DELTA 2 DEB
NORAD 25138
Debris
LEO
1998-002E
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LEO · NORAD 25138
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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
753 km
Apogee
1229 km
Inclination
26.9°
Period
104.9 min
Mean Motion
13.72449268 rev/day
TLE Epoch
2026-06-16 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude991 km
Orbital Velocity26,489 km/h
Velocity7.36 km/s
Orbital Period105 minutes
Orbits / Day13.72
Eccentricity0.0323
Semi-Major Axis7,362 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1998-01-10
Launch Site
Cape Canaveral, Florida
Int'l Designator
1998-002E
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
DELTA 2 DEB is a tracked piece of space debris attributed to United States, launched on 1998-01-10 from Cape Canaveral, Florida. With over 28 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 753 km and 1,229 km with an inclination of 26.9°. It travels at approximately 26,489 km/h (7.36 km/s), completing one full orbit every 105 minutes — that’s roughly 13.72 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, DELTA 2 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 2 DEB orbits at an average altitude of 991 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of DELTA 2 DEB’s average altitude, there are currently 275 active payloads and 894 tracked debris or rocket body fragments. With an inclination of 26.9°, DELTA 2 DEB passes over latitudes between 26.9°N and 26.9°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. United States operates approximately 12,259 active satellites in total, of which 85 share a similar altitude band with DELTA 2 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 2 DEB orbits in Low Earth Orbit (LEO) at altitudes between 753 km (perigee) and 1,229 km (apogee), with an average altitude of approximately 991 km. It completes one orbit every 105 minutes, travelling at approximately 26,489 km/h (16,460 mph).
DELTA 2 DEB (NORAD ID 25138) 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 was launched on 1998-01-10 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 2 DEB (NORAD ID 25138) 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 travels at approximately 26,489 km/h (16,460 mph) — roughly 7.36 km/s. It completes 13.72 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 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 7.36 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. Read more about debris statistics and the Kessler syndrome.