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LUCH (OLYMP) DEB

NORAD 67745 Debris MEO 2014-058D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
28656 km
Apogee
44193 km
Inclination
2.3°
Period
1468.8 min
Mean Motion
0.98039620 rev/day
TLE Epoch
2026-06-19 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,425 km
Orbital Velocity10,987 km/h
Velocity3.05 km/s
Orbital Period24.5 hours
Orbits / Day0.98
Eccentricity0.1815
Semi-Major Axis42,796 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2014-09-27
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2014-058D
Object Type
Debris
RCS Size
Unknown
📖 About This Object
LUCH (OLYMP) DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 2014-09-27 from Baikonur, Kazakhstan on the Olymp-K launch. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 28,656 km and 44,193 km with an inclination of 2.3°. It travels at approximately 10,987 km/h (3.05 km/s), completing one full orbit every 24.5 hours — that’s roughly 0.98 orbits per day. Its orbital eccentricity of 0.1815 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. As orbital debris, LUCH (OLYMP) 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
LUCH (OLYMP) DEB orbits at an average altitude of 36,425 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 LUCH (OLYMP) DEB’s average altitude, there are currently 19 active payloads and 22 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 2.3°, LUCH (OLYMP) DEB passes over latitudes between 2.3°N and 2.3°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. Russia (CIS) operates approximately 1,285 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
LUCH (OLYMP) DEB orbits in Medium Earth Orbit (MEO) at altitudes between 28,656 km (perigee) and 44,193 km (apogee), with an average altitude of approximately 36,425 km. It completes one orbit every 24.5 hours, travelling at approximately 10,987 km/h (6,827 mph).
LUCH (OLYMP) DEB (NORAD ID 67745) is a piece of tracked orbital debris attributed to Russia (CIS). 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.
LUCH (OLYMP) DEB was launched on 2014-09-27 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks LUCH (OLYMP) DEB (NORAD ID 67745) 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.
LUCH (OLYMP) DEB travels at approximately 10,987 km/h (6,827 mph) — roughly 3.05 km/s. It completes 0.98 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 2 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 3.05 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 LUCH (OLYMP) DEB. Read more about debris statistics and the Kessler syndrome.