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OBJECT E

NORAD 69586 Unknown LEO 2026-138E
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
833 km
Apogee
845 km
Inclination
55.1°
Period
101.7 min
Mean Motion
14.15995528 rev/day
TLE Epoch
2026-06-21 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude839 km
Orbital Velocity26,767 km/h
Velocity7.44 km/s
Orbital Period102 minutes
Orbits / Day14.16
Eccentricity0.0008
Semi-Major Axis7,210 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-06-17
Launch Site
Jiuquan, China
Int'l Designator
2026-138E
Object Type
Unknown
RCS Size
Unknown
📖 About This Object
OBJECT E (NORAD ID 69586) is a space object catalogued under China, launched on 2026-06-17 from Jiuquan, China on the Centispace 05 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 833 km and 845 km with an inclination of 55.1°. It travels at approximately 26,767 km/h (7.44 km/s), completing one full orbit every 102 minutes — that’s roughly 14.16 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 ~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 839 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 263 active payloads and 2,148 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 55.1°, OBJECT E passes over latitudes between 55.1°N and 55.1°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 121 share a similar altitude band with OBJECT E.
❓ Frequently Asked Questions
OBJECT E orbits in Low Earth Orbit (LEO) at altitudes between 833 km (perigee) and 845 km (apogee), with an average altitude of approximately 839 km. It completes one orbit every 102 minutes, travelling at approximately 26,767 km/h (16,632 mph).
OBJECT E was launched on 2026-06-17 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. 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 69586) 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 26,767 km/h (16,632 mph) — roughly 7.44 km/s. It completes 14.16 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.