CZ-2C DEB
NORAD 37734
Debris
LEO
2011-030E
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LEO · NORAD 37734
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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
221 km
Apogee
233 km
Inclination
98.2°
Period
89.0 min
Mean Motion
16.17348420 rev/day
TLE Epoch
2026-10-31 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude227 km
Orbital Velocity27,981 km/h
Velocity7.77 km/s
Orbital Period89 minutes
Orbits / Day16.17
Eccentricity0.0009
Semi-Major Axis6,598 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeWeeks to months
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2011-07-06
Launch Site
Jiuquan Satellite Launch Center, China
Int'l Designator
2011-030E
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CZ-2C DEB is a tracked piece of space debris attributed to China, launched on 2011-07-06 from Jiuquan Satellite Launch Center, China on the shijian shi yihao 03 xin launch. After 15 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 221 km and 233 km with an inclination of 98.2°. It travels at approximately 27,981 km/h (7.77 km/s), completing one full orbit every 89 minutes — that’s roughly 16.17 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 weeks to months. As orbital debris, CZ-2C 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
CZ-2C DEB orbits at an average altitude of 227 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 CZ-2C DEB’s average altitude, there are currently 40 active payloads and 5 tracked debris or rocket body fragments — notable neighbours include STARLINK-1209, STARLINK-1212, STARLINK-1267. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 98.2°, CZ-2C DEB passes over latitudes between 98.2°N and 98.2°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 1,650 active satellites in total, of which 4 share a similar altitude band with CZ-2C DEB.
🔗 Tracked Space Debris
This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.
❓ Frequently Asked Questions
CZ-2C DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 227 km altitude. Its 98.2° 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 89 minutes, travelling at 27,981 km/h.
CZ-2C DEB (NORAD ID 37734) 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.
CZ-2C DEB was launched on 2011-07-06 from Jiuquan Satellite Launch Center, 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: weeks to months. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-2C DEB (NORAD ID 37734) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
CZ-2C DEB travels at approximately 27,981 km/h (17,387 mph) — roughly 7.77 km/s. It completes 16.17 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 32 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 7.77 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 CZ-2C DEB. Read more about debris statistics and the Kessler syndrome.