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 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
329/11:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 222
2
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
335/11:30:08
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
1
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
337/13:40:13
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 220
8
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
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
Coasting Arc #1 (Orbit 3980)
---------------------------------------
Vector Time (GMT): 2019/326/11:23:54
315
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4413968
23 A = 6789998
56 meter
Y = 352483
30 meter E =
0002280
Z = 5148250
55 I = 51
27445
XDOT = -2217
614075 Wp = 324
67917
YDOT = 7196
259180 meter/sec RA = 295
76758 deg
ZDOT = 1410
759016 TA = 111
68034
MA = 111
65606
Ha = 226
931 n
mi
Hp = 222
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14481523
08 X = 4384690
86
Y = 1156441
27 feet Y = 401679
62 meter
Z = 16890585
80 Z = 5169621
20
XDOT = -7275
636728 XDOT = -2304
772717
YDOT = 23609
774213 feet/sec YDOT = 7170
972892 meter/sec
ZDOT = 4628
474461 ZDOT = 1399
774940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9896358
18 X = -3016409
97
Y = 10479287
47 feet Y = 3194086
82 meter
Z = 16987948
22 Z = 5177926
62
XDOT = -13073
634412 XDOT = -3984
843769
YDOT = -19756
100036 feet/sec YDOT = -6021
659291 meter/sec
ZDOT = 4577
783196 ZDOT = 1395
308318
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 19326
52570918
00016717 00000-0 10270-3 0 9005
2 25544 51
6396 296
2635 0006647 311
7905 48
2677 15
50014018 39814
Satellite: ISS
Catalog Number: 25544
Epoch time: 19326
52570918 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 296
2635 deg
Eccentricity:
0006647
Arg of perigee: 311
7905 deg
Mean anomaly: 48
2677 deg
Mean motion: 15
50014018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3981
Checksum: 323
Coasting Arc #2 (Orbit 3995)
---------------------------------------
Vector Time (GMT): 2019/327/11:23:54
315
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4331720
32 A = 6789678
48 meter
Y = -395422
00 meter E =
0011698
Z = -5222740
50 I = 51
26051
XDOT = 1909
042012 Wp = 54
69126
YDOT = -7341
181100 meter/sec RA = 290
78540 deg
ZDOT = -1022
532738 TA = 205
41790
MA = 205
47548
Ha = 227
174 n
mi
Hp = 222
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14211680
85 X = -4301606
96
Y = -1297316
26 feet Y = -443693
84 meter
Z = -17134975
38 Z = -5243709
67
XDOT = 6263
261194 XDOT = 1995
958350
YDOT = -24085
239828 feet/sec YDOT = -7319
346837 meter/sec
ZDOT = -3354
766201 ZDOT = -1013
048218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9659724
21 X = 2944283
94
Y = -10347066
69 feet Y = -3153785
93 meter
Z = -17230502
68 Z = -5251857
22
XDOT = 14434
581264 XDOT = 4399
660369
YDOT = 19016
421963 feet/sec YDOT = 5796
205414 meter/sec
ZDOT = -3310
910521 ZDOT = -1009
165527
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 19327
49279371
00016717 00000-0 10270-3 0 9012
2 25544 51
6402 291
4720 0006650 316
1950 43
8672 15
50022040 39963
Satellite: ISS
Catalog Number: 25544
Epoch time: 19327
49279371 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 291
4720 deg
Eccentricity:
0006650
Arg of perigee: 316
1950 deg
Mean anomaly: 43
8672 deg
Mean motion: 15
50022040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3996
Checksum: 299
Coasting Arc #3 (Orbit 4011)
---------------------------------------
Vector Time (GMT): 2019/328/11:23:54
315
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4259301
53 A = 6789455
28 meter
Y = 474280
03 meter E =
0004321
Z = 5267069
20 I = 51
24860
XDOT = -1595
023673 Wp = 336
63979
YDOT = 7467
480341 meter/sec RA = 285
80256 deg
ZDOT = 621
495587 TA = 107
41308
MA = 107
36583
Ha = 227
284 n
mi
Hp = 222
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13974086
40 X = 4228096
33
Y = 1556036
85 feet Y = 521735
84 meter
Z = 17280410
76 Z = 5287684
01
XDOT = -5233
017300 XDOT = -1681
427618
YDOT = 24499
607418 feet/sec YDOT = 7449
160517 meter/sec
ZDOT = 2039
027517 ZDOT = 613
537839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9544671
83 X = -2909215
97
Y = 10165692
88 feet Y = 3098503
19 meter
Z = 17374316
26 Z = 5295691
60
XDOT = -15738
804438 XDOT = -4797
187593
YDOT = -18176
476686 feet/sec YDOT = -5540
190094 meter/sec
ZDOT = 2002
130322 ZDOT = 610
249322
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 19328
52434982
00016717 00000-0 10270-3 0 9029
2 25544 51
6398 286
3614 0006765 320
0685 39
9967 15
50021681 40121
Satellite: ISS
Catalog Number: 25544
Epoch time: 19328
52434982 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 286
3614 deg
Eccentricity:
0006765
Arg of perigee: 320
0685 deg
Mean anomaly: 39
9967 deg
Mean motion: 15
50021681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4012
Checksum: 324
Coasting Arc #4 (Orbit 4026)
---------------------------------------
Vector Time (GMT): 2019/329/11:23:54
315
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4225605
51 A = 6789346
47 meter
Y = -540623
29 meter E =
0012242
Z = -5296055
64 I = 51
24052
XDOT = 1256
660225 Wp = 61
24638
YDOT = -7546
562690 meter/sec RA = 280
81877 deg
ZDOT = -226
925796 TA = 206
54323
MA = 206
60597
Ha = 227
465 n
mi
Hp = 222
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13863535
14 X = -4193520
11
Y = -1773698
45 feet Y = -587697
23 meter
Z = -17375510
61 Z = -5316504
66
XDOT = 4122
901000 XDOT = 1342
056994
YDOT = -24759
063944 feet/sec YDOT = -7532
032329 meter/sec
ZDOT = -744
507205 ZDOT = -220
614357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9479903
10 X = 2889474
46
Y = -10110857
47 feet Y = -3081789
36 meter
Z = -17468657
08 Z = -5324446
68
XDOT = 16929
818449 XDOT = 5160
208663
YDOT = 17139
181462 feet/sec YDOT = 5224
022510 meter/sec
ZDOT = -715
115405 ZDOT = -217
967175
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
49143210
00016717 00000-0 10270-3 0 9038
2 25544 51
6401 281
5700 0006782 323
2306 36
8379 15
50024988 40275
Satellite: ISS
Catalog Number: 25544
Epoch time: 19329
49143210 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 281
5700 deg
Eccentricity:
0006782
Arg of perigee: 323
2306 deg
Mean anomaly: 36
8379 deg
Mean motion: 15
50024988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4027
Checksum: 297
Coasting Arc #5 (Orbit 4026)
---------------------------------------
Vector Time (GMT): 2019/329/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3426209
01 A = 6790957
68 meter
Y = -3177933
87 meter E =
0008007
Z = -4933407
95 I = 51
24575
XDOT = 3053
878815 Wp = 75
19520
YDOT = -6673
067974 meter/sec RA = 280
77860 deg
ZDOT = 2182
664237 TA = 216
21977
MA = 216
27401
Ha = 227
458 n
mi
Hp = 222
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11240843
22 X = -3366453
44
Y = -10426292
21 feet Y = -3215913
70 meter
Z = -16185721
62 Z = -4949906
68
XDOT = 10019
287452 XDOT = 3117
669599
YDOT = -21893
267632 feet/sec YDOT = -6638
560817 meter/sec
ZDOT = 7160
971905 ZDOT = 2197
653688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14885006
44 X = 4536949
96
Y = -3327114
51 feet Y = -1014104
50 meter
Z = -16260645
81 Z = -4956244
84
XDOT = 12234
852819 XDOT = 3729
183139
YDOT = 19482
090770 feet/sec YDOT = 5938
141267 meter/sec
ZDOT = 7229
838768 ZDOT = 2203
654856
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
49143210
00016717 00000-0 10270-3 0 9049
2 25544 51
6400 281
5702 0006820 323
1028 36
9653 15
50015509 40274
Satellite: ISS
Catalog Number: 25544
Epoch time: 19329
49143210 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 281
5702 deg
Eccentricity:
0006820
Arg of perigee: 323
1028 deg
Mean anomaly: 36
9653 deg
Mean motion: 15
50015509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4027
Checksum: 277
Coasting Arc #6 (Orbit 4042)
---------------------------------------
Vector Time (GMT): 2019/330/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3525582
28 A = 6791487
78 meter
Y = 3290738
67 meter E =
0009671
Z = 4783332
99 I = 51
24401
XDOT = -2743
986810 Wp = 15
92842
YDOT = 6677
225158 meter/sec RA = 275
79548 deg
ZDOT = -2560
812734 TA = 99
51214
MA = 99
40283
Ha = 227
598 n
mi
Hp = 222
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11566871
01 X = 3465286
94
Y = 10796386
73 feet Y = 3329826
64 meter
Z = 15693349
70 Z = 4800313
21
XDOT = -9002
581397 XDOT = -2806
010249
YDOT = 21906
906685 feet/sec YDOT = 6646
193406 meter/sec
ZDOT = -8401
616583 ZDOT = -2574
292325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15315675
70 X = -4668217
95
Y = 3654882
75 feet Y = 1114008
26 meter
Z = 15770466
26 Z = 4806838
12
XDOT = -13136
789911 XDOT = -4004
093565
YDOT = -18383
549337 feet/sec YDOT = -5603
305838 meter/sec
ZDOT = -8463
596620 ZDOT = -2579
704250
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
52298401
00016717 00000-0 10270-3 0 9059
2 25544 51
6414 276
4596 0006874 326
7356 33
3362 15
50042505 40437
Satellite: ISS
Catalog Number: 25544
Epoch time: 19330
52298401 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 276
4596 deg
Eccentricity:
0006874
Arg of perigee: 326
7356 deg
Mean anomaly: 33
3362 deg
Mean motion: 15
50042505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4043
Checksum: 300
Coasting Arc #7 (Orbit 4057)
---------------------------------------
Vector Time (GMT): 2019/331/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3667649
66 A = 6792146
30 meter
Y = -3362391
00 meter E =
0006896
Z = -4627752
07 I = 51
24394
XDOT = 2431
846477 Wp = 68
31673
YDOT = -6651
580247 meter/sec RA = 270
81264 deg
ZDOT = 2911
539653 TA = 230
83478
MA = 230
89607
Ha = 227
748 n
mi
Hp = 221
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12032971
31 X = -3607298
34
Y = -11031466
55 feet Y = -3403067
27 meter
Z = -15182913
61 Z = -4645422
30
XDOT = 7978
498940 XDOT = 2491
902721
YDOT = -21822
769839 feet/sec YDOT = -6624
050164 meter/sec
ZDOT = 9552
295450 ZDOT = 2923
497986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15700112
71 X = 4785394
35
Y = -4189073
92 feet Y = -1276829
73 meter
Z = -15263179
19 Z = -4652217
02
XDOT = 13911
459656 XDOT = 4240
212903
YDOT = 17204
899901 feet/sec YDOT = 5244
053490 meter/sec
ZDOT = 9607
333785 ZDOT = 2928
315338
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
49006124
00016717 00000-0 10270-3 0 9066
2 25544 51
6415 271
6685 0006946 330
7828 29
2934 15
50028882 40580
Satellite: ISS
Catalog Number: 25544
Epoch time: 19331
49006124 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 271
6685 deg
Eccentricity:
0006946
Arg of perigee: 330
7828 deg
Mean anomaly: 29
2934 deg
Mean motion: 15
50028882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4058
Checksum: 320
Coasting Arc #8 (Orbit 4073)
---------------------------------------
Vector Time (GMT): 2019/332/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3818237
06 A = 6792835
33 meter
Y = 3454101
67 meter E =
0011068
Z = 4431451
67 I = 51
24698
XDOT = -2149
907887 Wp = 30
41317
YDOT = 6585
753268 meter/sec RA = 265
83060 deg
ZDOT = -3267
886289 TA = 92
81569
MA = 92
68901
Ha = 227
910 n
mi
Hp = 221
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12527024
49 X = 3757802
66
Y = 11332354
56 feet Y = 3496461
41 meter
Z = 14538883
44 Z = 4449853
18
XDOT = -7053
503567 XDOT = -2207
518098
YDOT = 21606
802059 feet/sec YDOT = 6561
389780 meter/sec
ZDOT = -10721
411709 ZDOT = -3278
468976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16141781
49 X = -4920015
00
Y = 4727946
47 feet Y = 1441078
09 meter
Z = 14622487
69 Z = 4456934
25
XDOT = -14485
968277 XDOT = -4415
323131
YDOT = -16016
155814 feet/sec YDOT = -4881
724292 meter/sec
ZDOT = -10770
166868 ZDOT = -3282
746861
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
52160860
00016717 00000-0 10270-3 0 9070
2 25544 51
6414 266
5585 0006972 334
8757 25
2053 15
50049792 40745
Satellite: ISS
Catalog Number: 25544
Epoch time: 19332
52160860 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 266
5585 deg
Eccentricity:
0006972
Arg of perigee: 334
8757 deg
Mean anomaly: 25
2053 deg
Mean motion: 15
50049792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4074
Checksum: 319
Coasting Arc #9 (Orbit 4088)
---------------------------------------
Vector Time (GMT): 2019/333/10:24:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2724502
94 A = 6793498
23 meter
Y = -4556615
79 meter E =
0007751
Z = 4230314
85 I = 51
25241
XDOT = 3794
965412 Wp = 63
20661
YDOT = 5607
454872 meter/sec RA = 261
12472 deg
ZDOT = 3594
178825 TA = 349
83143
MA = 349
84710
Ha = 227
843 n
mi
Hp = 221
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8938657
95 X = 2754705
13
Y = -14949526
86 feet Y = -4525980
15 meter
Z = 13878985
72 Z = 4243622
36
XDOT = 12450
673925 XDOT = 3714
520467
YDOT = 18397
161653 feet/sec YDOT = 5649
442592 meter/sec
ZDOT = 11791
925280 ZDOT = 3612
418878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3800987
83 X = 1158541
09
Y = 16948249
77 feet Y = 5165826
53 meter
Z = 13939997
31 Z = 4248911
18
XDOT = -20380
689477 XDOT = -6212
034153
YDOT = -5200
673924 feet/sec YDOT = -1585
165412 meter/sec
ZDOT = 11874
642823 ZDOT = 3619
391132
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
48868147
00016717 00000-0 10270-3 0 9080
2 25544 51
6410 261
7678 0006847 337
0390 23
0453 15
50078794 40890
Satellite: ISS
Catalog Number: 25544
Epoch time: 19333
48868147 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 261
7678 deg
Eccentricity:
0006847
Arg of perigee: 337
0390 deg
Mean anomaly: 23
0453 deg
Mean motion: 15
50078794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4089
Checksum: 334
Coasting Arc #10 (Orbit 4103)
---------------------------------------
Vector Time (GMT): 2019/334/10:24:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2572850
05 A = 6792799
01 meter
Y = 4458132
02 meter E =
0011830
Z = -4443843
36 I = 51
25660
XDOT = -4072
287417 Wp = 33
38131
YDOT = -5600
897140 meter/sec RA = 256
14257 deg
ZDOT = -3255
638949 TA = 203
53298
MA = 203
58715
Ha = 228
182 n
mi
Hp = 221
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8441109
08 X = -2600925
11
Y = 14626417
39 feet Y = 4429204
16 meter
Z = -14579538
59 Z = -4456409
03
XDOT = -13360
523023 XDOT = -3993
539713
YDOT = -18375
646785 feet/sec YDOT = -5645
995631 meter/sec
ZDOT = -10681
230148 ZDOT = -3275
230137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4226373
02 X = -1288198
50
Y = -16298429
52 feet Y = -4967761
32 meter
Z = -14637155
47 Z = -4461404
99
XDOT = 21151
731068 XDOT = 6447
047629
YDOT = 4203
705276 feet/sec YDOT = 1281
289368 meter/sec
ZDOT = -10770
129465 ZDOT = -3282
735461
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
45575389
00016717 00000-0 10270-3 0 9092
2 25544 51
6414 256
9763 0006997 341
8334 18
2565 15
50062447 41048
Satellite: ISS
Catalog Number: 25544
Epoch time: 19334
45575389 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 256
9763 deg
Eccentricity:
0006997
Arg of perigee: 341
8334 deg
Mean anomaly: 18
2565 deg
Mean motion: 15
50062447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4104
Checksum: 334
Coasting Arc #11 (Orbit 4119)
---------------------------------------
Vector Time (GMT): 2019/335/10:24:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2446490
19 A = 6791986
45 meter
Y = -4322517
70 meter E =
0006485
Z = 4626207
69 I = 51
26305
XDOT = 4370
709347 Wp = 60
22353
YDOT = 5586
000682 meter/sec RA = 251
16140 deg
ZDOT = 2908
016368 TA =
67698
MA =
67610
Ha = 228
129 n
mi
Hp = 221
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8026542
63 X = 2472172
40
Y = -14181488
52 feet Y = -4295016
22 meter
Z = 15177846
74 Z = 4638153
77
XDOT = 14339
597596 XDOT = 4293
794646
YDOT = 18326
773892 feet/sec YDOT = 5634
446670 meter/sec
ZDOT = 9540
736115 ZDOT = 2929
061500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4485084
65 X = 1367053
80
Y = 15612759
41 feet Y = 4758769
07 meter
Z = 15232622
70 Z = 4642903
40
XDOT = -21925
706365 XDOT = -6682
955300
YDOT = -3102
783438 feet/sec YDOT = -945
728392 meter/sec
ZDOT = 9636
288623 ZDOT = 2937
140772
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
48729228
00016717 00000-0 10270-3 0 9101
2 25544 51
6412 251
8661 0006996 344
7885 15
3054 15
50088732 41203
Satellite: ISS
Catalog Number: 25544
Epoch time: 19335
48729228 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 251
8661 deg
Eccentricity:
0006996
Arg of perigee: 344
7885 deg
Mean anomaly: 15
3054 deg
Mean motion: 15
50088732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4120
Checksum: 318
Coasting Arc #12 (Orbit 4119)
---------------------------------------
Vector Time (GMT): 2019/335/11:30:08
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4406584
87 A = 6795240
03 meter
Y = -3583195
39 meter E =
0006890
Z = -3729266
34 I = 51
27443
XDOT = 1456
535933 Wp = 35
75508
YDOT = -6204
180301 meter/sec RA = 250
88727 deg
ZDOT = 4249
575839 TA = 279
53311
MA = 279
61097
Ha = 228
252 n
mi
Hp = 221
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14457299
46 X = -4348074
27
Y = -11755890
39 feet Y = -3632145
38 meter
Z = -12235125
78 Z = -3750530
22
XDOT = 4778
661198 XDOT = 1505
162486
YDOT = -20354
922246 feet/sec YDOT = -6187
620854 meter/sec
ZDOT = 13942
177948 ZDOT = 4256
768609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17169040
11 X = 5233123
43
Y = -7075524
58 feet Y = -2156619
89 meter
Z = -12331819
94 Z = -3758738
72
XDOT = 15178
913537 XDOT = 4626
532846
YDOT = 12528
493937 feet/sec YDOT = 3818
684952 meter/sec
ZDOT = 13975
415750 ZDOT = 4259
706721
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
48729390
00016717 00000-0 10270-3 0 9112
2 25544 51
6414 251
8664 0007076 345
8437 14
2514 15
50052443 41202
Satellite: ISS
Catalog Number: 25544
Epoch time: 19335
48729390 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 251
8664 deg
Eccentricity:
0007076
Arg of perigee: 345
8437 deg
Mean anomaly: 14
2514 deg
Mean motion: 15
50052443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4120
Checksum: 298
Coasting Arc #13 (Orbit 4135)
---------------------------------------
Vector Time (GMT): 2019/336/11:30:08
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4629420
00 A = 6796091
24 meter
Y = 3585982
18 meter E =
0013105
Z = 3446741
91 I = 51
28914
XDOT = -1283
732497 Wp = 56
98849
YDOT = 6036
706215 meter/sec RA = 245
90895 deg
ZDOT = -4536
741514 TA = 82
46502
MA = 82
31617
Ha = 228
422 n
mi
Hp = 220
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15188385
84 X = 4572234
04
Y = 11765033
41 feet Y = 3637431
57 meter
Z = 11308208
38 Z = 3469091
39
XDOT = -4211
720791 XDOT = -1329
104277
YDOT = 19805
466585 feet/sec YDOT = 6022
097336 meter/sec
ZDOT = -14884
322551 ZDOT = -4543
087068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17391469
33 X = -5300919
85
Y = 8020616
96 feet Y = 2444684
05 meter
Z = 11409870
75 Z = 3477728
60
XDOT = -15119
857282 XDOT = -4608
532500
YDOT = -11478
636807 feet/sec YDOT = -3498
688499 meter/sec
ZDOT = -14913
672059 ZDOT = -4545
687244
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
51883222
00016717 00000-0 10270-3 0 9123
2 25544 51
6413 246
7564 0007071 349
5651 10
5352 15
50057757 41366
Satellite: ISS
Catalog Number: 25544
Epoch time: 19336
51883222 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 246
7564 deg
Eccentricity:
0007071
Arg of perigee: 349
5651 deg
Mean anomaly: 10
5352 deg
Mean motion: 15
50057757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4136
Checksum: 303
Coasting Arc #14 (Orbit 4137)
---------------------------------------
Vector Time (GMT): 2019/336/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4726602
70 A = 6791505
33 meter
Y = 1210528
54 meter E =
0011866
Z = 4724218
20 I = 51
27715
XDOT = 889
967149 Wp = 26
93811
YDOT = 7113
934060 meter/sec RA = 245
29236 deg
ZDOT = -2700
214130 TA = 89
98710
MA = 89
85112
Ha = 228
295 n
mi
Hp = 220
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15507226
71 X = 4689767
25
Y = 3971550
34 feet Y = 1263178
37 meter
Z = 15499403
54 Z = 4747088
96
XDOT = 2919
839729 XDOT = 823
467091
YDOT = 23339
678674 feet/sec YDOT = 7123
514718 meter/sec
ZDOT = -8858
970242 ZDOT = -2696
051873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 912697
38 X = 278190
16
Y = 15879962
53 feet Y = 4840212
58 meter
Z = 15603607
79 Z = 4755979
66
XDOT = -20161
375586 XDOT = -6145
187279
YDOT = 9887
249709 feet/sec YDOT = 3013
633711 meter/sec
ZDOT = -8840
477873 ZDOT = -2694
577656
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
64777181
00016717 00000-0 10270-3 0 9134
2 25544 51
6424 246
1181 0007182 348
5637 11
5349 15
50105657 41385
Satellite: ISS
Catalog Number: 25544
Epoch time: 19336
64777181 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 246
1181 deg
Eccentricity:
0007182
Arg of perigee: 348
5637 deg
Mean anomaly: 11
5349 deg
Mean motion: 15
50105657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4138
Checksum: 313
Coasting Arc #15 (Orbit 4152)
---------------------------------------
Vector Time (GMT): 2019/337/13:40:13
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4541745
43 A = 6790175
55 meter
Y = -183297
58 meter E =
0010696
Z = 5044152
85 I = 51
28770
XDOT = 2322
389967 Wp = 18
89143
YDOT = 7070
202599 meter/sec RA = 240
49205 deg
ZDOT = -1823
124822 TA = 88
92460
MA = 88
80206
Ha = 228
350 n
mi
Hp = 220
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14900739
58 X = 4518955
80
Y = -601370
01 feet Y = -132636
38 meter
Z = 16549057
91 Z = 5066159
65
XDOT = 7619
389656 XDOT = 2252
012049
YDOT = 23196
202752 feet/sec YDOT = 7095
779835 meter/sec
ZDOT = -5981
380649 ZDOT = -1812
013886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2208719
15 X = 673217
60
Y = 14634998
45 feet Y = 4460747
53 meter
Z = 16649425
93 Z = 5074745
02
XDOT = -21155
527211 XDOT = -6448
204694
YDOT = 9981
289911 feet/sec YDOT = 3042
297165 meter/sec
ZDOT = -5931
178603 ZDOT = -1807
823238
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
61483721
00016717 00000-0 10270-3 0 9147
2 25544 51
6430 241
3270 0007136 351
5825 8
5204 15
50106249 41531
Satellite: ISS
Catalog Number: 25544
Epoch time: 19337
61483721 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 241
3270 deg
Eccentricity:
0007136
Arg of perigee: 351
5825 deg
Mean anomaly: 8
5204 deg
Mean motion: 15
50106249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4153
Checksum: 282
Coasting Arc #16 (Orbit 4167)
---------------------------------------
Vector Time (GMT): 2019/338/13:40:13
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4671814
83 A = 6790732
85 meter
Y = 178282
82 meter E =
0011951
Z = -4933683
68 I = 51
30683
XDOT = -2576
998206 Wp = 71
89148
YDOT = -6863
518986 meter/sec RA = 235
51180 deg
ZDOT = 2200
251109 TA = 219
67471
MA = 219
76221
Ha = 228
566 n
mi
Hp = 220
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15327476
48 X = -4649496
02
Y = 584917
38 feet Y = 126164
40 meter
Z = -16186626
25 Z = -4956323
49
XDOT = -8454
718523 XDOT = -2510
744455
YDOT = -22518
106910 feet/sec YDOT = -6891
966496 meter/sec
ZDOT = 7218
671617 ZDOT = 2187
893430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2497947
65 X = -761374
45
Y = -15022659
87 feet Y = -4578906
73 meter
Z = -16289888
91 Z = -4965158
14
XDOT = 20170
376781 XDOT = 6147
930843
YDOT = -11092
394222 feet/sec YDOT = -3380
961759 meter/sec
ZDOT = 7162
749427 ZDOT = 2183
206025
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
58190081
00016717 00000-0 10270-3 0 9159
2 25544 51
6430 236
5353 0007197 355
5902 4
5183 15
50081684 41689
Satellite: ISS
Catalog Number: 25544
Epoch time: 19338
58190081 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 236
5353 deg
Eccentricity:
0007197
Arg of perigee: 355
5902 deg
Mean anomaly: 4
5183 deg
Mean motion: 15
50081684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4168
Checksum: 312
Coasting Arc #17 (Orbit 4170)
---------------------------------------
Vector Time (GMT): 2019/338/17:51:47
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3463783
86 A = 6800834
76 meter
Y = 5813876
72 meter E =
0006684
Z = -671531
35 I = 51
34041
XDOT = -4427
402827 Wp = 98
55907
YDOT = 1958
704209 meter/sec RA = 234
66134 deg
ZDOT = -5930
763058 TA = 88
70564
MA = 88
62907
Ha = 228
626 n
mi
Hp = 220
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11364120
28 X = 3401775
90
Y = 19074398
70 feet Y = 5852264
54 meter
Z = -2203186
85 Z = -654855
74
XDOT = -14525
599825 XDOT = -4420
168077
YDOT = 6426
194910 feet/sec YDOT = 1909
234690 meter/sec
ZDOT = -19457
884050 ZDOT = -5952
252136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4285631
77 X = 1306260
56
Y = 21793050
33 feet Y = 6642521
74 meter
Z = -2127502
19 Z = -648462
67
XDOT = -14127
805733 XDOT = -4306
155188
YDOT = 886
319634 feet/sec YDOT = 270
150225 meter/sec
ZDOT = -19556
012393 ZDOT = -5960
672577
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
77531248
00016717 00000-0 10270-3 0 9165
2 25544 51
6393 235
5723 0007128 357
5915 2
5200 15
50115672 41714
Satellite: ISS
Catalog Number: 25544
Epoch time: 19338
77531248 = yrday
fracday
Element set: 916
Inclination: 51
6393 deg
RA of node: 235
5723 deg
Eccentricity:
0007128
Arg of perigee: 357
5915 deg
Mean anomaly: 2
5200 deg
Mean motion: 15
50115672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4171
Checksum: 303
Coasting Arc #18 (Orbit 4186)
---------------------------------------
Vector Time (GMT): 2019/339/17:51:47
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3690788
62 A = 6800744
10 meter
Y = -5607418
71 meter E =
0018324
Z = 1017333
95 I = 51
35935
XDOT = 4538
655686 Wp = 38
70635
YDOT = -1913
155639 meter/sec RA = 229
68851 deg
ZDOT = 5877
281008 TA = 332
35331
MA = 332
45062
Ha = 228
677 n
mi
Hp = 220
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12108886
54 X = -3632752
20
Y = -18397043
00 feet Y = -5648367
27 meter
Z = 3337709
81 Z = 999545
98
XDOT = 14890
602643 XDOT = 4531
163039
YDOT = -6276
757347 feet/sec YDOT = -1862
443416 meter/sec
ZDOT = 19282
418006 ZDOT = 5899
309962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5589807
07 X = -1703773
19
Y = -21315795
92 feet Y = -6497054
60 meter
Z = 3256920
71 Z = 992709
43
XDOT = 14438
566871 XDOT = 4400
875182
YDOT = -802
416575 feet/sec YDOT = -244
576572 meter/sec
ZDOT = 19383
010376 ZDOT = 5907
941563
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
80684564
00016717 00000-0 10270-3 0 9171
2 25544 51
6388 230
4612 0006765 2
0162 358
1015 15
50069990 41873
Satellite: ISS
Catalog Number: 25544
Epoch time: 19339
80684564 = yrday
fracday
Element set: 917
Inclination: 51
6388 deg
RA of node: 230
4612 deg
Eccentricity:
0006765
Arg of perigee: 2
0162 deg
Mean anomaly: 358
1015 deg
Mean motion: 15
50069990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4187
Checksum: 318
Coasting Arc #19 (Orbit 4186)
---------------------------------------
Vector Time (GMT): 2019/339/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -292766
28 A = 6792802
56 meter
Y = 5137352
07 meter E =
0013360
Z = -4447843
83 I = 51
33490
XDOT = -6146
961967 Wp = 42
04034
YDOT = -3178
197944 meter/sec RA = 229
50178 deg
ZDOT = -3262
271035 TA = 194
83860
MA = 194
87784
Ha = 228
705 n
mi
Hp = 220
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -960519
29 X = -328586
56
Y = 16854829
64 feet Y = 5133878
13 meter
Z = -14592663
49 Z = -4449352
70
XDOT = -20167
198053 XDOT = -6095
119150
YDOT = -10427
158608 feet/sec YDOT = -3246
647558 meter/sec
ZDOT = -10702
988961 ZDOT = -3292
005176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2068539
37 X = -630490
80
Y = 16748700
15 feet Y = 5105003
81 meter
Z = -14599859
43 Z = -4450037
15
XDOT = -18073
337633 XDOT = -5508
753311
YDOT = -11691
451900 feet/sec YDOT = -3563
554539 meter/sec
ZDOT = -10838
414551 ZDOT = -3303
548755
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
80684586
00016717 00000-0 10270-3 0 9186
2 25544 51
6399 230
4617 0006754 2
4408 357
6775 15
50077037 41873
Satellite: ISS
Catalog Number: 25544
Epoch time: 19339
80684586 = yrday
fracday
Element set: 918
Inclination: 51
6399 deg
RA of node: 230
4617 deg
Eccentricity:
0006754
Arg of perigee: 2
4408 deg
Mean anomaly: 357
6775 deg
Mean motion: 15
50077037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4187
Checksum: 343
Coasting Arc #20 (Orbit 4202)
---------------------------------------
Vector Time (GMT): 2019/340/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 240794
19 A = 6792007
36 meter
Y = -4955666
49 meter E =
0008630
Z = 4629901
95 I = 51
35513
XDOT = 6409
311658 Wp = 69
13442
YDOT = 3035
506091 meter/sec RA = 224
52540 deg
ZDOT = 2914
356106 TA = 351
73664
MA = 351
75085
Ha = 228
649 n
mi
Hp = 220
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 790007
18 X = 273702
26
Y = -16258748
33 feet Y = -4952790
03 meter
Z = 15189967
03 Z = 4631151
29
XDOT = 21027
925388 XDOT = 6360
734911
YDOT = 9959
009485 feet/sec YDOT = 3106
907764 meter/sec
ZDOT = 9561
535780 ZDOT = 2945
372676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1573321
23 X = 479548
31
Y = -16196096
80 feet Y = -4936570
30 meter
Z = 15195960
51 Z = 4631728
76
XDOT = 19207
156436 XDOT = 5854
341282
YDOT = 10973
777379 feet/sec YDOT = 3344
807345 meter/sec
ZDOT = 9702
837146 ZDOT = 2957
424762
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
83837585
00016717 00000-0 10270-3 0 9191
2 25544 51
6400 225
3503 0006641 4
5504 355
5705 15
50095175 42030
Satellite: ISS
Catalog Number: 25544
Epoch time: 19340
83837585 = yrday
fracday
Element set: 919
Inclination: 51
6400 deg
RA of node: 225
3503 deg
Eccentricity:
0006641
Arg of perigee: 4
5504 deg
Mean anomaly: 355
5705 deg
Mean motion: 15
50095175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4203
Checksum: 295
Coasting Arc #21 (Orbit 4211)
---------------------------------------
Vector Time (GMT): 2019/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1904435
39 A = 6795790
72 meter
Y = 5463079
85 meter E =
0009711
Z = -3577729
62 I = 51
38703
XDOT = -6201
272960 Wp = 38
03230
YDOT = -734
231373 meter/sec RA = 221
18497 deg
ZDOT = -4421
048674 TA = 184
27517
MA = 184
28347
Ha = 228
937 n
mi
Hp = 220
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6248147
61 X = 1860582
95
Y = 17923490
31 feet Y = 5484131
62 meter
Z = -11737958
06 Z = -3568584
63
XDOT = -20345
383728 XDOT = -6171
126401
YDOT = -2408
895580 feet/sec YDOT = -803
409549 meter/sec
ZDOT = -14504
752867 ZDOT = -4451
099353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18687449
17 X = -5695934
51
Y = -3469903
53 feet Y = -1057626
60 meter
Z = -11696560
44 Z = -3565111
62
XDOT = 11947
006216 XDOT = 3641
447495
YDOT = -14974
433023 feet/sec YDOT = -4564
207185 meter/sec
ZDOT = -14641
794709 ZDOT = -4462
819027
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
48308253
00016717 00000-0 10270-3 0 9200
2 25544 51
6431 222
1618 0007184 6
0133 354
1102 15
50073695 42123
Satellite: ISS
Catalog Number: 25544
Epoch time: 19341
48308253 = yrday
fracday
Element set: 920
Inclination: 51
6431 deg
RA of node: 222
1618 deg
Eccentricity:
0007184
Arg of perigee: 6
0133 deg
Mean anomaly: 354
1102 deg
Mean motion: 15
50073695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4212
Checksum: 267
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