SATCOM 3 DEB
NORAD 29003
Debris
MEO
1979-101F
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MEO · NORAD 29003
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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
8009 km
Apogee
35643 km
Inclination
9.3°
Period
785.6 min
Mean Motion
1.83290663 rev/day
TLE Epoch
2026-06-20 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude21,826 km
Orbital Velocity13,535 km/h
Velocity3.76 km/s
Orbital Period13 hours 6 minutes
Orbits / Day1.83
Eccentricity0.4900
Semi-Major Axis28,197 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1979-12-07
Launch Site
Cape Canaveral, Florida
Int'l Designator
1979-101F
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SATCOM 3 DEB is a tracked piece of space debris attributed to United States, launched on 1979-12-07 from Cape Canaveral, Florida on the RCA-C launch. With over 47 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 8,009 km and 35,643 km with an inclination of 9.3°. It travels at approximately 13,535 km/h (3.76 km/s), completing one full orbit every 13 hours 6 minutes — that’s roughly 1.83 orbits per day. Its orbital eccentricity of 0.4900 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, SATCOM 3 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
SATCOM 3 DEB orbits at an average altitude of 21,826 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 SATCOM 3 DEB’s average altitude, there are currently 0 active payloads and 22 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 9.3°, SATCOM 3 DEB passes over latitudes between 9.3°N and 9.3°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. United States operates approximately 12,358 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
SATCOM 3 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 8,009 km (perigee) and 35,643 km (apogee), with an average altitude of approximately 21,826 km. It completes one orbit every 13 hours 6 minutes, travelling at approximately 13,535 km/h (8,410 mph).
SATCOM 3 DEB (NORAD ID 29003) is a piece of tracked orbital debris attributed to United States. 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.
SATCOM 3 DEB was launched on 1979-12-07 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 SATCOM 3 DEB (NORAD ID 29003) 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.
SATCOM 3 DEB travels at approximately 13,535 km/h (8,410 mph) — roughly 3.76 km/s. It completes 1.83 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 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 3.76 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 SATCOM 3 DEB. Read more about debris statistics and the Kessler syndrome.