YAOGAN 29 DEB
NORAD 42673
Debris
LEO
2015-069F
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LEO · NORAD 42673
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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
592 km
Apogee
597 km
Inclination
97.9°
Period
96.6 min
Mean Motion
14.91191930 rev/day
TLE Epoch
2026-06-19 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude595 km
Orbital Velocity27,233 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.91
Eccentricity0.0004
Semi-Major Axis6,966 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2015-11-26
Launch Site
Taiyuan, China
Int'l Designator
2015-069F
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
YAOGAN 29 DEB is a tracked piece of space debris attributed to China, launched on 2015-11-26 from Taiyuan, China. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 592 km and 597 km with an inclination of 97.9°. It travels at approximately 27,233 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.91 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. 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 ~3–10 years. As orbital debris, YAOGAN 29 DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
YAOGAN 29 DEB orbits at an average altitude of 595 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 YAOGAN 29 DEB’s average altitude, there are currently 2,119 active payloads and 624 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 12.2% of all active satellites. With an inclination of 97.9°, YAOGAN 29 DEB passes over latitudes between 97.9°N and 97.9°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 YAOGAN 29 DEB.
🔗 Yaogan Reconnaissance Series
This satellite is part of China's Yaogan series, officially described as “remote sensing” satellites but widely assessed by analysts to serve military reconnaissance, signals intelligence and ocean surveillance missions. The series includes optical imaging, synthetic aperture radar (SAR) and electronic intelligence (ELINT) variants, some operating in coordinated orbital formations for persistent maritime monitoring.
❓ Frequently Asked Questions
YAOGAN 29 DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 595 km altitude. Its 97.9° 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 97 minutes, travelling at 27,233 km/h.
YAOGAN 29 DEB (NORAD ID 42673) is a piece of tracked orbital debris attributed to China. It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
YAOGAN 29 DEB was launched on 2015-11-26 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks YAOGAN 29 DEB (NORAD ID 42673) 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.
YAOGAN 29 DEB travels at approximately 27,233 km/h (16,922 mph) — roughly 7.56 km/s. It completes 14.91 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.56 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like YAOGAN 29 DEB. Read more about debris statistics and the Kessler syndrome.