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CRRES DEB (CANISTER)

NORAD 21778 Debris MEO 1990-065R
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
357 km
Apogee
31880 km
Inclination
17.6°
Period
559.7 min
Mean Motion
2.57294249 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude16,119 km
Orbital Velocity15,156 km/h
Velocity4.21 km/s
Orbital Period9 hours 20 minutes
Orbits / Day2.57
Eccentricity0.7008
Semi-Major Axis22,490 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1990-07-25
Launch Site
Cape Canaveral, Florida
Int'l Designator
1990-065R
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CRRES DEB (CANISTER) is a tracked piece of space debris attributed to United States, launched on 1990-07-25 from Cape Canaveral, Florida on the CRRES launch. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 357 km and 31,880 km with an inclination of 17.6°. It travels at approximately 15,156 km/h (4.21 km/s), completing one full orbit every 9 hours 20 minutes — that’s roughly 2.57 orbits per day. Its orbital eccentricity of 0.7008 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, CRRES DEB (CANISTER) 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
CRRES DEB (CANISTER) orbits at an average altitude of 16,119 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 CRRES DEB (CANISTER)’s average altitude, there are currently 1 active payload and 6 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 17.6°, CRRES DEB (CANISTER) passes over latitudes between 17.6°N and 17.6°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. United States operates approximately 12,358 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
CRRES DEB (CANISTER) orbits in Medium Earth Orbit (MEO) at altitudes between 357 km (perigee) and 31,880 km (apogee), with an average altitude of approximately 16,119 km. It completes one orbit every 9 hours 20 minutes, travelling at approximately 15,156 km/h (9,417 mph).
CRRES DEB (CANISTER) (NORAD ID 21778) is a piece of tracked orbital debris attributed to United States. 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.
CRRES DEB (CANISTER) was launched on 1990-07-25 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. 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 CRRES DEB (CANISTER) (NORAD ID 21778) 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.
CRRES DEB (CANISTER) travels at approximately 15,156 km/h (9,417 mph) — roughly 4.21 km/s. It completes 2.57 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 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 4.21 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 CRRES DEB (CANISTER). Read more about debris statistics and the Kessler syndrome.