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P/L 153 DEB

NORAD 19245 Debris LEO 1967-053K
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
813 km
Apogee
818 km
Inclination
70.0°
Period
101.2 min
Mean Motion
14.22993070 rev/day
TLE Epoch
2026-06-17 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude816 km
Orbital Velocity26,811 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.23
Eccentricity0.0003
Semi-Major Axis7,187 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1967-05-31
Launch Site
Vandenberg SFB, California
Int'l Designator
1967-053K
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
P/L 153 DEB is a tracked piece of space debris attributed to United States, launched on 1967-05-31 from Vandenberg SFB, California. After more than 59 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 813 km and 818 km with an inclination of 70.0°. It travels at approximately 26,811 km/h (7.45 km/s), completing one full orbit every 101 minutes — that’s roughly 14.23 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, P/L 153 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
P/L 153 DEB orbits at an average altitude of 816 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of P/L 153 DEB’s average altitude, there are currently 397 active payloads and 2,296 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 70.0°, P/L 153 DEB passes over latitudes between 70.0°N and 70.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 12,259 active satellites in total, of which 138 share a similar altitude band with P/L 153 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
P/L 153 DEB orbits in Low Earth Orbit (LEO) at altitudes between 813 km (perigee) and 818 km (apogee), with an average altitude of approximately 816 km. It completes one orbit every 101 minutes, travelling at approximately 26,811 km/h (16,660 mph).
P/L 153 DEB (NORAD ID 19245) 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.
P/L 153 DEB was launched on 1967-05-31 from Vandenberg SFB, California, 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks P/L 153 DEB (NORAD ID 19245) 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.
P/L 153 DEB travels at approximately 26,811 km/h (16,660 mph) — roughly 7.45 km/s. It completes 14.23 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.45 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 P/L 153 DEB. Read more about debris statistics and the Kessler syndrome.