OBJECT BE
NORAD 43810
Unknown
LEO
2018-099BE
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LEO · NORAD 43810
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
530 km
Apogee
539 km
Inclination
97.4°
Period
95.3 min
Mean Motion
15.10694354 rev/day
TLE Epoch
2026-06-20 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude535 km
Orbital Velocity27,351 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.11
Eccentricity0.0007
Semi-Major Axis6,906 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
Unknown
Launch Date
2018-12-03
Launch Site
Vandenberg SFB, California
Int'l Designator
2018-099BE
Object Type
Unknown
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OBJECT BE (NORAD ID 43810) is a space object catalogued under Unknown, launched on 2018-12-03 from Vandenberg SFB, California on the SSO-A launch. It orbits in Low Earth Orbit (LEO) at altitudes between 530 km and 539 km with an inclination of 97.4°. It travels at approximately 27,351 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.11 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks OBJECT BE in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OBJECT BE orbits at an average altitude of 535 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of OBJECT BE’s average altitude, there are currently 3,510 active payloads and 312 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 20.1% of all active satellites. With an inclination of 97.4°, OBJECT BE passes over latitudes between 97.4°N and 97.4°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet.
❓ Frequently Asked Questions
OBJECT BE is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 535 km altitude. Its 97.4° 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 95 minutes, travelling at 27,351 km/h.
OBJECT BE was launched on 2018-12-03 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT BE (NORAD ID 43810) 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. You can also browse the satellite directory to find other tracked objects.
OBJECT BE travels at approximately 27,351 km/h (16,995 mph) — roughly 7.60 km/s. It completes 15.11 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.