
Y = 2370789
25 feet Y = 722616
56 meter
Z = 17310398
45 Z = 5276209
45
XDOT = -7101
799362 XDOT = -2164
628445
YDOT = -22941
064861 feet/sec YDOT = -6992
436570 meter/sec
ZDOT = -2485
879797 ZDOT = -757
696162
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 19251
74430193
00016717 00000-0 10270-3 0 9039
2 25544 51
6407 306
8227 0008272 18
1284 342
0160 15
50438489 28212
Satellite: ISS
Catalog Number: 25544
Epoch time: 19251
74430193 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 306
8227 deg
Eccentricity:
0008272
Arg of perigee: 18
1284 deg
Mean anomaly: 342
0160 deg
Mean motion: 15
50438489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 295
Coasting Arc #5 (Orbit 2835)
---------------------------------------
Vector Time (GMT): 2019/252/16:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2808145
12 A = 6788726
18 meter
Y = -3380587
37 meter E =
0017714
Z = -5187876
90 I = 51
29392
XDOT = 4752
261889 Wp = 72
01558
YDOT = -5862
733355 meter/sec RA = 301
35833 deg
ZDOT = 1256
912211 TA = 210
08643
MA = 210
18830
Ha = 229
126 n
mi
Hp = 218
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9213074
55 X = -2744934
17
Y = -11091165
92 feet Y = -3411636
75 meter
Z = -17020593
49 Z = -5201364
03
XDOT = 15591
410396 XDOT = 4811
362158
YDOT = -19234
689484 feet/sec YDOT = -5809
259725 meter/sec
ZDOT = 4123
727725 ZDOT = 1280
140377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14209639
51 X = 4331098
12
Y = -1974760
80 feet Y = -601907
09 meter
Z = -17081620
87 Z = -5206478
04
XDOT = 8145
530194 XDOT = 2482
757603
YDOT = 22276
095183 feet/sec YDOT = 6789
753812 meter/sec
ZDOT = 4229
872328 ZDOT = 1289
265085
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
71112993
00016717 00000-0 10270-3 0 9043
2 25544 51
6403 302
0307 0008373 21
7305 338
4200 15
50419005 28364
Satellite: ISS
Catalog Number: 25544
Epoch time: 19252
71112993 = yrday
fracday
Element set: 904
Inclination: 51
6403 deg
RA of node: 302
0307 deg
Eccentricity:
0008373
Arg of perigee: 21
7305 deg
Mean anomaly: 338
4200 deg
Mean motion: 15
50419005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2836
Checksum: 271
Coasting Arc #6 (Orbit 2851)
---------------------------------------
Vector Time (GMT): 2019/253/16:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2708906
61 A = 6789224
58 meter
Y = 3641958
54 meter E =
0013366
Z = 5044917
91 I = 51
27890
XDOT = -4544
555098 Wp = 36
70760
YDOT = 5902
608990 meter/sec RA = 296
37357 deg
ZDOT = -1807
875346 TA = 70
95953
MA = 70
81479
Ha = 229
108 n
mi
Hp = 218
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8887488
89 X = 2643474
74
Y = 11948682
87 feet Y = 3671885
82 meter
Z = 16551567
95 Z = 5057917
51
XDOT = -14909
957672 XDOT = -4601
440473
YDOT = 19365
515060 feet/sec YDOT = 5851
470423 meter/sec
ZDOT = -5931
349562 ZDOT = -1830
089252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14749232
49 X = -4495566
06
Y = 1506259
37 feet Y = 459107
86 meter
Z = 16610364
43 Z = 5062839
08
XDOT = -9043
787169 XDOT = -2756
546329
YDOT = -21559
100887 feet/sec YDOT = -6571
213950 meter/sec
ZDOT = -6032
868366 ZDOT = -1838
818278
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
74241185
00016717 00000-0 10270-3 0 9054
2 25544 51
6397 296
9183 0008333 24
8221 335
3329 15
50444054 28524
Satellite: ISS
Catalog Number: 25544
Epoch time: 19253
74241185 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 296
9183 deg
Eccentricity:
0008333
Arg of perigee: 24
8221 deg
Mean anomaly: 335
3329 deg
Mean motion: 15
50444054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2852
Checksum: 312
Coasting Arc #7 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2019/253/21:33:27
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -634772
02 A = 6797224
13 meter
Y = 6236655
52 meter E =
0017423
Z = 2619640
48 I = 51
30564
XDOT = -5385
374517 Wp = 75
03073
YDOT = 1647
588588 meter/sec RA = 295
36698 deg
ZDOT = -5193
925289 TA = 75
36490
MA = 75
17179
Ha = 229
221 n
mi
Hp = 218
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2082585
35 X = -717189
52
Y = 20461468
25 feet Y = 6229096
36 meter
Z = 8594620
99 Z = 2616356
55
XDOT = -17668
551564 XDOT = -5378
169188
YDOT = 5405
474369 feet/sec YDOT = 1587
405563 meter/sec
ZDOT = -17040
437301 ZDOT = -5220
067674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16617641
54 X = -5065057
14
Y = 12129652
23 feet Y = 3697118
00 meter
Z = 8579153
87 Z = 2614926
10
XDOT = -14893
411335 XDOT = -4539
511775
YDOT = -8189
492307 feet/sec YDOT = -2496
157255 meter/sec
ZDOT = -17159
450773 ZDOT = -5230
200595
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
93577825
00016717 00000-0 10270-3 0 9069
2 25544 51
6430 295
9614 0008316 25
9080 334
2486 15
50428791 28551
Satellite: ISS
Catalog Number: 25544
Epoch time: 19253
93577825 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 295
9614 deg
Eccentricity:
0008316
Arg of perigee: 25
9080 deg
Mean anomaly: 334
2486 deg
Mean motion: 15
50428791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 334
Coasting Arc #8 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2019/254/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2430021
13 A = 6790571
90 meter
Y = -4222800
10 meter E =
0014940
Z = -4741070
41 I = 51
26997
XDOT = 4495
007554 Wp = 74
97609
YDOT = -5583
788049 meter/sec RA = 291
38321 deg
ZDOT = 2680
399701 TA = 221
64453
MA = 221
75838
Ha = 229
256 n
mi
Hp = 218
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7972510
28 X = -2359590
75
Y = -13854331
05 feet Y = -4249580
82 meter
Z = -15554692
96 Z = -4752703
07
XDOT = 14747
400110 XDOT = 4544
093272
YDOT = -18319
514596 feet/sec YDOT = -5533
247078 meter/sec
ZDOT = 8793
962273 ZDOT = 2702
354074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15932855
13 X = 4856334
24
Y = -101102
41 feet Y = -30816
02 meter
Z = -15607235
11 Z = -4757085
26
XDOT = 8808
273261 XDOT = 2684
761690
YDOT = 20600
529090 feet/sec YDOT = 6279
041267 meter/sec
ZDOT = 8894
255763 ZDOT = 2710
969157
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
70923667
00016717 00000-0 10270-3 0 9075
2 25544 51
6403 292
1258 0008402 28
3796 331
7811 15
50428877 28673
Satellite: ISS
Catalog Number: 25544
Epoch time: 19254
70923667 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 292
1258 deg
Eccentricity:
0008402
Arg of perigee: 28
3796 deg
Mean anomaly: 331
7811 deg
Mean motion: 15
50428877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 332
Coasting Arc #9 (Orbit 2882)
---------------------------------------
Vector Time (GMT): 2019/255/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2422605
49 A = 6791489
77 meter
Y = 4490327
43 meter E =
0016564
Z = 4477141
32 I = 51
26229
XDOT = -4281
805456 Wp = 50
28387
YDOT = 5502
822707 meter/sec RA = 286
39782 deg
ZDOT = -3183
825081 TA = 71
98206
MA = 71
80163
Ha = 229
288 n
mi
Hp = 218
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7948180
75 X = 2350466
06
Y = 14732045
36 feet Y = 4517015
71 meter
Z = 14688783
84 Z = 4488733
73
XDOT = -14047
918164 XDOT = -4327
556284
YDOT = 18053
880272 feet/sec YDOT = 5454
684472 meter/sec
ZDOT = -10445
620346 ZDOT = -3204
735836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16693199
92 X = -5088087
34
Y = -56420
97 feet Y = -17197
11 meter
Z = 14741132
98 Z = 4493097
33
XDOT = -9294
929258 XDOT = -2833
094438
YDOT = -19638
470263 feet/sec YDOT = -5985
805736 meter/sec
ZDOT = -10541
143821 ZDOT = -3212
940637
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
74051336
00016717 00000-0 10270-3 0 9086
2 25544 51
6404 287
0131 0008478 31
5022 328
6635 15
50458945 28834
Satellite: ISS
Catalog Number: 25544
Epoch time: 19255
74051336 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 287
0131 deg
Eccentricity:
0008478
Arg of perigee: 31
5022 deg
Mean anomaly: 328
6635 deg
Mean motion: 15
50458945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2883
Checksum: 314
Coasting Arc #10 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2019/256/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2500641
73 A = 6792529
40 meter
Y = -4709156
87 meter E =
0013131
Z = -4216200
18 I = 51
25653
XDOT = 4054
772741 Wp = 71
08549
YDOT = -5386
580062 meter/sec RA = 281
41338 deg
ZDOT = 3624
960183 TA = 236
23568
MA = 236
36084
Ha = 229
404 n
mi
Hp = 218
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8204205
15 X = -2427316
91
Y = -15449989
74 feet Y = -4736711
23 meter
Z = -13832677
75 Z = -4228168
73
XDOT = 13303
060175 XDOT = 4097
097762
YDOT = -17672
506764 feet/sec YDOT = -5340
999736 meter/sec
ZDOT = 11892
913986 ZDOT = 3644
759912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17449775
48 X = 5318691
57
Y = -134701
98 feet Y = -41057
16 meter
Z = -13886732
16 Z = -4232675
96
XDOT = 9644
819775 XDOT = 2939
741067
YDOT = 18574
892056 feet/sec YDOT = 5661
627099 meter/sec
ZDOT = 11983
359105 ZDOT = 3652
527855
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
70733460
00016717 00000-0 10270-3 0 9099
2 25544 51
6396 282
2206 0008512 35
0252 325
1457 15
50436140 28980
Satellite: ISS
Catalog Number: 25544
Epoch time: 19256
70733460 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 282
2206 deg
Eccentricity:
0008512
Arg of perigee: 35
0252 deg
Mean anomaly: 325
1457 deg
Mean motion: 15
50436140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 303
Coasting Arc #11 (Orbit 2909)
---------------------------------------
Vector Time (GMT): 2019/257/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 951418
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4073134
85 A = 6788338
03 meter
Y = -1409799
66 meter E =
0020299
Z = -5260959
00 I = 51
24010
XDOT = 1606
403201 Wp = 75
70028
YDOT = -7439
307145 meter/sec RA = 277
60339 deg
ZDOT = 757
218719 TA = 201
55116
MA = 201
63672
Ha = 229
429 n
mi
Hp = 218
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13363303
33 X = -4031512
63
Y = -4625326
97 feet Y = -1455116
14 meter
Z = -17260364
18 Z = -5280643
44
XDOT = 5270
351708 XDOT = 1685
794161
YDOT = -24407
175673 feet/sec YDOT = -7420
899232 meter/sec
ZDOT = 2484
313381 ZDOT = 765
215573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10865861
27 X = 3311914
51
Y = 8877533
16 feet Y = 2705872
11 meter
Z = -17349759
68 Z = -5288206
75
XDOT = -12636
114090 XDOT = -3851
487575
YDOT = 20346
507302 feet/sec YDOT = 6201
615426 meter/sec
ZDOT = 2521
235205 ZDOT = 768
472490
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
48079032
00016717 00000-0 10270-3 0 9105
2 25544 51
6417 278
3857 0008325 38
8416 321
3331 15
50432115 29109
Satellite: ISS
Catalog Number: 25544
Epoch time: 19257
48079032 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 278
3857 deg
Eccentricity:
0008325
Arg of perigee: 38
8416 deg
Mean anomaly: 321
3331 deg
Mean motion: 15
50432115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2910
Checksum: 298
Coasting Arc #12 (Orbit 2925)
---------------------------------------
Vector Time (GMT): 2019/258/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 951418
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4068060
84 A = 6788590
09 meter
Y = 1694340
16 meter E =
0012717
Z = 5157424
14 I = 51
23754
XDOT = -1401
644376 Wp = 47
07318
YDOT = 7422
112202 meter/sec RA = 272
61449 deg
ZDOT = -1322
163848 TA = 55
76220
MA = 55
64180
Ha = 229
372 n
mi
Hp = 217
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13346656
31 X = 4023759
99
Y = 5558858
79 feet Y = 1739584
93 meter
Z = 16920682
88 Z = 5177077
47
XDOT = -4598
570786 XDOT = -1478
114069
YDOT = 24350
761819 feet/sec YDOT = 7406
010316 meter/sec
ZDOT = -4337
807901 ZDOT = -1329
159033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10699278
99 X = -3261140
24
Y = -9567222
72 feet Y = -2916089
48 meter
Z = 17009918
68 Z = 5184623
21
XDOT = 11554
894113 XDOT = 3521
931725
YDOT = -20753
487830 feet/sec YDOT = -6325
663091 meter/sec
ZDOT = -4370
154552 ZDOT = -1332
023108
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
51206195
00016717 00000-0 10270-3 0 9113
2 25544 51
6411 273
2730 0008461 43
0642 317
1170 15
50476647 29266
Satellite: ISS
Catalog Number: 25544
Epoch time: 19258
51206195 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 273
2730 deg
Eccentricity:
0008461
Arg of perigee: 43
0642 deg
Mean anomaly: 317
1170 deg
Mean motion: 15
50476647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2926
Checksum: 293
Coasting Arc #13 (Orbit 2940)
---------------------------------------
Vector Time (GMT): 2019/259/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 951418
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4132622
20 A = 6789250
21 meter
Y = -1933148
15 meter E =
0018933
Z = -5043264
22 I = 51
24056
XDOT = 1182
004446 Wp = 81
48039
YDOT = -7327
767289 meter/sec RA = 267
62639 deg
ZDOT = 1848
990449 TA = 206
52934
MA = 206
62636
Ha = 229
562 n
mi
Hp = 217
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13558471
80 X = -4086200
55
Y = -6342349
58 feet Y = -1979103
02 meter
Z = -16546142
47 Z = -5063226
08
XDOT = 3877
967341 XDOT = 1254
876402
YDOT = -24041
231263 feet/sec YDOT = -7314
141635 meter/sec
ZDOT = 6066
241632 ZDOT = 1854
909971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10823631
01 X = 3299042
73
Y = 10193103
34 feet Y = 3106857
90 meter
Z = -16636767
78 Z = -5070886
82
XDOT = -10344
922009 XDOT = -3153
132228
YDOT = 20884
153417 feet/sec YDOT = 6365
489961 meter/sec
ZDOT = 6093
673521 ZDOT = 1857
351689
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
47887769
00016717 00000-0 10270-3 0 9122
2 25544 51
6427 268
4801 0008475 45
5482 314
6361 15
50441962 29415
Satellite: ISS
Catalog Number: 25544
Epoch time: 19259
47887769 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 268
4801 deg
Eccentricity:
0008475
Arg of perigee: 45
5482 deg
Mean anomaly: 314
6361 deg
Mean motion: 15
50441962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2941
Checksum: 341
Coasting Arc #14 (Orbit 2956)
---------------------------------------
Vector Time (GMT): 2019/260/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 951418
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4207035
76 A = 6789889
80 meter
Y = 2201438
77 meter E =
0015435
Z = 4846111
87 I = 51
24377
XDOT = -1003
966170 Wp = 54
13605
YDOT = 7215
768112 meter/sec RA = 262
63834 deg
ZDOT = -2392
062794 TA = 59
52069
MA = 59
36835
Ha = 229
508 n
mi
Hp = 217
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13802610
75 X = 4158566
05
Y = 7222568
13 feet Y = 2248214
26 meter
Z = 15899317
17 Z = 4866430
30
XDOT = -3293
852263 XDOT = -1072
960952
YDOT = 23673
779894 feet/sec YDOT = 7204
155049 meter/sec
ZDOT = -7847
975047 ZDOT = -2397
107998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10977008
38 X = -3345792
15
Y = -10919773
34 feet Y = -3328346
91 meter
Z = 15991550
20 Z = 4874224
50
XDOT = 9239
827560 XDOT = 2816
299440
YDOT = -20883
765018 feet/sec YDOT = -6365
371578 meter/sec
ZDOT = -7871
409048 ZDOT = -2399
205478
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
51014576
00016717 00000-0 10270-3 0 9138
2 25544 51
6408 263
3673 0008583 49
9608 310
2294 15
50485563 29572
Satellite: ISS
Catalog Number: 25544
Epoch time: 19260
51014576 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 263
3673 deg
Eccentricity:
0008583
Arg of perigee: 49
9608 deg
Mean anomaly: 310
2294 deg
Mean motion: 15
50485563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2957
Checksum: 324
Coasting Arc #15 (Orbit 2960)
---------------------------------------
Vector Time (GMT): 2019/260/17:57:49
846
Vector Time (MET): N/A
Weight (LBS) : 951168
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3663996
95 A = 6790506
08 meter
Y = 2747637
90 meter E =
0019137
Z = -5031109
25 I = 51
24386
XDOT = -2602
133994 Wp = 64
89987
YDOT = -6937
460787 meter/sec RA = 261
26472 deg
ZDOT = -1891
424392 TA = 186
59513
MA = 186
62035
Ha = 229
645 n
mi
Hp = 219
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12020987
35 X = -3670010
96
Y = 9014560
05 feet Y = 2706630
41 meter
Z = -16506263
93 Z = -5048922
59
XDOT = -8537
185020 XDOT = -2515
176333
YDOT = -22760
698121 feet/sec YDOT = -6966
073650 meter/sec
ZDOT = -6205
460603 ZDOT = -1903
852843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7929230
08 X = -2416829
33
Y = -12657296
63 feet Y = -3857944
01 meter
Z = -16587444
99 Z = -5055853
23
XDOT = 22498
042792 XDOT = 6857
403443
YDOT = -5878
551721 feet/sec YDOT = -1791
782565 meter/sec
ZDOT = -6261
498897 ZDOT = -1908
504864
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
76796650
00016717 00000-0 10270-3 0 9146
2 25544 51
6420 262
0895 0006883 44
0251 316
1447 15
50038525 29611
Satellite: ISS
Catalog Number: 25544
Epoch time: 19260
76796650 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 262
0895 deg
Eccentricity:
0006883
Arg of perigee: 44
0251 deg
Mean anomaly: 316
1447 deg
Mean motion: 15
50038525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2961
Checksum: 311
Coasting Arc #16 (Orbit 2976)
---------------------------------------
Vector Time (GMT): 2019/261/17:57:49
846
Vector Time (MET): N/A
Weight (LBS) : 951168
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3583376
17 A = 6790017
71 meter
Y = -2643014
13 meter E =
0008980
Z = 5118162
84 I = 51
24875
XDOT = 2939
979462 Wp = 78
51042
YDOT = 6919
049818 meter/sec RA = 256
28164 deg
ZDOT = 1514
118684 TA = 356
82149
MA = 356
82719
Ha = 229
459 n
mi
Hp = 219
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11756483
49 X = 3587803
32
Y = -8671306
19 feet Y = -2602917
14 meter
Z = 16791872
83 Z = 5135580
69
XDOT = 9645
601911 XDOT = 2855
035310
YDOT = 22700
294677 feet/sec YDOT = 6951
451905 meter/sec
ZDOT = 4967
580984 ZDOT = 1528
193311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7822276
83 X = 2384229
98
Y = 12228919
84 feet Y = 3727374
77 meter
Z = 16871246
34 Z = 5142355
89
XDOT = -22433
667563 XDOT = -6837
781873
YDOT = 7406
478902 feet/sec YDOT = 2257
494769 meter/sec
ZDOT = 5031
119892 ZDOT = 1533
485343
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
79952576
00016717 00000-0 10270-3 0 9152
2 25544 51
6421 256
9791 0006678 47
2740 312
8972 15
50050827 29771
Satellite: ISS
Catalog Number: 25544
Epoch time: 19261
79952576 = yrday
fracday
Element set: 915
Inclination: 51
6421 deg
RA of node: 256
9791 deg
Eccentricity:
0006678
Arg of perigee: 47
2740 deg
Mean anomaly: 312
8972 deg
Mean motion: 15
50050827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2977
Checksum: 347
Coasting Arc #17 (Orbit 2991)
---------------------------------------
Vector Time (GMT): 2019/262/17:57:49
846
Vector Time (MET): N/A
Weight (LBS) : 951168
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3549634
92 A = 6789701
68 meter
Y = 2554862
74 meter E =
0020320
Z = -5211395
48 I = 51
25793
XDOT = -3260
780194 Wp = 71
39945
YDOT = -6824
873502 meter/sec RA = 251
29873 deg
ZDOT = -1122
111988 TA = 187
74039
MA = 187
77180
Ha = 229
690 n
mi
Hp = 218
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11645783
87 X = -3552625
95
Y = 8382095
62 feet Y = 2515151
20 meter
Z = -17097754
20 Z = -5228645
89
XDOT = -10698
097748 XDOT = -3178
769474
YDOT = -22391
317264 feet/sec YDOT = -6860
879360 meter/sec
ZDOT = -3681
469778 ZDOT = -1137
752233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7748726
26 X = -2361811
76
Y = -11964401
00 feet Y = -3646749
42 meter
Z = -17176360
42 Z = -5235354
66
XDOT = 22060
764418 XDOT = 6724
120995
YDOT = -8888
117262 feet/sec YDOT = -2709
098142 meter/sec
ZDOT = -3752
148951 ZDOT = -1143
655000
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
76661115
00016717 00000-0 10270-3 0 9167
2 25544 51
6434 252
1880 0006831 50
3046 309
8705 15
50048901 29924
Satellite: ISS
Catalog Number: 25544
Epoch time: 19262
76661115 = yrday
fracday
Element set: 916
Inclination: 51
6434 deg
RA of node: 252
1880 deg
Eccentricity:
0006831
Arg of perigee: 50
3046 deg
Mean anomaly: 309
8705 deg
Mean motion: 15
50048901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2992
Checksum: 305
Coasting Arc #18 (Orbit 3007)
---------------------------------------
Vector Time (GMT): 2019/263/17:57:49
846
Vector Time (MET): N/A
Weight (LBS) : 951168
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3527534
36 A = 6789401
78 meter
Y = -2446005
59 meter E =
0008640
Z = 5252722
52 I = 51
26853
XDOT = 3591
365954 Wp = 73
15305
YDOT = 6736
712473 meter/sec RA = 246
31631 deg
ZDOT = 726
684838 TA = 9
87831
MA = 9
86134
Ha = 229
568 n
mi
Hp = 218
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11573275
46 X = 3529109
04
Y = -8024952
72 feet Y = -2406549
20 meter
Z = 17233341
61 Z = 5269862
07
XDOT = 11782
696698 XDOT = 3512
237299
YDOT = 22102
075044 feet/sec YDOT = 6776
431253 meter/sec
ZDOT = 2384
136609 ZDOT = 743
938069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7599157
51 X = 2316223
21
Y = 11742893
15 feet Y = 3579233
83 meter
Z = 17311438
41 Z = 5276526
43
XDOT = -21661
812506 XDOT = -6602
520452
YDOT = 10395
282802 feet/sec YDOT = 3168
482198 meter/sec
ZDOT = 2462
173084 ZDOT = 750
470356
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
79816550
00016717 00000-0 10270-3 0 9177
2 25544 51
6430 247
0774 0006790 54
0948 306
0832 15
50058760 30084
Satellite: ISS
Catalog Number: 25544
Epoch time: 19263
79816550 = yrday
fracday
Element set: 917
Inclination: 51
6430 deg
RA of node: 247
0774 deg
Eccentricity:
0006790
Arg of perigee: 54
0948 deg
Mean anomaly: 306
0832 deg
Mean motion: 15
50058760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3008
Checksum: 315
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