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CHINASAT 7

NORAD 24282 Payload HEO 1996-048A ● Active
CONNECTING… HEO · NORAD 24282
NOW PASSING OVER
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
19871 km
Apogee
48301 km
Inclination
16.6°
Period
1350.1 min
Mean Motion
1.06658884 rev/day
TLE Epoch
2026-06-19 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude34,086 km
Orbital Velocity11,300 km/h
Velocity3.14 km/s
Orbital Period22 hours 30 minutes
Orbits / Day1.07
Eccentricity0.3514
Semi-Major Axis40,457 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Satellite Communications (China)
Launch Date
1996-08-18
Launch Site
Xichang, 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 China Satellite Communications (China), launched on 1996-08-18 from Xichang, China. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 19,871 km and 48,301 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 0.3514 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 19,871 km (perigee) and 48,301 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. 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 1,219 active satellites in total.
❓ Frequently Asked Questions
CHINASAT 7 follows a Highly Elliptical Orbit, swinging between 19,871 km (perigee) and 48,301 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 China Satellite Communications (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, China. View the full satellite launch log.
Yes — Orbital Radar tracks CHINASAT 7 (NORAD ID 24282) 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.
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.