Skip to content
Home Library Satellite Directory MSG 2 DEB (BAFFLE COVER)

MSG 2 DEB (BAFFLE COVER)

NORAD 29676 Debris GEO 2005-049F
CONNECTING… GEO · NORAD 29676
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
35179 km
Apogee
35312 km
Inclination
12.6°
Period
1408.5 min
Mean Motion
1.02233926 rev/day
TLE Epoch
2026-06-19 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,246 km
Orbital Velocity11,141 km/h
Velocity3.09 km/s
Orbital Period23 hours 29 minutes
Orbits / Day1.02
Eccentricity0.0016
Semi-Major Axis41,617 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Eumetsat
Launch Date
2005-12-21
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2005-049F
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
MSG 2 DEB (BAFFLE COVER) is a tracked piece of space debris attributed to Eumetsat, launched on 2005-12-21 from Guiana Space Centre, Kourou on the Insat 4A launch. With over 21 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,179 km and 35,312 km with an inclination of 12.6°. It travels at approximately 11,141 km/h (3.09 km/s), completing one full orbit every 23 hours 29 minutes — that’s roughly 1.02 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, MSG 2 DEB (BAFFLE COVER) 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
MSG 2 DEB (BAFFLE COVER) 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 12.6°, 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 MSG 2 DEB (BAFFLE COVER)’s average altitude, there are currently 3 active payloads and 14 tracked debris or rocket body fragments. Eumetsat operates approximately 10 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
MSG 2 DEB (BAFFLE COVER) orbits at approximately 35,246 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 11,141 km/h — it just keeps pace with the ground below. With an inclination of 12.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
MSG 2 DEB (BAFFLE COVER) (NORAD ID 29676) is a piece of tracked orbital debris attributed to Eumetsat. 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.
MSG 2 DEB (BAFFLE COVER) was launched on 2005-12-21 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 MSG 2 DEB (BAFFLE COVER) (NORAD ID 29676) 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.
MSG 2 DEB (BAFFLE COVER) travels at approximately 11,141 km/h (6,923 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 MSG 2 DEB (BAFFLE COVER). Read more about debris statistics and the Kessler syndrome.