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KYOKKO 1 DEB

NORAD 12330 Debris MEO 1978-014D
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Altitude (km)
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
634 km
Apogee
3917 km
Inclination
65.4°
Period
133.5 min
Mean Motion
10.78479232 rev/day
TLE Epoch
2026-06-20 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,276 km
Orbital Velocity24,443 km/h
Velocity6.79 km/s
Orbital Period2 hours 14 minutes
Orbits / Day10.78
Eccentricity0.1898
Semi-Major Axis8,647 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1978-02-04
Launch Site
Uchinoura, Japan
Int'l Designator
1978-014D
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
KYOKKO 1 DEB is a tracked piece of space debris attributed to Japan, launched on 1978-02-04 from Uchinoura, Japan on the EXOS-A launch. With over 48 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 634 km and 3,917 km with an inclination of 65.4°. It travels at approximately 24,443 km/h (6.79 km/s), completing one full orbit every 2 hours 14 minutes — that’s roughly 10.78 orbits per day. Its orbital eccentricity of 0.1898 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, KYOKKO 1 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
KYOKKO 1 DEB orbits at an average altitude of 2,276 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of KYOKKO 1 DEB’s average altitude, there are currently 1 active payload and 9 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 65.4°, KYOKKO 1 DEB passes over latitudes between 65.4°N and 65.4°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Japan operates approximately 189 active satellites in total.
🔗 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
KYOKKO 1 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 634 km (perigee) and 3,917 km (apogee), with an average altitude of approximately 2,276 km. It completes one orbit every 2 hours 14 minutes, travelling at approximately 24,443 km/h (15,188 mph).
KYOKKO 1 DEB (NORAD ID 12330) is a piece of tracked orbital debris attributed to Japan. 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.
KYOKKO 1 DEB was launched on 1978-02-04 from Uchinoura, Japan. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks KYOKKO 1 DEB (NORAD ID 12330) 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.
KYOKKO 1 DEB travels at approximately 24,443 km/h (15,188 mph) — roughly 6.79 km/s. It completes 10.78 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 22 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 6.79 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 KYOKKO 1 DEB. Read more about debris statistics and the Kessler syndrome.