OBJECT E
NORAD 55137
Unknown
LEO
2023-003E
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LEO · NORAD 55137
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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
398 km
Apogee
405 km
Inclination
97.1°
Period
92.6 min
Mean Motion
15.55323637 rev/day
TLE Epoch
2026-06-21 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude402 km
Orbital Velocity27,618 km/h
Velocity7.67 km/s
Orbital Period93 minutes
Orbits / Day15.55
Eccentricity0.0005
Semi-Major Axis6,773 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Shanghai Weixing Keji (China)
Launch Date
2023-01-09
Launch Site
Jiuquan, China
Int'l Designator
2023-003E
Object Type
Unknown
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OBJECT E (NORAD ID 55137) is a space object catalogued under China, launched on 2023-01-09 from Jiuquan, China on the Keji-1/Tianmu/Tianqi launch. It orbits in Low Earth Orbit (LEO) at altitudes between 398 km and 405 km with an inclination of 97.1°. It travels at approximately 27,618 km/h (7.67 km/s), completing one full orbit every 93 minutes — that’s roughly 15.55 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 ~1–3 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 402 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 1,355 active payloads and 97 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 7.8% of all active satellites. With an inclination of 97.1°, OBJECT E passes over latitudes between 97.1°N and 97.1°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 44 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 402 km altitude. Its 97.1° 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 93 minutes, travelling at 27,618 km/h.
OBJECT E was launched on 2023-01-09 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT E (NORAD ID 55137) 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 27,618 km/h (17,161 mph) — roughly 7.67 km/s. It completes 15.55 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.