OBJECT E
NORAD 65548
Unknown
LEO
2025-199E
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LEO · NORAD 65548
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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
811 km
Inclination
86.0°
Period
100.9 min
Mean Motion
14.27181178 rev/day
TLE Epoch
2026-06-21 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude801 km
Orbital Velocity26,838 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.27
Eccentricity0.0014
Semi-Major Axis7,172 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-09-06
Launch Site
Taiyuan, China
Int'l Designator
2025-199E
Object Type
Unknown
RCS Size
Large (>1 m²)
📖 About This Object
OBJECT E (NORAD ID 65548) is a space object catalogued under China, launched on 2025-09-06 from Taiyuan, China on the Yaogan 40-03 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 811 km with an inclination of 86.0°. It travels at approximately 26,838 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.27 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks OBJECT E 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 E orbits at an average altitude of 801 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of OBJECT E’s average altitude, there are currently 442 active payloads and 2,253 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 86.0°, OBJECT E passes over latitudes between 86.0°N and 86.0°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. China operates approximately 1,218 active satellites in total, of which 106 share a similar altitude band with OBJECT E.
❓ Frequently Asked Questions
OBJECT E orbits in Low Earth Orbit (LEO) at altitudes between 791 km (perigee) and 811 km (apogee), with an average altitude of approximately 801 km. It completes one orbit every 101 minutes, travelling at approximately 26,838 km/h (16,676 mph).
OBJECT E was launched on 2025-09-06 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT E (NORAD ID 65548) 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 E travels at approximately 26,838 km/h (16,676 mph) — roughly 7.46 km/s. It completes 14.27 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.