INTELSAT 33E DEB
NORAD 64394
Debris
MEO
2016-053Y
CONNECTING…
MEO · NORAD 64394
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
31170 km
Apogee
36154 km
Inclination
1.3°
Period
1328.9 min
Mean Motion
1.08356301 rev/day
TLE Epoch
2026-06-18 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude33,662 km
Orbital Velocity11,360 km/h
Velocity3.16 km/s
Orbital Period22 hours 9 minutes
Orbits / Day1.08
Eccentricity0.0622
Semi-Major Axis40,033 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
2016-053Y
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 31,170 km and 36,154 km with an inclination of 1.3°. It travels at approximately 11,360 km/h (3.16 km/s), completing one full orbit every 22 hours 9 minutes — that’s roughly 1.08 orbits per day. 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 33,662 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 2 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 1.3°, INTELSAT 33E DEB passes over latitudes between 1.3°N and 1.3°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 31,170 km (perigee) and 36,154 km (apogee), with an average altitude of approximately 33,662 km. It completes one orbit every 22 hours 9 minutes, travelling at approximately 11,360 km/h (7,059 mph).
INTELSAT 33E DEB (NORAD ID 64394) 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 64394) 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 11,360 km/h (7,059 mph) — roughly 3.16 km/s. It completes 1.08 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 3.16 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.