INTELSAT 33E DEB
NORAD 64408
Debris
MEO
2016-053AN
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MEO · NORAD 64408
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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
27856 km
Apogee
42098 km
Inclination
2.7°
Period
1394.9 min
Mean Motion
1.03230257 rev/day
TLE Epoch
2026-06-18 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude34,977 km
Orbital Velocity11,177 km/h
Velocity3.10 km/s
Orbital Period23 hours 15 minutes
Orbits / Day1.03
Eccentricity0.1722
Semi-Major Axis41,348 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
Intelsat (ITSO)
Launch Date
2016-08-24
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2016-053AN
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 Medium Earth Orbit (MEO) at altitudes between 27,856 km and 42,098 km with an inclination of 2.7°. It travels at approximately 11,177 km/h (3.10 km/s), completing one full orbit every 23 hours 15 minutes — that’s roughly 1.03 orbits per day. Its orbital eccentricity of 0.1722 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. It is part of the Intelsat constellation group. 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 orbits at an average altitude of 34,977 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of INTELSAT 33E DEB’s average altitude, there are currently 0 active payloads and 12 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 2.7°, INTELSAT 33E DEB passes over latitudes between 2.7°N and 2.7°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. 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 in Medium Earth Orbit (MEO) at altitudes between 27,856 km (perigee) and 42,098 km (apogee), with an average altitude of approximately 34,977 km. It completes one orbit every 23 hours 15 minutes, travelling at approximately 11,177 km/h (6,945 mph).
INTELSAT 33E DEB (NORAD ID 64408) 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 64408) 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 11,177 km/h (6,945 mph) — roughly 3.10 km/s. It completes 1.03 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 2 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 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.