Skip to content
Home › Library › Satellite Directory › DELTA 1 DEB

DELTA 1 DEB

NORAD 27480 Debris MEO 1968-055H
CONNECTING… MEO · NORAD 27480
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
1279 km
Apogee
4892 km
Inclination
121.3°
Period
152.7 min
Mean Motion
9.43019085 rev/day
TLE Epoch
2026-10-30 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude3,086 km
Orbital Velocity23,373 km/h
Velocity6.49 km/s
Orbital Period2 hours 33 minutes
Orbits / Day9.43
Eccentricity0.1910
Semi-Major Axis9,457 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1968-07-04
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1968-055H
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
DELTA 1 DEB is a tracked piece of space debris attributed to United States, launched on 1968-07-04 from Vandenberg Space Force Base, United States on the RAE A launch. After more than 58 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 1,279 km and 4,892 km with an inclination of 121.3°. It travels at approximately 23,373 km/h (6.49 km/s), completing one full orbit every 2 hours 33 minutes — that’s roughly 9.43 orbits per day. Its orbital eccentricity of 0.1910 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 3,086 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 2 active payloads and 8 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 121.3°, DELTA 1 DEB passes over latitudes between 121.3°N and 121.3°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,342 active satellites in total, of which 2 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 1,279 km (perigee) and 4,892 km (apogee), with an average altitude of approximately 3,086 km. It completes one orbit every 2 hours 33 minutes, travelling at approximately 23,373 km/h (14,523 mph).
DELTA 1 DEB (NORAD ID 27480) 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 1968-07-04 from Vandenberg Space Force Base, United States, 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 DEB (NORAD ID 27480) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 23,373 km/h (14,523 mph) — roughly 6.49 km/s. It completes 9.43 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 19 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 6.49 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.