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BEESAT-1

NORAD 35933 Payload LEO 2009-051C ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
684 km
Apogee
692 km
Inclination
98.4°
Period
98.5 min
Mean Motion
14.61551734 rev/day
TLE Epoch
2026-03-17 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude688 km
Orbital Velocity27,052 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.62
Eccentricity0.0006
Semi-Major Axis7,059 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇩🇪 Germany
Launch Date
2009-09-23
Launch Site
SRI
Int'l Designator
2009-051C
Object Type
Payload
RCS Size
Small (<0.1 m²)
🔗 Constellation / Groups
cubesatamateur
📖 About This Object
BEESAT-1 is an active satellite operated by Germany, launched on 2009-09-23 from SRI. After 17 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 684 km and 692 km with an inclination of 98.4°. It travels at approximately 27,052 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.62 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. It is part of the Cubesat constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks BEESAT-1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
BEESAT-1 operates in a sun-synchronous orbit (SSO), a special subset of LEO where the orbital plane precesses to keep a constant angle relative to the Sun. This means the satellite crosses any given latitude at approximately the same local solar time on every pass, providing consistent lighting conditions — essential for Earth observation, weather monitoring and environmental science. SSO orbits typically sit between 600 and 800 km altitude with inclinations near 97–99°.
❓ Frequently Asked Questions
BEESAT-1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 688 km altitude. Its 98.4° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 99 minutes, travelling at 27,052 km/h.
BEESAT-1 is operated by Germany. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 35933. You can track BEESAT-1 in real time on Orbital Radar’s live tracker.
BEESAT-1 was launched on 2009-09-23 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years.
Yes — Orbital Radar tracks BEESAT-1 (NORAD ID 35933) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time.
BEESAT-1 travels at approximately 27,052 km/h (16,809 mph) — roughly 7.51 km/s. It completes 14.62 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.
BEESAT-1 is a member of the Cubesat constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Cubesat satellites on Orbital Radar’s live tracker.