OPS 5798 DEB
NORAD 903
Debris
LEO
1964-063F
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LEO · NORAD 903
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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
945 km
Apogee
977 km
Inclination
90.2°
Period
104.3 min
Mean Motion
13.80852193 rev/day
TLE Epoch
2026-09-16 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude961 km
Orbital Velocity26,544 km/h
Velocity7.37 km/s
Orbital Period104 minutes
Orbits / Day13.81
Eccentricity0.0022
Semi-Major Axis7,332 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1964-10-06
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1964-063F
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
OPS 5798 DEB is a tracked piece of space debris attributed to United States, launched on 1964-10-06 from Vandenberg Space Force Base, United States on the NNS O-1 launch. After more than 62 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 945 km and 977 km with an inclination of 90.2°. It travels at approximately 26,544 km/h (7.37 km/s), completing one full orbit every 104 minutes — that’s roughly 13.81 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, OPS 5798 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 5798 DEB orbits at an average altitude of 961 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 5798 DEB’s average altitude, there are currently 380 active payloads and 1,258 tracked debris or rocket body fragments. With an inclination of 90.2°, OPS 5798 DEB passes over latitudes between 90.2°N and 90.2°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 13,206 active satellites in total, of which 134 share a similar altitude band with OPS 5798 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 5798 DEB orbits in Low Earth Orbit (LEO) at altitudes between 945 km (perigee) and 977 km (apogee), with an average altitude of approximately 961 km. It completes one orbit every 104 minutes, travelling at approximately 26,544 km/h (16,493 mph).
OPS 5798 DEB (NORAD ID 903) 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 5798 DEB was launched on 1964-10-06 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks OPS 5798 DEB (NORAD ID 903) 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 5798 DEB travels at approximately 26,544 km/h (16,493 mph) — roughly 7.37 km/s. It completes 13.81 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 7.37 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 5798 DEB. Read more about debris statistics and the Kessler syndrome.