CZ-4C DEB
NORAD 35248
Debris
LEO
2007-055C
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LEO · NORAD 35248
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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
409 km
Apogee
452 km
Inclination
97.9°
Period
93.2 min
Mean Motion
15.45377849 rev/day
TLE Epoch
2026-06-16 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude431 km
Orbital Velocity27,559 km/h
Velocity7.66 km/s
Orbital Period93 minutes
Orbits / Day15.45
Eccentricity0.0032
Semi-Major Axis6,802 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2007-11-11
Launch Site
Taiyuan, China
Int'l Designator
2007-055C
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
CZ-4C DEB is a tracked piece of space debris attributed to China, launched on 2007-11-11 from Taiyuan, China. After 19 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 409 km and 452 km with an inclination of 97.9°. It travels at approximately 27,559 km/h (7.66 km/s), completing one full orbit every 93 minutes — that’s roughly 15.45 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 ~1–3 years. As orbital debris, CZ-4C 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-4C DEB orbits at an average altitude of 431 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-4C DEB’s average altitude, there are currently 4,296 active payloads and 144 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 24.8% of all active satellites. With an inclination of 97.9°, CZ-4C 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 1,194 active satellites in total, of which 71 share a similar altitude band with CZ-4C 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-4C DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 431 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 93 minutes, travelling at 27,559 km/h.
CZ-4C DEB (NORAD ID 35248) 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-4C DEB was launched on 2007-11-11 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4C DEB (NORAD ID 35248) 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.
CZ-4C DEB travels at approximately 27,559 km/h (17,125 mph) — roughly 7.66 km/s. It completes 15.45 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 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 7.66 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-4C DEB. Read more about debris statistics and the Kessler syndrome.