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CHINASAT 7

NORAD 24282 Payload HEO 1996-048A ● Active
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Longitude
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🛰️ Orbital Parameters
Perigee
19926 km
Apogee
48247 km
Inclination
16.6°
Period
1350.1 min
Mean Motion
1.06658281 rev/day
TLE Epoch
2026-10-31 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude34,087 km
Orbital Velocity11,300 km/h
Velocity3.14 km/s
Orbital Period22 hours 30 minutes
Orbits / Day1.07
Eccentricity0.3500
Semi-Major Axis40,458 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 Chinasat (China)
Launch Date
1996-08-18
Launch Site
Xichang Satellite Launch Center, China
Int'l Designator
1996-048A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
CHINASAT 7 is an active satellite operated by Chinasat (China), launched on 1996-08-18 from Xichang Satellite Launch Center, China on the Zhongxing 7 launch. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 19,926 km and 48,247 km with an inclination of 16.6°. It travels at approximately 11,300 km/h (3.14 km/s), completing one full orbit every 22 hours 30 minutes — that’s roughly 1.07 orbits per day. Its orbital eccentricity of 0.3500 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks CHINASAT 7 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CHINASAT 7 follows a Highly Elliptical Orbit, sweeping between 19,926 km (perigee) and 48,247 km (apogee). It spends most of its 22 hours 30 minutes orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. Within ±50 km of CHINASAT 7’s average altitude, there are currently 2 active payloads and 1 tracked debris or rocket body fragment. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 16.6°, CHINASAT 7 passes over latitudes between 16.6°N and 16.6°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. China operates approximately 1,341 active satellites in total.
❓ Frequently Asked Questions
CHINASAT 7 follows a Highly Elliptical Orbit, swinging between 19,926 km (perigee) and 48,247 km (apogee). It spends most of its 22 hours 30 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
CHINASAT 7 is operated by Chinasat (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24282. You can track CHINASAT 7 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CHINASAT 7 was launched on 1996-08-18 from Xichang Satellite Launch Center, China. View the full satellite launch log.
Yes — Orbital Radar tracks CHINASAT 7 (NORAD ID 24282) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
CHINASAT 7’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 11,300 km/h (3.14 km/s), completing one revolution every 22 hours 30 minutes. Learn more about highly elliptical orbits.