Orbital Minotaur I - Manual (Page 88)

Minotaur I User’s Guide Appendix A
SATELLITE IDENTIFICATION
FULL NAME:
ACRONYM:
OWNER/OPERATOR:
INTEGRATOR(s):
SPACE CRAFT AND
MISSION DESCRIPTION
ORBIT INSERTION REQUIREMENTS*
SPHEROID  Standard (WGS-84, R
e
= 6378.137 km)
 Other:
ALTITUDE Insertion Apse: Opposite Apse:
±
 nmi
 km ±
 nmi
 km
or... Semi-Major Axis: Eccentricity:
±
 nmi
 km ≤ e ≤
INCLINATION
± deg
ORIENTATION Argument of Perigee: Longitude of Ascending Node (LAN):
± deg ± deg
Right Ascension of Ascending Node (RAAN):
± deg For Launch Date:
* Note: Mean orbital elements
Release 3.0 March 2014 A-2