YAOGAN 30 DEB
NORAD 42677
Debris
LEO
2016-029C
CONNECTING…
LEO · NORAD 42677
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
621 km
Apogee
949 km
Inclination
98.0°
Period
100.6 min
Mean Motion
14.31992781 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude785 km
Orbital Velocity26,868 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.32
Eccentricity0.0229
Semi-Major Axis7,156 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2016-05-15
Launch Site
Jiuquan, China
Int'l Designator
2016-029C
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
YAOGAN 30 DEB is a tracked piece of space debris attributed to China, launched on 2016-05-15 from Jiuquan, China. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 621 km and 949 km with an inclination of 98.0°. It travels at approximately 26,868 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.32 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 ~25–100 years. As orbital debris, YAOGAN 30 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 30 DEB orbits at an average altitude of 785 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 30 DEB’s average altitude, there are currently 417 active payloads and 2,232 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.0°, YAOGAN 30 DEB passes over latitudes between 98.0°N and 98.0°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 88 share a similar altitude band with YAOGAN 30 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 30 DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 785 km altitude. Its 98.0° 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 101 minutes, travelling at 26,868 km/h.
YAOGAN 30 DEB (NORAD ID 42677) 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 30 DEB was launched on 2016-05-15 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks YAOGAN 30 DEB (NORAD ID 42677) 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 30 DEB travels at approximately 26,868 km/h (16,695 mph) — roughly 7.46 km/s. It completes 14.32 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.46 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 30 DEB. Read more about debris statistics and the Kessler syndrome.