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JIELONG 3 DEB

NORAD 62575 Debris LEO 2025-007A
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
630 km
Apogee
650 km
Inclination
55.0°
Period
97.5 min
Mean Motion
14.76626013 rev/day
TLE Epoch
2026-06-20 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude640 km
Orbital Velocity27,144 km/h
Velocity7.54 km/s
Orbital Period98 minutes
Orbits / Day14.77
Eccentricity0.0014
Semi-Major Axis7,011 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-01-13
Launch Site
YSLA
Int'l Designator
2025-007A
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
JIELONG 3 DEB is a tracked piece of space debris attributed to China, launched on 2025-01-13 from YSLA on the Weili Kongjian 01 zu 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 630 km and 650 km with an inclination of 55.0°. It travels at approximately 27,144 km/h (7.54 km/s), completing one full orbit every 98 minutes — that’s roughly 14.77 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. As orbital debris, JIELONG 3 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
JIELONG 3 DEB orbits at an average altitude of 640 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of JIELONG 3 DEB’s average altitude, there are currently 742 active payloads and 919 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0050. With an inclination of 55.0°, JIELONG 3 DEB passes over latitudes between 55.0°N and 55.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,217 active satellites in total, of which 155 share a similar altitude band with JIELONG 3 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
JIELONG 3 DEB orbits in Low Earth Orbit (LEO) at altitudes between 630 km (perigee) and 650 km (apogee), with an average altitude of approximately 640 km. It completes one orbit every 98 minutes, travelling at approximately 27,144 km/h (16,867 mph).
JIELONG 3 DEB (NORAD ID 62575) 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.
JIELONG 3 DEB was launched on 2025-01-13 from YSLA. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks JIELONG 3 DEB (NORAD ID 62575) 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.
JIELONG 3 DEB travels at approximately 27,144 km/h (16,867 mph) — roughly 7.54 km/s. It completes 14.77 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 7.54 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 JIELONG 3 DEB. Read more about debris statistics and the Kessler syndrome.