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OBJECT E

NORAD 49047 Unknown LEO 2021-062E
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
794 km
Apogee
803 km
Inclination
98.7°
Period
100.8 min
Mean Motion
14.27866792 rev/day
TLE Epoch
2026-06-20 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude799 km
Orbital Velocity26,843 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.28
Eccentricity0.0006
Semi-Major Axis7,170 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2021-07-04
Launch Site
Jiuquan, China
Int'l Designator
2021-062E
Object Type
Unknown
RCS Size
Small (<0.1 m²)
📖 About This Object
OBJECT E (NORAD ID 49047) is a space object catalogued under China, launched on 2021-07-04 from Jiuquan, China on the FY-3E launch. It orbits in Low Earth Orbit (LEO) at altitudes between 794 km and 803 km with an inclination of 98.7°. It travels at approximately 26,843 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.28 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. 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 ~25–100 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 799 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of OBJECT E’s average altitude, there are currently 438 active payloads and 2,254 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.7°, OBJECT E passes over latitudes between 98.7°N and 98.7°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 100 share a similar altitude band with OBJECT E.
❓ Frequently Asked Questions
OBJECT E is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 799 km altitude. Its 98.7° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 101 minutes, travelling at 26,843 km/h.
OBJECT E was launched on 2021-07-04 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT E (NORAD ID 49047) 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 26,843 km/h (16,679 mph) — roughly 7.46 km/s. It completes 14.28 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.