Orbital Antares - Manual (Page 88)

Antares
®
OSP-3
User’s Guide
Appendix A
– Payload Questionnaire
Release 1.1 July 2013 A-2
SPACECRAFT IDENTIFICATION
FULL NAME:
ACRONYM:
OWNER/OPERATOR:
INTEGRATOR(s):
ORBIT INSERTION REQUIREMENTS*
SPHEROID  Standard
 Other:
ALTITUDE Insertion Apse:
±  km
±  nmi
Opposite Apse:
±  km
±  nmi
or... Semi-Major Axis:
±  km
±  nmi
Eccentricity:

e

INCLINATION
± deg
ORIENTATION Argument of Perigee:
± deg
Longitude of Ascending Node (LAN):
± deg
Right Ascension of Ascending Node (RAAN):
± deg...for Launch Date:
* Note: Mean orbital elements
LAUNCH WINDOW REQUIREMENTS
NOMINAL LAUNCH DATE:
OTHER CONSTRAINTS (if not already implicit from LAN or RAAN requirements, e.g., solar beta angle, eclipse
time constraints, early on-orbit ops, etc):