[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 11th 2018
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) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
222/19:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 213
6
227/00:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 695)
---------------------------------------
Vector Time (GMT): 2018/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1764025
23 A = 6783126
08 meter
Y = -5118773
72 meter E =
0015598
Z = 4078820
78 I = 52
00129
XDOT = 4629
079793 Wp = 65
02949
YDOT = -4714
669702 meter/sec RA = 107
03987 deg
ZDOT = -3896
700647 TA = 65
19036
MA = 65
02820
Ha = 223
224 n
mi
Hp = 213
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5787484
35 X = -1726466
87
Y = -16793877
04 feet Y = -5138290
47 meter
Z = 13381957
94 Z = 4070342
93
XDOT = 15187
269661 XDOT = 4700
384156
YDOT = -15468
076449 feet/sec YDOT = -4662
505254 meter/sec
ZDOT = -12784
450941 ZDOT = -3874
041765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6857988
02 X = -2090314
75
Y = 16416395
10 feet Y = 5003717
23 meter
Z = 13344513
93 Z = 4067407
84
XDOT = -20501
964348 XDOT = -6248
998733
YDOT = 1792
523131 feet/sec YDOT = 546
361050 meter/sec
ZDOT = -12682
147225 ZDOT = -3865
518474
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 18222
54112969
00016717 00000-0 10270-3 0 9009
2 25544 51
6423 107
8301 0005699 40
9515 319
2064 15
53848644 6960
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
54112969 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 107
8301 deg
Eccentricity:
0005699
Arg of perigee: 40
9515 deg
Mean anomaly: 319
2064 deg
Mean motion: 15
53848644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 696
Checksum: 313
Coasting Arc #2 (Orbit 700)
---------------------------------------
Vector Time (GMT): 2018/222/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4286288
61 A = 6778579
52 meter
Y = 116789
21 meter E =
0007180
Z = 5243786
39 I = 51
98729
XDOT = 1170
724682 Wp = 77
84521
YDOT = -7500
204990 meter/sec RA = 105
51906 deg
ZDOT = 1124
177002 TA = 1
44004
MA = 1
43798
Ha = 223
264 n
mi
Hp = 213
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14062626
66 X = -4312746
93
Y = 383166
69 feet Y = 68708
82 meter
Z = 17204023
60 Z = 5222901
35
XDOT = 3840
960243 XDOT = 1249
046512
YDOT = -24606
971751 feet/sec YDOT = -7486
675257 meter/sec
ZDOT = 3688
244757 ZDOT = 1130
053761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4287546
90 X = 1306844
29
Y = -13518114
15 feet Y = -4120321
19 meter
Z = 17110238
01 Z = 5215200
55
XDOT = 21007
137402 XDOT = 6402
975480
YDOT = 11364
956606 feet/sec YDOT = 3464
038774 meter/sec
ZDOT = 3715
540473 ZDOT = 1132
496736
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 18222
86270376
00016717 00000-0 10270-3 0 9012
2 25544 51
6405 106
2219 0005272 46
0385 314
1201 15
53849062 7019
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
86270376 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 106
2219 deg
Eccentricity:
0005272
Arg of perigee: 46
0385 deg
Mean anomaly: 314
1201 deg
Mean motion: 15
53849062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 701
Checksum: 275
Coasting Arc #3 (Orbit 715)
---------------------------------------
Vector Time (GMT): 2018/223/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3939099
22 A = 6778359
09 meter
Y = 1533672
13 meter E =
0018853
Z = -5314753
86 I = 51
99367
XDOT = -1930
363309 Wp = 83
90340
YDOT = 7373
675873 meter/sec RA = 100
54786 deg
ZDOT = 701
175241 TA = 192
74892
MA = 192
79666
Ha = 223
222 n
mi
Hp = 213
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12923553
87 X = 3947472
12
Y = 5031732
72 feet Y = 1577768
74 meter
Z = -17436856
51 Z = -5295599
23
XDOT = -6333
212957 XDOT = -2016
080174
YDOT = 24191
849978 feet/sec YDOT = 7351
609936 meter/sec
ZDOT = 2300
443703 ZDOT = 691
590333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8844769
21 X = -2695885
66
Y = 10820912
84 feet Y = 3298214
23 meter
Z = -17351035
90 Z = -5288595
74
XDOT = -20218
069157 XDOT = -6162
467479
YDOT = -12929
099313 feet/sec YDOT = -3940
789470 meter/sec
ZDOT = 2256
505111 ZDOT = 687
782758
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 18223
82742664
00016717 00000-0 10270-3 0 9024
2 25544 51
6399 101
4165 0005379 51
0223 309
1408 15
53838966 7163
Satellite: ISS
Catalog Number: 25544
Epoch time: 18223
82742664 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 101
4165 deg
Eccentricity:
0005379
Arg of perigee: 51
0223 deg
Mean anomaly: 309
1408 deg
Mean motion: 15
53838966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 716
Checksum: 311
Coasting Arc #4 (Orbit 731)
---------------------------------------
Vector Time (GMT): 2018/224/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3514781
93 A = 6780306
59 meter
Y = -3138669
50 meter E =
0012440
Z = 4868709
43 I = 52
00506
XDOT = 2606
021839 Wp = 57
79248
YDOT = -6778
011173 meter/sec RA = 95
57679 deg
ZDOT = -2477
140451 TA = 56
45164
MA = 56
33290
Ha = 223
425 n
mi
Hp = 213
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11531436
77 X = -3503072
30
Y = -10297472
12 feet Y = -3177908
67 meter
Z = 15973456
13 Z = 4851664
74
XDOT = 8549
940418 XDOT = 2693
654107
YDOT = -22237
569464 feet/sec YDOT = -6748
378895 meter/sec
ZDOT = -8127
101216 ZDOT = -2464
268642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13274183
00 X = 4045970
98
Y = -8076819
40 feet Y = -2461814
55 meter
Z = 15897305
46 Z = 4845498
71
XDOT = 18115
717834 XDOT = 5521
670796
YDOT = 13820
377861 feet/sec YDOT = 4212
451172 meter/sec
ZDOT = -8068
467849 ZDOT = -2459
269001
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 18224
85646271
00016717 00000-0 10270-3 0 9036
2 25544 51
6401 96
2882 0005392 55
1285 305
0374 15
53802016 7324
Satellite: ISS
Catalog Number: 25544
Epoch time: 18224
85646271 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 96
2882 deg
Eccentricity:
0005392
Arg of perigee: 55
1285 deg
Mean anomaly: 305
0374 deg
Mean motion: 15
53802016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 732
Checksum: 294
Coasting Arc #5 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2018/225/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3081554
43 A = 6783472
43 meter
Y = 4529838
44 meter E =
0011063
Z = -4008840
11 I = 52
01887
XDOT = -3186
300267 Wp = 85
49741
YDOT = 5700
643746 meter/sec RA = 90
61405 deg
ZDOT = 4002
563515 TA = 225
98272
MA = 226
07393
Ha = 223
310 n
mi
Hp = 213
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10110086
72 X = 3050143
95
Y = 14861674
69 feet Y = 4564122
75 meter
Z = -13152362
56 Z = -3993947
73
XDOT = -10453
741033 XDOT = -3269
251591
YDOT = 18702
899429 feet/sec YDOT = 5664
548666 meter/sec
ZDOT = 13131
770061 ZDOT = 3986
884202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17114979
04 X = -5216645
61
Y = 5648061
45 feet Y = 1721529
13 meter
Z = -13086052
24 Z = -3988628
72
XDOT = -14610
160071 XDOT = -4453
176790
YDOT = -14090
817174 feet/sec YDOT = -4294
881075 meter/sec
ZDOT = 13060
654295 ZDOT = 3980
887429
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 18225
82117960
00016717 00000-0 10270-3 0 9043
2 25544 51
6409 91
4817 0005345 56
9273 303
2392 15
53826067 7479
Satellite: ISS
Catalog Number: 25544
Epoch time: 18225
82117960 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 91
4817 deg
Eccentricity:
0005345
Arg of perigee: 56
9273 deg
Mean anomaly: 303
2392 deg
Mean motion: 15
53826067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 316
Coasting Arc #6 (Orbit 762)
---------------------------------------
Vector Time (GMT): 2018/226/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2570049
03 A = 6787105
13 meter
Y = -5646954
36 meter E =
0018045
Z = 2735990
82 I = 52
02952
XDOT = 3741
123559 Wp = 90
25532
YDOT = -4231
525672 meter/sec RA = 85
65975 deg
ZDOT = -5190
083795 TA = 58
95866
MA = 58
78162
Ha = 223
411 n
mi
Hp = 213
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8431919
39 X = -2520002
01
Y = -18526753
16 feet Y = -5675414
49 meter
Z = 8976347
85 Z = 2723628
40
XDOT = 12274
027424 XDOT = 3813
373913
YDOT = -13882
958240 feet/sec YDOT = -4189
286082 meter/sec
ZDOT = -17027
833972 ZDOT = -5171
735329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20104810
97 X = 6127946
38
Y = -3333955
79 feet Y = -1016189
72 meter
Z = 8921545
99 Z = 2719287
22
XDOT = 9905
380530 XDOT = 3019
159986
YDOT = 14129
238379 feet/sec YDOT = 4306
591858 meter/sec
ZDOT = -16944
908119 ZDOT = -5164
807995
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 18226
85021055
00016717 00000-0 10270-3 0 9057
2 25544 51
6402 86
3539 0005451 62
0841 298
0863 15
53816624 7633
Satellite: ISS
Catalog Number: 25544
Epoch time: 18226
85021055 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 86
3539 deg
Eccentricity:
0005451
Arg of perigee: 62
0841 deg
Mean anomaly: 298
0863 deg
Mean motion: 15
53816624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 763
Checksum: 304
Coasting Arc #7 (Orbit 765)
---------------------------------------
Vector Time (GMT): 2018/227/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3409666
62 A = 6783978
46 meter
Y = -4436878
92 meter E =
0016792
Z = 3825187
02 I = 52
01827
XDOT = 2770
652145 Wp = 74
76809
YDOT = -5780
276816 meter/sec RA = 84
71632 deg
ZDOT = -4215
272655 TA = 59
50859
MA = 59
34288
Ha = 223
428 n
mi
Hp = 213
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11186570
26 X = -3378379
28
Y = -14556689
36 feet Y = -4474833
07 meter
Z = 12549826
17 Z = 3808700
45
XDOT = 9090
066094 XDOT = 2855
558160
YDOT = -18964
162781 feet/sec YDOT = -5748
818905 meter/sec
ZDOT = -13829
634694 ZDOT = -4201
607517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -394361
87 X = -120201
50
Y = -18404340
75 feet Y = -5609643
06 meter
Z = 12476354
30 Z = 3802792
79
XDOT = 17323
223464 XDOT = 5280
118512
YDOT = -9748
222281 feet/sec YDOT = -2971
258151 meter/sec
ZDOT = -13767
542151 ZDOT = -4196
346848
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 18227
04315193
00016717 00000-0 10270-3 0 9069
2 25544 51
6395 85
3953 0005667 58
7025 301
4682 15
53859220 7668
Satellite: ISS
Catalog Number: 25544
Epoch time: 18227
04315193 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 85
3953 deg
Eccentricity:
0005667
Arg of perigee: 58
7025 deg
Mean anomaly: 301
4682 deg
Mean motion: 15
53859220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 766
Checksum: 321
Coasting Arc #8 (Orbit 780)
---------------------------------------
Vector Time (GMT): 2018/228/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3023080
84 A = 6787356
44 meter
Y = 5512492
26 meter E =
0010899
Z = -2556264
37 I = 52
02623
XDOT = -3429
503434 Wp = 57
44783
YDOT = 4333
013833 meter/sec RA = 79
76313 deg
ZDOT = 5310
322409 TA = 274
00998
MA = 274
13457
Ha = 223
451 n
mi
Hp = 213
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9918244
22 X = 2973630
80
Y = 18085604
53 feet Y = 5546021
86 meter
Z = -8386694
12 Z = -2541699
75
XDOT = -11251
651685 XDOT = -3503
495982
YDOT = 14215
924648 feet/sec YDOT = 4294
249227 meter/sec
ZDOT = 17422
317615 ZDOT = 5293
483375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2394906
54 X = -729967
51
Y = 20513557
41 feet Y = 6252532
30 meter
Z = -8321999
93 Z = -2536545
58
XDOT = -16017
314022 XDOT = -4882
077314
YDOT = 5137
381923 feet/sec YDOT = 1565
874010 meter/sec
ZDOT = 17346
147232 ZDOT = 5287
105676
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 18228
00786789
00016717 00000-0 10270-3 0 9070
2 25544 51
6401 80
5882 0005742 64
0347 296
1397 15
53867157 7813
Satellite: ISS
Catalog Number: 25544
Epoch time: 18228
00786789 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 80
5882 deg
Eccentricity:
0005742
Arg of perigee: 64
0347 deg
Mean anomaly: 296
1397 deg
Mean motion: 15
53867157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 781
Checksum: 337
Coasting Arc #9 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2018/229/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2496939
69 A = 6789759
36 meter
Y = -6228540
60 meter E =
0017320
Z = 997480
18 I = 52
02731
XDOT = 4094
756749 Wp = 107
77518
YDOT = -2605
055305 meter/sec RA = 74
81736 deg
ZDOT = -5937
193528 TA = 61
47528
MA = 61
30102
Ha = 223
504 n
mi
Hp = 213
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8192059
34 X = -2431950
04
Y = -20434844
48 feet Y = -6256099
70 meter
Z = 3272572
78 Z = 985509
02
XDOT = 13434
241303 XDOT = 4152
422394
YDOT = -8546
769372 feet/sec YDOT = -2558
942620 meter/sec
ZDOT = -19478
981391 ZDOT = -5917
162656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4823898
82 X = 1470324
36
Y = -21488750
98 feet Y = -6549771
30 meter
Z = 3219630
28 Z = 981343
31
XDOT = 14452
096974 XDOT = 4404
999158
YDOT = 299
673460 feet/sec YDOT = 91
340470 meter/sec
ZDOT = -19388
694666 ZDOT = -5909
674134
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 18229
03689461
00016717 00000-0 10270-3 0 9084
2 25544 51
6404 75
4603 0005797 66
5454 293
6308 15
53840950 7979
Satellite: ISS
Catalog Number: 25544
Epoch time: 18229
03689461 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 75
4603 deg
Eccentricity:
0005797
Arg of perigee: 66
5454 deg
Mean anomaly: 293
6308 deg
Mean motion: 15
53840950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 337
Coasting Arc #10 (Orbit 812)
---------------------------------------
Vector Time (GMT): 2018/230/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1880784
01 A = 6790024
47 meter
Y = 6488378
45 meter E =
0018791
Z = 597509
96 I = 52
01883
XDOT = -4702
877105 Wp = 56
62908
YDOT = 798
424958 meter/sec RA = 69
87493 deg
ZDOT = 6007
572487 TA = 309
78870
MA = 309
95402
Ha = 223
554 n
mi
Hp = 213
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6170551
21 X = 1805187
02
Y = 21287330
87 feet Y = 6508988
00 meter
Z = 1960334
50 Z = 606462
40
XDOT = -15429
386829 XDOT = -4740
637202
YDOT = 2619
504454 feet/sec YDOT = 745
623073 meter/sec
ZDOT = 19709
883486 ZDOT = 5984
635980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6638457
99 X = -2023401
99
Y = 21142404
14 feet Y = 6444204
78 meter
Z = 1999672
94 Z = 609500
31
XDOT = -12872
923273 XDOT = -3923
667014
YDOT = -5934
571722 feet/sec YDOT = -1808
857461 meter/sec
ZDOT = 19606
783591 ZDOT = 5976
147639
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 18230
06591965
00016717 00000-0 10270-3 0 9091
2 25544 51
6407 70
3334 0005862 68
8214 291
3564 15
53837041 8134
Satellite: ISS
Catalog Number: 25544
Epoch time: 18230
06591965 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 70
3334 deg
Eccentricity:
0005862
Arg of perigee: 68
8214 deg
Mean anomaly: 291
3564 deg
Mean motion: 15
53837041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 813
Checksum: 309
Coasting Arc #11 (Orbit 827)
---------------------------------------
Vector Time (GMT): 2018/231/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1071318
07 A = 6788153
60 meter
Y = -6334964
90 meter E =
0010083
Z = -2193665
13 I = 51
99893
XDOT = 5227
103036 Wp = 106
33325
YDOT = 1015
513684 meter/sec RA = 64
92953 deg
ZDOT = -5509
088838 TA = 97
87452
MA = 97
76005
Ha = 223
536 n
mi
Hp = 213
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3514823
06 X = -989743
53
Y = -20784005
58 feet Y = -6346489
01 meter
Z = -7197064
08 Z = -2198671
05
XDOT = 17149
288176 XDOT = 5242
118840
YDOT = 3331
737808 feet/sec YDOT = 1074
050724 meter/sec
ZDOT = -18074
438444 ZDOT = -5483
661106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8270109
50 X = 2520729
38
Y = -19380981
36 feet Y = -5907323
12 meter
Z = -7218687
62 Z = -2200255
99
XDOT = 11345
203309 XDOT = 3458
017969
YDOT = 11501
854874 feet/sec YDOT = 3505
765366 meter/sec
ZDOT = -17960
395169 ZDOT = -5474
328447
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 18231
03062977
00016717 00000-0 10270-3 0 9107
2 25544 51
6394 65
5265 0005741 73
4804 286
6979 15
53825375 8281
Satellite: ISS
Catalog Number: 25544
Epoch time: 18231
03062977 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 65
5265 deg
Eccentricity:
0005741
Arg of perigee: 73
4804 deg
Mean anomaly: 286
6979 deg
Mean motion: 15
53825375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 828
Checksum: 332
Coasting Arc #12 (Orbit 843)
---------------------------------------
Vector Time (GMT): 2018/232/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 147609
58 A = 6784859
51 meter
Y = 5779675
52 meter E =
0017740
Z = 3534473
30 I = 51
97291
XDOT = -5610
240270 Wp = 86
55605
YDOT = -2635
271245 meter/sec RA = 59
97607 deg
ZDOT = 4525
109974 TA = 314
90809
MA = 315
05193
Ha = 223
552 n
mi
Hp = 213
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 484283
41 X = 65800
24
Y = 18962190
02 feet Y = 5780868
74 meter
Z = 11596041
00 Z = 3534991
67
XDOT = -18406
300100 XDOT = -5602
335369
YDOT = -8645
903035 feet/sec YDOT = -2697
964670 meter/sec
ZDOT = 14846
161333 ZDOT = 4497
876806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9587485
15 X = -2922265
47
Y = 16365930
43 feet Y = 4988335
60 meter
Z = 11597577
23 Z = 3534941
54
XDOT = -10039
711173 XDOT = -3060
103966
YDOT = -16358
584681 feet/sec YDOT = -4986
096611 meter/sec
ZDOT = 14724
234830 ZDOT = 4487
946776
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 18232
05965187
00016717 00000-0 10270-3 0 9116
2 25544 51
6393 60
3990 0005772 75
4554 284
7239 15
53842321 8442
Satellite: ISS
Catalog Number: 25544
Epoch time: 18232
05965187 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 60
3990 deg
Eccentricity:
0005772
Arg of perigee: 75
4554 deg
Mean anomaly: 284
7239 deg
Mean motion: 15
53842321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 844
Checksum: 322
Coasting Arc #13 (Orbit 858)
---------------------------------------
Vector Time (GMT): 2018/233/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 949823
09 A = 6781266
39 meter
Y = -4912878
03 meter E =
0015896
Z = -4592295
21 I = 51
94334
XDOT = 5750
750518 Wp = 72
87482
YDOT = 3996
849538 meter/sec RA = 55
01230 deg
ZDOT = -3090
708207 TA = 166
29857
MA = 166
25537
Ha = 223
585 n
mi
Hp = 213
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3116217
49 X = 1026996
35
Y = -16118366
24 feet Y = -4901824
90 meter
Z = -15066585
34 Z = -4587493
97
XDOT = 18867
291725 XDOT = 5720
642089
YDOT = 13113
023417 feet/sec YDOT = 4060
990097 meter/sec
ZDOT = -10140
118790 ZDOT = -3062
846467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10975389
06 X = 3345298
58
Y = -12236137
40 feet Y = -3729574
68 meter
Z = -15044344
86 Z = -4585516
31
XDOT = 8727
851264 XDOT = 2660
249065
YDOT = 20125
478215 feet/sec YDOT = 6134
245760 meter/sec
ZDOT = -10015
563360 ZDOT = -3052
743712
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 18233
02435807
00016717 00000-0 10270-3 0 9126
2 25544 51
6391 55
5920 0005899 78
8333 281
3483 15
53845818 8595
Satellite: ISS
Catalog Number: 25544
Epoch time: 18233
02435807 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 55
5920 deg
Eccentricity:
0005899
Arg of perigee: 78
8333 deg
Mean anomaly: 281
3483 deg
Mean motion: 15
53845818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 859
Checksum: 335
Coasting Arc #14 (Orbit 874)
---------------------------------------
Vector Time (GMT): 2018/234/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2107794
01 A = 6778804
18 meter
Y = 3812602
90 meter E =
0009438
Z = 5185917
50 I = 51
91365
XDOT = -5634
737438 Wp = 99
79394
YDOT = -5020
145135 meter/sec RA = 50
03926 deg
ZDOT = 1396
793712 TA = 336
81533
MA = 336
85788
Ha = 223
648 n
mi
Hp = 213
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6915334
69 X = -2175461
03
Y = 12508539
71 feet Y = 3788653
70 meter
Z = 17014165
01 Z = 5175514
40
XDOT = -18486
671384 XDOT = -5584
966793
YDOT = -16470
292437 feet/sec YDOT = -5082
878396 meter/sec
ZDOT = 4582
656536 ZDOT = 1369
543343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12292904
24 X = -3746877
21
Y = 7401042
94 feet Y = 2255837
89 meter
Z = 16966917
80 Z = 5171516
55
XDOT = -7416
396895 XDOT = -2260
517774
YDOT = -22573
321952 feet/sec YDOT = -6880
348531 meter/sec
ZDOT = 4460
996189 ZDOT = 1359
711639
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 18234
05337710
00016717 00000-0 10270-3 0 9135
2 25544 51
6376 50
4644 0005760 81
7308 278
4498 15
53837094 8755
Satellite: ISS
Catalog Number: 25544
Epoch time: 18234
05337710 = yrday
fracday
Element set: 913
Inclination: 51
6376 deg
RA of node: 50
4644 deg
Eccentricity:
0005760
Arg of perigee: 81
7308 deg
Mean anomaly: 278
4498 deg
Mean motion: 15
53837094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 875
Checksum: 324
Coasting Arc #15 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2018/235/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3307959
02 A = 6778311
27 meter
Y = -2603926
67 meter E =
0020484
Z = -5330159
19 I = 51
89014
XDOT = 5148
029426 Wp = 90
91989
YDOT = 5645
451439 meter/sec RA = 45
06074 deg
ZDOT = 438
105081 TA = 183
24584
MA = 183
25915
Ha = 223
581 n
mi
Hp = 213
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10852883
91 X = 3362721
66
Y = -8543066
49 feet Y = -2566628
58 meter
Z = -17487398
91 Z = -5313957
54
XDOT = 16889
860320 XDOT = 5082
389769
YDOT = 18521
822305 feet/sec YDOT = 5702
653252 meter/sec
ZDOT = 1437
352628 ZDOT = 462
952586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13721960
96 X = 4182453
70
Y = -2242490
35 feet Y = -683511
06 meter
Z = -17414282
05 Z = -5307873
17
XDOT = 5775
140875 XDOT = 1760
262939
YDOT = 23345
360268 feet/sec YDOT = 7115
665810 meter/sec
ZDOT = 1548
127978 ZDOT = 471
869408
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 18235
01808100
00016717 00000-0 10270-3 0 9149
2 25544 51
6380 45
6576 0005776 85
1766 275
0046 15
53828077 8903
Satellite: ISS
Catalog Number: 25544
Epoch time: 18235
01808100 = yrday
fracday
Element set: 914
Inclination: 51
6380 deg
RA of node: 45
6576 deg
Eccentricity:
0005776
Arg of perigee: 85
1766 deg
Mean anomaly: 275
0046 deg
Mean motion: 15
53828077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 316
Coasting Arc #16 (Orbit 905)
---------------------------------------
Vector Time (GMT): 2018/236/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4425896
27 A = 6779841
41 meter
Y = 1350203
87 meter E =
0011884
Z = 4946846
48 I = 51
87144
XDOT = -4321
720275 Wp = 71
52025
YDOT = -5933
673239 meter/sec RA = 40
08137 deg
ZDOT = -2238
981784 TA = 40
29338
MA = 40
20536
Ha = 223
664 n
mi
Hp = 213
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14520657
05 X = -4464694
41
Y = 4429802
72 feet Y = 1300493
56 meter
Z = 16229811
27 Z = 4925253
15
XDOT = -14178
872292 XDOT = -4244
171509
YDOT = -19467
431886 feet/sec YDOT = -5981
568132 meter/sec
ZDOT = -7345
740760 ZDOT = -2259
786396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15013869
66 X = -4576227
47
Y = -2863617
54 feet Y = -872830
63 meter
Z = 16132663
13 Z = 4917235
72
XDOT = -3690
255933 XDOT = -1124
790008
YDOT = -22707
110231 feet/sec YDOT = -6921
127198 meter/sec
ZDOT = -7438
314850 ZDOT = -2267
198366
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 18236
04709535
00016717 00000-0 10270-3 0 9156
2 25544 51
6380 40
5295 0005718 87
8459 272
3348 15
53856764 9066
Satellite: ISS
Catalog Number: 25544
Epoch time: 18236
04709535 = yrday
fracday
Element set: 915
Inclination: 51
6380 deg
RA of node: 40
5295 deg
Eccentricity:
0005718
Arg of perigee: 87
8459 deg
Mean anomaly: 272
3348 deg
Mean motion: 15
53856764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 906
Checksum: 336
Coasting Arc #17 (Orbit 920)
---------------------------------------
Vector Time (GMT): 2018/237/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5381330
90 A = 6783073
12 meter
Y = -189036
21 meter E =
0012997
Z = -4137675
81 I = 51
85571
XDOT = 3129
526611 Wp = 100
33017
YDOT = 5858
087247 meter/sec RA = 35
10756 deg
ZDOT = 3810
427044 TA = 208
88759
MA = 208
95960
Ha = 223
598 n
mi
Hp = 213
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17655285
09 X = 5403143
07
Y = -620197
53 feet Y = -128736
60 meter
Z = -13575051
87 Z = -4111482
68
XDOT = 10267
475758 XDOT = 3045
278571
YDOT = 19219
446347 feet/sec YDOT = 5892
612830 meter/sec
ZDOT = 12501
401064 ZDOT = 3825
424123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16136606
21 X = 4918437
57
Y = 7408344
42 feet Y = 2258063
38 meter
Z = -13457419
63 Z = -4101821
50
XDOT = 1015
752409 XDOT = 309
601334
YDOT = 20569
906105 feet/sec YDOT = 6269
707381 meter/sec
ZDOT = 12567
903786 ZDOT = 3830
697074
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 18237
01179536
00016717 00000-0 10270-3 0 9167
2 25544 51
6378 35
7228 0005772 90
2958 269
8856 15
53832273 9218
Satellite: ISS
Catalog Number: 25544
Epoch time: 18237
01179536 = yrday
fracday
Element set: 916
Inclination: 51
6378 deg
RA of node: 35
7228 deg
Eccentricity:
0005772
Arg of perigee: 90
2958 deg
Mean anomaly: 269
8856 deg
Mean motion: 15
53832273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 921
Checksum: 339
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