[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 21st 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 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
328/13:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 213
6
333/15:51:27
380 0
5 1
2 1
2
N/A -1
0 -0
0 221
5
000/00:02:54
761 0
2 -0
0 214
6
334/13:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 214
6
338/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 214
9
338/19:53:38
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 606)
---------------------------------------
Vector Time (GMT): 2017/324/13:12:23
285
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6183037
58 A = 6785734
73 meter
Y = -84173
05 meter E =
0016013
Z = 2781189
17 I = 51
51131
XDOT = -2238
078182 Wp = 91
48653
YDOT = 5265
347979 meter/sec RA = 338
26616 deg
ZDOT = 5109
088565 TA = 300
11764
MA = 300
27627
Ha = 222
035 n
mi
Hp = 213
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20285556
38 X = 6170009
34
Y = -276158
29 feet Y = -15103
11 meter
Z = 9124636
39 Z = 2811193
48
XDOT = -7342
776189 XDOT = -2321
608374
YDOT = 17274
763711 feet/sec YDOT = 5239
852908 meter/sec
ZDOT = 16762
101590 ZDOT = 5098
013860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4291173
19 X = -1307949
59
Y = 19766615
87 feet Y = 6024864
52 meter
Z = 9257741
62 Z = 2821759
65
XDOT = -13709
954262 XDOT = -4178
794059
YDOT = -10842
635214 feet/sec YDOT = -3304
835213 meter/sec
ZDOT = 16712
027180 ZDOT = 5093
825884
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 17324
60884514
00016717 00000-0 10270-3 0 9000
2 25544 51
6384 338
5422 0003974 135
1491 224
9983 15
54204731 6075
Satellite: ISS
Catalog Number: 25544
Epoch time: 17324
60884514 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 338
5422 deg
Eccentricity:
0003974
Arg of perigee: 135
1491 deg
Mean anomaly: 224
9983 deg
Mean motion: 15
54204731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 607
Checksum: 309
Coasting Arc #2 (Orbit 621)
---------------------------------------
Vector Time (GMT): 2017/325/13:12:23
285
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5314277
84 A = 6781933
03 meter
Y = -984185
41 meter E =
0009928
Z = -4105253
11 I = 51
46822
XDOT = 3925
571235 Wp = 91
88949
YDOT = -5367
714955 meter/sec RA = 333
27156 deg
ZDOT = -3803
128900 TA = 138
75554
MA = 138
68049
Ha = 222
085 n
mi
Hp = 213
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17435294
74 X = -5282935
75
Y = -3228954
77 feet Y = -1043437
78 meter
Z = -13468678
20 Z = -4130992
67
XDOT = 12879
170720 XDOT = 4003
776796
YDOT = -17610
613368 feet/sec YDOT = -5323
379007 meter/sec
ZDOT = -12477
457021 ZDOT = -3783
869726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6778229
81 X = 2066004
45
Y = -16290720
76 feet Y = -4965411
69 meter
Z = -13582671
37 Z = -4139998
23
XDOT = 13331
937491 XDOT = 4063
574547
YDOT = 15855
904152 feet/sec YDOT = 4832
879586 meter/sec
ZDOT = -12391
064770 ZDOT = -3776
796542
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 17325
57334014
00016717 00000-0 10270-3 0 9013
2 25544 51
6383 333
7328 0004005 136
7508 223
3960 15
54175550 6229
Satellite: ISS
Catalog Number: 25544
Epoch time: 17325
57334014 = yrday
fracday
Element set: 901
Inclination: 51
6383 deg
RA of node: 333
7328 deg
Eccentricity:
0004005
Arg of perigee: 136
7508 deg
Mean anomaly: 223
3960 deg
Mean motion: 15
54175550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 622
Checksum: 286
Coasting Arc #3 (Orbit 637)
---------------------------------------
Vector Time (GMT): 2017/326/13:12:23
285
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4115522
54 A = 6778607
19 meter
Y = 2100908
29 meter E =
0009874
Z = 4955071
30 I = 51
42883
XDOT = -5218
254433 Wp = 129
28546
YDOT = 5210
990901 meter/sec RA = 328
26569 deg
ZDOT = 2115
733000 TA = 300
01167
MA = 300
10962
Ha = 221
903 n
mi
Hp = 213
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13502370
54 X = 4067654
05
Y = 6892743
74 feet Y = 2146662
89 meter
Z = 16256795
60 Z = 4974947
44
XDOT = -17120
257325 XDOT = -5286
414656
YDOT = 17096
426842 feet/sec YDOT = 5152
255564 meter/sec
ZDOT = 6941
381233 ZDOT = 2090
218725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9335220
54 X = -2845375
22
Y = 11824368
29 feet Y = 3604067
46 meter
Z = 16344580
19 Z = 4981828
04
XDOT = -12625
218326 XDOT = -3848
166546
YDOT = -19445
127778 feet/sec YDOT = -5926
874947 meter/sec
ZDOT = 6827
278551 ZDOT = 2080
954502
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 17326
60212907
00016717 00000-0 10270-3 0 9025
2 25544 51
6387 328
6040 0003867 140
2566 219
8871 15
54189927 6387
Satellite: ISS
Catalog Number: 25544
Epoch time: 17326
60212907 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 328
6040 deg
Eccentricity:
0003867
Arg of perigee: 140
2566 deg
Mean anomaly: 219
8871 deg
Mean motion: 15
54189927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 638
Checksum: 326
Coasting Arc #4 (Orbit 652)
---------------------------------------
Vector Time (GMT): 2017/327/13:12:23
285
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2696866
70 A = 6777201
11 meter
Y = -3270131
40 meter E =
0017424
Z = -5302931
71 I = 51
39650
XDOT = 6044
639751 Wp = 98
82569
YDOT = -4694
999056 meter/sec RA = 323
25036 deg
ZDOT = -181
962338 TA = 169
44980
MA = 169
41320
Ha = 221
992 n
mi
Hp = 213
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8847987
85 X = -2634339
38
Y = -10728777
55 feet Y = -3299939
64 meter
Z = -17398069
92 Z = -5315880
78
XDOT = 19831
495247 XDOT = 6097
575132
YDOT = -15403
540210 feet/sec YDOT = -4627
107774 meter/sec
ZDOT = -596
989299 ZDOT = -152
470685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12092209
79 X = 3685705
54
Y = -6722389
67 feet Y = -2048984
37 meter
Z = -17454922
89 Z = -5320260
50
XDOT = 11207
286134 XDOT = 3415
980814
YDOT = 21341
314186 feet/sec YDOT = 6504
832564 meter/sec
ZDOT = -465
345158 ZDOT = -141
837204
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 17327
56661513
00016717 00000-0 10270-3 0 9033
2 25544 51
6386 323
7955 0003862 142
8134 217
3286 15
54185280 6539
Satellite: ISS
Catalog Number: 25544
Epoch time: 17327
56661513 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 323
7955 deg
Eccentricity:
0003862
Arg of perigee: 142
8134 deg
Mean anomaly: 217
3286 deg
Mean motion: 15
54185280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 653
Checksum: 316
Coasting Arc #5 (Orbit 668)
---------------------------------------
Vector Time (GMT): 2017/328/13:12:23
285
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1204641
76 A = 6778198
00 meter
Y = 4342362
61 meter E =
0006470
Z = 5057637
40 I = 51
37406
XDOT = -6408
549722 Wp = 90
64138
YDOT = 3834
033115 meter/sec RA = 318
23300 deg
ZDOT = -1763
515535 TA = 16
47756
MA = 16
45654
Ha = 221
812 n
mi
Hp = 213
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3952236
73 X = 1131426
96
Y = 14246596
47 feet Y = 4355424
07 meter
Z = 16593298
56 Z = 5063311
67
XDOT = -21025
425597 XDOT = -6442
380218
YDOT = 12578
848801 feet/sec YDOT = 3762
179278 meter/sec
ZDOT = -5785
812122 ZDOT = -1794
728590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14676124
20 X = -4473282
65
Y = 1544885
58 feet Y = 470881
12 meter
Z = 16617699
92 Z = 5065074
94
XDOT = -8993
672470 XDOT = -2741
271369
YDOT = -21639
744821 feet/sec YDOT = -6595
794221 meter/sec
ZDOT = -5924
929999 ZDOT = -1805
918664
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 17328
59539752
00016717 00000-0 10270-3 0 9047
2 25544 51
6383 318
6667 0003771 148
0593 212
0789 15
54206031 6690
Satellite: ISS
Catalog Number: 25544
Epoch time: 17328
59539752 = yrday
fracday
Element set: 904
Inclination: 51
6383 deg
RA of node: 318
6667 deg
Eccentricity:
0003771
Arg of perigee: 148
0593 deg
Mean anomaly: 212
0789 deg
Mean motion: 15
54206031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 669
Checksum: 331
Coasting Arc #6 (Orbit 668)
---------------------------------------
Vector Time (GMT): 2017/328/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5409873
57 A = 6781964
60 meter
Y = 481535
75 meter E =
0009119
Z = -4068966
02 I = 51
38690
XDOT = 2331
051958 Wp = 94
38579
YDOT = -6205
186548 meter/sec RA = 318
16244 deg
ZDOT = -3841
721421 TA = 135
72925
MA = 135
65627
Ha = 221
832 n
mi
Hp = 213
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17748929
04 X = -5395090
89
Y = 1579841
70 feet Y = 421121
74 meter
Z = -13349626
07 Z = -4095209
88
XDOT = 7647
808262 XDOT = 2418
928177
YDOT = -20358
223582 feet/sec YDOT = -6178
627565 meter/sec
ZDOT = -12604
072905 ZDOT = -3830
184681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1220412
93 X = -371981
86
Y = -17689186
30 feet Y = -5391663
99 meter
Z = -13466112
21 Z = -4104471
00
XDOT = 18908
509216 XDOT = 5763
313609
YDOT = 8230
530631 feet/sec YDOT = 2508
665736 meter/sec
ZDOT = -12551
808549 ZDOT = -3825
791246
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 17328
59539777
00016717 00000-0 10270-3 0 9055
2 25544 51
6388 318
6663 0003779 146
9408 213
1981 15
54206799 6698
Satellite: ISS
Catalog Number: 25544
Epoch time: 17328
59539777 = yrday
fracday
Element set: 905
Inclination: 51
6388 deg
RA of node: 318
6663 deg
Eccentricity:
0003779
Arg of perigee: 146
9408 deg
Mean anomaly: 213
1981 deg
Mean motion: 15
54206799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 669
Checksum: 367
Coasting Arc #7 (Orbit 684)
---------------------------------------
Vector Time (GMT): 2017/329/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4551998
42 A = 6778518
64 meter
Y = 914292
87 meter E =
0009593
Z = 4935005
48 I = 51
35298
XDOT = -3635
494992 Wp = 133
76642
YDOT = 6401
293476 meter/sec RA = 313
15182 deg
ZDOT = 2158
247578 TA = 295
07014
MA = 295
16968
Ha = 221
572 n
mi
Hp = 213
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14934378
01 X = 4517464
15
Y = 2999648
54 feet Y = 965003
11 meter
Z = 16190962
86 Z = 4957034
07
XDOT = -11927
477007 XDOT = -3717
289587
YDOT = 21001
619017 feet/sec YDOT = 6360
181447 meter/sec
ZDOT = 7080
864758 ZDOT = 2140
388912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3046506
36 X = -928575
14
Y = 14818373
09 feet Y = 4516640
12 meter
Z = 16288506
19 Z = 4964736
69
XDOT = -19884
811141 XDOT = -6060
890436
YDOT = -11815
971697 feet/sec YDOT = -3601
508173 meter/sec
ZDOT = 7000
538652 ZDOT = 2133
764181
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 17329
62417430
00016717 00000-0 10270-3 0 9062
2 25544 51
6398 313
5381 0003681 153
6911 206
4429 15
54245917 6851
Satellite: ISS
Catalog Number: 25544
Epoch time: 17329
62417430 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 313
5381 deg
Eccentricity:
0003681
Arg of perigee: 153
6911 deg
Mean anomaly: 206
4429 deg
Mean motion: 15
54245917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 685
Checksum: 317
Coasting Arc #8 (Orbit 699)
---------------------------------------
Vector Time (GMT): 2017/330/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3488393
92 A = 6777127
62 meter
Y = -2421264
08 meter E =
0016686
Z = -5296054
85 I = 51
32588
XDOT = 4584
827930 Wp = 99
68905
YDOT = -6128
132803 meter/sec RA = 308
13037 deg
ZDOT = -221
601350 TA = 168
20597
MA = 168
16684
Ha = 221
725 n
mi
Hp = 213
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11444861
95 X = -3435333
53
Y = -7943779
78 feet Y = -2459976
83 meter
Z = -17375508
02 Z = -5312871
76
XDOT = 15042
086384 XDOT = 4654
090040
YDOT = -20105
422583 feet/sec YDOT = -6076
474849 meter/sec
ZDOT = -727
038551 ZDOT = -199
161411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7784324
28 X = 2372662
04
Y = -11441585
97 feet Y = -3487395
40 meter
Z = -17449675
84 Z = -5318661
20
XDOT = 19481
801989 XDOT = 5938
053246
YDOT = 14193
223701 feet/sec YDOT = 4326
094584 meter/sec
ZDOT = -626
454974 ZDOT = -190
943476
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 17330
58865005
00016717 00000-0 10270-3 0 9075
2 25544 51
6395 308
7288 0003639 154
3180 205
8154 15
54212025 7009
Satellite: ISS
Catalog Number: 25544
Epoch time: 17330
58865005 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 308
7288 deg
Eccentricity:
0003639
Arg of perigee: 154
3180 deg
Mean anomaly: 205
8154 deg
Mean motion: 15
54212025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 700
Checksum: 298
Coasting Arc #9 (Orbit 715)
---------------------------------------
Vector Time (GMT): 2017/331/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2325469
89 A = 6778110
07 meter
Y = 3855271
88 meter E =
0005763
Z = 5061664
47 I = 51
30965
XDOT = -5173
563870 Wp = 92
95705
YDOT = 5395
388029 meter/sec RA = 303
10871 deg
ZDOT = -1731
160446 TA = 13
85249
MA = 13
83669
Ha = 221
572 n
mi
Hp = 213
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7629494
38 X = 2257598
99
Y = 12648529
80 feet Y = 3880897
28 meter
Z = 16606510
74 Z = 5072796
25
XDOT = -16973
634743 XDOT = -5225
102803
YDOT = 17701
404293 feet/sec YDOT = 5337
245566 meter/sec
ZDOT = -5679
660256 ZDOT = -1756
417392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12408114
14 X = -3781993
19
Y = 7912835
01 feet Y = 2411832
11 meter
Z = 16655222
46 Z = 5076511
81
XDOT = -17645
838348 XDOT = -5378
451528
YDOT = -15468
213514 feet/sec YDOT = -4714
711479 meter/sec
ZDOT = -5792
597797 ZDOT = -1765
583809
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 17331
61741988
00016717 00000-0 10270-3 0 9084
2 25544 51
6393 303
6007 0003632 157
8894 202
2416 15
54219766 7161
Satellite: ISS
Catalog Number: 25544
Epoch time: 17331
61741988 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 303
6007 deg
Eccentricity:
0003632
Arg of perigee: 157
8894 deg
Mean anomaly: 202
2416 deg
Mean motion: 15
54219766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 716
Checksum: 319
Coasting Arc #10 (Orbit 730)
---------------------------------------
Vector Time (GMT): 2017/332/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1170159
88 A = 6781207
38 meter
Y = -5121808
24 meter E =
0011014
Z = -4299293
61 I = 51
30317
XDOT = 5394
769003 Wp = 125
10692
YDOT = -4164
668422 meter/sec RA = 298
09033 deg
ZDOT = 3493
259198 TA = 180
65582
MA = 180
65727
Ha = 221
570 n
mi
Hp = 213
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3839107
21 X = -1091915
31
Y = -16803832
79 feet Y = -5134456
21 meter
Z = -14105293
99 Z = -4304788
00
XDOT = 17699
373368 XDOT = 5423
969697
YDOT = -13663
610309 feet/sec YDOT = -4104
177209 meter/sec
ZDOT = 11460
824142 ZDOT = 3519
536568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16603468
76 X = 5060737
28
Y = -4557280
61 feet Y = -1389059
13 meter
Z = -14128796
06 Z = -4306457
04
XDOT = 14169
310618 XDOT = 4318
805876
YDOT = 15729
255361 feet/sec YDOT = 4794
277034 meter/sec
ZDOT = 11578
066376 ZDOT = 3528
994632
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 17332
58188668
00016717 00000-0 10270-3 0 9092
2 25544 51
6395 298
7919 0003584 162
9959 197
1315 15
54223023 7312
Satellite: ISS
Catalog Number: 25544
Epoch time: 17332
58188668 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 298
7919 deg
Eccentricity:
0003584
Arg of perigee: 162
9959 deg
Mean anomaly: 197
1315 deg
Mean motion: 15
54223023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 731
Checksum: 348
Coasting Arc #11 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2017/333/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 69846
68 A = 6785060
41 meter
Y = 6054836
97 meter E =
0014707
Z = 3043306
94 I = 51
30221
XDOT = -5340
774142 Wp = 108
76148
YDOT = 2529
551127 meter/sec RA = 293
08110 deg
ZDOT = -4895
320257 TA = 36
11169
MA = 36
01246
Ha = 221
446 n
mi
Hp = 214
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 229155
76 X = -12648
49
Y = 19864950
70 feet Y = 6055156
73 meter
Z = 9984602
83 Z = 3043445
98
XDOT = -17522
224875 XDOT = -5344
883823
YDOT = 8299
052254 feet/sec YDOT = 2469
804050 meter/sec
ZDOT = -16060
761997 ZDOT = -4921
274492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19812142
60 X = -6038741
06
Y = 1468229
12 feet Y = 447516
24 meter
Z = 9984206
60 Z = 3043186
17
XDOT = -9316
829319 XDOT = -2839
769576
YDOT = -15388
832237 feet/sec YDOT = -4690
516066 meter/sec
ZDOT = -16176
288246 ZDOT = -4930
532657
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 17333
61064644
00016717 00000-0 10270-3 0 9106
2 25544 51
6400 293
6624 0003486 165
0327 195
0929 15
54245309 7476
Satellite: ISS
Catalog Number: 25544
Epoch time: 17333
61064644 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 293
6624 deg
Eccentricity:
0003486
Arg of perigee: 165
0327 deg
Mean anomaly: 195
0929 deg
Mean motion: 15
54245309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 306
Coasting Arc #12 (Orbit 747)
---------------------------------------
Vector Time (GMT): 2017/333/15:52:54
761
Vector Time (MET): N/A
Weight (LBS) : 934805
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3043708
58 A = 6778563
50 meter
Y = -3303024
27 meter E =
0014453
Z = -5089796
16 I = 51
27903
XDOT = 4054
504569 Wp = 115
16235
YDOT = -6282
767162 meter/sec RA = 292
64378 deg
ZDOT = 1650
259561 TA = 170
88590
MA = 170
85963
Ha = 221
487 n
mi
Hp = 214
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9985920
53 X = -2981822
87
Y = -10836693
80 feet Y = -3336714
98 meter
Z = -16698806
31 Z = -5104431
58
XDOT = 13302
180344 XDOT = 4116
442515
YDOT = -20612
753156 feet/sec YDOT = -6237
080635 meter/sec
ZDOT = 5414
237406 ZDOT = 1670
105776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2942456
34 X = 896860
69
Y = -14364577
57 feet Y = -4378323
24 meter
Z = -16763160
07 Z = -5109411
19
XDOT = 23423
916262 XDOT = 7139
609677
YDOT = -1632
986754 feet/sec YDOT = -497
734363 meter/sec
ZDOT = 5503
302402 ZDOT = 1677
406572
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 17333
67494380
00016717 00000-0 10270-3 0 9117
2 25544 51
6418 293
3426 0003251 180
4344 179
6807 15
54034934 7486
Satellite: ISS
Catalog Number: 25544
Epoch time: 17333
67494380 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 293
3426 deg
Eccentricity:
0003251
Arg of perigee: 180
4344 deg
Mean anomaly: 179
6807 deg
Mean motion: 15
54034934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 748
Checksum: 317
Coasting Arc #13 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2017/334/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 934805
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4061248
97 A = 6777649
82 meter
Y = -1244963
89 meter E =
0014988
Z = -5294088
61 I = 51
26305
XDOT = 2329
653156 Wp = 101
81433
YDOT = -7294
264326 meter/sec RA = 288
16278 deg
ZDOT = -75
010434 TA = 167
48477
MA = 167
44751
Ha = 221
420 n
mi
Hp = 214
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13324307
66 X = -4021308
98
Y = -4084527
19 feet Y = -1290156
07 meter
Z = -17369057
11 Z = -5313720
35
XDOT = 7643
219017 XDOT = 2411
410801
YDOT = -23931
313405 feet/sec YDOT = -7267
755415 meter/sec
ZDOT = -246
097225 ZDOT = -63
495104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4088480
43 X = 1246168
84
Y = -13209091
13 feet Y = -4026130
98 meter
Z = -17455913
64 Z = -5320562
48
XDOT = 22966
678607 XDOT = 7000
243639
YDOT = 7351
007484 feet/sec YDOT = 2240
587081 meter/sec
ZDOT = -193
818964 ZDOT = -59
076020
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 17334
57522861
00016717 00000-0 10270-3 0 9124
2 25544 51
6395 288
8543 0003233 183
7968 176
3161 15
54028562 7620
Satellite: ISS
Catalog Number: 25544
Epoch time: 17334
57522861 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 288
8543 deg
Eccentricity:
0003233
Arg of perigee: 183
7968 deg
Mean anomaly: 176
3161 deg
Mean motion: 15
54028562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 328
Coasting Arc #14 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2017/335/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 934805
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3472964
08 A = 6778698
92 meter
Y = 2908654
80 meter E =
0004009
Z = 5039210
38 I = 51
25806
XDOT = -3071
763610 Wp = 91
28427
YDOT = 6794
063541 meter/sec RA = 283
13909 deg
ZDOT = -1803
383023 TA = 16
26397
MA = 16
25111
Ha = 221
185 n
mi
Hp = 214
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11394239
12 X = 3415702
02
Y = 9542830
70 feet Y = 2947171
42 meter
Z = 16532842
45 Z = 5055942
43
XDOT = -10077
964599 XDOT = -3138
748193
YDOT = 22290
234714 feet/sec YDOT = 6759
338543 meter/sec
ZDOT = -5916
610969 ZDOT = -1818
467387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9350850
95 X = -2850139
37
Y = 11446077
16 feet Y = 3488764
32 meter
Z = 16606567
57 Z = 5061681
80
XDOT = -21622
642690 XDOT = -6590
581492
YDOT = -8976
280761 feet/sec YDOT = -2735
970376 meter/sec
ZDOT = -5984
626597 ZDOT = -1824
114187
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 17335
60412144
00016717 00000-0 10270-3 0 9132
2 25544 51
6401 283
7269 0003237 188
9988 171
1107 15
54041796 7784
Satellite: ISS
Catalog Number: 25544
Epoch time: 17335
60412144 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 283
7269 deg
Eccentricity:
0003237
Arg of perigee: 188
9988 deg
Mean anomaly: 171
1107 deg
Mean motion: 15
54041796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 320
Coasting Arc #15 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2017/336/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 934805
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2846543
72 A = 6781682
13 meter
Y = -4422714
75 meter E =
0009500
Z = -4291295
07 I = 51
26246
XDOT = 3655
881623 Wp = 129
76111
YDOT = -5749
199827 meter/sec RA = 278
11848 deg
ZDOT = 3499
428320 TA = 176
09764
MA = 176
09023
Ha = 221
235 n
mi
Hp = 214
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9339054
20 X = -2776030
69
Y = -14510219
00 feet Y = -4454152
14 meter
Z = -14079052
07 Z = -4304952
10
XDOT = 11994
362281 XDOT = 3702
900105
YDOT = -18862
204158 feet/sec YDOT = -5708
054645 meter/sec
ZDOT = 11481
064043 ZDOT = 3517
301616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14186609
73 X = 4324078
65
Y = -9737339
29 feet Y = -2967941
02 meter
Z = -14138897
55 Z = -4309535
97
XDOT = 18547
863278 XDOT = 5653
388727
YDOT = 10231
895417 feet/sec YDOT = 3118
681723 meter/sec
ZDOT = 11561
272340 ZDOT = 3523
875809
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 17336
56870237
00016717 00000-0 10270-3 0 9140
2 25544 51
6408 278
9182 0003201 191
8767 168
2311 15
54055560 7935
Satellite: ISS
Catalog Number: 25544
Epoch time: 17336
56870237 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 278
9182 deg
Eccentricity:
0003201
Arg of perigee: 191
8767 deg
Mean anomaly: 168
2311 deg
Mean motion: 15
54055560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 793
Checksum: 319
Coasting Arc #16 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2017/337/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 934805
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2173270
12 A = 6785472
57 meter
Y = 5629846
64 meter E =
0012837
Z = 3086668
01 I = 51
27150
XDOT = -4132
845332 Wp = 109
29668
YDOT = 4265
306927 meter/sec RA = 273
10900 deg
ZDOT = -4857
338436 TA = 34
99057
MA = 34
90628
Ha = 221
104 n
mi
Hp = 215
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7130151
32 X = 2095160
33
Y = 18470625
47 feet Y = 5653712
58 meter
Z = 10126863
56 Z = 3097036
16
XDOT = -13559
203846 XDOT = -4156
638941
YDOT = 13993
789130 feet/sec YDOT = 4218
958095 meter/sec
ZDOT = -15936
149726 ZDOT = -4877
472266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18084044
66 X = -5512016
81
Y = 8003467
83 feet Y = 2439456
99 meter
Z = 10171934
93 Z = 3100405
77
XDOT = -14081
802796 XDOT = -4292
133492
YDOT = -11398
488783 feet/sec YDOT = -3474
259381 meter/sec
ZDOT = -16026
141006 ZDOT = -4884
767779
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 17337
59758408
00016717 00000-0 10270-3 0 9150
2 25544 51
6409 273
7906 0003165 195
1283 164
9775 15
54052509 8097
Satellite: ISS
Catalog Number: 25544
Epoch time: 17337
59758408 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 273
7906 deg
Eccentricity:
0003165
Arg of perigee: 195
1283 deg
Mean anomaly: 164
9775 deg
Mean motion: 15
54052509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 341
Coasting Arc #17 (Orbit 823)
---------------------------------------
Vector Time (GMT): 2017/338/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 919827
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4168637
04 A = 6778268
57 meter
Y = -1543464
89 meter E =
0013602
Z = -5129150
13 I = 51
24710
XDOT = 944
273324 Wp = 114
53483
YDOT = -7455
550065 meter/sec RA = 268
16261 deg
ZDOT = 1473
629377 TA = 169
76399
MA = 169
73626
Ha = 221
042 n
mi
Hp = 214
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13676630
70 X = -4126152
53
Y = -5063861
17 feet Y = -1589843
28 meter
Z = -16827920
39 Z = -5149297
36
XDOT = 3098
009593 XDOT = 1020
414833
YDOT = -24460
466093 feet/sec YDOT = -7444
564998 meter/sec
ZDOT = 4834
742050 ZDOT = 1478
400482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5024691
39 X = 1531525
93
Y = -13580800
19 feet Y = -4139427
90 meter
Z = -16917037
70 Z = -5156313
09
XDOT = 23478
788495 XDOT = 7156
334733
YDOT = 2626
533727 feet/sec YDOT = 800
567480 meter/sec
ZDOT = 4857
104473 ZDOT = 1480
445443
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
56215623
00016717 00000-0 10270-3 0 9166
2 25544 51
6412 268
9828 0003162 200
3063 159
7964 15
54065193 8244
Satellite: ISS
Catalog Number: 25544
Epoch time: 17338
56215623 = yrday
fracday
Element set: 916
Inclination: 51
6412 deg
RA of node: 268
9828 deg
Eccentricity:
0003162
Arg of perigee: 200
3063 deg
Mean anomaly: 159
7964 deg
Mean motion: 15
54065193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 824
Checksum: 314
Coasting Arc #18 (Orbit 828)
---------------------------------------
Vector Time (GMT): 2017/338/19:53:38
000
Vector Time (MET): N/A
Weight (LBS) : 919827
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3176291
28 A = 6781737
18 meter
Y = -4223849
27 meter E =
0010258
Z = 4246782
64 I = 51
25546
XDOT = 3196
319013 Wp = 126
81263
YDOT = 5993
966318 meter/sec RA = 266
79124 deg
ZDOT = 3558
948446 TA = 286
61699
MA = 286
72960
Ha = 220
974 n
mi
Hp = 215
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10420903
14 X = 3202658
38
Y = -13857773
21 feet Y = -4188182
90 meter
Z = 13933013
91 Z = 4262275
81
XDOT = 10486
610934 XDOT = 3111
767479
YDOT = 19665
243827 feet/sec YDOT = 6029
236555 meter/sec
ZDOT = 11676
340046 ZDOT = 3574
270726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7398417
44 X = 2255037
63
Y = -15619147
36 feet Y = -4760716
11 meter
Z = 14002415
24 Z = 4267936
17
XDOT = 12939
254674 XDOT = 3943
884825
YDOT = 16692
019547 feet/sec YDOT = 5087
727558 meter/sec
ZDOT = 11743
344192 ZDOT = 3579
371310
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
88367758
00016717 00000-0 10270-3 0 9179
2 25544 51
6375 267
3764 0003528 201
7632 158
3371 15
54082757 8294
Satellite: ISS
Catalog Number: 25544
Epoch time: 17338
88367758 = yrday
fracday
Element set: 917
Inclination: 51
6375 deg
RA of node: 267
3764 deg
Eccentricity:
0003528
Arg of perigee: 201
7632 deg
Mean anomaly: 158
3371 deg
Mean motion: 15
54082757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 829
Checksum: 347
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