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INTELSAT 805 DEB

NORAD 100396 Debris GEO 1998-037D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36058 km
Apogee
36290 km
Inclination
8.1°
Period
1455.9 min
Mean Motion
0.98906709 rev/day
TLE Epoch
2026-08-20 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,174 km
Orbital Velocity11,019 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0027
Semi-Major Axis42,545 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Intelsat (ITSO)
Launch Date
1998-06-18
Launch Site
Cape Canaveral, Florida
Int'l Designator
1998-037D
Object Type
Debris
RCS Size
Unknown
🔗 Constellation / Groups
intelsat
📖 About This Object
INTELSAT 805 DEB is a tracked piece of space debris attributed to ITSO, launched on 1998-06-18 from Cape Canaveral, Florida on the INTELSAT 805 launch. With over 28 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,058 km and 36,290 km with an inclination of 8.1°. It travels at approximately 11,019 km/h (3.06 km/s), completing one full orbit every 24.3 hours — that’s roughly 0.99 orbits per day. It is part of the Intelsat constellation group. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. As orbital debris, INTELSAT 805 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
INTELSAT 805 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 8.1°, 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 INTELSAT 805 DEB’s average altitude, there are currently 150 active payloads and 13 tracked debris or rocket body fragments. ITSO operates approximately 72 active satellites in total, of which 15 share a similar altitude band with INTELSAT 805 DEB.
🔗 Intelsat Communications

This satellite is operated by Intelsat, one of the pioneering commercial satellite operators, with a fleet of 50+ geostationary satellites providing television distribution, enterprise networking, mobility connectivity and government communications worldwide. Intelsat was founded in 1964 as an intergovernmental organisation and privatised in 2001.

❓ Frequently Asked Questions
INTELSAT 805 DEB orbits at approximately 36,174 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 11,019 km/h — it just keeps pace with the ground below. With an inclination of 8.1°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INTELSAT 805 DEB (NORAD ID 100396) is a piece of tracked orbital debris attributed to ITSO. 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.
INTELSAT 805 DEB was launched on 1998-06-18 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 INTELSAT 805 DEB (NORAD ID 100396) 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.
INTELSAT 805 DEB travels at approximately 11,019 km/h (6,847 mph) — roughly 3.06 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 3.06 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 INTELSAT 805 DEB. Read more about debris statistics and the Kessler syndrome.