CRRES DEB (CANISTER)
NORAD 21589
Debris
MEO
1990-065E
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MEO · NORAD 21589
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
344 km
Apogee
30843 km
Inclination
17.7°
Period
540.2 min
Mean Motion
2.66568928 rev/day
TLE Epoch
2026-09-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude15,594 km
Orbital Velocity15,336 km/h
Velocity4.26 km/s
Orbital Period9 hours
Orbits / Day2.67
Eccentricity0.6943
Semi-Major Axis21,965 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1990-07-25
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1990-065E
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 Space Force Station, United States 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 344 km and 30,843 km with an inclination of 17.7°. It travels at approximately 15,336 km/h (4.26 km/s), completing one full orbit every 9 hours — that’s roughly 2.67 orbits per day. Its orbital eccentricity of 0.6943 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 15,594 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 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 17.7°, CRRES DEB (CANISTER) passes over latitudes between 17.7°N and 17.7°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. United States operates approximately 13,198 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 344 km (perigee) and 30,843 km (apogee), with an average altitude of approximately 15,594 km. It completes one orbit every 9 hours, travelling at approximately 15,336 km/h (9,529 mph).
CRRES DEB (CANISTER) (NORAD ID 21589) 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 Space Force Station, United States, 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 21589) 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 15,336 km/h (9,529 mph) — roughly 4.26 km/s. It completes 2.67 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 4.26 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.