OBJECT A
NORAD 65226
Unknown
LEO
2025-177A
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LEO · NORAD 65226
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
791 km
Apogee
796 km
Inclination
11.0°
Period
100.7 min
Mean Motion
14.29399690 rev/day
TLE Epoch
2026-06-20 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude794 km
Orbital Velocity26,852 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.29
Eccentricity0.0003
Semi-Major Axis7,165 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-08-17
Launch Site
Xichang, China
Int'l Designator
2025-177A
Object Type
Unknown
RCS Size
Large (>1 m²)
📖 About This Object
OBJECT A (NORAD ID 65226) is a space object catalogued under China, launched on 2025-08-17 from Xichang, China on the SY28B-02 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 791 km and 796 km with an inclination of 11.0°. It travels at approximately 26,852 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.29 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks OBJECT A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OBJECT A orbits at an average altitude of 794 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of OBJECT A’s average altitude, there are currently 428 active payloads and 2,255 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 11.0°, OBJECT A passes over latitudes between 11.0°N and 11.0°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. China operates approximately 1,218 active satellites in total, of which 96 share a similar altitude band with OBJECT A.
❓ Frequently Asked Questions
OBJECT A orbits in Low Earth Orbit (LEO) at altitudes between 791 km (perigee) and 796 km (apogee), with an average altitude of approximately 794 km. It completes one orbit every 101 minutes, travelling at approximately 26,852 km/h (16,685 mph).
OBJECT A was launched on 2025-08-17 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT A (NORAD ID 65226) 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.
OBJECT A travels at approximately 26,852 km/h (16,685 mph) — roughly 7.46 km/s. It completes 14.29 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.