OBJECT E
NORAD 66997
Unknown
LEO
2025-292E
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LEO · NORAD 66997
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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
537 km
Apogee
557 km
Inclination
97.6°
Period
95.6 min
Mean Motion
15.06412146 rev/day
TLE Epoch
2026-06-20 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude547 km
Orbital Velocity27,326 km/h
Velocity7.59 km/s
Orbital Period96 minutes
Orbits / Day15.06
Eccentricity0.0014
Semi-Major Axis6,918 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-12-10
Launch Site
Jiuquan, China
Int'l Designator
2025-292E
Object Type
Unknown
RCS Size
Large (>1 m²)
📖 About This Object
OBJECT E (NORAD ID 66997) is a space object catalogued under China, launched on 2025-12-10 from Jiuquan, China on the Jilin-1/UAE-813 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 537 km and 557 km with an inclination of 97.6°. It travels at approximately 27,326 km/h (7.59 km/s), completing one full orbit every 96 minutes — that’s roughly 15.06 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 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 547 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 3,496 active payloads and 353 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 20.1% of all active satellites. With an inclination of 97.6°, OBJECT E passes over latitudes between 97.6°N and 97.6°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 1,217 active satellites in total, of which 181 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 547 km altitude. Its 97.6° 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 96 minutes, travelling at 27,326 km/h.
OBJECT E was launched on 2025-12-10 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT E (NORAD ID 66997) 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 27,326 km/h (16,980 mph) — roughly 7.59 km/s. It completes 15.06 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.