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BSAT-2A

NORAD 26720 Payload GEO 2001-011B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36073 km
Apogee
36120 km
Inclination
10.5°
Period
1452.0 min
Mean Motion
0.99176079 rev/day
TLE Epoch
2026-03-17 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,097 km
Orbital Velocity11,029 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0006
Semi-Major Axis42,468 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2001-03-08
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2001-011B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
BSAT-2A is an active satellite operated by Japan, launched on 2001-03-08 from Guiana Space Centre, Kourou. With over 25 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,073 km and 36,120 km with an inclination of 10.5°. It travels at approximately 11,029 km/h (3.06 km/s), completing one full orbit every 24.2 hours — that’s roughly 0.99 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks BSAT-2A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
BSAT-2A occupies geostationary orbit (GEO) at approximately 35,786 km above the equator. At this precise altitude, the satellite’s orbital period matches the Earth’s rotation — so it appears to hover over a fixed point on the equator. GEO is used primarily for broadcast television, weather monitoring (Meteosat, GOES) and wideband communications. Only about 560 active satellites occupy the GEO belt, but its commercial value is immense: a single GEO slot can cover roughly one-third of the Earth’s surface. This satellite has a non-zero inclination of 10.5°, meaning it traces a small figure-of-eight pattern relative to the ground rather than remaining perfectly stationary. This can indicate an aging satellite whose stationkeeping fuel is running low, or a deliberate inclined-orbit strategy to extend operational life.
❓ Frequently Asked Questions
BSAT-2A orbits at approximately 36,097 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,029 km/h — it just keeps pace with the ground below. With an inclination of 10.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed.
BSAT-2A is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26720. You can track BSAT-2A in real time on Orbital Radar’s live tracker.
BSAT-2A was launched on 2001-03-08 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions.
Yes — Orbital Radar tracks BSAT-2A (NORAD ID 26720) 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.
BSAT-2A travels at approximately 11,029 km/h (6,853 mph) — roughly 3.06 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.