USA 32 DEB
NORAD 101046
Debris
LEO
1988-078S
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LEO · NORAD 101046
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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
725 km
Apogee
772 km
Inclination
85.1°
Period
99.8 min
Mean Motion
14.43066383 rev/day
TLE Epoch
2026-10-22 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude749 km
Orbital Velocity26,937 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.43
Eccentricity0.0033
Semi-Major Axis7,120 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
1988-078S
Object Type
Debris
RCS Size
Medium (0.1–1 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 725 km and 772 km with an inclination of 85.1°. It travels at approximately 26,937 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.43 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 749 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 410 active payloads and 2,130 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179, LANDSAT 9. With an inclination of 85.1°, USA 32 DEB passes over latitudes between 85.1°N and 85.1°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 13,274 active satellites in total, of which 182 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 725 km (perigee) and 772 km (apogee), with an average altitude of approximately 749 km. It completes one orbit every 100 minutes, travelling at approximately 26,937 km/h (16,738 mph).
USA 32 DEB (NORAD ID 101046) 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 101046) 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 26,937 km/h (16,738 mph) — roughly 7.48 km/s. It completes 14.43 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 7.48 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.