DELTA 1 DEB
NORAD 2888
Debris
MEO
1965-089D
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MEO · NORAD 2888
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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
1157 km
Apogee
2318 km
Inclination
59.2°
Period
121.3 min
Mean Motion
11.87432558 rev/day
TLE Epoch
2026-09-15 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,738 km
Orbital Velocity25,241 km/h
Velocity7.01 km/s
Orbital Period2 hours 1 minutes
Orbits / Day11.87
Eccentricity0.0716
Semi-Major Axis8,109 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1965-11-06
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1965-089D
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DELTA 1 DEB is a tracked piece of space debris attributed to United States, launched on 1965-11-06 from Cape Canaveral Space Force Station, United States on the GEOS A launch. After more than 61 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,157 km and 2,318 km with an inclination of 59.2°. It travels at approximately 25,241 km/h (7.01 km/s), completing one full orbit every 2 hours 1 minutes — that’s roughly 11.87 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, DELTA 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
DELTA 1 DEB orbits at an average altitude of 1,738 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 DELTA 1 DEB’s average altitude, there are currently 16 active payloads and 47 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 59.2°, DELTA 1 DEB passes over latitudes between 59.2°N and 59.2°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 13,206 active satellites in total, of which 4 share a similar altitude band with DELTA 1 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
DELTA 1 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 1,157 km (perigee) and 2,318 km (apogee), with an average altitude of approximately 1,738 km. It completes one orbit every 2 hours 1 minutes, travelling at approximately 25,241 km/h (15,684 mph).
DELTA 1 DEB (NORAD ID 2888) 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.
DELTA 1 DEB was launched on 1965-11-06 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 DEB (NORAD ID 2888) 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.
DELTA 1 DEB travels at approximately 25,241 km/h (15,684 mph) — roughly 7.01 km/s. It completes 11.87 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 24 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 7.01 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 DELTA 1 DEB. Read more about debris statistics and the Kessler syndrome.