[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 6th 2017
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) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 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
340/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 215
1
341/18:07:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 215
2
342/18:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 215
4
344/22:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
5
348/01:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
5
348/05:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
6
351/07:21:01
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
7
353/08:42:47
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 215
7
Coasting Arc #1 (Orbit 823)
---------------------------------------
Vector Time (GMT): 2017/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 740626
73 A = 6788930
92 meter
Y = -6644976
48 meter E =
0011371
Z = 1151109
69 I = 51
28152
XDOT = 4724
433862 Wp = 67
48881
YDOT = 1545
169511 meter/sec RA = 268
42643 deg
ZDOT = 5838
010655 TA = 305
07103
MA = 305
17762
Ha = 221
049 n
mi
Hp = 215
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2429877
74 X = 809285
99
Y = -21801103
94 feet Y = -6636310
53 meter
Z = 3776606
61 Z = 1154873
46
XDOT = 15500
111095 XDOT = 4678
445631
YDOT = 5069
453776 feet/sec YDOT = 1597
743530 meter/sec
ZDOT = 19153
578265 ZDOT = 5860
849310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20087612
90 X = 6122704
41
Y = 8806006
68 feet Y = 2684070
84 meter
Z = 3794370
92 Z = 1156524
26
XDOT = -8788
909147 XDOT = -2678
859508
YDOT = 11692
950779 feet/sec YDOT = 3564
011397 meter/sec
ZDOT = 19254
632739 ZDOT = 5868
812059
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 17338
56206329
00016717 00000-0 10270-3 0 9002
2 25544 51
6402 268
9807 0003151 199
7850 160
3181 15
54071038 8247
Satellite: ISS
Catalog Number: 25544
Epoch time: 17338
56206329 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 268
9807 deg
Eccentricity:
0003151
Arg of perigee: 199
7850 deg
Mean anomaly: 160
3181 deg
Mean motion: 15
54071038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 824
Checksum: 303
Coasting Arc #2 (Orbit 838)
---------------------------------------
Vector Time (GMT): 2017/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1517235
16 A = 6786244
09 meter
Y = 6018419
28 meter E =
0006035
Z = -2738831
25 I = 51
27573
XDOT = -4531
817886 Wp = 152
03017
YDOT = -3467
781674 meter/sec RA = 263
42761 deg
ZDOT = -5119
579459 TA = 59
13241
MA = 59
07306
Ha = 220
893 n
mi
Hp = 215
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4977805
66 X = -1571117
97
Y = 19745470
08 feet Y = 6001151
57 meter
Z = -8985666
83 Z = -2746331
72
XDOT = -14868
168916 XDOT = -4467
834803
YDOT = -11377
236462 feet/sec YDOT = -3518
101190 meter/sec
ZDOT = -16796
520534 ZDOT = -5141
438817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17554280
58 X = -5350544
72
Y = -10290434
42 feet Y = -3136524
41 meter
Z = -9019896
84 Z = -2749264
56
XDOT = 14330
219745 XDOT = 4367
850978
YDOT = -9666
652562 feet/sec YDOT = -2946
395701 meter/sec
ZDOT = -16892
937595 ZDOT = -5148
967379
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 17339
52662648
00016717 00000-0 10270-3 0 9010
2 25544 51
6413 264
1729 0003044 203
9830 156
1182 15
54086385 8398
Satellite: ISS
Catalog Number: 25544
Epoch time: 17339
52662648 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 264
1729 deg
Eccentricity:
0003044
Arg of perigee: 203
9830 deg
Mean anomaly: 156
1182 deg
Mean motion: 15
54086385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 839
Checksum: 312
Coasting Arc #3 (Orbit 854)
---------------------------------------
Vector Time (GMT): 2017/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2273007
90 A = 6782557
94 meter
Y = -4965020
87 meter E =
0010424
Z = 4018736
70 I = 51
26740
XDOT = 4223
149536 Wp = 118
19387
YDOT = 5087
901693 meter/sec RA = 258
42038 deg
ZDOT = 3884
751414 TA = 291
25659
MA = 291
36788
Ha = 220
844 n
mi
Hp = 215
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7457374
99 X = 2308838
06
Y = -16289438
55 feet Y = -4939402
64 meter
Z = 13184831
69 Z = 4029864
78
XDOT = 13855
477480 XDOT = 4147
071119
YDOT = 16692
590855 feet/sec YDOT = 5134
702034 meter/sec
ZDOT = 12745
247420 ZDOT = 3905
081990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13745151
73 X = 4189522
25
Y = 11432591
25 feet Y = 3484653
81 meter
Z = 13234980
09 Z = 4034021
93
XDOT = -18918
511039 XDOT = -5766
362165
YDOT = 7839
694823 feet/sec YDOT = 2389
538982 meter/sec
ZDOT = 12834
645572 ZDOT = 3911
999970
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 17340
55548899
00016717 00000-0 10270-3 0 9027
2 25544 51
6406 259
0450 0003021 206
6352 153
4646 15
54083935 8559
Satellite: ISS
Catalog Number: 25544
Epoch time: 17340
55548899 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 259
0450 deg
Eccentricity:
0003021
Arg of perigee: 206
6352 deg
Mean anomaly: 153
4646 deg
Mean motion: 15
54083935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 855
Checksum: 310
Coasting Arc #4 (Orbit 854)
---------------------------------------
Vector Time (GMT): 2017/340/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 919378
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3673105
23 A = 6784767
61 meter
Y = -4667291
59 meter E =
0004020
Z = -3285309
29 I = 51
27671
XDOT = 2701
001893 Wp = 125
17226
YDOT = -5424
627248 meter/sec RA = 258
12659 deg
ZDOT = 4688
504305 TA = 196
48141
MA = 196
49449
Ha = 220
846 n
mi
Hp = 215
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12050870
19 X = -3604682
88
Y = -15312636
46 feet Y = -4707983
84 meter
Z = -10778573
79 Z = -3302986
46
XDOT = 8861
554766 XDOT = 2738
686279
YDOT = -17797
333490 feet/sec YDOT = -5394
212598 meter/sec
ZDOT = 15382
231972 ZDOT = 4701
715913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14854957
56 X = 4527791
07
Y = -12543909
30 feet Y = -3823383
55 meter
Z = -10856267
13 Z = -3308990
22
XDOT = 17196
380133 XDOT = 5241
456664
YDOT = 7005
487241 feet/sec YDOT = 2135
272511 meter/sec
ZDOT = 15441
695505 ZDOT = 4706
628790
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 17340
55548870
00016717 00000-0 10270-3 0 9037
2 25544 51
6420 259
0452 0003040 206
9584 153
1412 15
54101475 8556
Satellite: ISS
Catalog Number: 25544
Epoch time: 17340
55548870 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 259
0452 deg
Eccentricity:
0003040
Arg of perigee: 206
9584 deg
Mean anomaly: 153
1412 deg
Mean motion: 15
54101475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 855
Checksum: 287
Coasting Arc #5 (Orbit 870)
---------------------------------------
Vector Time (GMT): 2017/341/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 919378
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3224002
01 A = 6788115
65 meter
Y = 5689924
74 meter E =
0014000
Z = 1789088
81 I = 51
29427
XDOT = -3564
687244 Wp = 127
27694
YDOT = 3797
870775 meter/sec RA = 253
12630 deg
ZDOT = -5632
737553 TA = 32
95959
MA = 32
87239
Ha = 220
789 n
mi
Hp = 215
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10577434
41 X = 3151445
62
Y = 18667732
08 feet Y = 5725571
89 meter
Z = 5869713
94 Z = 1804574
27
XDOT = -11695
168122 XDOT = -3579
530068
YDOT = 12460
205956 feet/sec YDOT = 3757
925508 meter/sec
ZDOT = -18480
110083 ZDOT = -5650
089405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18065307
01 X = -5506305
58
Y = 11541669
30 feet Y = 3517900
80 meter
Z = 5937544
46 Z = 1809763
55
XDOT = -12230
004316 XDOT = -3727
705315
YDOT = -9558
907785 feet/sec YDOT = -2913
555093 meter/sec
ZDOT = -18557
684568 ZDOT = -5656
382256
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 17341
58434790
00016717 00000-0 10270-3 0 9047
2 25544 51
6410 253
9179 0003142 209
9504 150
1469 15
54069337 8719
Satellite: ISS
Catalog Number: 25544
Epoch time: 17341
58434790 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 253
9179 deg
Eccentricity:
0003142
Arg of perigee: 209
9504 deg
Mean anomaly: 150
1469 deg
Mean motion: 15
54069337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 871
Checksum: 310
Coasting Arc #6 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2017/341/18:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 919378
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2244851
39 A = 6781026
00 meter
Y = 4621227
61 meter E =
0007087
Z = -4432162
53 I = 51
26879
XDOT = -4464
203017 Wp = 86
15061
YDOT = -5300
183056 meter/sec RA = 252
12712 deg
ZDOT = -3269
265812 TA = 150
71080
MA = 150
67105
Ha = 220
747 n
mi
Hp = 215
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7364998
01 X = -2274831
11
Y = 15161507
90 feet Y = 4595956
89 meter
Z = -14541215
65 Z = -4443139
74
XDOT = -14646
335356 XDOT = -4388
722691
YDOT = -17389
052022 feet/sec YDOT = -5349
682518 meter/sec
ZDOT = -10725
937705 ZDOT = -3290
768612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10330344
91 X = -3148689
13
Y = 13264950
30 feet Y = 4043156
85 meter
Z = -14590631
84 Z = -4447224
58
XDOT = -9571
455811 XDOT = -2917
379731
YDOT = -19341
246648 feet/sec YDOT = -5895
211978 meter/sec
ZDOT = -10820
531418 ZDOT = -3298
097976
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 17341
77725664
00016717 00000-0 10270-3 0 9052
2 25544 51
6370 252
9523 0003189 210
2567 149
8401 15
54102850 8743
Satellite: ISS
Catalog Number: 25544
Epoch time: 17341
77725664 = yrday
fracday
Element set: 905
Inclination: 51
6370 deg
RA of node: 252
9523 deg
Eccentricity:
0003189
Arg of perigee: 210
2567 deg
Mean anomaly: 149
8401 deg
Mean motion: 15
54102850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 309
Coasting Arc #7 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2017/342/18:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 919378
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3106511
54 A = 6778329
06 meter
Y = -3184910
30 meter E =
0005749
Z = 5113278
20 I = 51
27063
XDOT = 4008
374279 Wp = 158
69282
YDOT = 6358
945717 meter/sec RA = 247
10614 deg
ZDOT = 1519
754449 TA = 276
55847
MA = 276
62391
Ha = 220
645 n
mi
Hp = 215
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10191966
98 X = 3117057
42
Y = -10449180
78 feet Y = -3150112
52 meter
Z = 16775847
11 Z = 5128394
06
XDOT = 13150
834248 XDOT = 3929
586722
YDOT = 20862
682797 feet/sec YDOT = 6403
329475 meter/sec
ZDOT = 4986
071028 ZDOT = 1539
034891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11934260
86 X = 3637562
71
Y = -8268240
36 feet Y = -2520159
66 meter
Z = 16843403
32 Z = 5133869
33
XDOT = 8169
495123 XDOT = 2490
062114
YDOT = 22159
933161 feet/sec YDOT = 6754
347627 meter/sec
ZDOT = 5070
665096 ZDOT = 1545
538721
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 17342
80611084
00016717 00000-0 10270-3 0 9068
2 25544 51
6372 247
8228 0003166 215
5657 144
5285 15
54064643 8900
Satellite: ISS
Catalog Number: 25544
Epoch time: 17342
80611084 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 247
8228 deg
Eccentricity:
0003166
Arg of perigee: 215
5657 deg
Mean anomaly: 144
5285 deg
Mean motion: 15
54064643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 312
Coasting Arc #8 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2017/342/18:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 919378
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4715081
50 A = 6781184
15 meter
Y = 2110395
39 meter E =
0006843
Z = 4387352
10 I = 51
28059
XDOT = 20
354540 Wp = 86
29152
YDOT = 6906
180464 meter/sec RA = 247
02596 deg
ZDOT = -3338
922501 TA = 37
64152
MA = 37
59365
Ha = 220
575 n
mi
Hp = 215
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15469427
50 X = 4669820
49
Y = 6923869
39 feet Y = 2162869
31 meter
Z = 14394199
81 Z = 4410146
67
XDOT = 66
779987 XDOT = -40
654915
YDOT = 22658
072388 feet/sec YDOT = 6906
067164 meter/sec
ZDOT = -10954
470149 ZDOT = -3338
971380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14233646
27 X = 4338415
38
Y = 9040662
40 feet Y = 2755593
90 meter
Z = 14495029
50 Z = 4418084
99
XDOT = -2424
681669 XDOT = -739
042973
YDOT = 21408
768028 feet/sec YDOT = 6525
392495 meter/sec
ZDOT = -10955
730249 ZDOT = -3339
306580
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 17342
80610982
00016717 00000-0 10270-3 0 9075
2 25544 51
6372 247
8226 0003339 215
1253 144
9680 15
54079618 8909
Satellite: ISS
Catalog Number: 25544
Epoch time: 17342
80610982 = yrday
fracday
Element set: 907
Inclination: 51
6372 deg
RA of node: 247
8226 deg
Eccentricity:
0003339
Arg of perigee: 215
1253 deg
Mean anomaly: 144
9680 deg
Mean motion: 15
54079618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 318
Coasting Arc #9 (Orbit 904)
---------------------------------------
Vector Time (GMT): 2017/343/18:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 919378
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4809382
81 A = 6784869
30 meter
Y = -3533642
26 meter E =
0003445
Z = -3232387
77 I = 51
30737
XDOT = 1157
855928 Wp = 127
58243
YDOT = -5909
005572 meter/sec RA = 242
01555 deg
ZDOT = 4738
392593 TA = 194
81501
MA = 194
82511
Ha = 220
677 n
mi
Hp = 215
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15778815
00 X = -4753809
88
Y = -11593314
51 feet Y = -3587113
19 meter
Z = -10604946
74 Z = -3255615
44
XDOT = 3798
739920 XDOT = 1200
829176
YDOT = -19386
501221 feet/sec YDOT = -5895
817578 meter/sec
ZDOT = 15545
907458 ZDOT = 4744
121198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14134473
20 X = -4308187
43
Y = -13468739
98 feet Y = -4105271
95 meter
Z = -10707499
73 Z = -3263645
92
XDOT = 5110
883301 XDOT = 1557
797230
YDOT = -17739
575165 feet/sec YDOT = -5407
022510 meter/sec
ZDOT = 15572
207867 ZDOT = 4746
408958
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 17343
77065588
00016717 00000-0 10270-3 0 9089
2 25544 51
6377 243
0138 0003245 214
7842 145
3098 15
54109800 9051
Satellite: ISS
Catalog Number: 25544
Epoch time: 17343
77065588 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 243
0138 deg
Eccentricity:
0003245
Arg of perigee: 214
7842 deg
Mean anomaly: 145
3098 deg
Mean motion: 15
54109800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 905
Checksum: 314
Coasting Arc #10 (Orbit 920)
---------------------------------------
Vector Time (GMT): 2017/344/18:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4645559
20 A = 6788057
93 meter
Y = 4629542
70 meter E =
0013381
Z = 1720298
56 I = 51
33324
XDOT = -2441
634804 Wp = 128
91086
YDOT = 4562
582571 meter/sec RA = 237
01713 deg
ZDOT = -5663
516618 TA = 32
12666
MA = 32
04519
Ha = 220
452 n
mi
Hp = 215
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15241335
96 X = 4585088
76
Y = 15188788
40 feet Y = 4681154
34 meter
Z = 5644024
15 Z = 1742718
61
XDOT = -8010
612873 XDOT = -2464
962705
YDOT = 14969
102922 feet/sec YDOT = 4535
148326 meter/sec
ZDOT = -18581
091265 ZDOT = -5675
433836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13473745
41 X = 4106797
60
Y = 16743073
60 feet Y = 5103288
83 meter
Z = 5742847
24 Z = 1750419
84
XDOT = -8238
308578 XDOT = -2511
036455
YDOT = 13045
082932 feet/sec YDOT = 3976
141278 meter/sec
ZDOT = -18634
649332 ZDOT = -5679
841116
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 17344
79950113
00016717 00000-0 10270-3 0 9090
2 25544 51
6366 237
8853 0003293 221
7979 138
2922 15
54119923 9218
Satellite: ISS
Catalog Number: 25544
Epoch time: 17344
79950113 = yrday
fracday
Element set: 909
Inclination: 51
6366 deg
RA of node: 237
8853 deg
Eccentricity:
0003293
Arg of perigee: 221
7979 deg
Mean anomaly: 138
2922 deg
Mean motion: 15
54119923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 921
Checksum: 332
Coasting Arc #11 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2017/344/22:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3242923
19 A = 6777367
97 meter
Y = -2752342
30 meter E =
0003473
Z = 5276479
39 I = 51
30539
XDOT = 4542
173801 Wp = 176
79078
YDOT = 6164
787012 meter/sec RA = 236
13948 deg
ZDOT = 420
665603 TA = 269
15923
MA = 269
19903
Ha = 220
355 n
mi
Hp = 215
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10639511
76 X = 3247828
97
Y = -9029994
41 feet Y = -2716050
48 meter
Z = 17311284
09 Z = 5292244
37
XDOT = 14902
145018 XDOT = 4470
856522
YDOT = 20225
679174 feet/sec YDOT = 6215
181930 meter/sec
ZDOT = 1380
136493 ZDOT = 442
557161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2222268
39 X = -677347
41
Y = -13687958
55 feet Y = -4172089
77 meter
Z = 17381653
56 Z = 5297928
01
XDOT = 24024
902436 XDOT = 7322
790262
YDOT = -2011
501705 feet/sec YDOT = -613
105720 meter/sec
ZDOT = 1476
392418 ZDOT = 450
004409
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 17344
99240845
00016717 00000-0 10270-3 0 9108
2 25544 51
6411 236
9252 0003465 222
4298 137
6587 15
54144580 9245
Satellite: ISS
Catalog Number: 25544
Epoch time: 17344
99240845 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 236
9252 deg
Eccentricity:
0003465
Arg of perigee: 222
4298 deg
Mean anomaly: 137
6587 deg
Mean motion: 15
54144580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 924
Checksum: 317
Coasting Arc #12 (Orbit 938)
---------------------------------------
Vector Time (GMT): 2017/345/22:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4265869
39 A = 6778069
53 meter
Y = 1248347
30 meter E =
0012107
Z = -5127947
74 I = 51
32674
XDOT = -3717
944754 Wp = 114
50703
YDOT = -6525
937816 meter/sec RA = 231
11790 deg
ZDOT = 1502
110977 TA = 170
05308
MA = 170
02910
Ha = 220
373 n
mi
Hp = 215
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13995634
47 X = -4254602
49
Y = 4095627
61 feet Y = 1200706
63 meter
Z = -16823975
52 Z = -5148642
72
XDOT = -12197
981478 XDOT = -3651
990203
YDOT = -21410
557139 feet/sec YDOT = -6567
145701 meter/sec
ZDOT = 4928
185619 ZDOT = 1484
210180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3498534
45 X = -1066353
30
Y = 14046599
57 feet Y = 4281403
55 meter
Z = -16916010
14 Z = -5155999
89
XDOT = -23631
030299 XDOT = -7202
738035
YDOT = -36
994144 feet/sec YDOT = -11
275815 meter/sec
ZDOT = 4849
676975 ZDOT = 1478
181542
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 17345
95694862
00016717 00000-0 10270-3 0 9118
2 25544 51
6411 232
1177 0003340 226
8057 133
2817 15
54132300 9393
Satellite: ISS
Catalog Number: 25544
Epoch time: 17345
95694862 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 232
1177 deg
Eccentricity:
0003340
Arg of perigee: 226
8057 deg
Mean anomaly: 133
2817 deg
Mean motion: 15
54132300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 295
Coasting Arc #13 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2017/346/22:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5123374
02 A = 6780813
16 meter
Y = 213695
44 meter E =
0006058
Z = 4432333
54 I = 51
35792
XDOT = 2567
937219 Wp = 77
88570
YDOT = 6443
671264 meter/sec RA = 226
10219 deg
ZDOT = -3273
923787 TA = 45
26441
MA = 45
21511
Ha = 220
100 n
mi
Hp = 215
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16808969
88 X = 5099073
35
Y = 701100
51 feet Y = 270852
43 meter
Z = 14541776
70 Z = 4457162
50
XDOT = 8424
990875 XDOT = 2511
594754
YDOT = 21140
653753 feet/sec YDOT = 6472
072818 meter/sec
ZDOT = -10741
219773 ZDOT = -3261
585982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8823675
07 X = 2689456
16
Y = -14211233
42 feet Y = -4331583
95 meter
Z = 14651958
33 Z = 4465916
90
XDOT = 21549
851015 XDOT = 6568
394589
YDOT = 2344
423855 feet/sec YDOT = 714
580391 meter/sec
ZDOT = -10687
377293 ZDOT = -3257
512599
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 17346
98578697
00016717 00000-0 10270-3 0 9120
2 25544 51
6416 226
9890 0003246 232
4610 127
6248 15
54145600 9554
Satellite: ISS
Catalog Number: 25544
Epoch time: 17346
98578697 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 226
9890 deg
Eccentricity:
0003246
Arg of perigee: 232
4610 deg
Mean anomaly: 127
6248 deg
Mean motion: 15
54145600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 328
Coasting Arc #14 (Orbit 969)
---------------------------------------
Vector Time (GMT): 2017/347/22:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5738173
86 A = 6784632
46 meter
Y = -1521006
87 meter E =
0002536
Z = -3288446
02 I = 51
39271
XDOT = -1114
606655 Wp = 128
54511
YDOT = -5950
392403 meter/sec RA = 221
09848 deg
ZDOT = 4698
082788 TA = 193
13154
MA = 193
13814
Ha = 220
207 n
mi
Hp = 215
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18826029
74 X = -5704765
27
Y = -4990180
03 feet Y = -1584988
06 meter
Z = -10788864
89 Z = -3316239
52
XDOT = -3656
845980 XDOT = -1070
806138
YDOT = -19522
284788 feet/sec YDOT = -5962
612074 meter/sec
ZDOT = 15413
657440 ZDOT = 4692
774350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13321413
23 X = -4060366
75
Y = 14113412
18 feet Y = 4301768
03 meter
Z = -10912032
08 Z = -3325987
38
XDOT = -17925
307313 XDOT = -5463
633669
YDOT = -5021
909088 feet/sec YDOT = -1530
677890 meter/sec
ZDOT = 15390
938427 ZDOT = 4691
158033
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 17347
95032193
00016717 00000-0 10270-3 0 9135
2 25544 51
6403 222
1819 0003307 234
9296 125
1547 15
54131215 9703
Satellite: ISS
Catalog Number: 25544
Epoch time: 17347
95032193 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 222
1819 deg
Eccentricity:
0003307
Arg of perigee: 234
9296 deg
Mean anomaly: 125
1547 deg
Mean motion: 15
54131215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 970
Checksum: 292
Coasting Arc #15 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2017/348/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2617054
20 A = 6777423
56 meter
Y = 3333932
47 meter E =
0012397
Z = -5299269
74 I = 51
37135
XDOT = -5901
526509 Wp = 96
43166
YDOT = -4880
158450 meter/sec RA = 220
52987 deg
ZDOT = -157
456478 TA = 172
07029
MA = 172
05067
Ha = 220
254 n
mi
Hp = 215
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8586135
84 X = -2628399
12
Y = 10938098
64 feet Y = 3304603
67 meter
Z = -17386055
58 Z = -5312010
06
XDOT = -19361
963613 XDOT = -5845
751799
YDOT = -16011
018536 feet/sec YDOT = -4945
841489 meter/sec
ZDOT = -516
589496 ZDOT = -185
989386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12713988
05 X = 3875223
56
Y = 5452690
09 feet Y = 1661979
94 meter
Z = -17443088
54 Z = -5316653
39
XDOT = -10237
320197 XDOT = -3120
335196
YDOT = 21832
284892 feet/sec YDOT = 6654
480435 meter/sec
ZDOT = -642
563181 ZDOT = -195
853258
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 17348
07892702
00016717 00000-0 10270-3 0 9140
2 25544 51
6405 221
5415 0003046 236
0285 124
0579 15
54109464 9727
Satellite: ISS
Catalog Number: 25544
Epoch time: 17348
07892702 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 221
5415 deg
Eccentricity:
0003046
Arg of perigee: 236
0285 deg
Mean anomaly: 124
0579 deg
Mean motion: 15
54109464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 972
Checksum: 301
Coasting Arc #16 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2017/348/05:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 925316
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 464787
09 A = 6779197
08 meter
Y = -4683364
23 meter E =
0005960
Z = 4878383
18 I = 51
37826
XDOT = 6621
405208 Wp = 147
71079
YDOT = 3089
256553 meter/sec RA = 219
76251 deg
ZDOT = 2328
642069 TA = 279
38428
MA = 279
45165
Ha = 220
132 n
mi
Hp = 215
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1524892
03 X = 493426
15
Y = -15365368
21 feet Y = -4678006
85 meter
Z = 16005194
16 Z = 4880710
26
XDOT = 21723
770366 XDOT = 6575
056679
YDOT = 10135
356146 feet/sec YDOT = 3163
042334 meter/sec
ZDOT = 7639
901800 ZDOT = 2360
694755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6294360
92 X = -1918521
21
Y = 14087183
44 feet Y = 4293773
51 meter
Z = 16016190
55 Z = 4881734
88
XDOT = -16223
946388 XDOT = -4945
058859
YDOT = -16119
791828 feet/sec YDOT = -4913
312549 meter/sec
ZDOT = 7781
758516 ZDOT = 2371
879996
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 17348
27183326
00016717 00000-0 10270-3 0 9158
2 25544 51
6374 220
5805 0003046 240
6766 119
4082 15
54135378 9752
Satellite: ISS
Catalog Number: 25544
Epoch time: 17348
27183326 = yrday
fracday
Element set: 915
Inclination: 51
6374 deg
RA of node: 220
5805 deg
Eccentricity:
0003046
Arg of perigee: 240
6766 deg
Mean anomaly: 119
4082 deg
Mean motion: 15
54135378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 314
Coasting Arc #17 (Orbit 989)
---------------------------------------
Vector Time (GMT): 2017/349/05:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 925316
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1994641
47 A = 6777453
97 meter
Y = 3754645
25 meter E =
0012090
Z = -5288516
40 I = 51
39871
XDOT = -6478
076424 Wp = 91
96695
YDOT = -4063
255715 meter/sec RA = 214
74648 deg
ZDOT = -442
740315 TA = 173
79902
MA = 173
78404
Ha = 220
132 n
mi
Hp = 215
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6544099
31 X = -2010789
40
Y = 12318389
91 feet Y = 3732249
94 meter
Z = -17350775
58 Z = -5298244
77
XDOT = -21253
531576 XDOT = -6430
007906
YDOT = -13330
891454 feet/sec YDOT = -4135
429191 meter/sec
ZDOT = -1452
560088 ZDOT = -474
092692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9889159
07 X = 3014215
68
Y = -9759778
74 feet Y = -2974780
56 meter
Z = -17394500
02 Z = -5301843
61
XDOT = 15435
891934 XDOT = 4704
859861
YDOT = 18468
940942 feet/sec YDOT = 5629
333199 meter/sec
ZDOT = -1591
188760 ZDOT = -484
994334
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 17349
23636473
00016717 00000-0 10270-3 0 9162
2 25544 51
6379 215
7719 0002940 243
8228 116
2623 15
54121596 9907
Satellite: ISS
Catalog Number: 25544
Epoch time: 17349
23636473 = yrday
fracday
Element set: 916
Inclination: 51
6379 deg
RA of node: 215
7719 deg
Eccentricity:
0002940
Arg of perigee: 243
8228 deg
Mean anomaly: 116
2623 deg
Mean motion: 15
54121596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 990
Checksum: 323
Coasting Arc #18 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2017/350/05:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 925316
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3491228
15 A = 6778041
89 meter
Y = -2720188
21 meter E =
0001899
Z = 5133072
42 I = 51
42830
XDOT = 5863
015436 Wp = 32
12278
YDOT = 4714
546144 meter/sec RA = 209
73158 deg
ZDOT = -1487
466267 TA = 72
25157
MA = 72
23084
Ha = 219
934 n
mi
Hp = 215
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11454160
59 X = 3496452
39
Y = -8924502
01 feet Y = -2681118
19 meter
Z = 16840788
78 Z = 5150044
30
XDOT = 19235
614949 XDOT = 5817
085807
YDOT = 15467
671075 feet/sec YDOT = 4779
853724 meter/sec
ZDOT = -4880
138671 ZDOT = -1459
096412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13440398
55 X = -4096633
48
Y = 5257678
68 feet Y = 1602540
46 meter
Z = 16916536
28 Z = 5156160
26
XDOT = -13581
926935 XDOT = -4139
771330
YDOT = -19402
130380 feet/sec YDOT = -5913
769340 meter/sec
ZDOT = -4754
824869 ZDOT = -1449
270620
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 17350
26519429
00016717 00000-0 10270-3 0 9179
2 25544 51
6378 210
6434 0002938 249
9088 110
1749 15
54129271 10061
Satellite: ISS
Catalog Number: 25544
Epoch time: 17350
26519429 = yrday
fracday
Element set: 917
Inclination: 51
6378 deg
RA of node: 210
6434 deg
Eccentricity:
0002938
Arg of perigee: 249
9088 deg
Mean anomaly: 110
1749 deg
Mean motion: 15
54129271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 314
Coasting Arc #19 (Orbit 1020)
---------------------------------------
Vector Time (GMT): 2017/351/05:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 925316
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4837827
07 A = 6780830
01 meter
Y = 1676847
77 meter E =
0007276
Z = -4453108
55 I = 51
46577
XDOT = -4751
979496 Wp = 124
57347
YDOT = -5047
675183 meter/sec RA = 204
72341 deg
ZDOT = 3261
545132 TA = 178
39901
MA = 178
39668
Ha = 219
992 n
mi
Hp = 215
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15872136
05 X = -4834587
32
Y = 5501469
06 feet Y = 1622766
48 meter
Z = -14609936
19 Z = -4476601
31
XDOT = -15590
483912 XDOT = -4711
024943
YDOT = -16560
614116 feet/sec YDOT = -5100
586427 meter/sec
ZDOT = 10700
607390 ZDOT = 3238
560269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16677933
40 X = 5083434
10
Y = -985348
42 feet Y = -300334
20 meter
Z = -14714507
33 Z = -4484981
83
XDOT = 10474
018272 XDOT = 3192
480769
YDOT = 18989
294093 feet/sec YDOT = 5787
936839 meter/sec
ZDOT = 10599
235181 ZDOT = 3230
646883
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 17351
22971966
00016717 00000-0 10270-3 0 9185
2 25544 51
6371 205
8355 0002958 254
9679 105
1147 15
54122094 10215
Satellite: ISS
Catalog Number: 25544
Epoch time: 17351
22971966 = yrday
fracday
Element set: 918
Inclination: 51
6371 deg
RA of node: 205
8355 deg
Eccentricity:
0002958
Arg of perigee: 254
9679 deg
Mean anomaly: 105
1147 deg
Mean motion: 15
54122094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1021
Checksum: 314
Coasting Arc #20 (Orbit 1022)
---------------------------------------
Vector Time (GMT): 2017/351/07:21:01
000
Vector Time (MET): N/A
Weight (LBS) : 925316
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -588557
28 A = 6778832
54 meter
Y = -4593075
65 meter E =
0004910
Z = 4950073
32 I = 51
46345
XDOT = 7229
272016 Wp = 150
62038
YDOT = 1392
534508 meter/sec RA = 204
33117 deg
ZDOT = 2146
555693 TA = 278
38385
MA = 278
43951
Ha = 219
911 n
mi
Hp = 215
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1930962
20 X = -561197
70
Y = -15069145
82 feet Y = -4599504
86 meter
Z = 16240398
03 Z = 4947280
23
XDOT = 23718
084042 XDOT = 7202
736050
YDOT = 4568
682770 feet/sec YDOT = 1473
228563 meter/sec
ZDOT = 7042
505555 ZDOT = 2181
609170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5990263
98 X = 1825832
46
Y = 13975205
46 feet Y = 4259642
62 meter
Z = 16228637
31 Z = 4946488
65
XDOT = -23012
342263 XDOT = -7014
161922
YDOT = 1485
819574 feet/sec YDOT = 452
877806 meter/sec
ZDOT = 7197
991533 ZDOT = 2193
947819
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 17351
35832208
00016717 00000-0 10270-3 0 9195
2 25544 51
6386 205
1952 0003072 254
3696 105
7118 15
54167574 10236
Satellite: ISS
Catalog Number: 25544
Epoch time: 17351
35832208 = yrday
fracday
Element set: 919
Inclination: 51
6386 deg
RA of node: 205
1952 deg
Eccentricity:
0003072
Arg of perigee: 254
3696 deg
Mean anomaly: 105
7118 deg
Mean motion: 15
54167574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1023
Checksum: 305
Coasting Arc #21 (Orbit 1037)
---------------------------------------
Vector Time (GMT): 2017/352/07:21:01
000
Vector Time (MET): N/A
Weight (LBS) : 925316
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1138711
54 A = 6777312
31 meter
Y = 4074282
52 meter E =
0011909
Z = -5305174
18 I = 51
48910
XDOT = -7286
300489 Wp = 90
24446
YDOT = -2350
646542 meter/sec RA = 199
32061 deg
ZDOT = -241
832744 TA = 177
44624
MA = 177
44015
Ha = 219
907 n
mi
Hp = 215
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3735930
24 X = -1158416
62
Y = 13367068
65 feet Y = 4061439
11 meter
Z = -17405427
11 Z = -5310753
10
XDOT = -23905
185333 XDOT = -7258
298688
YDOT = -7712
094953 feet/sec YDOT = -2431
970338 meter/sec
ZDOT = -793
414516 ZDOT = -277
159698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -320275
79 X = -97620
06
Y = -13843771
71 feet Y = -4219581
62 meter
Z = -17430777
39 Z = -5312900
95
XDOT = 24095
979261 XDOT = 7344
454479
YDOT = 636
551494 feet/sec YDOT = 194
020895 meter/sec
ZDOT = -950
006573 ZDOT = -289
562003
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 17352
32284607
00016717 00000-0 10270-3 0 9209
2 25544 51
6392 200
3865 0002963 259
5776 100
5043 15
54152928 10380
Satellite: ISS
Catalog Number: 25544
Epoch time: 17352
32284607 = yrday
fracday
Element set: 920
Inclination: 51
6392 deg
RA of node: 200
3865 deg
Eccentricity:
0002963
Arg of perigee: 259
5776 deg
Mean anomaly: 100
5043 deg
Mean motion: 15
54152928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1038
Checksum: 303
Coasting Arc #22 (Orbit 1053)
---------------------------------------
Vector Time (GMT): 2017/353/07:21:01
000
Vector Time (MET): N/A
Weight (LBS) : 925316
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2850132
25 A = 6778115
07 meter
Y = -3448907
54 meter E =
0002886
Z = 5091305
99 I = 51
52323
XDOT = 6798
656671 Wp = 23
34067
YDOT = 3120
179266 meter/sec RA = 194
31240 deg
ZDOT = -1689
345317 TA = 83
01876
MA = 82
98594
Ha = 219
736 n
mi
Hp = 215
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9350827
59 X = 2863755
99
Y = -11315313
46 feet Y = -3416959
84 meter
Z = 16703759
81 Z = 5105183
73
XDOT = 22305
304038 XDOT = 6771
466703
YDOT = 10236
808615 feet/sec YDOT = 3196
054661 meter/sec
ZDOT = -5542
471512 ZDOT = -1656
385243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5417764
10 X = -1651334
50
Y = 13566227
77 feet Y = 4134986
22 meter
Z = 16765893
46 Z = 5110244
33
XDOT = -23394
581912 XDOT = -7130
668567
YDOT = -2661
709863 feet/sec YDOT = -811
289166 meter/sec
ZDOT = -5396
474858 ZDOT = -1644
845537
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 17353
35166590
00016717 00000-0 10270-3 0 9214
2 25544 51
6390 195
2582 0003018 265
6872 94
3936 15
54173248 10540
Satellite: ISS
Catalog Number: 25544
Epoch time: 17353
35166590 = yrday
fracday
Element set: 921
Inclination: 51
6390 deg
RA of node: 195
2582 deg
Eccentricity:
0003018
Arg of perigee: 265
6872 deg
Mean anomaly: 94
3936 deg
Mean motion: 15
54173248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1054
Checksum: 318
Coasting Arc #23 (Orbit 1054)
---------------------------------------
Vector Time (GMT): 2017/353/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1938752
32 A = 6779646
39 meter
Y = -4399618
47 meter E =
0005394
Z = 4778395
77 I = 51
53100
XDOT = 7203
446727 Wp = 136
46137
YDOT = -333
499992 meter/sec RA = 194
06251 deg
ZDOT = 2610
022942 TA = 287
74385
MA = 287
80272
Ha = 219
958 n
mi
Hp = 215
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6360735
95 X = -1912621
59
Y = -14434443
79 feet Y = -4421153
38 meter
Z = 15677151
49 Z = 4769040
87
XDOT = 23633
355405 XDOT = 7193
962441
YDOT = -1094
160078 feet/sec YDOT = -252
999463 meter/sec
ZDOT = 8563
067394 ZDOT = 2644
991952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13975349
79 X = 4259686
62
Y = 7401620
92 feet Y = 2256014
06 meter
Z = 15636202
04 Z = 4765914
38
XDOT = -17374
058461 XDOT = -5295
613019
YDOT = 14347
849093 feet/sec YDOT = 4373
224404 meter/sec
ZDOT = 8718
470602 ZDOT = 2657
389840
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 17353
41596767
00016717 00000-0 10270-3 0 9225
2 25544 51
6404 194
9374 0002932 264
2885 95
7934 15
54143745 10557
Satellite: ISS
Catalog Number: 25544
Epoch time: 17353
41596767 = yrday
fracday
Element set: 922
Inclination: 51
6404 deg
RA of node: 194
9374 deg
Eccentricity:
0002932
Arg of perigee: 264
2885 deg
Mean anomaly: 95
7934 deg
Mean motion: 15
54143745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1055
Checksum: 336
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