OBJECT A
NORAD 65938
Payload
LEO
2025-226A
● Active
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LEO · NORAD 65938
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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
502 km
Apogee
521 km
Inclination
97.6°
Period
94.8 min
Mean Motion
15.18178228 rev/day
TLE Epoch
2026-11-03 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude512 km
Orbital Velocity27,397 km/h
Velocity7.61 km/s
Orbital Period95 minutes
Orbits / Day15.18
Eccentricity0.0014
Semi-Major Axis6,883 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Changguang WJ (China)
Launch Date
2025-10-11
Launch Site
Yellow Sea launch area (Haiyang), China
Int'l Designator
2025-226A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OBJECT A is an active satellite operated by Changguang WJ (China), launched on 2025-10-11 from Yellow Sea launch area (Haiyang), China on the Jilin-1 Kuanfu 02B07 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. Independent catalogue analysis identifies this object as Jilin-1 Kuanfu-02B 07, attributed to Chang Guang. It orbits in Low Earth Orbit (LEO) at altitudes between 502 km and 521 km with an inclination of 97.6°. It travels at approximately 27,397 km/h (7.61 km/s), completing one full orbit every 95 minutes — that’s roughly 15.18 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 A 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 A orbits at an average altitude of 512 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 A’s average altitude, there are currently 10,758 active payloads and 269 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 54.8% of all active satellites. With an inclination of 97.6°, OBJECT A 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 1,650 active satellites in total, of which 430 share a similar altitude band with OBJECT A.
❓ Frequently Asked Questions
OBJECT A is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 512 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 95 minutes, travelling at 27,397 km/h.
OBJECT A is operated by Changguang WJ (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 65938. You can track OBJECT A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OBJECT A was launched on 2025-10-11 from Yellow Sea launch area (Haiyang), China. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT A (NORAD ID 65938) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 A travels at approximately 27,397 km/h (17,024 mph) — roughly 7.61 km/s. It completes 15.18 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.