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SJ 16-02 DEB

NORAD 43428 Debris LEO 2016-043C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
587 km
Apogee
928 km
Inclination
75.0°
Period
100.0 min
Mean Motion
14.40333888 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude758 km
Orbital Velocity26,920 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.40
Eccentricity0.0239
Semi-Major Axis7,129 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2016-06-29
Launch Site
Jiuquan, China
Int'l Designator
2016-043C
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
SJ 16-02 DEB is a tracked piece of space debris attributed to China, launched on 2016-06-29 from Jiuquan, China on the SJ-16-02 launch. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 587 km and 928 km with an inclination of 75.0°. It travels at approximately 26,920 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.40 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, SJ 16-02 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
SJ 16-02 DEB orbits at an average altitude of 758 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 SJ 16-02 DEB’s average altitude, there are currently 357 active payloads and 2,000 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179. With an inclination of 75.0°, SJ 16-02 DEB passes over latitudes between 75.0°N and 75.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,218 active satellites in total, of which 52 share a similar altitude band with SJ 16-02 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
SJ 16-02 DEB orbits in Low Earth Orbit (LEO) at altitudes between 587 km (perigee) and 928 km (apogee), with an average altitude of approximately 758 km. It completes one orbit every 100 minutes, travelling at approximately 26,920 km/h (16,727 mph).
SJ 16-02 DEB (NORAD ID 43428) 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.
SJ 16-02 DEB was launched on 2016-06-29 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 SJ 16-02 DEB (NORAD ID 43428) 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.
SJ 16-02 DEB travels at approximately 26,920 km/h (16,727 mph) — roughly 7.48 km/s. It completes 14.40 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 7.48 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 SJ 16-02 DEB. Read more about debris statistics and the Kessler syndrome.