[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 4th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
066/23:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 224
6
000/00:00:00
000 0
0 0
0 215
4
067/07:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
4
073/19:14:11
000 0
0 0
0 0
0
N/A 0
0 0
0 224
4
000/00:00:00
000 0
0 0
0 215
4
074/01:07:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
3
000/00:00:00
000 0
0 0
0 215
5
Coasting Arc #1 (Orbit 3898)
---------------------------------------
Vector Time (GMT): 2019/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926995
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4606390
67 A = 6784733
86 meter
Y = -2131303
14 meter E =
0012263
Z = 4493581
06 I = 51
75563
XDOT = 5264
120600 Wp = 103
14820
YDOT = -4552
758920 meter/sec RA = 160
57825 deg
ZDOT = 3226
775549 TA = 314
41923
MA = 314
51954
Ha = 224
480 n
mi
Hp = 215
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15112830
28 X = -4604042
29
Y = -6992464
37 feet Y = -2182801
49 meter
Z = 14742720
02 Z = 4471211
36
XDOT = 17270
736877 XDOT = 5298
966083
YDOT = -14936
873097 feet/sec YDOT = -4493
696722 meter/sec
ZDOT = 10586
533953 ZDOT = 3252
431113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12121769
27 X = -3694715
27
Y = -11546523
43 feet Y = -3519380
34 meter
Z = 14641738
19 Z = 4462801
80
XDOT = 20271
714568 XDOT = 6178
818600
YDOT = -7667
301461 feet/sec YDOT = -2336
993485 meter/sec
ZDOT = 10702
862775 ZDOT = 3262
232574
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 19063
55416178
00016717 00000-0 10270-3 0 9003
2 25544 51
6409 161
4585 0003513 80
5950 279
5599 15
52804535 38999
Satellite: ISS
Catalog Number: 25544
Epoch time: 19063
55416178 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 161
4585 deg
Eccentricity:
0003513
Arg of perigee: 80
5950 deg
Mean anomaly: 279
5599 deg
Mean motion: 15
52804535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3899
Checksum: 336
Coasting Arc #2 (Orbit 3913)
---------------------------------------
Vector Time (GMT): 2019/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926995
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3622717
46 A = 6782624
17 meter
Y = 2730118
57 meter E =
0016282
Z = -5057220
73 I = 51
77926
XDOT = -5978
732658 Wp = 77
28749
YDOT = 4374
258946 meter/sec RA = 155
60608 deg
ZDOT = -1923
146268 TA = 174
06922
MA = 174
04992
Ha = 224
407 n
mi
Hp = 215
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11885555
96 X = 3616483
89
Y = 8957081
91 feet Y = 2770594
94 meter
Z = -16591931
53 Z = -5039638
74
XDOT = -19615
264627 XDOT = -6017
861139
YDOT = 14351
243261 feet/sec YDOT = 4307
181596 meter/sec
ZDOT = -6309
534999 ZDOT = -1952
283562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8655007
70 X = 2638046
35
Y = 12215228
52 feet Y = 3723201
65 meter
Z = -16512631
00 Z = -5033049
93
XDOT = -22150
211779 XDOT = -6751
384550
YDOT = 6994
276344 feet/sec YDOT = 2131
855430 meter/sec
ZDOT = -6441
606934 ZDOT = -1963
401794
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 19064
51953612
00016717 00000-0 10270-3 0 9010
2 25544 51
6410 156
6566 0003443 82
2963 277
8580 15
52759508 39149
Satellite: ISS
Catalog Number: 25544
Epoch time: 19064
51953612 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 156
6566 deg
Eccentricity:
0003443
Arg of perigee: 82
2963 deg
Mean anomaly: 277
8580 deg
Mean motion: 15
52759508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3914
Checksum: 323
Coasting Arc #3 (Orbit 3929)
---------------------------------------
Vector Time (GMT): 2019/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926995
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2561337
58 A = 6781284
44 meter
Y = -3348887
09 meter E =
0006183
Z = 5306109
46 I = 51
80573
XDOT = 6458
109092 Wp = 97
41885
YDOT = -4107
174488 meter/sec RA = 150
63216 deg
ZDOT = 523
929678 TA = 347
58825
MA = 347
60347
Ha = 224
457 n
mi
Hp = 215
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8403338
50 X = -2549472
65
Y = -10987162
38 feet Y = -3377462
80 meter
Z = 17408495
62 Z = 5293696
90
XDOT = 21188
021957 XDOT = 6501
011793
YDOT = -13474
981916 feet/sec YDOT = -4034
715451 meter/sec
ZDOT = 1718
929389 ZDOT = 555
404825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4946344
69 X = -1507645
86
Y = -12992695
58 feet Y = -3960173
61 meter
Z = 17352610
48 Z = 5289075
67
XDOT = 23237
316636 XDOT = 7082
734111
YDOT = -6354
523122 feet/sec YDOT = -1936
858648 meter/sec
ZDOT = 1861
567849 ZDOT = 567
405880
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 19065
54926253
00016717 00000-0 10270-3 0 9026
2 25544 51
6415 151
5340 0003541 84
1225 276
0331 15
52812236 39300
Satellite: ISS
Catalog Number: 25544
Epoch time: 19065
54926253 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 151
5340 deg
Eccentricity:
0003541
Arg of perigee: 84
1225 deg
Mean anomaly: 276
0331 deg
Mean motion: 15
52812236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3930
Checksum: 280
Coasting Arc #4 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2019/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926995
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1492166
45 A = 6781538
38 meter
Y = 4006434
63 meter E =
0018026
Z = -5279847
16 I = 51
83331
XDOT = -6650
076811 Wp = 95
02026
YDOT = 3675
950746 meter/sec RA = 145
65976 deg
ZDOT = 911
099330 TA = 183
68266
MA = 183
69595
Ha = 224
435 n
mi
Hp = 215
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4895559
23 X = 1472900
63
Y = 13144470
56 feet Y = 4023012
69 meter
Z = -17322333
19 Z = -5272646
18
XDOT = -21817
837306 XDOT = -6695
113635
YDOT = 12060
205858 feet/sec YDOT = 3601
333234 meter/sec
ZDOT = 2989
171031 ZDOT = 878
686417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1202753
04 X = 366599
13
Y = 14014774
94 feet Y = 4271703
40 meter
Z = -17290063
68 Z = -5270011
41
XDOT = -23290
419653 XDOT = -7098
919910
YDOT = 5500
724122 feet/sec YDOT = 1676
620713 meter/sec
ZDOT = 2842
308680 ZDOT = 866
335686
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 19066
51463080
00016717 00000-0 10270-3 0 9039
2 25544 51
6401 146
7323 0003601 86
3151 273
8413 15
52779884 39454
Satellite: ISS
Catalog Number: 25544
Epoch time: 19066
51463080 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 146
7323 deg
Eccentricity:
0003601
Arg of perigee: 86
3151 deg
Mean anomaly: 273
8413 deg
Mean motion: 15
52779884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3945
Checksum: 307
Coasting Arc #5 (Orbit 3952)
---------------------------------------
Vector Time (GMT): 2019/066/23:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 926995
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4263012
90 A = 6782769
94 meter
Y = -1707167
38 meter E =
0009549
Z = 4985021
47 I = 51
85076
XDOT = 4755
046284 Wp = 108
74311
YDOT = -5630
072475 meter/sec RA = 143
31838 deg
ZDOT = 2131
948435 TA = 320
52779
MA = 320
59731
Ha = 224
604 n
mi
Hp = 215
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13986262
78 X = -4267820
17
Y = -5600942
84 feet Y = -1754865
61 meter
Z = 16355057
33 Z = 4964302
19
XDOT = 15600
545552 XDOT = 4807
294266
YDOT = -18471
366388 feet/sec YDOT = -5576
605814 meter/sec
ZDOT = 6994
581479 ZDOT = 2155
173960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10670743
27 X = 3252442
55
Y = 10778386
54 feet Y = 3285252
22 meter
Z = 16261476
85 Z = 4956498
14
XDOT = -20865
198792 XDOT = -6359
712592
YDOT = 9913
402860 feet/sec YDOT = 3021
605192 meter/sec
ZDOT = 7100
044569 ZDOT = 2164
093585
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 19067
02949330
00016717 00000-0 10270-3 0 9044
2 25544 51
6403 144
1730 0003767 84
2091 275
9491 15
52799723 39535
Satellite: ISS
Catalog Number: 25544
Epoch time: 19067
02949330 = yrday
fracday
Element set: 904
Inclination: 51
6403 deg
RA of node: 144
1730 deg
Eccentricity:
0003767
Arg of perigee: 84
2091 deg
Mean anomaly: 275
9491 deg
Mean motion: 15
52799723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3953
Checksum: 323
Coasting Arc #6 (Orbit 3957)
---------------------------------------
Vector Time (GMT): 2019/067/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5923756
01 A = 6790774
77 meter
Y = 2253383
34 meter E =
0017355
Z = 2417718
65 I = 51
88373
XDOT = 125
557167 Wp = 78
03232
YDOT = -5468
999668 meter/sec RA = 141
75852 deg
ZDOT = 5375
868065 TA = 308
90538
MA = 309
06001
Ha = 224
500 n
mi
Hp = 215
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19434895
03 X = -5960257
50
Y = 7392989
97 feet Y = 2186935
98 meter
Z = 7932147
80 Z = 2388854
69
XDOT = 411
932964 XDOT = 160
591081
YDOT = -17942
912296 feet/sec YDOT = -5467
399026 meter/sec
ZDOT = 17637
362418 ZDOT = 5376
563756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7330298
45 X = -2234274
97
Y = -19511401
91 feet Y = -5947075
30 meter
Z = 7801431
59 Z = 2377876
35
XDOT = 16517
896728 XDOT = 5034
654923
YDOT = 886
598867 feet/sec YDOT = 270
235335 meter/sec
ZDOT = 17640
918732 ZDOT = 5376
952029
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 19067
35128071
00016717 00000-0 10270-3 0 9052
2 25544 51
6381 142
5671 0003739 93
0259 267
1321 15
52810237 39583
Satellite: ISS
Catalog Number: 25544
Epoch time: 19067
35128071 = yrday
fracday
Element set: 905
Inclination: 51
6381 deg
RA of node: 142
5671 deg
Eccentricity:
0003739
Arg of perigee: 93
0259 deg
Mean anomaly: 267
1321 deg
Mean motion: 15
52810237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 309
Coasting Arc #7 (Orbit 3972)
---------------------------------------
Vector Time (GMT): 2019/068/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5620698
16 A = 6788132
17 meter
Y = -1513259
67 meter E =
0008754
Z = -3499759
99 I = 51
90064
XDOT = -1206
888611 Wp = 90
94616
YDOT = 6035
216860 meter/sec RA = 136
80463 deg
ZDOT = -4557
835630 TA = 129
95749
MA = 129
88056
Ha = 224
514 n
mi
Hp = 215
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18440610
76 X = 5654201
87
Y = -4964762
71 feet Y = -1450218
20 meter
Z = -11482152
20 Z = -3472375
42
XDOT = -3959
608304 XDOT = -1252
147168
YDOT = 19800
580250 feet/sec YDOT = 6021
466960 meter/sec
ZDOT = -14953
528971 ZDOT = -4563
808872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5223533
37 X = 1592132
97
Y = 18445906
20 feet Y = 5622312
21 meter
Z = -11358171
36 Z = -3461970
63
XDOT = -18506
435449 XDOT = -5640
761525
YDOT = -3963
586553 feet/sec YDOT = -1208
101181 meter/sec
ZDOT = -14981
007173 ZDOT = -4566
210986
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 19068
31664327
00016717 00000-0 10270-3 0 9069
2 25544 51
6385 137
7640 0003796 94
1087 266
0499 15
52797035 39734
Satellite: ISS
Catalog Number: 25544
Epoch time: 19068
31664327 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 137
7640 deg
Eccentricity:
0003796
Arg of perigee: 94
1087 deg
Mean anomaly: 266
0499 deg
Mean motion: 15
52797035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3973
Checksum: 347
Coasting Arc #8 (Orbit 3988)
---------------------------------------
Vector Time (GMT): 2019/069/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5164227
25 A = 6785265
77 meter
Y = 666562
75 meter E =
0013505
Z = 4341396
99 I = 51
91481
XDOT = 2120
394460 Wp = 105
31180
YDOT = -6485
434922 meter/sec RA = 131
84716 deg
ZDOT = 3505
488877 TA = 309
13657
MA = 309
25653
Ha = 224
561 n
mi
Hp = 215
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16943002
79 X = -5192385
12
Y = 2186885
67 feet Y = 608655
81 meter
Z = 14243428
44 Z = 4316242
77
XDOT = 6956
674738 XDOT = 2175
731202
YDOT = -21277
673628 feet/sec YDOT = -6461
413374 meter/sec
ZDOT = 11500
947759 ZDOT = 3515
924062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2717625
91 X = -828332
38
Y = -16961492
62 feet Y = -5169862
95 meter
Z = 14129591
07 Z = 4306699
36
XDOT = 20244
073801 XDOT = 6170
393695
YDOT = 6411
455389 feet/sec YDOT = 1954
211602 meter/sec
ZDOT = 11548
656957 ZDOT = 3520
030640
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 19069
34635882
00016717 00000-0 10270-3 0 9078
2 25544 51
6385 132
6411 0003770 98
4148 261
7431 15
52822084 39899
Satellite: ISS
Catalog Number: 25544
Epoch time: 19069
34635882 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 132
6411 deg
Eccentricity:
0003770
Arg of perigee: 98
4148 deg
Mean anomaly: 261
7431 deg
Mean motion: 15
52822084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 331
Coasting Arc #9 (Orbit 4003)
---------------------------------------
Vector Time (GMT): 2019/070/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4618531
88 A = 6782897
55 meter
Y = 332512
58 meter E =
0015702
Z = -4970687
27 I = 51
92779
XDOT = -2875
680546 Wp = 80
33519
YDOT = 6735
430766 meter/sec RA = 126
88609 deg
ZDOT = -2224
800270 TA = 168
01560
MA = 167
97820
Ha = 224
470 n
mi
Hp = 215
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15152663
64 X = 4638615
15
Y = 1090920
54 feet Y = 384272
02 meter
Z = -16308029
09 Z = -4948203
48
XDOT = -9434
647461 XDOT = -2939
977495
YDOT = 22097
869966 feet/sec YDOT = 6702
913162 meter/sec
ZDOT = -7299
213483 ZDOT = -2238
926063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -350735
62 X = -106904
22
Y = 15296293
22 feet Y = 4662310
17 meter
Z = -16206342
41 Z = -4939693
17
XDOT = -21409
872201 XDOT = -6525
729047
YDOT = -8280
722256 feet/sec YDOT = -2523
964144 meter/sec
ZDOT = -7363
655184 ZDOT = -2244
442100
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 19070
31171699
00016717 00000-0 10270-3 0 9089
2 25544 51
6382 127
8389 0003790 101
2680 258
8898 15
52799597 40047
Satellite: ISS
Catalog Number: 25544
Epoch time: 19070
31171699 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 127
8389 deg
Eccentricity:
0003790
Arg of perigee: 101
2680 deg
Mean anomaly: 258
8898 deg
Mean motion: 15
52799597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 350
Coasting Arc #10 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2019/071/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4008839
68 A = 6781354
96 meter
Y = -1389697
54 meter E =
0006942
Z = 5284838
27 I = 51
94319
XDOT = 3461
808533 Wp = 112
17721
YDOT = -6794
614970 meter/sec RA = 121
92115 deg
ZDOT = 835
836007 TA = 329
84906
MA = 329
88900
Ha = 224
501 n
mi
Hp = 215
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13152361
15 X = -4018672
52
Y = -4559375
13 feet Y = -1434581
72 meter
Z = 17338708
24 Z = 5265341
10
XDOT = 11357
639544 XDOT = 3533
470532
YDOT = -22292
043865 feet/sec YDOT = -6755
501849 meter/sec
ZDOT = 2742
244117 ZDOT = 852
826772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3679102
46 X = 1121390
43
Y = -13538236
92 feet Y = -4126454
61 meter
Z = 17250613
18 Z = 5257986
90
XDOT = 21999
666617 XDOT = 6705
498385
YDOT = 9585
821941 feet/sec YDOT = 2921
758528 meter/sec
ZDOT = 2819
672812 ZDOT = 859
436273
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 19071
34142766
00016717 00000-0 10270-3 0 9097
2 25544 51
6393 122
7150 0003668 104
6828 255
4731 15
52836005 40207
Satellite: ISS
Catalog Number: 25544
Epoch time: 19071
34142766 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 122
7150 deg
Eccentricity:
0003668
Arg of perigee: 104
6828 deg
Mean anomaly: 255
4731 deg
Mean motion: 15
52836005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 298
Coasting Arc #11 (Orbit 4034)
---------------------------------------
Vector Time (GMT): 2019/072/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3398917
27 A = 6781265
19 meter
Y = 2503935
20 meter E =
0018492
Z = -5322913
50 I = 51
95997
XDOT = -3878
527955 Wp = 97
21219
YDOT = 6568
429909 meter/sec RA = 116
95738 deg
ZDOT = 612
787978 TA = 178
62586
MA = 178
62077
Ha = 224
429 n
mi
Hp = 215
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11151303
39 X = 3396520
64
Y = 8215010
51 feet Y = 2541930
52 meter
Z = -17463626
97 Z = -5306408
86
XDOT = -12724
829248 XDOT = -3954
666315
YDOT = 21549
966892 feet/sec YDOT = 6524
631822 meter/sec
ZDOT = 2010
459244 ZDOT = 593
762231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7254155
72 X = -2211066
66
Y = 11908421
64 feet Y = 3629686
91 meter
Z = -17389161
88 Z = -5300216
54
XDOT = -21661
055621 XDOT = -6602
289753
YDOT = -10383
760532 feet/sec YDOT = -3164
970210 meter/sec
ZDOT = 1923
819538 ZDOT = 586
380195
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 19072
30678078
00016717 00000-0 10270-3 0 9106
2 25544 51
6398 117
9132 0003873 106
3322 253
8256 15
52827731 40350
Satellite: ISS
Catalog Number: 25544
Epoch time: 19072
30678078 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 117
9132 deg
Eccentricity:
0003873
Arg of perigee: 106
3322 deg
Mean anomaly: 253
8256 deg
Mean motion: 15
52827731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 310
Coasting Arc #12 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2019/073/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2791205
82 A = 6782535
78 meter
Y = -3586620
10 meter E =
0008835
Z = 5027870
02 I = 51
97798
XDOT = 4178
400314 Wp = 77
27811
YDOT = -6105
237358 meter/sec RA = 111
99456 deg
ZDOT = -2030
642706 TA = 32
38212
MA = 32
32793
Ha = 224
584 n
mi
Hp = 215
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9157499
40 X = -2775314
25
Y = -11767126
33 feet Y = -3617744
20 meter
Z = 16495636
55 Z = 5014350
24
XDOT = 13708
662447 XDOT = 4256
223946
YDOT = -20030
306294 feet/sec YDOT = -6058
076531 meter/sec
ZDOT = -6662
213601 ZDOT = -2010
156373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10782317
37 X = 3286450
33
Y = -10395721
06 feet Y = -3168615
78 meter
Z = 16434771
01 Z = 5009318
20
XDOT = 20545
276758 XDOT = 6262
200356
YDOT = 10898
845456 feet/sec YDOT = 3321
968095 meter/sec
ZDOT = -6568
982000 ZDOT = -2002
225714
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 19073
33648872
00016717 00000-0 10270-3 0 9110
2 25544 51
6396 112
7898 0003916 109
5151 250
6424 15
52802805 40518
Satellite: ISS
Catalog Number: 25544
Epoch time: 19073
33648872 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 112
7898 deg
Eccentricity:
0003916
Arg of perigee: 109
5151 deg
Mean anomaly: 250
6424 deg
Mean motion: 15
52802805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 312
Coasting Arc #13 (Orbit 4058)
---------------------------------------
Vector Time (GMT): 2019/073/19:14:11
000
Vector Time (MET): N/A
Weight (LBS) : 901547
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4224037
79 A = 6781341
59 meter
Y = -442136
27 meter E =
0006898
Z = 5281521
17 I = 51
97983
XDOT = 1881
911156 Wp = 112
97160
YDOT = -7384
191590 meter/sec RA = 109
49829 deg
ZDOT = 883
414485 TA = 328
60226
MA = 328
64342
Ha = 224
446 n
mi
Hp = 215
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13858391
69 X = -4244434
28
Y = -1450578
32 feet Y = -489486
21 meter
Z = 17327825
36 Z = 5260953
00
XDOT = 6174
249198 XDOT = 1960
052302
YDOT = -24226
350361 feet/sec YDOT = -7362
709788 meter/sec
ZDOT = 2898
341487 ZDOT = 892
746175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 944439
95 X = 287865
30
Y = 14017233
14 feet Y = 4272452
66 meter
Z = 17234788
58 Z = 5253163
56
XDOT = -23897
275371 XDOT = -7283
889533
YDOT = -2020
565783 feet/sec YDOT = -615
868451 meter/sec
ZDOT = 2941
219325 ZDOT = 896
483650
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 19073
85134029
00016717 00000-0 10270-3 0 9122
2 25544 51
6389 110
2328 0003553 105
4336 254
7208 15
52848082 40598
Satellite: ISS
Catalog Number: 25544
Epoch time: 19073
85134029 = yrday
fracday
Element set: 912
Inclination: 51
6389 deg
RA of node: 110
2328 deg
Eccentricity:
0003553
Arg of perigee: 105
4336 deg
Mean anomaly: 254
7208 deg
Mean motion: 15
52848082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4059
Checksum: 304
Coasting Arc #14 (Orbit 4062)
---------------------------------------
Vector Time (GMT): 2019/074/01:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 916818
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2908411
79 A = 6792649
14 meter
Y = 6029485
23 meter E =
0016111
Z = 1113881
90 I = 52
01851
XDOT = -3876
808145 Wp = 66
82906
YDOT = -2973
093593 meter/sec RA = 108
28642 deg
ZDOT = 5909
443303 TA = 305
19013
MA = 305
34090
Ha = 224
341 n
mi
Hp = 215
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9542033
44 X = -2981029
62
Y = 19781775
68 feet Y = 5996555
35 meter
Z = 3654468
16 Z = 1099577
39
XDOT = -12719
186827 XDOT = -3871
978614
YDOT = -9754
244072 feet/sec YDOT = -3016
419501 meter/sec
ZDOT = 19387
937345 ZDOT = 5890
623232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6638965
49 X = 2023556
68
Y = -20946740
94 feet Y = -6384566
64 meter
Z = 3589201
85 Z = 1093988
72
XDOT = 12583
880047 XDOT = 3835
566638
YDOT = 7331
125679 feet/sec YDOT = 2234
527107 meter/sec
ZDOT = 19303
033272 ZDOT = 5883
564541
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 19074
10876607
00016717 00000-0 10270-3 0 9137
2 25544 51
6375 108
9502 0003539 107
6011 252
5527 15
52814380 40638
Satellite: ISS
Catalog Number: 25544
Epoch time: 19074
10876607 = yrday
fracday
Element set: 913
Inclination: 51
6375 deg
RA of node: 108
9502 deg
Eccentricity:
0003539
Arg of perigee: 107
6011 deg
Mean anomaly: 252
5527 deg
Mean motion: 15
52814380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4063
Checksum: 299
Coasting Arc #15 (Orbit 4077)
---------------------------------------
Vector Time (GMT): 2019/075/01:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 916818
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3194990
68 A = 6790815
90 meter
Y = -5509711
24 meter E =
0009090
Z = -2353084
06 I = 52
02196
XDOT = 3346
298042 Wp = 125
15422
YDOT = 4249
852417 meter/sec RA = 103
34521 deg
ZDOT = -5427
244631 TA = 80
92791
MA = 80
82506
Ha = 224
339 n
mi
Hp = 215
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10482252
88 X = 3267794
21
Y = -18076480
46 feet Y = -5473575
66 meter
Z = -7720092
08 Z = -2337387
11
XDOT = 10978
668117 XDOT = 3324
888521
YDOT = 13943
085359 feet/sec YDOT = 4287
153110 meter/sec
ZDOT = -17805
920704 ZDOT = -5411
041949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7505439
99 X = -2287658
11
Y = 19529582
35 feet Y = 5952616
70 meter
Z = -7648553
87 Z = -2331279
22
XDOT = -11761
346110 XDOT = -3584
858294
YDOT = -11439
214647 feet/sec YDOT = -3486
672625 meter/sec
ZDOT = -17732
975698 ZDOT = -5405
010993
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 19075
07411319
00016717 00000-0 10270-3 0 9140
2 25544 51
6375 104
1467 0003548 109
0818 251
0719 15
52825077 40785
Satellite: ISS
Catalog Number: 25544
Epoch time: 19075
07411319 = yrday
fracday
Element set: 914
Inclination: 51
6375 deg
RA of node: 104
1467 deg
Eccentricity:
0003548
Arg of perigee: 109
0818 deg
Mean anomaly: 251
0719 deg
Mean motion: 15
52825077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4078
Checksum: 309
Coasting Arc #16 (Orbit 4093)
---------------------------------------
Vector Time (GMT): 2019/076/01:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 916818
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3397448
24 A = 6788210
04 meter
Y = 4777007
02 meter E =
0015734
Z = 3411087
45 I = 52
01936
XDOT = -2875
283775 Wp = 95
35182
YDOT = -5379
277931 meter/sec RA = 98
39982 deg
ZDOT = 4649
739139 TA = 304
29716
MA = 304
44601
Ha = 224
314 n
mi
Hp = 215
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11146483
73 X = -3467182
50
Y = 15672595
20 feet Y = 4738624
66 meter
Z = 11191231
81 Z = 3394414
54
XDOT = -9433
345718 XDOT = -2837
502976
YDOT = -17648
549641 feet/sec YDOT = -5411
219859 meter/sec
ZDOT = 15255
049670 ZDOT = 4635
864364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8270364
71 X = 2520807
16
Y = -17411735
18 feet Y = -5307096
88 meter
Z = 11115329
72 Z = 3387952
50
XDOT = 11238
095912 XDOT = 3425
371634
YDOT = 15078
489949 feet/sec YDOT = 4595
923736 meter/sec
ZDOT = 15192
745827 ZDOT = 4630
748928
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 19076
10381335
00016717 00000-0 10270-3 0 9150
2 25544 51
6369 99
0230 0003557 115
7985 244
3534 15
52842756 40948
Satellite: ISS
Catalog Number: 25544
Epoch time: 19076
10381335 = yrday
fracday
Element set: 915
Inclination: 51
6369 deg
RA of node: 99
0230 deg
Eccentricity:
0003557
Arg of perigee: 115
7985 deg
Mean anomaly: 244
3534 deg
Mean motion: 15
52842756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4094
Checksum: 322
Coasting Arc #17 (Orbit 4108)
---------------------------------------
Vector Time (GMT): 2019/077/01:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 916818
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3604232
96 A = 6785325
36 meter
Y = -3812619
99 meter E =
0011288
Z = -4313206
49 I = 52
01269
XDOT = 2417
248797 Wp = 84
06656
YDOT = 6323
955791 meter/sec RA = 93
44941 deg
ZDOT = -3576
975210 TA = 149
61610
MA = 149
55063
Ha = 224
368 n
mi
Hp = 215
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11824911
29 X = 3667549
68
Y = -12508595
76 feet Y = -3771961
24 meter
Z = -14150939
92 Z = -4295544
71
XDOT = 7930
606289 XDOT = 2363
727533
YDOT = 20747
886452 feet/sec YDOT = 6350
687627 meter/sec
ZDOT = -11735
482974 ZDOT = -3565
363805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9267985
13 X = -2824881
87
Y = 14583007
17 feet Y = 4444900
59 meter
Z = -14070641
38 Z = -4288731
49
XDOT = -10815
878831 XDOT = -3296
679868
YDOT = -18124
934846 feet/sec YDOT = -5524
480141 meter/sec
ZDOT = -11683
515481 ZDOT = -3561
135519
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 19077
06915817
00016717 00000-0 10270-3 0 9165
2 25544 51
6362 94
2198 0003804 116
9812 243
1729 15
52832876 41090
Satellite: ISS
Catalog Number: 25544
Epoch time: 19077
06915817 = yrday
fracday
Element set: 916
Inclination: 51
6362 deg
RA of node: 94
2198 deg
Eccentricity:
0003804
Arg of perigee: 116
9812 deg
Mean anomaly: 243
1729 deg
Mean motion: 15
52832876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4109
Checksum: 329
Coasting Arc #18 (Orbit 4124)
---------------------------------------
Vector Time (GMT): 2019/078/01:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 916818
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3781073
30 A = 6782962
30 meter
Y = 2711165
99 meter E =
0010328
Z = 4930098
78 I = 52
00547
XDOT = -2000
500985 Wp = 121
45149
YDOT = -7031
061815 meter/sec RA = 88
49321 deg
ZDOT = 2323
454155 TA = 305
89610
MA = 305
99193
Ha = 224
418 n
mi
Hp = 215
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12405096
14 X = -3835056
58
Y = 8894901
53 feet Y = 2668582
05 meter
Z = 16174864
75 Z = 4911600
67
XDOT = -6563
323440 XDOT = -1933
014833
YDOT = -23067
788106 feet/sec YDOT = -7053
055238 meter/sec
ZDOT = 7622
881087 ZDOT = 2313
901274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10357598
38 X = 3156995
99
Y = -11332949
58 feet Y = -3454283
03 meter
Z = 16090877
62 Z = 4904499
50
XDOT = 10499
957008 XDOT = 3200
386896
YDOT = 20400
343308 feet/sec YDOT = 6218
024640 meter/sec
ZDOT = 7580
304338 ZDOT = 2310
476762
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 19078
09885606
00016717 00000-0 10270-3 0 9172
2 25544 51
6362 89
0959 0003646 121
7164 238
4344 15
52810004 41252
Satellite: ISS
Catalog Number: 25544
Epoch time: 19078
09885606 = yrday
fracday
Element set: 917
Inclination: 51
6362 deg
RA of node: 89
0959 deg
Eccentricity:
0003646
Arg of perigee: 121
7164 deg
Mean anomaly: 238
4344 deg
Mean motion: 15
52810004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4125
Checksum: 318
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