OBJECT E
NORAD 100795
Unknown
LEO
2026-221E
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LEO · NORAD 100795
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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
1094 km
Apogee
1104 km
Inclination
50.0°
Period
107.2 min
Mean Motion
13.42762289 rev/day
TLE Epoch
2026-09-25 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,099 km
Orbital Velocity26,297 km/h
Velocity7.30 km/s
Orbital Period107 minutes
Orbits / Day13.43
Eccentricity0.0007
Semi-Major Axis7,470 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-09-23
Launch Site
Wenchang Space Launch Site, China
Int'l Designator
2026-221E
Object Type
Unknown
RCS Size
Unknown
📖 About This Object
OBJECT E (NORAD ID 100795) is a space object catalogued under China, launched on 2026-09-23 from Wenchang Space Launch Site, China on the WHDW 26 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 1,094 km and 1,104 km with an inclination of 50.0°. It travels at approximately 26,297 km/h (7.30 km/s), completing one full orbit every 107 minutes — that’s roughly 13.43 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 1,099 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 333 active payloads and 509 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 50.0°, OBJECT E passes over latitudes between 50.0°N and 50.0°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. China operates approximately 1,291 active satellites in total, of which 282 share a similar altitude band with OBJECT E.
❓ Frequently Asked Questions
OBJECT E orbits in Low Earth Orbit (LEO) at altitudes between 1,094 km (perigee) and 1,104 km (apogee), with an average altitude of approximately 1,099 km. It completes one orbit every 107 minutes, travelling at approximately 26,297 km/h (16,340 mph).
OBJECT E was launched on 2026-09-23 from Wenchang Space Launch Site, 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 100795) 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 26,297 km/h (16,340 mph) — roughly 7.30 km/s. It completes 13.43 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.