GAOFEN 13 DEB
NORAD 62337
Debris
GEO
2020-071C
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GEO · NORAD 62337
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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
32904 km
Apogee
38694 km
Inclination
3.1°
Period
1436.7 min
Mean Motion
1.00220569 rev/day
TLE Epoch
2026-09-04 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,799 km
Orbital Velocity11,068 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0687
Semi-Major Axis42,170 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 CNSA (China)
Launch Date
2020-10-11
Launch Site
Xichang, China
Int'l Designator
2020-071C
Object Type
Debris
RCS Size
Unknown
📖 About This Object
GAOFEN 13 DEB is a tracked piece of space debris attributed to China, launched on 2020-10-11 from Xichang, China on the Gao Fen 13 launch. It orbits in Geostationary Orbit (GEO) at altitudes between 32,904 km and 38,694 km with an inclination of 3.1°. It travels at approximately 11,068 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. As orbital debris, GAOFEN 13 DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
GAOFEN 13 DEB occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 3.1°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of GAOFEN 13 DEB’s average altitude, there are currently 709 active payloads and 59 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. China operates approximately 1,276 active satellites in total, of which 110 share a similar altitude band with GAOFEN 13 DEB.
🔗 Gaofen High-Resolution Imaging
This satellite is part of China's Gaofen high-resolution Earth observation programme, part of the China High-resolution Earth Observation System (CHEOS). Gaofen satellites provide sub-metre optical and radar imagery for agriculture, disaster monitoring, urban planning and environmental surveillance.
❓ Frequently Asked Questions
GAOFEN 13 DEB orbits at approximately 35,799 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 11,068 km/h — it just keeps pace with the ground below. With an inclination of 3.1°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
GAOFEN 13 DEB (NORAD ID 62337) is a piece of tracked orbital debris attributed to China. It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
GAOFEN 13 DEB was launched on 2020-10-11 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks GAOFEN 13 DEB (NORAD ID 62337) 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.
GAOFEN 13 DEB travels at approximately 11,068 km/h (6,877 mph) — roughly 3.07 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.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 3.07 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like GAOFEN 13 DEB. Read more about debris statistics and the Kessler syndrome.