----+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8
ELEMS1 8986390.0780 8283790.5802 -1502498.2249
----+----0----+----0----+----0----+----0----+----0----+----0----+----0----+----0
COLUMNS FORMAT DESCRIPTION DEFAULT VALUE & UNITS
1-6 A6 ELEMS1 - Introduces the first three
components of the orbital elements for
the S/C.
7 I1 Form of elements 0
0 - Either Cartesian or Keplerian
1 - Cartesian
2 - Keplerian
3 - Non-singular Keplerian
5 - Cartesian non-elliptic
6 - Keplerian non-elliptic
8 I1 Coordinate system of input elements NOTE(2) 0
11-14 I4 Central body for input elements. 300
0100 - Mercury
0200 - Venus
0300 - Earth
0301 - Earth's moon
0400 - Mars
0500 - Jupiter
0600 - Saturn
0700 - Uranus
0800 - Neptune
0900 - Pluto
9999 - Sun
DEC 1999
9912.0
ARC SET - MANDATORY CARDS
ELEMS1 (cont)
COLUMNS FORMAT DESCRIPTION DEFAULT VALUE & UNITS
21-40 D20.14 Element 1 see Table on next page 0 M
41-60 D20.14 Element 2 see Table on next page 0 M or none
61-80 D20.14 Element 3 see Table on next page 0 M, DEG
or none
UNITS: KM =Kilometers; M =Meters ; S =Seconds ; Kg =Kilograms
DEG=Degrees ; RAD=Radians ; AS =Arc seconds; MAS=Milli-arc seconds
NOTE: [1] GEODYN II expects the elements to be refered to the IAU system
regardless of which planet the S/C is orbiting about.
NOTE: [2] The coordinate system of input elements should be the same system
as specified on column 11 of the REFSYS option.