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TJS-3

NORAD 43874 Payload GEO 2018-110A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35778 km
Apogee
35796 km
Inclination
2.5°
Period
1436.1 min
Mean Motion
1.00270373 rev/day
TLE Epoch
2026-06-17 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,787 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0002
Semi-Major Axis42,158 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Academy of Space Technology (CAST) (China)
Launch Date
2018-12-24
Launch Site
Xichang, China
Int'l Designator
2018-110A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
TJS-3 is an active satellite operated by China Academy of Space Technology (CAST) (China), launched on 2018-12-24 from Xichang, China. It orbits in Geostationary Orbit (GEO) at altitudes between 35,778 km and 35,796 km with an inclination of 2.5°. It travels at approximately 11,070 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 TJS-3 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TJS-3 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 2.5°, 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 TJS-3’s average altitude, there are currently 713 active payloads and 58 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 108 share a similar altitude band with TJS-3.
❓ Frequently Asked Questions
TJS-3 orbits at approximately 35,787 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 11,070 km/h — it just keeps pace with the ground below. With an inclination of 2.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
TJS-3 is operated by China Academy of Space Technology (CAST) (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43874. You can track TJS-3 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TJS-3 was launched on 2018-12-24 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks TJS-3 (NORAD ID 43874) 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.
TJS-3 travels at approximately 11,070 km/h (6,878 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.