DFH-3 2
NORAD 24798
Payload
GEO
1997-021A
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GEO · NORAD 24798
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Altitude (km)
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Longitude
🛰️ Orbital Parameters
Perigee
35767 km
Apogee
35833 km
Inclination
13.5°
Period
1436.8 min
Mean Motion
1.00223351 rev/day
TLE Epoch
2026-06-18 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,800 km
Orbital Velocity11,068 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0008
Semi-Major Axis42,171 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
1997-05-11
Launch Site
Xichang, China
Int'l Designator
1997-021A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
DFH-3 2 is an active satellite operated by China, launched on 1997-05-11 from Xichang, China. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,767 km and 35,833 km with an inclination of 13.5°. 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. Orbital Radar tracks DFH-3 2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
DFH-3 2 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 13.5°, 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 DFH-3 2’s average altitude, there are currently 713 active payloads and 64 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. China operates approximately 1,219 active satellites in total, of which 110 share a similar altitude band with DFH-3 2.
❓ Frequently Asked Questions
DFH-3 2 orbits at approximately 35,800 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 13.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
DFH-3 2 is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24798. You can track DFH-3 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DFH-3 2 was launched on 1997-05-11 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks DFH-3 2 (NORAD ID 24798) 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.
DFH-3 2 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.