[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 4th 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) : 77 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 664 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
There are no maneuvers
Coasting Arc #1 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2017/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5428086
23 A = 6788726
62 meter
Y = -3891209
41 meter E =
0016247
Z = 1161980
28 I = 51
40359
XDOT = 1998
687892 Wp = 41
63661
YDOT = 4545
575534 meter/sec RA = 316
38209 deg
ZDOT = 5850
239166 TA = 331
03213
MA = 331
12220
Ha = 221
459 n
mi
Hp = 214
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17808681
87 X = 5465551
01
Y = -12766435
07 feet Y = -3830299
51 meter
Z = 3812271
27 Z = 1188438
85
XDOT = 6557
374973 XDOT = 1919
291938
YDOT = 14913
305557 feet/sec YDOT = 4567
481701 meter/sec
ZDOT = 19193
698052 ZDOT = 5859
755787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15882563
87 X = -4841005
47
Y = -15065369
92 feet Y = -4591924
75 meter
Z = 3929786
36 Z = 1197798
88
XDOT = 12340
813590 XDOT = 3761
479982
YDOT = -7963
626101 feet/sec YDOT = -2427
313236 meter/sec
ZDOT = 19234
844183 ZDOT = 5862
780507
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 17184
56198132
00016717 00000-0 10270-3 0 9003
2 25544 51
6411 316
7086 0004897 351
0652 9
0413 15
54128637 24297
Satellite: ISS
Catalog Number: 25544
Epoch time: 17184
56198132 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 316
7086 deg
Eccentricity:
0004897
Arg of perigee: 351
0652 deg
Mean anomaly: 9
0413 deg
Mean motion: 15
54128637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 304
Coasting Arc #2 (Orbit 2443)
---------------------------------------
Vector Time (GMT): 2017/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5487590
51 A = 6786019
08 meter
Y = 2890964
31 meter E =
0004482
Z = -2759840
37 I = 51
37135
XDOT = -429
012015 Wp = 54
40805
YDOT = -5690
523826 meter/sec RA = 311
39072 deg
ZDOT = -5111
161373 TA = 156
94989
MA = 156
92977
Ha = 221
639 n
mi
Hp = 214
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18003905
88 X = -5506104
24
Y = 9484791
04 feet Y = 2829495
15 meter
Z = -9054594
38 Z = -2786542
02
XDOT = -1407
519733 XDOT = -340
519685
YDOT = -18669
697591 feet/sec YDOT = -5694
825959 meter/sec
ZDOT = -16768
902144 ZDOT = -5113
031092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12959877
63 X = 3950170
70
Y = 15620032
99 feet Y = 4760986
05 meter
Z = -9172987
99 Z = -2795926
74
XDOT = -16869
977654 XDOT = -5141
969189
YDOT = 4151
353726 feet/sec YDOT = 1265
332616 meter/sec
ZDOT = -16776
086883 ZDOT = -5113
351282
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 17185
52651955
00016717 00000-0 10270-3 0 9018
2 25544 51
6407 311
9008 0004981 355
1879 4
9225 15
54127138 24440
Satellite: ISS
Catalog Number: 25544
Epoch time: 17185
52651955 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 311
9008 deg
Eccentricity:
0004981
Arg of perigee: 355
1879 deg
Mean anomaly: 4
9225 deg
Mean motion: 15
54127138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2444
Checksum: 312
Coasting Arc #3 (Orbit 2459)
---------------------------------------
Vector Time (GMT): 2017/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5196070
77 A = 6782174
84 meter
Y = -1594525
12 meter E =
0010460
Z = 4045914
36 I = 51
33835
XDOT = -997
106770 Wp = 75
41213
YDOT = 6557
187600 meter/sec RA = 306
38844 deg
ZDOT = 3859
008572 TA = 334
46817
MA = 334
51979
Ha = 221
499 n
mi
Hp = 214
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17047476
29 X = 5193861
95
Y = -5231381
61 feet Y = -1536431
99 meter
Z = 13273997
24 Z = 4071149
67
XDOT = -3271
347671 XDOT = -1089
102007
YDOT = 21513
082676 feet/sec YDOT = 6545
522414 meter/sec
ZDOT = 12660
789279 ZDOT = 3853
942324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8860560
88 X = -2700698
96
Y = -15378459
68 feet Y = -4687354
51 meter
Z = 13385673
05 Z = 4079953
15
XDOT = 20600
968962 XDOT = 6279
175339
YDOT = -853
566343 feet/sec YDOT = -260
167021 meter/sec
ZDOT = 12637
206832 ZDOT = 3851
820642
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 17186
55535488
00016717 00000-0 10270-3 0 9025
2 25544 51
6411 306
7723 0004941 357
8377 2
2754 15
54157231 24602
Satellite: ISS
Catalog Number: 25544
Epoch time: 17186
55535488 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 306
7723 deg
Eccentricity:
0004941
Arg of perigee: 357
8377 deg
Mean anomaly: 2
2754 deg
Mean motion: 15
54157231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2460
Checksum: 311
Coasting Arc #4 (Orbit 2474)
---------------------------------------
Vector Time (GMT): 2017/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4666255
37 A = 6778927
84 meter
Y = 68144
05 meter E =
0014707
Z = -4930176
49 I = 51
30956
XDOT = 2213
641074 Wp = 54
71624
YDOT = -6996
004485 meter/sec RA = 301
37506 deg
ZDOT = -2188
137558 TA = 193
78760
MA = 193
82781
Ha = 221
792 n
mi
Hp = 214
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15309236
76 X = -4642722
27
Y = 223569
71 feet Y = 16095
06 meter
Z = -16175119
72 Z = -4952786
48
XDOT = 7262
601948 XDOT = 2302
336578
YDOT = -22952
770619 feet/sec YDOT = -6970
753827 meter/sec
ZDOT = -7178
928997 ZDOT = -2177
169928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3841159
36 X = 1170785
37
Y = 14711544
30 feet Y = 4484078
70 meter
Z = -16274924
60 Z = -4960597
02
XDOT = -22961
483084 XDOT = -6998
660044
YDOT = -1904
989378 feet/sec YDOT = -580
640762 meter/sec
ZDOT = -7129
228131 ZDOT = -2172
988734
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 17187
51988596
00016717 00000-0 10270-3 0 9035
2 25544 51
6420 301
9650 0005031 1
2996 358
8169 15
54127722 24754
Satellite: ISS
Catalog Number: 25544
Epoch time: 17187
51988596 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 301
9650 deg
Eccentricity:
0005031
Arg of perigee: 1
2996 deg
Mean anomaly: 358
8169 deg
Mean motion: 15
54127722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2475
Checksum: 323
Coasting Arc #5 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2017/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3937679
42 A = 6777219
62 meter
Y = 1585331
28 meter E =
0005446
Z = 5280474
26 I = 51
28852
XDOT = -3191
608917 Wp = 32
22438
YDOT = 6969
935955 meter/sec RA = 296
35205 deg
ZDOT = 291
840419 TA = 55
00672
MA = 54
95561
Ha = 221
722 n
mi
Hp = 214
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12918895
73 X = 3894009
38
Y = 5201218
12 feet Y = 1629120
17 meter
Z = 17324390
63 Z = 5299496
33
XDOT = -10471
157865 XDOT = -3270
728978
YDOT = 22867
243946 feet/sec YDOT = 6933
802792 meter/sec
ZDOT = 957
481690 ZDOT = 276
145470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1763473
80 X = 537506
82
Y = -13708928
16 feet Y = -4178481
30 meter
Z = 17408058
37 Z = 5305976
19
XDOT = 23783
977932 XDOT = 7249
356474
YDOT = 4167
551480 feet/sec YDOT = 1270
269691 meter/sec
ZDOT = 886
931505 ZDOT = 270
336723
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 17188
54871167
00016717 00000-0 10270-3 0 9045
2 25544 51
6423 296
8358 0005158 5
4095 354
7113 15
54179280 24918
Satellite: ISS
Catalog Number: 25544
Epoch time: 17188
54871167 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 296
8358 deg
Eccentricity:
0005158
Arg of perigee: 5
4095 deg
Mean anomaly: 354
7113 deg
Mean motion: 15
54179280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 327
Coasting Arc #6 (Orbit 2505)
---------------------------------------
Vector Time (GMT): 2017/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3135073
64 A = 6778134
40 meter
Y = -3204104
72 meter E =
0014239
Z = -5095771
53 I = 51
27755
XDOT = 3895
699518 Wp = 80
90919
YDOT = -6389
906762 meter/sec RA = 291
32937 deg
ZDOT = 1627
188146 TA = 204
85911
MA = 204
92777
Ha = 221
942 n
mi
Hp = 213
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10285674
66 X = -3074258
96
Y = -10512154
59 feet Y = -3238822
49 meter
Z = -16718410
54 Z = -5110853
35
XDOT = 12781
166399 XDOT = 3958
959594
YDOT = -20964
261031 feet/sec YDOT = -6345
988927 meter/sec
ZDOT = 5338
543785 ZDOT = 1646
264834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7352887
84 X = -2241160
21
Y = 12650088
64 feet Y = 3855747
02 meter
Z = -16784398
89 Z = -5115884
78
XDOT = -22715
999449 XDOT = -6923
836632
YDOT = -6033
678680 feet/sec YDOT = -1839
065262 meter/sec
ZDOT = 5423
903461 ZDOT = 1653
205775
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 17189
51323467
00016717 00000-0 10270-3 0 9059
2 25544 51
6420 292
0296 0005193 10
2781 349
8477 15
54170281 25066
Satellite: ISS
Catalog Number: 25544
Epoch time: 17189
51323467 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 292
0296 deg
Eccentricity:
0005193
Arg of perigee: 10
2781 deg
Mean anomaly: 349
8477 deg
Mean motion: 15
54170281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2506
Checksum: 309
Coasting Arc #7 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2017/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2264748
36 A = 6781180
64 meter
Y = 4679683
91 meter E =
0013134
Z = 4349813
45 I = 51
27667
XDOT = -4387
344157 Wp = 51
44173
YDOT = 5294
897567 meter/sec RA = 286
30918 deg
ZDOT = -3397
125884 TA = 73
22199
MA = 73
07793
Ha = 222
055 n
mi
Hp = 213
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7430276
76 X = 2191121
58
Y = 15353293
67 feet Y = 4704597
61 meter
Z = 14271041
50 Z = 4360636
56
XDOT = -14394
173742 XDOT = -4429
725651
YDOT = 17371
711178 feet/sec YDOT = 5245
598790 meter/sec
ZDOT = -11145
426128 ZDOT = -3418
540222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12588079
07 X = 3836846
50
Y = -11451246
63 feet Y = -3490339
97 meter
Z = 14317977
54 Z = 4364119
55
XDOT = 19926
350497 XDOT = 6073
551632
YDOT = 7788
158181 feet/sec YDOT = 2373
830614 meter/sec
ZDOT = -11240
896643 ZDOT = -3426
225297
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 17190
54205455
00016717 00000-0 10270-3 0 9061
2 25544 51
6421 286
9007 0005229 14
1115 346
0183 15
54152093 25225
Satellite: ISS
Catalog Number: 25544
Epoch time: 17190
54205455 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 286
9007 deg
Eccentricity:
0005229
Arg of perigee: 14
1115 deg
Mean anomaly: 346
0183 deg
Mean motion: 15
54152093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 280
Coasting Arc #8 (Orbit 2536)
---------------------------------------
Vector Time (GMT): 2017/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1432298
67 A = 6784971
56 meter
Y = -5821773
63 meter E =
0008436
Z = -3174787
45 I = 51
28110
XDOT = 4664
495545 Wp = 44
27763
YDOT = -3751
540403 meter/sec RA = 281
29913 deg
ZDOT = 4788
670548 TA = 278
86703
MA = 278
96254
Ha = 222
131 n
mi
Hp = 213
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4699142
61 X = -1351670
27
Y = -19100307
18 feet Y = -5837339
36 meter
Z = -10415969
34 Z = -3181549
89
XDOT = 15303
463073 XDOT = 4682
838910
YDOT = -12308
203422 feet/sec YDOT = -3699
276864 meter/sec
ZDOT = 15710
861377 ZDOT = 4811
372998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16782183
61 X = -5115209
56
Y = 10230381
38 feet Y = 3118220
24 meter
Z = -10444793
10 Z = -3183572
94
XDOT = -15606
835309 XDOT = -4756
963402
YDOT = -9504
338416 feet/sec YDOT = -2896
922349 meter/sec
ZDOT = 15811
735764 ZDOT = 4819
417061
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 17191
50656771
00016717 00000-0 10270-3 0 9070
2 25544 51
6421 282
0934 0005347 15
5576 344
5740 15
54147737 25375
Satellite: ISS
Catalog Number: 25544
Epoch time: 17191
50656771 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 282
0934 deg
Eccentricity:
0005347
Arg of perigee: 15
5576 deg
Mean anomaly: 344
5740 deg
Mean motion: 15
54147737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2537
Checksum: 319
Coasting Arc #9 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2017/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 585278
21 A = 6788120
13 meter
Y = 6561097
49 meter E =
0014429
Z = 1623747
31 I = 51
28519
XDOT = -4793
821387 Wp = 94
83962
YDOT = 1846
749714 meter/sec RA = 276
29854 deg
ZDOT = -5691
639855 TA = 67
29763
MA = 67
14516
Ha = 222
262 n
mi
Hp = 213
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1920204
09 X = 503979
55
Y = 21525910
39 feet Y = 6567187
73 meter
Z = 5327254
96 Z = 1626393
60
XDOT = -15727
760456 XDOT = -4786
469187
YDOT = 6058
890139 feet/sec YDOT = 1793
183658 meter/sec
ZDOT = -18673
359105 ZDOT = -5714
908339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19781890
59 X = 6029520
25
Y = -8695767
56 feet Y = -2650469
95 meter
Z = 5337797
17 Z = 1626960
58
XDOT = 10112
024101 XDOT = 3082
144946
YDOT = 11392
380782 feet/sec YDOT = 3472
397662 meter/sec
ZDOT = -18776
394945 ZDOT = -5723
045179
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 17192
53537991
00016717 00000-0 10270-3 0 9087
2 25544 51
6410 276
9651 0005362 21
1592 338
9781 15
54159016 25532
Satellite: ISS
Catalog Number: 25544
Epoch time: 17192
53537991 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 276
9651 deg
Eccentricity:
0005362
Arg of perigee: 21
1592 deg
Mean anomaly: 338
9781 deg
Mean motion: 15
54159016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2553
Checksum: 323
Coasting Arc #10 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2017/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 200608
86 A = 6789299
70 meter
Y = -6776812
16 meter E =
0017436
Z = 57936
56 I = 51
28608
XDOT = 4795
079958 Wp = 39
13424
YDOT = 201
446363 meter/sec RA = 271
30313 deg
ZDOT = 5986
428048 TA = 321
49325
MA = 321
61752
Ha = 222
354 n
mi
Hp = 213
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 658165
55 X = 276092
63
Y = -22233635
70 feet Y = -6774146
77 meter
Z = 190080
57 Z = 59093
78
XDOT = 15731
889626 XDOT = 4763
392285
YDOT = 660
913263 feet/sec YDOT = 254
890498 meter/sec
ZDOT = 19640
511969 ZDOT = 6009
643749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21152563
29 X = -6447301
29
Y = 6879998
79 feet Y = 2097023
63 meter
Z = 196347
05 Z = 59846
58
XDOT = -4136
689574 XDOT = -1260
862982
YDOT = -13369
929371 feet/sec YDOT = -4075
154472 meter/sec
ZDOT = 19742
963320 ZDOT = 6017
655220
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 17193
56418946
00016717 00000-0 10270-3 0 9090
2 25544 51
6407 271
8365 0005503 23
7692 336
3714 15
54140077 25692
Satellite: ISS
Catalog Number: 25544
Epoch time: 17193
56418946 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 271
8365 deg
Eccentricity:
0005503
Arg of perigee: 23
7692 deg
Mean anomaly: 336
3714 deg
Mean motion: 15
54140077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2569
Checksum: 326
Coasting Arc #11 (Orbit 2583)
---------------------------------------
Vector Time (GMT): 2017/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1010887
78 A = 6787843
73 meter
Y = 6473340
21 meter E =
0007206
Z = -1778348
65 I = 51
28118
XDOT = -4671
450034 Wp = 97
64637
YDOT = -2271
177318 meter/sec RA = 266
30748 deg
ZDOT = -5632
453584 TA = 101
97105
MA = 101
89026
Ha = 222
394 n
mi
Hp = 213
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3316560
97 X = -1074561
03
Y = 21237992
81 feet Y = 6461679
88 meter
Z = -5834477
20 Z = -1783413
35
XDOT = -15326
279638 XDOT = -4618
346641
YDOT = -7451
369153 feet/sec YDOT = -2323
119319 meter/sec
ZDOT = -18479
178426 ZDOT = -5655
016900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21025629
62 X = 6408611
91
Y = -4438542
70 feet Y = -1352867
81 meter
Z = -5857924
32 Z = -1785495
33
XDOT = -1922
289778 XDOT = -585
913924
YDOT = 15324
574984 feet/sec YDOT = 4670
930455 meter/sec
ZDOT = -18578
405738 ZDOT = -5662
698069
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 17194
52869329
00016717 00000-0 10270-3 0 9104
2 25544 51
6401 267
0283 0005469 27
7349 332
4094 15
54172597 25843
Satellite: ISS
Catalog Number: 25544
Epoch time: 17194
52869329 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 267
0283 deg
Eccentricity:
0005469
Arg of perigee: 27
7349 deg
Mean anomaly: 332
4094 deg
Mean motion: 15
54172597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2584
Checksum: 331
Coasting Arc #12 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2017/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1788421
50 A = 6784583
61 meter
Y = -5657372
41 meter E =
0016385
Z = 3271105
31 I = 51
27342
XDOT = 4444
733451 Wp = 71
48539
YDOT = 4130
977013 meter/sec RA = 261
30474 deg
ZDOT = 4700
173184 TA = 326
74776
MA = 326
85060
Ha = 222
393 n
mi
Hp = 213
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5867524
60 X = 1835661
57
Y = -18560933
11 feet Y = -5637109
13 meter
Z = 10731972
79 Z = 3279907
20
XDOT = 14582
458830 XDOT = 4375
378572
YDOT = 13553
074191 feet/sec YDOT = 4180
292971 meter/sec
ZDOT = 15420
515697 ZDOT = 4721
595867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19388663
32 X = -5909664
58
Y = 1469719
75 feet Y = 447970
58 meter
Z = 10771767
80 Z = 3283234
83
XDOT = 7352
771763 XDOT = 2241
124833
YDOT = -17050
464148 feet/sec YDOT = -5196
981472 meter/sec
ZDOT = 15514
408637 ZDOT = 4728
791753
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 17195
55749457
00016717 00000-0 10270-3 0 9118
2 25544 51
6400 261
8991 0005545 31
4273 328
7210 15
54186997 26009
Satellite: ISS
Catalog Number: 25544
Epoch time: 17195
55749457 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 261
8991 deg
Eccentricity:
0005545
Arg of perigee: 31
4273 deg
Mean anomaly: 328
7210 deg
Mean motion: 15
54186997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 321
Coasting Arc #13 (Orbit 2614)
---------------------------------------
Vector Time (GMT): 2017/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2593666
00 A = 6780780
61 meter
Y = 4426157
80 meter E =
0014298
Z = -4448886
26 I = 51
26548
XDOT = -4049
729637 Wp = 57
03410
YDOT = -5631
106787 meter/sec RA = 256
29259 deg
ZDOT = -3241
349972 TA = 180
09527
MA = 180
09554
Ha = 222
559 n
mi
Hp = 213
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8509402
88 X = -2621357
37
Y = 14521515
08 feet Y = 4396999
08 meter
Z = -14596083
54 Z = -4461552
40
XDOT = -13286
514557 XDOT = -3970
715377
YDOT = -18474
759800 feet/sec YDOT = -5675
951638 meter/sec
ZDOT = -10634
350303 ZDOT = -3260
830541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16641105
95 X = 5072209
09
Y = 2168224
40 feet Y = 660874
80 meter
Z = -14652726
30 Z = -4466150
98
XDOT = -11797
301532 XDOT = -3595
817507
YDOT = 18102
293617 feet/sec YDOT = 5517
579094 meter/sec
ZDOT = -10719
437072 ZDOT = -3267
284420
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 17196
52199608
00016717 00000-0 10270-3 0 9124
2 25544 51
6391 257
0911 0005557 35
5741 324
5781 15
54168472 26156
Satellite: ISS
Catalog Number: 25544
Epoch time: 17196
52199608 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 257
0911 deg
Eccentricity:
0005557
Arg of perigee: 35
5741 deg
Mean anomaly: 324
5781 deg
Mean motion: 15
54168472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2615
Checksum: 324
Coasting Arc #14 (Orbit 2630)
---------------------------------------
Vector Time (GMT): 2017/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3364618
78 A = 6777867
03 meter
Y = -2878735
74 meter E =
0007463
Z = 5124760
00 I = 51
26528
XDOT = 3495
534862 Wp = 76
57121
YDOT = 6675
468384 meter/sec RA = 251
27054 deg
ZDOT = 1454
768023 TA = 359
36406
MA = 359
36501
Ha = 222
442 n
mi
Hp = 213
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11038775
52 X = 3371666
05
Y = -9444671
06 feet Y = -2841071
19 meter
Z = 16813517
07 Z = 5141121
14
XDOT = 11468
290230 XDOT = 3413
561706
YDOT = 21901
142991 feet/sec YDOT = 6714
099402 meter/sec
ZDOT = 4772
860967 ZDOT = 1471
549461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13034285
74 X = -3972850
29
Y = -6222038
98 feet Y = -1896477
48 meter
Z = 16886218
02 Z = 5146919
25
XDOT = 15019
792722 XDOT = 4578
032822
YDOT = -18312
179865 feet/sec YDOT = -5581
552423 meter/sec
ZDOT = 4845
877420 ZDOT = 1477
023438
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 17197
55079229
00016717 00000-0 10270-3 0 9135
2 25544 51
6396 251
9618 0005613 38
1943 321
9607 15
54195964 26316
Satellite: ISS
Catalog Number: 25544
Epoch time: 17197
55079229 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 251
9618 deg
Eccentricity:
0005613
Arg of perigee: 38
1943 deg
Mean anomaly: 321
9607 deg
Mean motion: 15
54195964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2631
Checksum: 335
Coasting Arc #15 (Orbit 2645)
---------------------------------------
Vector Time (GMT): 2017/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4098450
93 A = 6777326
12 meter
Y = 1196686
50 meter E =
0018867
Z = -5279244
52 I = 51
27492
XDOT = -2712
388043 Wp = 79
80871
YDOT = -7141
498031 meter/sec RA = 246
24454 deg
ZDOT = 491
678728 TA = 194
88590
MA = 194
94152
Ha = 222
713 n
mi
Hp = 212
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13446361
32 X = -4085884
08
Y = 3926136
81 feet Y = 1150925
48 meter
Z = -17320356
04 Z = -5299122
86
XDOT = -8898
910903 XDOT = -2634
716667
YDOT = -23430
111649 feet/sec YDOT = -7171
395543 meter/sec
ZDOT = 1613
119185 ZDOT = 478
690963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9125481
97 X = 2781446
91
Y = 10482841
22 feet Y = 3195170
01 meter
Z = -17408317
98 Z = -5306055
32
XDOT = -16818
402153 XDOT = -5126
248976
YDOT = 17200
260022 feet/sec YDOT = 5242
639255 meter/sec
ZDOT = 1556
912069 ZDOT = 474
546799
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 17198
51528784
00016717 00000-0 10270-3 0 9148
2 25544 51
6400 247
1535 0005790 41
4604 318
6987 15
54165498 26463
Satellite: ISS
Catalog Number: 25544
Epoch time: 17198
51528784 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 247
1535 deg
Eccentricity:
0005790
Arg of perigee: 41
4604 deg
Mean anomaly: 318
6987 deg
Mean motion: 15
54165498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2646
Checksum: 335
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