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Home Library Satellite Directory LES 8 9/SOL 11A B DEB *

LES 8 9/SOL 11A B DEB *

NORAD 13753 Debris GEO 1976-023K
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35476 km
Apogee
35503 km
Inclination
4.8°
Period
1420.9 min
Mean Motion
1.01341742 rev/day
TLE Epoch
2026-06-20 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,490 km
Orbital Velocity11,109 km/h
Velocity3.09 km/s
Orbital Period23 hours 41 minutes
Orbits / Day1.01
Eccentricity0.0003
Semi-Major Axis41,861 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1976-03-15
Launch Site
Cape Canaveral, Florida
Int'l Designator
1976-023K
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
LES 8 9/SOL 11A B DEB * is a tracked piece of space debris attributed to United States, launched on 1976-03-15 from Cape Canaveral, Florida on the LES 8 launch. After more than 50 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Geostationary Orbit (GEO) at altitudes between 35,476 km and 35,503 km with an inclination of 4.8°. It travels at approximately 11,109 km/h (3.09 km/s), completing one full orbit every 23 hours 41 minutes — that’s roughly 1.01 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. As orbital debris, LES 8 9/SOL 11A B 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
LES 8 9/SOL 11A B DEB * occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 4.8°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of LES 8 9/SOL 11A B DEB *’s average altitude, there are currently 2 active payloads and 30 tracked debris or rocket body fragments. United States operates approximately 12,358 active satellites in total.
🔗 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
LES 8 9/SOL 11A B DEB * orbits at approximately 35,490 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,109 km/h — it just keeps pace with the ground below. With an inclination of 4.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
LES 8 9/SOL 11A B DEB * (NORAD ID 13753) 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.
LES 8 9/SOL 11A B DEB * was launched on 1976-03-15 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks LES 8 9/SOL 11A B DEB * (NORAD ID 13753) 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.
LES 8 9/SOL 11A B DEB * travels at approximately 11,109 km/h (6,903 mph) — roughly 3.09 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.
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 3.09 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 LES 8 9/SOL 11A B DEB *. Read more about debris statistics and the Kessler syndrome.