STTW-T2
NORAD 14899
Payload
GEO
1984-035A
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GEO · NORAD 14899
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
35772 km
Apogee
35831 km
Inclination
9.4°
Period
1436.8 min
Mean Motion
1.00218922 rev/day
TLE Epoch
2026-06-18 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,802 km
Orbital Velocity11,068 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0007
Semi-Major Axis42,173 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
1984-04-08
Launch Site
Xichang, China
Int'l Designator
1984-035A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
STTW-T2 is an active satellite operated by China, launched on 1984-04-08 from Xichang, China. With over 42 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,772 km and 35,831 km with an inclination of 9.4°. 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 STTW-T2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
STTW-T2 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 9.4°, 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 STTW-T2’s average altitude, there are currently 715 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 111 share a similar altitude band with STTW-T2.
❓ Frequently Asked Questions
STTW-T2 orbits at approximately 35,802 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 9.4°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
STTW-T2 is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 14899. You can track STTW-T2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
STTW-T2 was launched on 1984-04-08 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks STTW-T2 (NORAD ID 14899) 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.
STTW-T2 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.