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	    LAUNCH_DATE	=> <<'EOD',
This is the date the body was launched.
EOD
	    LAUNCH	=> <<'EOD',
This is the date the body was launched.
EOD
	    LAUNCH_NUM	=> <<'EOD',
This is the launch number in the year.
EOD
	    LAUNCH_PIECE	=> <<'EOD',
This is the launch piece.
EOD
	    LAUNCH_SITE	=> <<'EOD',
This is the name of a launch site.
EOD
	    LAUNCH_YEAR	=> <<'EOD',
This is the Gregorian year the body was launched.
EOD
	    MEAN_ANOMALY	=> <<'EOD',
This is the mean anomaly of the body's orbit, in degrees.
EOD
	    MEAN_ELEMENT_THEORY	=> <<'EOD',
The name of the model to use with this data set, e.g. 'SGP4'.
EOD
	    MEAN_MOTION	=> <<'EOD',
This is the mean motion of the body, in revolutions per day.
EOD
	    MEAN_MOTION_DOT	=> <<'EOD',
This is the first time derivative of the mean motion (i.e. the
acceleration), in revolutions per day squared. Also known as the
Ballistic Coefficient.
EOD
	    MEAN_MOTION_DDOT	=> <<'EOD',
This is the second time derivative of the mean motion, in revolutions
per day cubed.
EOD
	    NORAD_CAT_ID	=> <<'EOD',
This is the OID, or NORAD catalog ID. Note that there are no leading
zeroes.
EOD
	    OBJECT_ID		=> <<'EOD',
This is the international launch designator. It is made up of a numeric
four-digit Gregorian year, a dash, a three-digit launch number in the
year (with leading zeroes), and a launch piece which consists of one or
more upper-case alphabetic characters, with the payload being 'A'. For
example, the Zarya module of the International Space Station is
1998-067A.
EOD
	    OBJECT_NAME		=> <<'EOD',
This is the common name of the object.
EOD
	    OBJECT_NUMBER	=> <<'EOD',
This is the OID, or NORAD catalog ID. Note that there are no leading
zeroes.
EOD
	    OBJECT_TYPE	=> <<'EOD',
This is a computed value representing the general type of the body. It
can be 'DEBRIS', 'PAYLOAD', 'ROCKET BODY', 'TBA', 'UNKNOWN', or 'OTHER'.
EOD
	    ORBITAL_TBA		=> <<'EOD',	# boxscore
At a guess, number of objects on-orbit which are not yet classified.
EOD
	    PERIAPSIS		=> <<'EOD',
This is the perigee of the body's orbit in kilometers above the Earth's
surface.
EOD
	    PERIGEE		=> <<'EOD',
This is the perigee of the body's orbit in kilometers above the Earth's
surface.
EOD
	    PERIOD		=> <<'EOD',
This is the period of the body's orbit, in minutes.
EOD
	    RA_OF_ASC_NODE		=> <<'EOD',
This is the right ascension of the ascending node of the body's orbit,
in degrees (not hours).
EOD
	    RCSSOURCE	=> <<'EOD',
This is an abbreviation of the source for the radar cross-section data.
EOD
	    RCSVALUE	=> <<'EOD',
This is the radar cross-section of the body, in square meters. This is
now always carried as 0.
EOD
	    RCS_SIZE	=> <<'EOD',
This is a qualitative statement of the size of the RCS. Observed values
are 'SMALL', 'MEDIUM', 'LARGE', and null.
EOD
	    REV_AT_EPOCH		=> <<'EOD',
This is the number of revolutions the body has made at the epoch time.
In practice, this seems to be a whole-number value.
EOD
	    SEMIMAJOR_AXIS	=> <<'EOD',
This is the semimajor axis of the orbit, in kilometers.
EOD
	    SITE		=> <<'EOD',
This is an abbreviation for the site from which the body was launched.
EOD
	    SITE_CODE		=> <<'EOD',
This is an abbreviation for the site from which the body was launched.
EOD
	    TIME_SYSTEM	=> <<'EOD',
This appears to be a zone code, e.g. 'UTC',
EOD
	    TLE_LINE0		=> <<'EOD',
This is the common name of the object, with a '0 ' prefixed, since it is
the zeroth line of the TLE.
EOD
	    TLE_LINE1		=> <<'EOD',
This is the first line of the TLE data for this body's orbit, as
represented in a traditional TLE data set.
EOD
	    TLE_LINE2		=> <<'EOD',
This is the second line of the TLE data for this body's orbit, as
represented in a traditional TLE data set.
EOD
	},
	boxscore	=> {
	    COUNTRY			=> <<'EOD',
Owning country or agency.
EOD