OBJECT E
NORAD 69576
Unknown
LEO
2026-137E
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LEO · NORAD 69576
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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
1006 km
Apogee
1007 km
Inclination
50.0°
Period
105.3 min
Mean Motion
13.68113530 rev/day
TLE Epoch
2026-07-29 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,007 km
Orbital Velocity26,462 km/h
Velocity7.35 km/s
Orbital Period105 minutes
Orbits / Day13.68
Eccentricity0.0001
Semi-Major Axis7,378 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-06-17
Launch Site
Wenchang, China
Int'l Designator
2026-137E
Object Type
Unknown
RCS Size
Large (>1 m²)
📖 About This Object
OBJECT E (NORAD ID 69576) is a space object catalogued under China, launched on 2026-06-17 from Wenchang, China on the WHDW 22 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 1,006 km and 1,007 km with an inclination of 50.0°. It travels at approximately 26,462 km/h (7.35 km/s), completing one full orbit every 105 minutes — that’s roughly 13.68 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 ~500–1,000 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 1,007 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 242 active payloads and 838 tracked debris or rocket body fragments. With an inclination of 50.0°, OBJECT E passes over latitudes between 50.0°N and 50.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,249 active satellites in total, of which 67 share a similar altitude band with OBJECT E.
❓ Frequently Asked Questions
OBJECT E orbits in Low Earth Orbit (LEO) at altitudes between 1,006 km (perigee) and 1,007 km (apogee), with an average altitude of approximately 1,007 km. It completes one orbit every 105 minutes, travelling at approximately 26,462 km/h (16,442 mph).
OBJECT E was launched on 2026-06-17 from Wenchang, China, China’s newest coastal launch facility on Hainan Island, used for heavy-lift Long March 5 missions. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT E (NORAD ID 69576) 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 26,462 km/h (16,442 mph) — roughly 7.35 km/s. It completes 13.68 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.