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QUAKESAT (27845)
COSPAR: 2003-031F | Alt Name: QuakeSat
Image
Additional Sources
Launch Details
Launch Date
June 30, 2003
Launch Site
PLMSC
Launch Pad
LC133/3
Launch Vehicle
Rokot
Orbital Elements
NORAD ID
27845
International Designator
2003-031F
Epoch
Sat, 04 Jul 2026 00:17:07 GMT
Apogee
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Perigee
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Inclination
98.66°
Right Ascension
193.59°
Eccentricity
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Argument of Perigee
147.22°
Period
101.06 min
Mean Motion
14.25 rev/day
Latitude
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Longitude
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Altitude
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Velocity
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Polar Plot
3D Visualization
Basic Satellite Info
Name
QUAKESAT
Alternative Name
QuakeSat
Type
Payload
Status
Non-operational
Owner
QUAFI
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 27845U 03031F 26185.01188787 .00000439 00000-0 20647-3 0 9993
2 27845 98.6627 193.5934 0009230 147.2166 212.9588 14.24962685194007
Source: Celestrak
Summary
QUAKESAT (also known as QuakeSat) is a CubeSat (triple unit) satellite built by STAN for QUAFI and launched on June 30, 2003, from the Plesetsk Missile State Testing Range using a Rokot launch vehicle. Weighing in at 4 kilograms with dimensions of 0.3 meters in length, 0.1 meter diameter, and span of 0.6 meters, it was designed for Earth sciences missions. The satellite is equipped with a single axis search coil type magnetometer as its primary equipment and utilizes four deployable fixed solar arrays and batteries for power generation. QUAKESAT operated for an achieved lifetime of 1.5 years, surpassing the planned one-year mission duration.
Physical Characteristics
Length
0.3
Diameter
0.1
Span
0.6
Dry Mass
4
Launch Mass
4
Shape
Box + Ant
Radar Cross Section
0.2138
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
QuakeSat
Purpose
Earth sciences
Mission
Earth sciences
Manufacturer
STAN
Life Expectancy
1 year (planned), 1.5 years (achieved)
Bus
Cubesat 3U
Configuration
CubeSat (triple)
Motor
None
Equipment
single axis, search coil type magnetometer
Power System
4 deployable fixed solar arrays, solar cells, batteries
ADCS
Unknown
Transmitter Frequency
Unknown
Map
Next Pass
Azimuth Elevation Time (Local)
Start Azimuth
Max Elevation
Stop Azimuth
Time Until
Pass Duration
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