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OBJECT E

NORAD 51950 Unknown LEO 2022-023E
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
930 km
Apogee
1168 km
Inclination
63.5°
Period
106.2 min
Mean Motion
13.56287580 rev/day
TLE Epoch
2026-06-21 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,049 km
Orbital Velocity26,386 km/h
Velocity7.33 km/s
Orbital Period106 minutes
Orbits / Day13.56
Eccentricity0.0160
Semi-Major Axis7,420 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Galaxy Space (China)
Launch Date
2022-03-05
Launch Site
Xichang, China
Int'l Designator
2022-023E
Object Type
Unknown
RCS Size
Large (>1 m²)
📖 About This Object
OBJECT E (NORAD ID 51950) is a space object catalogued under China, launched on 2022-03-05 from Xichang, China on the Yinhe 2-01/06 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 930 km and 1,168 km with an inclination of 63.5°. It travels at approximately 26,386 km/h (7.33 km/s), completing one full orbit every 106 minutes — that’s roughly 13.56 orbits per day. 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 1,049 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 178 active payloads and 475 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 63.5°, OBJECT E passes over latitudes between 63.5°N and 63.5°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,217 active satellites in total, of which 150 share a similar altitude band with OBJECT E.
❓ Frequently Asked Questions
OBJECT E orbits in Low Earth Orbit (LEO) at altitudes between 930 km (perigee) and 1,168 km (apogee), with an average altitude of approximately 1,049 km. It completes one orbit every 106 minutes, travelling at approximately 26,386 km/h (16,395 mph).
OBJECT E was launched on 2022-03-05 from Xichang, China. 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 51950) 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 26,386 km/h (16,395 mph) — roughly 7.33 km/s. It completes 13.56 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.