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OPS 0100 DEB *

NORAD 4843 Debris LEO 1967-034E
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1043 km
Apogee
1082 km
Inclination
90.3°
Period
106.5 min
Mean Motion
13.52681559 rev/day
TLE Epoch
2026-09-19 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,063 km
Orbital Velocity26,362 km/h
Velocity7.32 km/s
Orbital Period106 minutes
Orbits / Day13.53
Eccentricity0.0026
Semi-Major Axis7,434 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1967-04-14
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1967-034E
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 0100 DEB * is a tracked piece of space debris attributed to United States, launched on 1967-04-14 from Vandenberg Space Force Base, United States on the NNS O-12 launch. 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 1,043 km and 1,082 km with an inclination of 90.3°. It travels at approximately 26,362 km/h (7.32 km/s), completing one full orbit every 106 minutes — that’s roughly 13.53 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. As orbital debris, OPS 0100 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 0100 DEB * orbits at an average altitude of 1,063 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 0100 DEB *’s average altitude, there are currently 309 active payloads and 601 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 90.3°, OPS 0100 DEB * passes over latitudes between 90.3°N and 90.3°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 13,196 active satellites in total, of which 42 share a similar altitude band with OPS 0100 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 0100 DEB * orbits in Low Earth Orbit (LEO) at altitudes between 1,043 km (perigee) and 1,082 km (apogee), with an average altitude of approximately 1,063 km. It completes one orbit every 106 minutes, travelling at approximately 26,362 km/h (16,380 mph).
OPS 0100 DEB * (NORAD ID 4843) 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 0100 DEB * was launched on 1967-04-14 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks OPS 0100 DEB * (NORAD ID 4843) 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 0100 DEB * travels at approximately 26,362 km/h (16,380 mph) — roughly 7.32 km/s. It completes 13.53 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 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 7.32 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 0100 DEB *. Read more about debris statistics and the Kessler syndrome.