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DELTA 2 DEB (DPAF)

NORAD 27000 Debris LEO 2001-055D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1315 km
Apogee
1328 km
Inclination
66.0°
Period
112.1 min
Mean Motion
12.85012756 rev/day
TLE Epoch
2026-06-20 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,322 km
Orbital Velocity25,914 km/h
Velocity7.20 km/s
Orbital Period112 minutes
Orbits / Day12.85
Eccentricity0.0008
Semi-Major Axis7,693 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2001-12-07
Launch Site
Vandenberg SFB, California
Int'l Designator
2001-055D
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
DELTA 2 DEB (DPAF) is a tracked piece of space debris attributed to United States, launched on 2001-12-07 from Vandenberg SFB, California on the Jason launch. With over 25 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,315 km and 1,328 km with an inclination of 66.0°. It travels at approximately 25,914 km/h (7.20 km/s), completing one full orbit every 112 minutes — that’s roughly 12.85 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, DELTA 2 DEB (DPAF) 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 2 DEB (DPAF) orbits at an average altitude of 1,322 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of DELTA 2 DEB (DPAF)’s average altitude, there are currently 13 active payloads and 229 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 66.0°, DELTA 2 DEB (DPAF) passes over latitudes between 66.0°N and 66.0°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 12,358 active satellites in total, of which 5 share a similar altitude band with DELTA 2 DEB (DPAF).
🔗 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 2 DEB (DPAF) orbits in Low Earth Orbit (LEO) at altitudes between 1,315 km (perigee) and 1,328 km (apogee), with an average altitude of approximately 1,322 km. It completes one orbit every 112 minutes, travelling at approximately 25,914 km/h (16,102 mph).
DELTA 2 DEB (DPAF) (NORAD ID 27000) 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 2 DEB (DPAF) was launched on 2001-12-07 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 2 DEB (DPAF) (NORAD ID 27000) 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 2 DEB (DPAF) travels at approximately 25,914 km/h (16,102 mph) — roughly 7.20 km/s. It completes 12.85 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 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 7.20 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 2 DEB (DPAF). Read more about debris statistics and the Kessler syndrome.