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DELTA 4H DEB

NORAD 32573 Debris MEO 2007-054AE
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
791 km
Apogee
4149 km
Inclination
27.9°
Period
138.1 min
Mean Motion
10.43033269 rev/day
TLE Epoch
2026-06-20 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,470 km
Orbital Velocity24,172 km/h
Velocity6.71 km/s
Orbital Period2 hours 18 minutes
Orbits / Day10.43
Eccentricity0.1899
Semi-Major Axis8,841 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2007-11-11
Launch Site
Cape Canaveral, Florida
Int'l Designator
2007-054AE
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DELTA 4H DEB is a tracked piece of space debris attributed to United States, launched on 2007-11-11 from Cape Canaveral, Florida on the DSP F23 launch. After 19 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 791 km and 4,149 km with an inclination of 27.9°. It travels at approximately 24,172 km/h (6.71 km/s), completing one full orbit every 2 hours 18 minutes — that’s roughly 10.43 orbits per day. Its orbital eccentricity of 0.1899 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, DELTA 4H 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 4H DEB orbits at an average altitude of 2,470 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 4H DEB’s average altitude, there are currently 1 active payload and 6 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 27.9°, DELTA 4H DEB passes over latitudes between 27.9°N and 27.9°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 12,358 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 4H DEB orbits in Medium Earth Orbit (MEO) at altitudes between 791 km (perigee) and 4,149 km (apogee), with an average altitude of approximately 2,470 km. It completes one orbit every 2 hours 18 minutes, travelling at approximately 24,172 km/h (15,020 mph).
DELTA 4H DEB (NORAD ID 32573) 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 4H DEB was launched on 2007-11-11 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 4H DEB (NORAD ID 32573) 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 4H DEB travels at approximately 24,172 km/h (15,020 mph) — roughly 6.71 km/s. It completes 10.43 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 21 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 6.71 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 4H DEB. Read more about debris statistics and the Kessler syndrome.