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OBJECT A

NORAD 65945 Unknown LEO 2025-227A
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
488 km
Apogee
502 km
Inclination
80.0°
Period
94.5 min
Mean Motion
15.23602049 rev/day
TLE Epoch
2026-06-20 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude495 km
Orbital Velocity27,430 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.24
Eccentricity0.0010
Semi-Major Axis6,866 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-10-13
Launch Site
Jiuquan, China
Int'l Designator
2025-227A
Object Type
Unknown
RCS Size
Large (>1 m²)
📖 About This Object
OBJECT A (NORAD ID 65945) is a space object catalogued under China, launched on 2025-10-13 from Jiuquan, China on the Shiyan 31 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 488 km and 502 km with an inclination of 80.0°. It travels at approximately 27,430 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.24 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 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 495 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of OBJECT A’s average altitude, there are currently 9,168 active payloads and 233 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 52.6% of all active satellites. With an inclination of 80.0°, OBJECT A passes over latitudes between 80.0°N and 80.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,218 active satellites in total, of which 190 share a similar altitude band with OBJECT A.
❓ Frequently Asked Questions
OBJECT A orbits in Low Earth Orbit (LEO) at altitudes between 488 km (perigee) and 502 km (apogee), with an average altitude of approximately 495 km. It completes one orbit every 95 minutes, travelling at approximately 27,430 km/h (17,044 mph).
OBJECT A was launched on 2025-10-13 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 A (NORAD ID 65945) 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 A travels at approximately 27,430 km/h (17,044 mph) — roughly 7.62 km/s. It completes 15.24 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.