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STTW-2

NORAD 18922 Payload GEO 1988-014A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35760 km
Apogee
35797 km
Inclination
13.3°
Period
1435.7 min
Mean Motion
1.00302206 rev/day
TLE Epoch
2026-06-19 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,779 km
Orbital Velocity11,071 km/h
Velocity3.08 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0004
Semi-Major Axis42,150 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
1988-03-07
Launch Site
Xichang, China
Int'l Designator
1988-014A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
STTW-2 is an active satellite operated by China, launched on 1988-03-07 from Xichang, China. With over 38 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,760 km and 35,797 km with an inclination of 13.3°. It travels at approximately 11,071 km/h (3.08 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-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
STTW-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 13.3°, 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-2’s average altitude, there are currently 706 active payloads and 60 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. China operates approximately 1,218 active satellites in total, of which 106 share a similar altitude band with STTW-2.
❓ Frequently Asked Questions
STTW-2 orbits at approximately 35,779 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 11,071 km/h — it just keeps pace with the ground below. With an inclination of 13.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
STTW-2 is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 18922. You can track STTW-2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
STTW-2 was launched on 1988-03-07 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks STTW-2 (NORAD ID 18922) 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-2 travels at approximately 11,071 km/h (6,879 mph) — roughly 3.08 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.