DELTA 1 DEB (YO)
NORAD 28144
Debris
MEO
1976-066D
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MEO · NORAD 28144
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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
429 km
Apogee
11103 km
Inclination
24.5°
Period
222.0 min
Mean Motion
6.48693075 rev/day
TLE Epoch
2026-06-19 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude5,766 km
Orbital Velocity20,631 km/h
Velocity5.73 km/s
Orbital Period3 hours 42 minutes
Orbits / Day6.49
Eccentricity0.4397
Semi-Major Axis12,137 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1976-07-08
Launch Site
Cape Canaveral, Florida
Int'l Designator
1976-066D
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DELTA 1 DEB (YO) is a tracked piece of space debris attributed to United States, launched on 1976-07-08 from Cape Canaveral, Florida on the Palapa A1 launch. After more than 50 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 429 km and 11,103 km with an inclination of 24.5°. It travels at approximately 20,631 km/h (5.73 km/s), completing one full orbit every 3 hours 42 minutes — that’s roughly 6.49 orbits per day. Its orbital eccentricity of 0.4397 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, DELTA 1 DEB (YO) 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 (YO) orbits at an average altitude of 5,766 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 (YO)’s average altitude, there are currently 0 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 24.5°, DELTA 1 DEB (YO) passes over latitudes between 24.5°N and 24.5°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 12,358 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
DELTA 1 DEB (YO) orbits in Medium Earth Orbit (MEO) at altitudes between 429 km (perigee) and 11,103 km (apogee), with an average altitude of approximately 5,766 km. It completes one orbit every 3 hours 42 minutes, travelling at approximately 20,631 km/h (12,819 mph).
DELTA 1 DEB (YO) (NORAD ID 28144) 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 (YO) was launched on 1976-07-08 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 DEB (YO) (NORAD ID 28144) 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 (YO) travels at approximately 20,631 km/h (12,819 mph) — roughly 5.73 km/s. It completes 6.49 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 13 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 5.73 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 (YO). Read more about debris statistics and the Kessler syndrome.