[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 29th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 ET - UTC (sec) : 67 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
087/01:36:05
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 211
3
092/18:33:27
071 -0
5 1
3 1
3
N/A 1
1 -0
1 220
3
000/00:02:54
142 0
5 -0
1 212
4
Coasting Arc #1 (Orbit 1532)
---------------------------------------
Vector Time (GMT): 2015/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4470202
36 A = 6775278
70 meter
Y = -856358
26 meter E =
0012601
Z = 5013865
61 I = 51
89840
XDOT = 3543
951565 Wp = 134
93442
YDOT = -6494
581746 meter/sec RA = 131
09825 deg
ZDOT = 2038
607860 TA = 295
27139
MA = 295
40192
Ha = 221
275 n
mi
Hp = 211
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14666018
23 X = -4484649
53
Y = -2809574
33 feet Y = -906427
29 meter
Z = 16449690
33 Z = 4992115
30
XDOT = 11627
137681 XDOT = 3606
409360
YDOT = -21307
682893 feet/sec YDOT = -6454
601554 meter/sec
ZDOT = 6688
345997 ZDOT = 2055
975938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14922636
96 X = -4548419
74
Y = -1831764
21 feet Y = -558321
73 meter
Z = 16356578
39 Z = 4985485
09
XDOT = 10026
138635 XDOT = 3055
967056
YDOT = -20933
910371 feet/sec YDOT = -6380
655881 meter/sec
ZDOT = 6763
845256 ZDOT = 2061
620034
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 15086
55178535
00016717 00000-0 10270-3 0 9006
2 25544 51
6435 131
8505 0006760 144
9586 215
2013 15
55324979 15331
Satellite: ISS
Catalog Number: 25544
Epoch time: 15086
55178535 = yrday
fracday
Element set: 900
Inclination: 51
6435 deg
RA of node: 131
8505 deg
Eccentricity:
0006760
Arg of perigee: 144
9586 deg
Mean anomaly: 215
2013 deg
Mean motion: 15
55324979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1533
Checksum: 311
Coasting Arc #2 (Orbit 1541)
---------------------------------------
Vector Time (GMT): 2015/087/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904364
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4493798
83 A = 6785740
59 meter
Y = 5055381
18 meter E =
0013692
Z = 507717
49 I = 51
94361
XDOT = -3236
128979 Wp = 78
27568
YDOT = -3493
605157 meter/sec RA = 128
26547 deg
ZDOT = 6009
229627 TA = 287
17917
MA = 287
32901
Ha = 220
983 n
mi
Hp = 211
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14743434
48 X = -4552461
60
Y = 16585896
25 feet Y = 5004800
63 meter
Z = 1665739
81 Z = 485744
61
XDOT = -10617
221060 XDOT = -3226
012603
YDOT = -11461
959177 feet/sec YDOT = -3529
736516 meter/sec
ZDOT = 19715
320300 ZDOT = 5993
534124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5109683
88 X = 1557431
65
Y = -21602302
48 feet Y = -6584381
80 meter
Z = 1570720
20 Z = 478755
52
XDOT = 13320
055626 XDOT = 4059
952955
YDOT = 4613
196892 feet/sec YDOT = 1406
102413 meter/sec
ZDOT = 19648
586849 ZDOT = 5988
889271
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 15087
13005705
00016717 00000-0 10270-3 0 9010
2 25544 51
6420 128
9608 0006441 147
7739 212
3809 15
55330028 15426
Satellite: ISS
Catalog Number: 25544
Epoch time: 15087
13005705 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 128
9608 deg
Eccentricity:
0006441
Arg of perigee: 147
7739 deg
Mean anomaly: 212
3809 deg
Mean motion: 15
55330028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1542
Checksum: 290
Coasting Arc #3 (Orbit 1556)
---------------------------------------
Vector Time (GMT): 2015/088/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904364
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4942302
04 A = 6783010
66 meter
Y = -3869824
48 meter E =
0011484
Z = -2562478
62 I = 51
95339
XDOT = 1450
219876 Wp = 141
48185
YDOT = 5348
499346 meter/sec RA = 123
30774 deg
ZDOT = -5301
644839 TA = 67
19882
MA = 67
07755
Ha = 220
938 n
mi
Hp = 211
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16214901
70 X = 4997655
50
Y = -12696274
54 feet Y = -3814247
21 meter
Z = -8407082
10 Z = -2538335
15
XDOT = 4757
939226 XDOT = 1416
057163
YDOT = 17547
570033 feet/sec YDOT = 5364
525061 meter/sec
ZDOT = -17393
847897 ZDOT = -5294
683553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7962516
58 X = -2426975
05
Y = 19038305
67 feet Y = 5802875
57 meter
Z = -8302933
23 Z = -2530734
05
XDOT = -11450
965992 XDOT = -3490
254434
YDOT = -12331
220720 feet/sec YDOT = -3758
556075 meter/sec
ZDOT = -17364
863270 ZDOT = -5292
810325
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 15088
09382958
00016717 00000-0 10270-3 0 9025
2 25544 51
6417 124
1474 0006431 150
6733 209
4782 15
55365683 15575
Satellite: ISS
Catalog Number: 25544
Epoch time: 15088
09382958 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 124
1474 deg
Eccentricity:
0006431
Arg of perigee: 150
6733 deg
Mean anomaly: 209
4782 deg
Mean motion: 15
55365683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1557
Checksum: 324
Coasting Arc #4 (Orbit 1572)
---------------------------------------
Vector Time (GMT): 2015/089/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904364
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4878315
60 A = 6778349
92 meter
Y = 2166909
11 meter E =
0015300
Z = 4172417
65 I = 51
95429
XDOT = 261
929868 Wp = 123
49992
YDOT = -6683
024613 meter/sec RA = 118
33700 deg
ZDOT = 3758
890217 TA = 287
94439
MA = 288
11112
Ha = 220
825 n
mi
Hp = 211
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16004972
45 X = -4922451
85
Y = 7109281
86 feet Y = 2112110
32 meter
Z = 13689034
30 Z = 4148612
42
XDOT = 859
349959 XDOT = 318
382393
YDOT = -21925
933770 feet/sec YDOT = -6679
779442 meter/sec
ZDOT = 12332
316986 ZDOT = 3760
300542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10301579
13 X = 3139921
32
Y = -14260870
36 feet Y = -4346713
28 meter
Z = 13586601
33 Z = 4141196
09
XDOT = 9353
211987 XDOT = 2850
859014
YDOT = 18569
559044 feet/sec YDOT = 5660
001597 meter/sec
ZDOT = 12339
452026 ZDOT = 3761
064978
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 15089
12183317
00016717 00000-0 10270-3 0 9039
2 25544 51
6413 119
0121 0006455 155
4242 204
7220 15
55400194 15737
Satellite: ISS
Catalog Number: 25544
Epoch time: 15089
12183317 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 119
0121 deg
Eccentricity:
0006455
Arg of perigee: 155
4242 deg
Mean anomaly: 204
7220 deg
Mean motion: 15
55400194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1573
Checksum: 270
Coasting Arc #5 (Orbit 1587)
---------------------------------------
Vector Time (GMT): 2015/090/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904364
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4408015
32 A = 6774408
42 meter
Y = -28866
61 meter E =
0016198
Z = -5156905
80 I = 51
95530
XDOT = -1793
755187 Wp = 101
85775
YDOT = 7276
758593 meter/sec RA = 113
35200 deg
ZDOT = -1581
421755 TA = 152
98594
MA = 152
90154
Ha = 220
750 n
mi
Hp = 211
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14461992
51 X = 4433060
69
Y = -94706
74 feet Y = 20566
04 meter
Z = -16918982
29 Z = -5135431
79
XDOT = -5885
023579 XDOT = -1867
310394
YDOT = 23873
879899 feet/sec YDOT = 7256
288169 meter/sec
ZDOT = -5188
391585 ZDOT = -1590
315052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12398276
97 X = -3778994
82
Y = 7651712
34 feet Y = 2332241
92 meter
Z = -16826888
75 Z = -5128835
69
XDOT = -6845
637485 XDOT = -2086
550305
YDOT = -22534
600978 feet/sec YDOT = -6868
546378 meter/sec
ZDOT = -5227
721966 ZDOT = -1593
409655
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 15090
08556831
00016717 00000-0 10270-3 0 9042
2 25544 51
6410 114
1979 0006634 157
0998 203
0452 15
55428970 15883
Satellite: ISS
Catalog Number: 25544
Epoch time: 15090
08556831 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 114
1979 deg
Eccentricity:
0006634
Arg of perigee: 157
0998 deg
Mean anomaly: 203
0452 deg
Mean motion: 15
55428970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1588
Checksum: 319
Coasting Arc #6 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2015/091/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904364
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3625143
25 A = 6773817
03 meter
Y = -2191973
34 meter E =
0006890
Z = 5280758
66 I = 51
96455
XDOT = 3018
103644 Wp = 133
00005
YDOT = -7006
815197 meter/sec RA = 108
35959 deg
ZDOT = -840
453791 TA = 324
96876
MA = 325
01406
Ha = 220
809 n
mi
Hp = 211
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11893514
61 X = -3626014
54
Y = -7191513
58 feet Y = -2232516
18 meter
Z = 17325323
69 Z = 5263146
66
XDOT = 9901
914844 XDOT = 3100
313801
YDOT = -22988
238834 feet/sec YDOT = -6972
605245 meter/sec
ZDOT = -2757
394326 ZDOT = -825
591792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13987893
55 X = 4263509
96
Y = -333702
17 feet Y = -101712
42 meter
Z = 17250155
80 Z = 5257847
49
XDOT = 3870
335792 XDOT = 1179
678349
YDOT = 23712
399734 feet/sec YDOT = 7227
539439 meter/sec
ZDOT = -2692
500444 ZDOT = -820
674135
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 15091
11353205
00016717 00000-0 10270-3 0 9058
2 25544 51
6406 109
0625 0006663 160
7701 199
3705 15
55416046 16042
Satellite: ISS
Catalog Number: 25544
Epoch time: 15091
11353205 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 109
0625 deg
Eccentricity:
0006663
Arg of perigee: 160
7701 deg
Mean anomaly: 199
3705 deg
Mean motion: 15
55416046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1604
Checksum: 284
Coasting Arc #7 (Orbit 1618)
---------------------------------------
Vector Time (GMT): 2015/092/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904364
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2652396
67 A = 6776627
25 meter
Y = 4266163
48 meter E =
0014867
Z = -4563077
98 I = 51
98415
XDOT = -3902
277709 Wp = 131
88491
YDOT = 5791
427842 meter/sec RA = 103
37146 deg
ZDOT = 3143
212705 TA = 169
52757
MA = 169
49658
Ha = 220
511 n
mi
Hp = 211
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8702088
82 X = 2626660
02
Y = 13996599
34 feet Y = 4295679
73 meter
Z = -14970728
29 Z = -4550256
30
XDOT = -12802
748388 XDOT = -3982
017360
YDOT = 19000
747513 feet/sec YDOT = 5747
344638 meter/sec
ZDOT = 10312
377640 ZDOT = 3124
061656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15033135
81 X = -4582099
79
Y = -6874456
48 feet Y = -2095334
33 meter
Z = -14916451
46 Z = -4546534
41
XDOT = -168
182279 XDOT = -51
261959
YDOT = -21850
111969 feet/sec YDOT = -6659
914128 meter/sec
ZDOT = 10229
279947 ZDOT = 3117
884528
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 15092
07722676
00016717 00000-0 10270-3 0 9067
2 25544 51
6410 104
2476 0006751 164
0519 196
0848 15
55488175 16190
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
07722676 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 104
2476 deg
Eccentricity:
0006751
Arg of perigee: 164
0519 deg
Mean anomaly: 196
0848 deg
Mean motion: 15
55488175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1619
Checksum: 321
Coasting Arc #8 (Orbit 1629)
---------------------------------------
Vector Time (GMT): 2015/092/18:34:54
142
Vector Time (MET): N/A
Weight (LBS) : 904237
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2651561
84 A = 6778110
42 meter
Y = 4502971
76 meter E =
0012167
Z = -4329629
82 I = 51
99517
XDOT = -3787
898641 Wp = 135
05571
YDOT = 5637
339486 meter/sec RA = 99
85675 deg
ZDOT = 3540
925250 TA = 170
87893
MA = 170
85681
Ha = 220
285 n
mi
Hp = 212
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8699349
87 X = 2622043
26
Y = 14773529
38 feet Y = 4532457
56 meter
Z = -14204822
24 Z = -4316821
38
XDOT = -12427
488979 XDOT = -3867
855723
YDOT = 18495
208286 feet/sec YDOT = 5594
534191 meter/sec
ZDOT = 11617
208824 ZDOT = 3522
329273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11179915
52 X = 3407638
25
Y = -13056857
50 feet Y = -3979730
17 meter
Z = -14150646
44 Z = -4313117
03
XDOT = 20573
201095 XDOT = 6270
711694
YDOT = 5104
561918 feet/sec YDOT = 1555
870473 meter/sec
ZDOT = 11536
509754 ZDOT = 3516
328173
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 15092
78392496
00016717 00000-0 10270-3 0 9079
2 25544 51
6443 100
7214 0005667 173
6583 186
4643 15
55278006 16308
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
78392496 = yrday
fracday
Element set: 907
Inclination: 51
6443 deg
RA of node: 100
7214 deg
Eccentricity:
0005667
Arg of perigee: 173
6583 deg
Mean anomaly: 186
4643 deg
Mean motion: 15
55278006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1630
Checksum: 321
Coasting Arc #9 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2015/093/18:34:54
142
Vector Time (MET): N/A
Weight (LBS) : 904237
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1663288
06 A = 6782723
02 meter
Y = -5951972
82 meter E =
0015837
Z = 2771917
39 I = 52
01489
XDOT = 4361
526062 Wp = 121
29470
YDOT = -3632
346159 meter/sec RA = 94
88902 deg
ZDOT = -5168
724992 TA = 27
42411
MA = 27
34061
Ha = 220
274 n
mi
Hp = 212
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5456981
83 X = -1610073
10
Y = -19527469
88 feet Y = -5970274
85 meter
Z = 9094217
16 Z = 2763967
53
XDOT = 14309
468708 XDOT = 4426
927558
YDOT = -11917
146192 feet/sec YDOT = -3583
207801 meter/sec
ZDOT = -16957
759159 ZDOT = -5147
378022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16532688
94 X = -5039163
59
Y = 11763145
43 feet Y = 3585406
73 meter
Z = 9061132
50 Z = 2761833
19
XDOT = -15216
712852 XDOT = -4638
054077
YDOT = -8360
363272 feet/sec YDOT = -2548
238725 meter/sec
ZDOT = -16865
590795 ZDOT = -5140
632074
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 15093
81198882
00016717 00000-0 10270-3 0 9088
2 25544 51
6440 95
5873 0005739 176
9964 183
1225 15
55287230 16462
Satellite: ISS
Catalog Number: 25544
Epoch time: 15093
81198882 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 95
5873 deg
Eccentricity:
0005739
Arg of perigee: 176
9964 deg
Mean anomaly: 183
1225 deg
Mean motion: 15
55287230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 344
Coasting Arc #10 (Orbit 1660)
---------------------------------------
Vector Time (GMT): 2015/094/18:34:54
142
Vector Time (MET): N/A
Weight (LBS) : 904237
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 631191
17 A = 6785516
69 meter
Y = 6707814
26 meter E =
0006800
Z = -798802
21 I = 52
02728
XDOT = -4662
660906 Wp = 70
42008
YDOT = 1145
163815 meter/sec RA = 89
93414 deg
ZDOT = 5975
477761 TA = 280
99038
MA = 281
06686
Ha = 219
980 n
mi
Hp = 212
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2070837
19 X = 560016
21
Y = 22007264
64 feet Y = 6714474
58 meter
Z = -2620742
15 Z = -795909
78
XDOT = -15297
443918 XDOT = -4704
146786
YDOT = 3757
099132 feet/sec YDOT = 1092
791758 meter/sec
ZDOT = 19604
585830 ZDOT = 5952
726312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19857412
96 X = 6052539
47
Y = -9713396
22 feet Y = -2960643
17 meter
Z = -2609489
86 Z = -795372
51
XDOT = 8246
953139 XDOT = 2513
671317
YDOT = 11657
501159 feet/sec YDOT = 3553
206353 meter/sec
ZDOT = 19506
813390 ZDOT = 5945
676721
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 15094
77577727
00016717 00000-0 10270-3 0 9094
2 25544 51
6447 90
7734 0005657 181
6900 178
4235 15
55346075 16612
Satellite: ISS
Catalog Number: 25544
Epoch time: 15094
77577727 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 90
7734 deg
Eccentricity:
0005657
Arg of perigee: 181
6900 deg
Mean anomaly: 178
4235 deg
Mean motion: 15
55346075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1661
Checksum: 340
Coasting Arc #11 (Orbit 1676)
---------------------------------------
Vector Time (GMT): 2015/095/18:34:54
142
Vector Time (MET): N/A
Weight (LBS) : 904237
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 470020
67 A = 6785056
90 meter
Y = -6626669
07 meter E =
0013569
Z = -1342046
00 I = 52
02516
XDOT = 4721
459469 Wp = 159
47733
YDOT = 1514
713547 meter/sec RA = 84
98438 deg
ZDOT = -5855
851340 TA = 35
07106
MA = 34
98180
Ha = 219
948 n
mi
Hp = 212
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1542062
56 X = 550605
96
Y = -21741040
26 feet Y = -6620962
58 meter
Z = -4403038
06 Z = -1339566
14
XDOT = 15490
352589 XDOT = 4732
616567
YDOT = 4969
532636 feet/sec YDOT = 1567
573646 meter/sec
ZDOT = -19212
110697 ZDOT = -5832
888210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20788829
40 X = -6336435
20
Y = 6555840
12 feet Y = 1998220
07 meter
Z = -4391248
65 Z = -1338452
59
XDOT = -659
521905 XDOT = -201
022277
YDOT = -14827
786367 feet/sec YDOT = -4519
509285 meter/sec
ZDOT = -19113
890676 ZDOT = -5825
913878
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 15095
80379832
00016717 00000-0 10270-3 0 9108
2 25544 51
6451 85
6390 0005796 186
1705 173
9378 15
55337324 16777
Satellite: ISS
Catalog Number: 25544
Epoch time: 15095
80379832 = yrday
fracday
Element set: 910
Inclination: 51
6451 deg
RA of node: 85
6390 deg
Eccentricity:
0005796
Arg of perigee: 186
1705 deg
Mean anomaly: 173
9378 deg
Mean motion: 15
55337324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1677
Checksum: 339
Coasting Arc #12 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2015/096/18:34:54
142
Vector Time (MET): N/A
Weight (LBS) : 904237
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1563441
58 A = 6781225
69 meter
Y = 5742732
21 meter E =
0012814
Z = 3245015
78 I = 52
00936
XDOT = -4498
152674 Wp = 111
93070
YDOT = -3946
471149 meter/sec RA = 80
02632 deg
ZDOT = 4797
123474 TA = 285
47058
MA = 285
61207
Ha = 219
701 n
mi
Hp = 212
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5129401
52 X = -1643305
27
Y = 18840984
93 feet Y = 5724802
59 meter
Z = 10646377
22 Z = 3237226
17
XDOT = -14757
718746 XDOT = -4476
990943
YDOT = -12947
739990 feet/sec YDOT = -3996
653591 meter/sec
ZDOT = 15738
594076 ZDOT = 4775
323843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19391379
54 X = 5910492
48
Y = -2449412
35 feet Y = -746580
89 meter
Z = 10611955
51 Z = 3234524
04
XDOT = -6415
145782 XDOT = -1955
336434
YDOT = 17279
601566 feet/sec YDOT = 5266
822557 meter/sec
ZDOT = 15645
796509 ZDOT = 4768
838776
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 15096
83179672
00016717 00000-0 10270-3 0 9113
2 25544 51
6453 80
5042 0005543 189
2700 170
8352 15
55390070 16939
Satellite: ISS
Catalog Number: 25544
Epoch time: 15096
83179672 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 80
5042 deg
Eccentricity:
0005543
Arg of perigee: 189
2700 deg
Mean anomaly: 170
8352 deg
Mean motion: 15
55390070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 306
Coasting Arc #13 (Orbit 1707)
---------------------------------------
Vector Time (GMT): 2015/097/18:34:54
142
Vector Time (MET): N/A
Weight (LBS) : 904237
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2668532
46 A = 6776343
48 meter
Y = -4136360
40 meter E =
0008630
Z = -4663430
32 I = 51
98740
XDOT = 3952
314916 Wp = 102
35789
YDOT = 5867
551480 meter/sec RA = 75
05286 deg
ZDOT = -2949
159520 TA = 138
44137
MA = 138
37574
Ha = 219
503 n
mi
Hp = 212
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8755027
77 X = 2737241
42
Y = -13570736
21 feet Y = -4106135
37 meter
Z = -15299968
25 Z = -4650299
66
XDOT = 12966
912454 XDOT = 3900
734934
YDOT = 19250
496983 feet/sec YDOT = 5911
460179 meter/sec
ZDOT = -9675
720210 ZDOT = -2930
085487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15981013
15 X = -4871012
81
Y = -2676797
30 feet Y = -815887
82 meter
Z = -15242912
97 Z = -4646039
87
XDOT = 12227
226251 XDOT = 3726
858561
YDOT = -18480
564593 feet/sec YDOT = -5632
876088 meter/sec
ZDOT = -9594
964741 ZDOT = -2924
545253
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 15097
79552349
00016717 00000-0 10270-3 0 9126
2 25544 51
6456 75
6905 0005583 194
8570 165
2420 15
55445389 17081
Satellite: ISS
Catalog Number: 25544
Epoch time: 15097
79552349 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 75
6905 deg
Eccentricity:
0005583
Arg of perigee: 194
8570 deg
Mean anomaly: 165
2420 deg
Mean motion: 15
55445389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1708
Checksum: 341
Coasting Arc #14 (Orbit 1723)
---------------------------------------
Vector Time (GMT): 2015/098/18:34:54
142
Vector Time (MET): N/A
Weight (LBS) : 904237
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3657935
80 A = 6773556
00 meter
Y = 2085275
05 meter E =
0006657
Z = 5305619
08 I = 51
96967
XDOT = -3066
028195 Wp = 171
55404
YDOT = -7003
546530 meter/sec RA = 70
06556 deg
ZDOT = 632
240501 TA = 272
40199
MA = 272
47821
Ha = 219
432 n
mi
Hp = 212
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12001101
71 X = -3706755
02
Y = 6841453
58 feet Y = 2044097
06 meter
Z = 17406886
75 Z = 5287730
57
XDOT = -10059
147622 XDOT = -2990
556228
YDOT = -22977
514861 feet/sec YDOT = -7037
410823 meter/sec
ZDOT = 2074
279860 ZDOT = 617
529988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11262160
00 X = 3432706
37
Y = 8165406
80 feet Y = 2488815
99 meter
Z = 17329787
06 Z = 5282119
10
XDOT = -16106
864109 XDOT = -4909
372181
YDOT = 17898
756591 feet/sec YDOT = 5455
541009 meter/sec
ZDOT = 2012
457439 ZDOT = 613
397027
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 15098
82347838
00016717 00000-0 10270-3 0 9137
2 25544 51
6460 70
5561 0005626 197
6696 162
4263 15
55474211 17244
Satellite: ISS
Catalog Number: 25544
Epoch time: 15098
82347838 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 70
5561 deg
Eccentricity:
0005626
Arg of perigee: 197
6696 deg
Mean anomaly: 162
4263 deg
Mean motion: 15
55474211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1724
Checksum: 325
Coasting Arc #15 (Orbit 1738)
---------------------------------------
Vector Time (GMT): 2015/099/18:34:54
142
Vector Time (MET): N/A
Weight (LBS) : 904237
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4474727
26 A = 6774413
56 meter
Y = 170265
87 meter E =
0013493
Z = -5094771
90 I = 51
96064
XDOT = 1793
956477 Wp = 127
82498
YDOT = 7224
114939 meter/sec RA = 65
07261 deg
ZDOT = 1812
271001 TA = 159
68107
MA = 159
62732
Ha = 219
130 n
mi
Hp = 213
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14680863
73 X = 4497239
49
Y = 558615
06 feet Y = 220430
73 meter
Z = -16715130
92 Z = -5072979
65
XDOT = 5885
683981 XDOT = 1704
237952
YDOT = 23701
164498 feet/sec YDOT = 7243
674605 meter/sec
ZDOT = 5945
771000 ZDOT = 1820
767392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5880846
00 X = -1792481
86
Y = -13578301
72 feet Y = -4138666
36 meter
Z = -16621696
21 Z = -5066293
00
XDOT = 17864
672058 XDOT = 5445
152043
YDOT = -15078
047998 feet/sec YDOT = -4595
789030 meter/sec
ZDOT = 5980
887120 ZDOT = 1822
974394
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 15099
78716447
00016717 00000-0 10270-3 0 9140
2 25544 51
6454 65
7413 0005630 202
5336 157
5571 15
55519033 17396
Satellite: ISS
Catalog Number: 25544
Epoch time: 15099
78716447 = yrday
fracday
Element set: 914
Inclination: 51
6454 deg
RA of node: 65
7413 deg
Eccentricity:
0005630
Arg of perigee: 202
5336 deg
Mean anomaly: 157
5571 deg
Mean motion: 15
55519033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1739
Checksum: 320
Coasting Arc #16 (Orbit 1754)
---------------------------------------
Vector Time (GMT): 2015/100/18:34:54
142
Vector Time (MET): N/A
Weight (LBS) : 904237
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4946070
99 A = 6778324
61 meter
Y = -2284991
18 meter E =
0008611
Z = 4023364
01 I = 51
96050
XDOT = -196
772249 Wp = 109
19516
YDOT = -6566
721920 meter/sec RA = 60
08934 deg
ZDOT = -3967
205129 TA = 21
84484
MA = 21
80814
Ha = 218
985 n
mi
Hp = 213
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16227267
03 X = -4939696
21
Y = -7496690
23 feet Y = -2340265
49 meter
Z = 13200013
16 Z = 3999352
41
XDOT = -645
578246 XDOT = -104
055644
YDOT = -21544
363256 feet/sec YDOT = -6568
404188 meter/sec
ZDOT = -13015
764859 ZDOT = -3967
935419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 588939
74 X = 179508
83
Y = 17940871
17 feet Y = 5468377
53 meter
Z = 13097450
09 Z = 3992102
79
XDOT = -17711
552585 XDOT = -5398
481228
YDOT = 10094
748775 feet/sec YDOT = 3076
879427 meter/sec
ZDOT = -13017
681171 ZDOT = -3967
789221
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 15100
81507332
00016717 00000-0 10270-3 0 9159
2 25544 51
6458 60
6069 0005582 207
6039 152
4819 15
55582926 17551
Satellite: ISS
Catalog Number: 25544
Epoch time: 15100
81507332 = yrday
fracday
Element set: 915
Inclination: 51
6458 deg
RA of node: 60
6069 deg
Eccentricity:
0005582
Arg of perigee: 207
6039 deg
Mean anomaly: 152
4819 deg
Mean motion: 15
55582926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1755
Checksum: 314
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