OPS 4988 DEB
NORAD 12099
Debris
LEO
1965-016K
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LEO · NORAD 12099
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Altitude (km)
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Speed (km/s)
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Longitude
🛰️ Orbital Parameters
Perigee
862 km
Apogee
892 km
Inclination
70.1°
Period
102.5 min
Mean Motion
14.04918727 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude877 km
Orbital Velocity26,697 km/h
Velocity7.42 km/s
Orbital Period103 minutes
Orbits / Day14.05
Eccentricity0.0021
Semi-Major Axis7,248 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1965-03-09
Launch Site
Vandenberg SFB, California
Int'l Designator
1965-016K
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 4988 DEB is a tracked piece of space debris attributed to United States, launched on 1965-03-09 from Vandenberg SFB, California on the Secor Type II S/N 1 launch. After more than 61 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 862 km and 892 km with an inclination of 70.1°. It travels at approximately 26,697 km/h (7.42 km/s), completing one full orbit every 103 minutes — that’s roughly 14.05 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, OPS 4988 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
OPS 4988 DEB orbits at an average altitude of 877 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 OPS 4988 DEB’s average altitude, there are currently 172 active payloads and 1,724 tracked debris or rocket body fragments — notable neighbours include NOAA 20. With an inclination of 70.1°, OPS 4988 DEB passes over latitudes between 70.1°N and 70.1°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 12,413 active satellites in total, of which 36 share a similar altitude band with OPS 4988 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
OPS 4988 DEB orbits in Low Earth Orbit (LEO) at altitudes between 862 km (perigee) and 892 km (apogee), with an average altitude of approximately 877 km. It completes one orbit every 103 minutes, travelling at approximately 26,697 km/h (16,589 mph).
OPS 4988 DEB (NORAD ID 12099) 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.
OPS 4988 DEB was launched on 1965-03-09 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 OPS 4988 DEB (NORAD ID 12099) 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.
OPS 4988 DEB travels at approximately 26,697 km/h (16,589 mph) — roughly 7.42 km/s. It completes 14.05 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 7.42 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 OPS 4988 DEB. Read more about debris statistics and the Kessler syndrome.