Polysat CP4

CalPoly 4, an exact replica of Polysat CP2

---

General

Designation	31132 / 07012Q
Launch date	17 Apr 2007
Country of origin	United States
Mission	Technology
Perigee/Apogee	646/793 km
Inclination	98°
Period	99 min
Launch vehicle	Dnepr #8

Built by California Polytech. The primary mission of CP3 is to implement an attitude control system using only magnetic torquers embedded within the side panels.

1 kg, downlink 437.325 MHz

CP 2 was destroyed in the Jul 2006 Dnepr launch failure.

---

External resources

http://www.polysat.calpoly.edu/CP2.php

sat-index articles

---