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EQUISAT

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EQUISAT is classified as:


NORAD ID: 43552
Int'l Code: 1998-067PA
Perigee: 385.0 km
Apogee: 391.9 km
Inclination: 51.6 °
Period: 92.2 minutes
Semi major axis: 6759 km
RCS: Unknown
Launch date: November 20, 1998
Source: United States (US)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

Uplink (MHz):
Downlink (MHz): 435.550
Beacon (MHz): 435.550
Mode: 4k8/9k6 4LFSK CW LED
Call sign:
Status: Active


EQUISAT is a 1U (one unit) CubeSat designed and built by Brown Space Engineering (formerly Brown CubeSat Team), an undergraduate student group at Brown University's School of Engineering. The primary mission of EQUiSat is to prove the accessibility of space to the masses through both demonstration of a low-cost DIY CubeSat and educational outreach. To further the primary mission, Brown Space Engineering will maintain EQUiSat as a low-cost and rigorously documented open source project, allowing others to replicate EQUiSat’s subsystems without large budgets or extensive expertise. The total cost of parts to reproduce EQUiSat is around $5,000
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 43552U 98067PA  19200.37930919 +.00006803 +00000-0 +81715-4 0  9995
2 43552 051.6374 187.2821 0005118 264.7778 095.2632 15.62187304057817
Source of the keplerian elements: AMSAT