S T A R B O O K C O M E T F I L E
1 , M c N a u g h t 2 0 1 0 R 1 , 2 0 1 0 , 6 , 2 . 6 7 8 4 1 , 1 3 0 . 7 0 0 9 5 , 3 2 2 . 6 2 1 8 8 , 7 7 . 0 3 2 2 6, 0 . 4 0 5 0 2 6 3 , 1 . 0 0 0 3 4 3 1
↑ ↑ ↑ ↑ ↑ ↑ ↑ ↑ ↑
Line number Name of comet (T/YY)
(T/TT)
(
ω
)
(Ω)
( i ) (q) (e)
(T/MM )
↓
S T A R B O O K S A T E L L I T E F I L E
1 , I S S
1 2 5 5 4 4 U 9 8 0 6 7 A 1 0 1 1 1 . 5 3 4 1 3 7 3 8 . 0 0 0 1 6 7 1 7 0 0 0 0 0 - 0 1 0 2 7 0 - 3 0 9 0 2 7
2 2 5 5 4 4 5 1 . 6 4 5 9 1 6 1 . 3 4 2 5 0 0 0 3 5 3 2 1 9 5 . 5 4 5 2 1 6 4 . 5 6 0 4 1 5 . 7 5 0 8 3 6 5 1 1 4 5 5 0
H
↓
↑
P
↑
O
↑
N
↑
M
↑
L
↑
K
↑
J
↑
I
↑
Line number
F
↓
G
↓
E
↓
D
↓
C
↓
B
↓
A
↓
←
Name of satellite
108
Chapter 5 APPLICATION
Data Transmission Forms
Form of Orbital Elements for Comet
Form of Orbital Elements for Artificial Satellite (TLE format)
Apply the following structure to create a list of the orbital elements. Send it to the STAR BOOK TEN by text file.
Example
Example
* The text of “STARBOOKCOMETFILE” identifies the orbital elements of comet. Do not change this part.
* Fill in all the items for entry. All items must be completed to have the data accepted.
* Do not use letters and characters other than the ones usable on the STAR BOOK TEN.
* Use a “,”(comma) between each entry.
* You may not leave space between the lines.
* The line numbers must be labeled from 1 and 10.
* The text of “STARBOOKSATELLITEFILE” identifies the orbital elements of artificial satellite. Do not change this part.
* Fill in all the items for entry. All items must be completed to have the data accepted.
* NORAD two-line element is applicable.
* Do not use letters and characters other than the ones usable on the STAR BOOK TEN.
* Use a “,”(comma) between each line number and name of satellite.
* You may not leave space between the lines.
* The line numbers must be labeled from 1 and 10.
STARBOOKCOMETFILE
Line number, Name of comet, Time of periapsis passage (T) (YY/MM/DD/TT), Argument of periapsis(
ω
), Longitude of the ascending node (Ω),
Inclination (i), Minimum distance from periapsis (q), Eccentricity (e).
STARBOOK SATELLITE FILE
Line number, Name of satellite
1 A A A A A A B B B B B B C C C C C . C C C C C C C C ± . D D D D D D D D E E E E E - E F F F F F - F G H H H H
2 I I I I I J J J . J J J J K K K . K K K K L L L L L L L M M M . M M M M N N N . N N N N O O . O O O O O O O O P P P P P
CAUTION
CAUTION
