ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19965 9774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
333/00:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 221
6
333/10:24:30
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 221
6
336/14:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 221
0
338/17:51:47
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 220
6
339/18:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 220
5
340/09:34:11
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 220
4
341/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 220
3
342/14:24:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 220
1
342/21:54:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 220
1
Coasting Arc #1 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2019/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3942168
65 A = 6794565
12 meter
Y = -3892077
16 meter E =
0007521
Z = 3925587
31 I = 51
25904
XDOT = 2105
923879 Wp = 63
25405
YDOT = 6182
171954 meter/sec RA = 280
71758 deg
ZDOT = 4011
931515 TA = 344
58512
MA = 344
60801
Ha = 227
273 n
mi
Hp = 222
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12933624
17 X = 3966329
20
Y = -12769282
04 feet Y = -3847858
23 meter
Z = 12879223
47 Z = 3944795
78
XDOT = 6909
199077 XDOT = 2017
148297
YDOT = 20282
716383 feet/sec YDOT = 6205
225229 meter/sec
ZDOT = 13162
504970 ZDOT = 4021
946360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5619882
30 X = 1712940
12
Y = 17218571
51 feet Y = 5248220
60 meter
Z = 12967085
76 Z = 3952367
74
XDOT = -19926
895077 XDOT = -6073
717619
YDOT = -3449
157571 feet/sec YDOT = -1051
303228 meter/sec
ZDOT = 13207
630115 ZDOT = 4025
685659
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19329
55589821
00016717 00000-0 10270-3 0 9004
2 25544 51
6410 281
2508 0006716 322
2570 37
8108 15
50066407 287
Satellite: ISS
Catalog Number: 25544
Epoch time: 19329
55589821 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 281
2508 deg
Eccentricity:
0006716
Arg of perigee: 322
2570 deg
Mean anomaly: 37
8108 deg
Mean motion: 15
50066407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 28
Checksum: 295
Coasting Arc #2 (Orbit 42)
---------------------------------------
Vector Time (GMT): 2019/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3743917
68 A = 6793816
49 meter
Y = 3859745
46 meter E =
0009103
Z = -4161174
16 I = 51
25224
XDOT = -2352
410628 Wp = 23
36575
YDOT = -6274
416472 meter/sec RA = 275
73575 deg
ZDOT = -3697
975850 TA = 208
32831
MA = 208
37784
Ha = 227
638 n
mi
Hp = 221
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12283194
49 X = -3766587
08
Y = 12663206
88 feet Y = 3817751
97 meter
Z = -13652146
21 Z = -4179415
84
XDOT = -7717
882639 XDOT = -2264
110309
YDOT = -20585
355878 feet/sec YDOT = -6300
228720 meter/sec
ZDOT = -12132
466700 ZDOT = -3709
189373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6104645
61 X = -1860695
98
Y = -16482761
19 feet Y = -5023945
61 meter
Z = -13735598
16 Z = -4186610
32
XDOT = 20656
723814 XDOT = 6296
169418
YDOT = 2516
675307 feet/sec YDOT = 767
082634 meter/sec
ZDOT = -12183
057275 ZDOT = -3713
395857
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19330
52297621
00016717 00000-0 10270-3 0 9018
2 25544 51
6419 276
4591 0006840 327
1971 32
8754 15
50055045 436
Satellite: ISS
Catalog Number: 25544
Epoch time: 19330
52297621 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 276
4591 deg
Eccentricity:
0006840
Arg of perigee: 327
1971 deg
Mean anomaly: 32
8754 deg
Mean motion: 15
50055045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 43
Checksum: 298
Coasting Arc #3 (Orbit 58)
---------------------------------------
Vector Time (GMT): 2019/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3557917
74 A = 6792973
99 meter
Y = -3785576
14 meter E =
0006137
Z = 4370237
02 I = 51
24768
XDOT = 2624
396986 Wp = 62
94832
YDOT = 6362
419211 meter/sec RA = 270
75426 deg
ZDOT = 3373
723454 TA = 352
68630
MA = 352
69525
Ha = 227
582 n
mi
Hp = 221
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11672958
46 X = 3578756
12
Y = -12419869
24 feet Y = -3745672
99 meter
Z = 14338047
96 Z = 4387570
57
XDOT = 8610
226332 XDOT = 2536
667514
YDOT = 20874
078776 feet/sec YDOT = 6391
276153 meter/sec
ZDOT = 11068
646504 ZDOT = 3386
259702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6423990
94 X = 1958032
44
Y = 15715055
23 feet Y = 4789948
83 meter
Z = 14417354
47 Z = 4394409
64
XDOT = -21384
184865 XDOT = -6517
899547
YDOT = -1467
949171 feet/sec YDOT = -447
430907 meter/sec
ZDOT = 11125
271437 ZDOT = 3390
982734
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19331
55452076
00016717 00000-0 10270-3 0 9020
2 25544 51
6421 271
3490 0006839 330
1554 29
9206 15
50076795 591
Satellite: ISS
Catalog Number: 25544
Epoch time: 19331
55452076 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 271
3490 deg
Eccentricity:
0006839
Arg of perigee: 330
1554 deg
Mean anomaly: 29
9206 deg
Mean motion: 15
50076795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 59
Checksum: 305
Coasting Arc #4 (Orbit 73)
---------------------------------------
Vector Time (GMT): 2019/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3402638
66 A = 6792305
23 meter
Y = 3712787
01 meter E =
0011726
Z = -4568401
01 I = 51
24560
XDOT = -2909
361521 Wp = 33
90348
YDOT = -6397
926285 meter/sec RA = 265
77200 deg
ZDOT = -3026
934594 TA = 205
58849
MA = 205
64657
Ha = 227
942 n
mi
Hp = 221
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11163512
66 X = -3421712
15
Y = 12181059
73 feet Y = 3674630
24 meter
Z = -14988192
28 Z = -4584975
85
XDOT = -9545
149348 XDOT = -2822
898432
YDOT = -20990
571800 feet/sec YDOT = -6429
976985 meter/sec
ZDOT = -9930
887777 ZDOT = -3040
858212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6682108
41 X = -2036706
64
Y = -15035705
35 feet Y = -4582882
99 meter
Z = -15064034
35 Z = -4591517
67
XDOT = 21934
384161 XDOT = 6685
600292
YDOT = 283
573287 feet/sec YDOT = 86
433138 meter/sec
ZDOT = -9993
849986 ZDOT = -3046
125476
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19332
52159477
00016717 00000-0 10270-3 0 9038
2 25544 51
6417 266
5582 0006919 335
4642 24
6179 15
50061431 748
Satellite: ISS
Catalog Number: 25544
Epoch time: 19332
52159477 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 266
5582 deg
Eccentricity:
0006919
Arg of perigee: 335
4642 deg
Mean anomaly: 24
6179 deg
Mean motion: 15
50061431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 74
Checksum: 310
Coasting Arc #5 (Orbit 81)
---------------------------------------
Vector Time (GMT): 2019/333/00:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4190530
88 A = 6789250
59 meter
Y = 770968
85 meter E =
0013539
Z = -5296378
56 I = 51
23846
XDOT = -1094
802907 Wp = 62
20761
YDOT = -7570
720418 meter/sec RA = 263
15530 deg
ZDOT = -230
076303 TA = 205
54929
MA = 205
61627
Ha = 227
755 n
mi
Hp = 221
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13748460
90 X = -4173113
45
Y = 2529425
35 feet Y = 724205
45 meter
Z = -17376570
08 Z = -5316692
44
XDOT = -3591
873054 XDOT = -1008
945943
YDOT = -24838
321580 feet/sec YDOT = -7582
483190 meter/sec
ZDOT = -754
843514 ZDOT = -235
186966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1273699
99 X = -388223
76
Y = 13804605
95 feet Y = 4207643
89 meter
Z = -17469227
24 Z = -5324620
46
XDOT = -23871
029667 XDOT = -7275
889843
YDOT = -3210
170081 feet/sec YDOT = -978
459841 meter/sec
ZDOT = -777
552420 ZDOT = -236
997978
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19333
03736567
00016717 00000-0 10270-3 0 9047
2 25544 51
6433 264
0008 0006494 334
1913 25
8912 15
50058777 823
Satellite: ISS
Catalog Number: 25544
Epoch time: 19333
03736567 = yrday
fracday
Element set: 904
Inclination: 51
6433 deg
RA of node: 264
0008 deg
Eccentricity:
0006494
Arg of perigee: 334
1913 deg
Mean anomaly: 25
8912 deg
Mean motion: 15
50058777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 82
Checksum: 304
Coasting Arc #6 (Orbit 88)
---------------------------------------
Vector Time (GMT): 2019/333/10:24:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2729972
98 A = 6793465
16 meter
Y = -4548489
87 meter E =
0007709
Z = 4235525
44 I = 51
25231
XDOT = 3789
964469 Wp = 63
44413
YDOT = 5615
843995 meter/sec RA = 261
12412 deg
ZDOT = 3586
316178 TA = 349
68794
MA = 349
70374
Ha = 227
823 n
mi
Hp = 221
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8956604
27 X = 2760058
58
Y = -14922867
02 feet Y = -4517793
71 meter
Z = 13896080
85 Z = 4248859
25
XDOT = 12434
266629 XDOT = 3709
464278
YDOT = 18424
685022 feet/sec YDOT = 5657
775483 meter/sec
ZDOT = 11766
129194 ZDOT = 3604
531805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3769732
82 X = 1149014
56
Y = 16941048
97 feet Y = 5163631
73 meter
Z = 13957211
66 Z = 4254158
11
XDOT = -20388
249788 XDOT = -6214
338535
YDOT = -5229
562876 feet/sec YDOT = -1593
970765 meter/sec
ZDOT = 11848
734750 ZDOT = 3611
494352
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19333
48866445
00016717 00000-0 10270-3 0 9056
2 25544 51
6410 261
7674 0006815 336
9411 23
1433 15
50083660 896
Satellite: ISS
Catalog Number: 25544
Epoch time: 19333
48866445 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 261
7674 deg
Eccentricity:
0006815
Arg of perigee: 336
9411 deg
Mean anomaly: 23
1433 deg
Mean motion: 15
50083660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 89
Checksum: 306
Coasting Arc #7 (Orbit 103)
---------------------------------------
Vector Time (GMT): 2019/334/10:24:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2579836
41 A = 6792763
92 meter
Y = 4448449
40 meter E =
0011827
Z = -4449442
73 I = 51
25650
XDOT = -4066
724521 Wp = 33
57010
YDOT = -5610
602498 meter/sec RA = 256
14191 deg
ZDOT = -3245
906520 TA = 203
45572
MA = 203
50971
Ha = 228
163 n
mi
Hp = 221
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8464030
23 X = -2607775
48
Y = 14594650
26 feet Y = 4419444
17 meter
Z = -14597909
23 Z = -4462042
01
XDOT = -13342
272052 XDOT = -3987
915977
YDOT = -18407
488512 feet/sec YDOT = -5655
638442 meter/sec
ZDOT = -10649
299606 ZDOT = -3265
470539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4187877
72 X = -1276465
13
Y = -16291572
75 feet Y = -4965671
37 meter
Z = -14655678
60 Z = -4467050
84
XDOT = 21161
522598 XDOT = 6450
032088
YDOT = 4236
291511 feet/sec YDOT = 1291
221653 meter/sec
ZDOT = -10738
074342 ZDOT = -3272
965059
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19334
45573389
00016717 00000-0 10270-3 0 9067
2 25544 51
6414 256
9759 0006965 341
7469 18
3431 15
50067174 1047
Satellite: ISS
Catalog Number: 25544
Epoch time: 19334
45573389 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 256
9759 deg
Eccentricity:
0006965
Arg of perigee: 341
7469 deg
Mean anomaly: 18
3431 deg
Mean motion: 15
50067174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 104
Checksum: 328
Coasting Arc #8 (Orbit 119)
---------------------------------------
Vector Time (GMT): 2019/335/10:24:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2455118
34 A = 6791949
48 meter
Y = -4311445
64 meter E =
0006433
Z = 4631963
06 I = 51
26294
XDOT = 4364
565485 Wp = 60
35254
YDOT = 5596
866019 meter/sec RA = 251
16069 deg
ZDOT = 2896
278229 TA =
67648
MA =
67561
Ha = 228
109 n
mi
Hp = 221
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8054850
18 X = 2480648
13
Y = -14145162
87 feet Y = -4283848
53 meter
Z = 15196729
21 Z = 4643950
69
XDOT = 14319
440568 XDOT = 4287
586759
YDOT = 18362
421321 feet/sec YDOT = 5645
242945 meter/sec
ZDOT = 9502
225161 ZDOT = 2917
293362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4439449
82 X = 1353144
31
Y = 15607176
07 feet Y = 4757067
26 meter
Z = 15251693
78 Z = 4648716
27
XDOT = -21937
402534 XDOT = -6686
520292
YDOT = -3138
685650 feet/sec YDOT = -956
671386 meter/sec
ZDOT = 9597
640118 ZDOT = 2925
360708
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19335
48726909
00016717 00000-0 10270-3 0 9070
2 25544 51
6412 251
8657 0006964 344
6956 15
3983 15
50093575 1209
Satellite: ISS
Catalog Number: 25544
Epoch time: 19335
48726909 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 251
8657 deg
Eccentricity:
0006964
Arg of perigee: 344
6956 deg
Mean anomaly: 15
3983 deg
Mean motion: 15
50093575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 120
Checksum: 333
Coasting Arc #9 (Orbit 134)
---------------------------------------
Vector Time (GMT): 2019/336/10:24:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2360797
30 A = 6791368
26 meter
Y = 4193315
67 meter E =
0014225
Z = -4804878
88 I = 51
27215
XDOT = -4653
462342 Wp = 42
59997
YDOT = -5522
360945 meter/sec RA = 246
17928 deg
ZDOT = -2527
218340 TA = 202
31912
MA = 202
38108
Ha = 228
432 n
mi
Hp = 220
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7745397
97 X = -2384173
24
Y = 13757597
34 feet Y = 4166785
31 meter
Z = -15764038
32 Z = -4816403
16
XDOT = -15267
264903 XDOT = -4579
087989
YDOT = -18117
982102 feet/sec YDOT = -5573
983162 meter/sec
ZDOT = -8291
398753 ZDOT = -2549
643036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4644264
73 X = -1415571
89
Y = -15034122
38 feet Y = -4582400
50 meter
Z = -15816875
42 Z = -4820983
63
XDOT = 22509
258549 XDOT = 6860
822006
YDOT = 1896
969990 feet/sec YDOT = 578
196453 meter/sec
ZDOT = -8393
269776 ZDOT = -2558
268628
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19336
45433472
00016717 00000-0 10270-3 0 9089
2 25544 51
6407 247
0746 0007060 349
7022 10
3983 15
50072664 1354
Satellite: ISS
Catalog Number: 25544
Epoch time: 19336
45433472 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 247
0746 deg
Eccentricity:
0007060
Arg of perigee: 349
7022 deg
Mean anomaly: 10
3983 deg
Mean motion: 15
50072664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 135
Checksum: 297
Coasting Arc #10 (Orbit 137)
---------------------------------------
Vector Time (GMT): 2019/336/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4728629
20 A = 6791516
08 meter
Y = 1226799
08 meter E =
0011853
Z = 4717988
01 I = 51
27720
XDOT = 876
243823 Wp = 27
16802
YDOT = 7110
385329 meter/sec RA = 245
29158 deg
ZDOT = -2714
033416 TA = 89
90565
MA = 89
76982
Ha = 228
276 n
mi
Hp = 220
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15513875
33 X = 4691641
92
Y = 4024931
38 feet Y = 1279470
72 meter
Z = 15478963
28 Z = 4740868
25
XDOT = 2874
815693 XDOT = 809
851594
YDOT = 23328
035857 feet/sec YDOT = 7119
813127 meter/sec
ZDOT = -8904
309108 ZDOT = -2709
937560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 863928
49 X = 263325
40
Y = 15902701
33 feet Y = 4847143
37 meter
Z = 15583209
64 Z = 4749762
30
XDOT = -20162
260270 XDOT = -6145
456930
YDOT = 9844
667848 feet/sec YDOT = 3000
654760 meter/sec
ZDOT = -8886
119274 ZDOT = -2708
489155
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19336
64774505
00016717 00000-0 10270-3 0 9096
2 25544 51
6424 246
1177 0007151 348
4769 11
6216 15
50110499 1381
Satellite: ISS
Catalog Number: 25544
Epoch time: 19336
64774505 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 246
1177 deg
Eccentricity:
0007151
Arg of perigee: 348
4769 deg
Mean anomaly: 11
6216 deg
Mean motion: 15
50110499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 138
Checksum: 311
Coasting Arc #11 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2019/337/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4894906
74 A = 6792253
38 meter
Y = -1216991
65 meter E =
0009127
Z = -4554478
97 I = 51
29422
XDOT = -1121
810206 Wp = 67
06410
YDOT = -6926
045482 meter/sec RA = 240
31117 deg
ZDOT = 3064
766614 TA = 233
75386
MA = 233
83824
Ha = 228
413 n
mi
Hp = 220
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16059405
33 X = -4858811
00
Y = -3992754
77 feet Y = -1271527
79 meter
Z = -14942516
31 Z = -4578169
09
XDOT = -3680
479680 XDOT = -1059
164749
YDOT = -22723
246331 feet/sec YDOT = -6938
240315 meter/sec
ZDOT = 10055
008576 ZDOT = 3059
468895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1344255
00 X = -409728
92
Y = -16395174
72 feet Y = -4997249
26 meter
Z = -15050468
70 Z = -4587382
86
XDOT = 19118
667482 XDOT = 5827
369848
YDOT = -10750
953133 feet/sec YDOT = -3276
890515 meter/sec
ZDOT = 10031
305887 ZDOT = 3057
542034
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19337
61480827
00016717 00000-0 10270-3 0 9107
2 25544 51
6423 241
3262 0007111 351
7919 8
3114 15
50079165 1533
Satellite: ISS
Catalog Number: 25544
Epoch time: 19337
61480827 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 241
3262 deg
Eccentricity:
0007111
Arg of perigee: 351
7919 deg
Mean anomaly: 8
3114 deg
Mean motion: 15
50079165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 153
Checksum: 284
Coasting Arc #12 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2019/338/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5076954
62 A = 6792938
49 meter
Y = 1229383
16 meter E =
0013282
Z = 4341462
81 I = 51
31499
XDOT = 1315
116585 Wp = 39
10245
YDOT = 6724
661221 meter/sec RA = 235
33199 deg
ZDOT = -3426
273242 TA = 85
92948
MA = 85
77767
Ha = 228
512 n
mi
Hp = 220
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16656675
26 X = 5041741
46
Y = 4033409
31 feet Y = 1285960
08 meter
Z = 14243644
38 Z = 4366039
42
XDOT = 4314
686960 XDOT = 1256
464732
YDOT = 22062
536814 feet/sec YDOT = 6739
040062 meter/sec
ZDOT = -11241
053945 ZDOT = -3420
026888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1791000
21 X = 545896
87
Y = 16949992
05 feet Y = 5166357
58 meter
Z = 14355650
96 Z = 4375602
41
XDOT = -18049
840171 XDOT = -5501
591284
YDOT = 11447
739687 feet/sec YDOT = 3489
271056 meter/sec
ZDOT = -11212
993640 ZDOT = -3417
720461
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19338
64633703
00016717 00000-0 10270-3 0 9115
2 25544 51
6428 236
2150 0007297 354
8608 5
2467 15
50117549 1694
Satellite: ISS
Catalog Number: 25544
Epoch time: 19338
64633703 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 236
2150 deg
Eccentricity:
0007297
Arg of perigee: 354
8608 deg
Mean anomaly: 5
2467 deg
Mean motion: 15
50117549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 169
Checksum: 313
Coasting Arc #13 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2019/338/17:51:47
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3451097
11 A = 6800811
89 meter
Y = 5819401
70 meter E =
0006636
Z = -688553
29 I = 51
34035
XDOT = -4440
003622 Wp = 98
74602
YDOT = 1937
566054 meter/sec RA = 234
66071 deg
ZDOT = -5928
301626 TA = 88
70390
MA = 88
62787
Ha = 228
606 n
mi
Hp = 220
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11322497
09 X = 3389111
00
Y = 19092525
28 feet Y = 5857647
77 meter
Z = -2259033
09 Z = -671939
25
XDOT = -14566
941016 XDOT = -4432
543519
YDOT = 6356
844008 feet/sec YDOT = 1887
956884 meter/sec
ZDOT = -19449
808484 ZDOT = -5949
851368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4240692
20 X = 1292562
98
Y = 21796214
90 feet Y = 6643486
30 meter
Z = -2183629
60 Z = -665570
30
XDOT = -14143
179163 XDOT = -4310
841009
YDOT = 810
353244 feet/sec YDOT = 246
995669 meter/sec
ZDOT = -19548
212162 ZDOT = -5958
295067
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19338
77527915
00016717 00000-0 10270-3 0 9127
2 25544 51
6393 235
5718 0007095 357
5190 2
5924 15
50120265 1719
Satellite: ISS
Catalog Number: 25544
Epoch time: 19338
77527915 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 235
5718 deg
Eccentricity:
0007095
Arg of perigee: 357
5190 deg
Mean anomaly: 2
5924 deg
Mean motion: 15
50120265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 171
Checksum: 310
Coasting Arc #14 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2019/339/17:51:47
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3676568
18 A = 6800714
37 meter
Y = -5613362
55 meter E =
0018293
Z = 1035800
39 I = 51
35926
XDOT = 4553
387111 Wp = 38
90607
YDOT = -1890
724233 meter/sec RA = 229
68785 deg
ZDOT = 5873
139294 TA = 332
35698
MA = 332
45412
Ha = 228
658 n
mi
Hp = 220
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12062231
56 X = -3618556
06
Y = -18416543
80 feet Y = -5654152
23 meter
Z = 3398295
24 Z = 1018081
44
XDOT = 14938
934092 XDOT = 4545
662653
YDOT = -6203
163495 feet/sec YDOT = -1839
848569 meter/sec
ZDOT = 19268
829704 ZDOT = 5895
239246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5539752
42 X = -1688516
54
Y = -21319430
84 feet Y = -6498162
52 meter
Z = 3317821
29 Z = 1011271
93
XDOT = 14460
562144 XDOT = 4407
579341
YDOT = -720
830940 feet/sec YDOT = -219
709271 meter/sec
ZDOT = 19369
744532 ZDOT = 5903
898133
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 19339
80680907
00016717 00000-0 10270-3 0 9134
2 25544 51
6388 230
4607 0006732 1
9281 358
1894 15
50074785 1870
Satellite: ISS
Catalog Number: 25544
Epoch time: 19339
80680907 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 230
4607 deg
Eccentricity:
0006732
Arg of perigee: 1
9281 deg
Mean anomaly: 358
1894 deg
Mean motion: 15
50074785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 187
Checksum: 328
Coasting Arc #15 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2019/339/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -312111
28 A = 6792749
33 meter
Y = 5127267
80 meter E =
0013380
Z = -4458090
18 I = 51
33474
XDOT = -6145
815128 Wp = 42
22149
YDOT = -3198
617570 meter/sec RA = 229
50088 deg
ZDOT = -3244
463478 TA = 194
86104
MA = 194
90040
Ha = 228
686 n
mi
Hp = 220
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1023987
13 X = -347767
59
Y = 16821744
74 feet Y = 5123578
44 meter
Z = -14626280
13 Z = -4459692
62
XDOT = -20163
435458 XDOT = -6093
830558
YDOT = -10494
152132 feet/sec YDOT = -3267
053568 meter/sec
ZDOT = -10644
565218 ZDOT = -3274
191705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2129242
39 X = -648993
08
Y = 16711162
38 feet Y = 5093562
29 meter
Z = -14633902
24 Z = -4460413
40
XDOT = -18067
910948 XDOT = -5507
099257
YDOT = -11753
601192 feet/sec YDOT = -3582
497643 meter/sec
ZDOT = -10779
962589 ZDOT = -3285
732597
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 19339
80680929
00016717 00000-0 10270-3 0 9149
2 25544 51
6399 230
4612 0006722 2
3585 357
7596 15
50081936 1879
Satellite: ISS
Catalog Number: 25544
Epoch time: 19339
80680929 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 230
4612 deg
Eccentricity:
0006722
Arg of perigee: 2
3585 deg
Mean anomaly: 357
7596 deg
Mean motion: 15
50081936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 187
Checksum: 332
Coasting Arc #16 (Orbit 196)
---------------------------------------
Vector Time (GMT): 2019/340/09:34:11
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 883502
14 A = 6791161
28 meter
Y = -4681186
21 meter E =
0007415
Z = 4832966
87 I = 51
34446
XDOT = 6241
588992 Wp = 61
96691
YDOT = 3713
462480 meter/sec RA = 226
44657 deg
ZDOT = 2456
362079 TA = 3
81409
MA = 3
80844
Ha = 228
712 n
mi
Hp = 220
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2898629
08 X = 912306
77
Y = -15358222
47 feet Y = -4671145
48 meter
Z = 15856190
53 Z = 4837328
33
XDOT = 20477
654173 XDOT = 6187
668324
YDOT = 12183
275853 feet/sec YDOT = 3782
958710 meter/sec
ZDOT = 8058
930707 ZDOT = 2486
550926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7143495
55 X = 2177337
44
Y = 13878303
62 feet Y = 4230106
94 meter
Z = 15876365
65 Z = 4839116
25
XDOT = -22605
592906 XDOT = -6890
184718
YDOT = 2261
181951 feet/sec YDOT = 689
208259 meter/sec
ZDOT = 8196
409006 ZDOT = 2498
265465
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 19340
45151328
00016717 00000-0 10270-3 0 9159
2 25544 51
6411 227
2712 0007079 2
8581 357
2608 15
50100334 1970
Satellite: ISS
Catalog Number: 25544
Epoch time: 19340
45151328 = yrday
fracday
Element set: 915
Inclination: 51
6411 deg
RA of node: 227
2712 deg
Eccentricity:
0007079
Arg of perigee: 2
8581 deg
Mean anomaly: 357
2608 deg
Mean motion: 15
50100334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 197
Checksum: 283
Coasting Arc #17 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2019/341/09:34:11
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -869499
17 A = 6790624
99 meter
Y = 4546616
43 meter E =
0016670
Z = -4983046
02 I = 51
36736
XDOT = -6472
336443 Wp = 51
23254
YDOT = -3512
479720 meter/sec RA = 221
47084 deg
ZDOT = -2069
956497 TA = 198
46924
MA = 198
52983
Ha = 228
945 n
mi
Hp = 220
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2852687
55 X = -896070
95
Y = 14916720
58 feet Y = 4536744
82 meter
Z = -16348576
19 Z = -4987334
03
XDOT = -21234
699617 XDOT = -6422
523005
YDOT = -11523
883597 feet/sec YDOT = -3584
579306 meter/sec
ZDOT = -6791
195856 ZDOT = -2101
276319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7144709
64 X = -2177707
50
Y = -13377249
65 feet Y = -4077385
69 meter
Z = -16368403
67 Z = -4989089
44
XDOT = 22779
007023 XDOT = 6943
041341
YDOT = -3659
714025 feet/sec YDOT = -1115
480835 meter/sec
ZDOT = -6933
863535 ZDOT = -2113
441606
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 19341
41857082
00016717 00000-0 10270-3 0 9167
2 25544 51
6420 222
4798 0007215 7
0775 353
0476 15
50091527 2123
Satellite: ISS
Catalog Number: 25544
Epoch time: 19341
41857082 = yrday
fracday
Element set: 916
Inclination: 51
6420 deg
RA of node: 222
4798 deg
Eccentricity:
0007215
Arg of perigee: 7
0775 deg
Mean anomaly: 353
0476 deg
Mean motion: 15
50091527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 212
Checksum: 294
Coasting Arc #18 (Orbit 212)
---------------------------------------
Vector Time (GMT): 2019/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938320
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1882078
40 A = 6795727
22 meter
Y = 5460332
56 meter E =
0009751
Z = -3593645
48 I = 51
38684
XDOT = -6209
961663 Wp = 38
04713
YDOT = -759
117347 meter/sec RA = 221
18410 deg
ZDOT = -4404
632648 TA = 184
49319
MA = 184
50195
Ha = 228
917 n
mi
Hp = 220
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6174797
89 X = 1838335
65
Y = 17914476
89 feet Y = 5481134
94 meter
Z = -11790175
46 Z = -3584608
83
XDOT = -20373
889969 XDOT = -6179
615916
YDOT = -2490
542477 feet/sec YDOT = -828
391574 meter/sec
ZDOT = -14450
894516 ZDOT = -4434
725053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18643180
17 X = -5682441
31
Y = -3528638
86 feet Y = -1075529
12 meter
Z = -11749271
89 Z = -3581178
07
XDOT = 12027
873417 XDOT = 3666
095817
YDOT = -14961
895158 feet/sec YDOT = -4560
385644 meter/sec
ZDOT = -14588
125244 ZDOT = -4446
460574
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 19341
48304066
00016717 00000-0 10270-3 0 9174
2 25544 51
6431 222
1613 0007153 5
9259 354
1975 15
50078915 2136
Satellite: ISS
Catalog Number: 25544
Epoch time: 19341
48304066 = yrday
fracday
Element set: 917
Inclination: 51
6431 deg
RA of node: 222
1613 deg
Eccentricity:
0007153
Arg of perigee: 5
9259 deg
Mean anomaly: 354
1975 deg
Mean motion: 15
50078915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 213
Checksum: 294
Coasting Arc #19 (Orbit 228)
---------------------------------------
Vector Time (GMT): 2019/342/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938320
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1955184
04 A = 6794938
70 meter
Y = -5236950
83 meter E =
0013789
Z = 3847473
28 I = 51
41035
XDOT = 6434
579070 Wp = 66
30802
YDOT = 632
383614 meter/sec RA = 216
21237 deg
ZDOT = 4124
332492 TA = 340
19042
MA = 340
24392
Ha = 229
103 n
mi
Hp = 220
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6414645
79 X = -1915166
79
Y = -17181597
21 feet Y = -5258591
63 meter
Z = 12622943
82 Z = 3838072
36
XDOT = 21110
823721 XDOT = 6406
995316
YDOT = 2074
749390 feet/sec YDOT = 704
185071 meter/sec
ZDOT = 13531
274581 ZDOT = 4155
522802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18178872
13 X = 5540920
22
Y = 2637599
97 feet Y = 803940
47 meter
Z = 12580355
67 Z = 3834492
41
XDOT = -11806
524294 XDOT = -3598
628605
YDOT = 16056
221726 feet/sec YDOT = 4893
936382 meter/sec
ZDOT = 13673
537068 ZDOT = 4167
694098
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 19342
51456541
00016717 00000-0 10270-3 0 9186
2 25544 51
6434 217
0500 0007286 10
7364 349
3941 15
50069391 2299
Satellite: ISS
Catalog Number: 25544
Epoch time: 19342
51456541 = yrday
fracday
Element set: 918
Inclination: 51
6434 deg
RA of node: 217
0500 deg
Eccentricity:
0007286
Arg of perigee: 10
7364 deg
Mean anomaly: 349
3941 deg
Mean motion: 15
50069391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 229
Checksum: 299
Coasting Arc #20 (Orbit 230)
---------------------------------------
Vector Time (GMT): 2019/342/14:24:30
000
Vector Time (MET): N/A
Weight (LBS) : 952754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4873717
30 A = 6791968
08 meter
Y = -1047419
64 meter E =
0013678
Z = 4610760
04 I = 51
40248
XDOT = 4057
011339 Wp = 39
41980
YDOT = 5788
239966 meter/sec RA = 215
45725 deg
ZDOT = -2958
272603 TA = 80
26001
MA = 80
10556
Ha = 228
881 n
mi
Hp = 220
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15989886
17 X = 4862670
77
Y = -3436416
14 feet Y = -992980
43 meter
Z = 15127165
49 Z = 4634408
19
XDOT = 13310
404655 XDOT = 4006
353895
YDOT = 18990
288602 feet/sec YDOT = 5833
325329 meter/sec
ZDOT = -9705
618775 ZDOT = -2938
687423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9203990
20 X = 2805376
21
Y = 13397549
25 feet Y = 4083573
01 meter
Z = 15235116
99 Z = 4643663
66
XDOT = -11521
473498 XDOT = -3511
745122
YDOT = 18907
064191 feet/sec YDOT = 5762
873165 meter/sec
ZDOT = -9616
596640 ZDOT = -2931
138656
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 19342
64350299
00016717 00000-0 10270-3 0 9194
2 25544 51
6411 216
4093 0007212 9
1249 351
0031 15
50098624 2311
Satellite: ISS
Catalog Number: 25544
Epoch time: 19342
64350299 = yrday
fracday
Element set: 919
Inclination: 51
6411 deg
RA of node: 216
4093 deg
Eccentricity:
0007212
Arg of perigee: 9
1249 deg
Mean anomaly: 351
0031 deg
Mean motion: 15
50098624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 231
Checksum: 279
Coasting Arc #21 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2019/342/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 952754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -284735
47 A = 6791339
80 meter
Y = -4798544
67 meter E =
0008487
Z = 4789278
29 I = 51
41079
XDOT = 6891
209091 Wp = 69
13538
YDOT = 2161
734938 meter/sec RA = 213
94498 deg
ZDOT = 2574
882289 TA = 355
41676
MA = 355
42452
Ha = 228
868 n
mi
Hp = 220
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -934171
49 X = -254319
61
Y = -15743256
79 feet Y = -4801559
13 meter
Z = 15712855
29 Z = 4787968
59
XDOT = 22608
953710 XDOT = 6854
016221
YDOT = 7092
306226 feet/sec YDOT = 2238
589124 meter/sec
ZDOT = 8447
776540 ZDOT = 2608
267596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11884325
93 X = -3622342
54
Y = -10376161
72 feet Y = -3162654
09 meter
Z = 15707154
33 Z = 4787540
64
XDOT = 20186
821159 XDOT = 6152
943089
YDOT = -10098
887820 feet/sec YDOT = -3078
141008 meter/sec
ZDOT = 8599
974137 ZDOT = 2621
272117
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 19342
96585420
00016717 00000-0 10270-3 0 9207
2 25544 51
6430 214
8112 0006784 11
8053 348
3255 15
50110518 2361
Satellite: ISS
Catalog Number: 25544
Epoch time: 19342
96585420 = yrday
fracday
Element set: 920
Inclination: 51
6430 deg
RA of node: 214
8112 deg
Eccentricity:
0006784
Arg of perigee: 11
8053 deg
Mean anomaly: 348
3255 deg
Mean motion: 15
50110518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 236
Checksum: 282
Coasting Arc #22 (Orbit 250)
---------------------------------------
Vector Time (GMT): 2019/343/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 952754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 268198
15 A = 6790889
39 meter
Y = 4658649
11 meter E =
0016819
Z = -4948886
34 I = 51
43564
XDOT = -7072
656370 Wp = 53
93757
YDOT = -1922
153156 meter/sec RA = 208
97504 deg
ZDOT = -2188
260504 TA = 194
57610
MA = 194
62466
Ha = 229
059 n
mi
Hp = 219
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 879915
20 X = 240123
18
Y = 15284281
87 feet Y = 4661491
86 meter
Z = -16236503
74 Z = -4947651
19
XDOT = -23204
253182 XDOT = -7040
007108
YDOT = -6306
276758 feet/sec YDOT = -2001
061803 meter/sec
ZDOT = -7179
332362 ZDOT = -2222
538301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11695244
11 X = 3564710
40
Y = 9888336
86 feet Y = 3013965
07 meter
Z = -16231131
70 Z = -4947248
94
XDOT = -19883
294035 XDOT = -6060
428022
YDOT = 11451
557214 feet/sec YDOT = 3490
434639 meter/sec
ZDOT = -7335
637121 ZDOT = -2235
902194
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 19343
93290816
00016717 00000-0 10270-3 0 9218
2 25544 51
6415 210
0210 0006800 15
2656 344
8698 15
50061406 2517
Satellite: ISS
Catalog Number: 25544
Epoch time: 19343
93290816 = yrday
fracday
Element set: 921
Inclination: 51
6415 deg
RA of node: 210
0210 deg
Eccentricity:
0006800
Arg of perigee: 15
2656 deg
Mean anomaly: 344
8698 deg
Mean motion: 15
50061406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 251
Checksum: 279
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