Skip to content
Home Library Satellite Directory OBJECT A

OBJECT A

NORAD 52153 Unknown LEO 2022-032A
CONNECTING… LEO · NORAD 52153
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
568 km
Apogee
583 km
Inclination
97.6°
Period
96.2 min
Mean Motion
14.97212595 rev/day
TLE Epoch
2026-06-21 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude576 km
Orbital Velocity27,270 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day14.97
Eccentricity0.0011
Semi-Major Axis6,947 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2022-03-30
Launch Site
Jiuquan, China
Int'l Designator
2022-032A
Object Type
Unknown
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OBJECT A (NORAD ID 52153) is a space object catalogued under China, launched on 2022-03-30 from Jiuquan, China on the Tianping-2A/2B/2C launch. It orbits in Low Earth Orbit (LEO) at altitudes between 568 km and 583 km with an inclination of 97.6°. It travels at approximately 27,270 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 14.97 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 576 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 3,070 active payloads and 511 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-2112, STARLINK-2722. This makes it one of the more crowded altitude bands, containing roughly 17.6% 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 1,218 active satellites in total, of which 178 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 576 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 27,270 km/h.
OBJECT A was launched on 2022-03-30 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 A (NORAD ID 52153) 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 27,270 km/h (16,945 mph) — roughly 7.58 km/s. It completes 14.97 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.