OBJECT A
NORAD 66175
Unknown
LEO
2025-242A
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LEO · NORAD 66175
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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
488 km
Apogee
503 km
Inclination
97.4°
Period
94.5 min
Mean Motion
15.23430728 rev/day
TLE Epoch
2026-09-18 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude496 km
Orbital Velocity27,429 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.23
Eccentricity0.0011
Semi-Major Axis6,867 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Yaogan Zongti (China)
Launch Date
2025-10-26
Launch Site
Xichang Satellite Launch Center, China
Int'l Designator
2025-242A
Object Type
Unknown
RCS Size
Large (>1 m²)
📖 About This Object
OBJECT A (NORAD ID 66175) is a space object catalogued under China, launched on 2025-10-26 from Xichang Satellite Launch Center, China on the GF14-02 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. Independent catalogue analysis identifies this object as Gaofen 14-02, attributed to Yaogan Zongti. It orbits in Low Earth Orbit (LEO) at altitudes between 488 km and 503 km with an inclination of 97.4°. It travels at approximately 27,429 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.23 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 ~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 496 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 10,267 active payloads and 220 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 54.9% of all active satellites. With an inclination of 97.4°, OBJECT A passes over latitudes between 97.4°N and 97.4°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 1,288 active satellites in total, of which 193 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 496 km altitude. Its 97.4° 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 27,429 km/h.
OBJECT A was launched on 2025-10-26 from Xichang Satellite Launch Center, China. 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 66175) 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 27,429 km/h (17,043 mph) — roughly 7.62 km/s. It completes 15.23 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.