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INTELSAT 33E DEB

NORAD 62004 Debris GEO 2016-053W
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
34261 km
Apogee
36015 km
Inclination
2.5°
Period
1403.1 min
Mean Motion
1.02631688 rev/day
TLE Epoch
2026-06-19 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,138 km
Orbital Velocity11,156 km/h
Velocity3.10 km/s
Orbital Period23 hours 23 minutes
Orbits / Day1.03
Eccentricity0.0211
Semi-Major Axis41,509 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Intelsat (ITSO)
Launch Date
2016-08-24
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2016-053W
Object Type
Debris
RCS Size
Unknown
🔗 Constellation / Groups
intelsat
📖 About This Object
INTELSAT 33E DEB is a tracked piece of space debris attributed to ITSO, launched on 2016-08-24 from Guiana Space Centre, Kourou. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 34,261 km and 36,015 km with an inclination of 2.5°. It travels at approximately 11,156 km/h (3.10 km/s), completing one full orbit every 23 hours 23 minutes — that’s roughly 1.03 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 33E 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 33E 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 2.5°, 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 33E DEB’s average altitude, there are currently 1 active payload and 4 tracked debris or rocket body fragments. ITSO operates approximately 72 active satellites in total.
🔗 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 33E DEB orbits at approximately 35,138 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 11,156 km/h — it just keeps pace with the ground below. With an inclination of 2.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INTELSAT 33E DEB (NORAD ID 62004) 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 33E DEB was launched on 2016-08-24 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. View the full satellite launch log.
Yes — Orbital Radar tracks INTELSAT 33E DEB (NORAD ID 62004) 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 33E DEB travels at approximately 11,156 km/h (6,932 mph) — roughly 3.10 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 3.10 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 33E DEB. Read more about debris statistics and the Kessler syndrome.