USA 32 DEB
NORAD 101032
Debris
LEO
1988-078C
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LEO · NORAD 101032
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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
771 km
Apogee
785 km
Inclination
85.0°
Period
100.4 min
Mean Motion
14.34133001 rev/day
TLE Epoch
2026-10-19 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude778 km
Orbital Velocity26,881 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.34
Eccentricity0.0010
Semi-Major Axis7,149 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1988-09-05
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1988-078C
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
USA 32 DEB is a tracked piece of space debris attributed to United States, launched on 1988-09-05 from Vandenberg Space Force Base, United States on the P-11 No. 5103 launch. With over 38 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 771 km and 785 km with an inclination of 85.0°. It travels at approximately 26,881 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.34 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, USA 32 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
USA 32 DEB orbits at an average altitude of 778 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of USA 32 DEB’s average altitude, there are currently 446 active payloads and 2,397 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 85.0°, USA 32 DEB passes over latitudes between 85.0°N and 85.0°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 13,283 active satellites in total, of which 187 share a similar altitude band with USA 32 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
USA 32 DEB orbits in Low Earth Orbit (LEO) at altitudes between 771 km (perigee) and 785 km (apogee), with an average altitude of approximately 778 km. It completes one orbit every 100 minutes, travelling at approximately 26,881 km/h (16,703 mph).
USA 32 DEB (NORAD ID 101032) 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.
USA 32 DEB was launched on 1988-09-05 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks USA 32 DEB (NORAD ID 101032) 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.
USA 32 DEB travels at approximately 26,881 km/h (16,703 mph) — roughly 7.47 km/s. It completes 14.34 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.47 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 USA 32 DEB. Read more about debris statistics and the Kessler syndrome.