Skip to content
Home Library Satellite Directory OBJECT A

OBJECT A

NORAD 69572 Unknown LEO 2026-137A
CONNECTING… LEO · NORAD 69572
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
1019 km
Apogee
1020 km
Inclination
50.0°
Period
105.5 min
Mean Motion
13.64525385 rev/day
TLE Epoch
2026-08-01 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,020 km
Orbital Velocity26,438 km/h
Velocity7.34 km/s
Orbital Period106 minutes
Orbits / Day13.65
Eccentricity0.0001
Semi-Major Axis7,391 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-06-17
Launch Site
Wenchang, China
Int'l Designator
2026-137A
Object Type
Unknown
RCS Size
Large (>1 m²)
📖 About This Object
OBJECT A (NORAD ID 69572) is a space object catalogued under China, launched on 2026-06-17 from Wenchang, China on the WHDW 22 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 1,019 km and 1,020 km with an inclination of 50.0°. It travels at approximately 26,438 km/h (7.34 km/s), completing one full orbit every 106 minutes — that’s roughly 13.65 orbits per day. 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 ~500–1,000 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 1,020 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of OBJECT A’s average altitude, there are currently 357 active payloads and 745 tracked debris or rocket body fragments. With an inclination of 50.0°, OBJECT A passes over latitudes between 50.0°N and 50.0°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. China operates approximately 1,249 active satellites in total, of which 192 share a similar altitude band with OBJECT A.
❓ Frequently Asked Questions
OBJECT A orbits in Low Earth Orbit (LEO) at altitudes between 1,019 km (perigee) and 1,020 km (apogee), with an average altitude of approximately 1,020 km. It completes one orbit every 106 minutes, travelling at approximately 26,438 km/h (16,428 mph).
OBJECT A was launched on 2026-06-17 from Wenchang, China, China’s newest coastal launch facility on Hainan Island, used for heavy-lift Long March 5 missions. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT A (NORAD ID 69572) 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 26,438 km/h (16,428 mph) — roughly 7.34 km/s. It completes 13.65 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.