GLOBALSTAR DEB
NORAD 27772
Debris
LEO
1999-031F
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LEO · NORAD 27772
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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
872 km
Apogee
1062 km
Inclination
52.0°
Period
104.4 min
Mean Motion
13.79081938 rev/day
TLE Epoch
2026-06-20 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude967 km
Orbital Velocity26,533 km/h
Velocity7.37 km/s
Orbital Period104 minutes
Orbits / Day13.79
Eccentricity0.0129
Semi-Major Axis7,338 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
Globalstar (Globalstar)
Launch Date
1999-06-10
Launch Site
Cape Canaveral, Florida
Int'l Designator
1999-031F
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
GLOBALSTAR DEB is a tracked piece of space debris attributed to Globalstar, launched on 1999-06-10 from Cape Canaveral, Florida on the Globalstar D-3 launch. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 872 km and 1,062 km with an inclination of 52.0°. It travels at approximately 26,533 km/h (7.37 km/s), completing one full orbit every 104 minutes — that’s roughly 13.79 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, GLOBALSTAR 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
GLOBALSTAR DEB orbits at an average altitude of 967 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of GLOBALSTAR DEB’s average altitude, there are currently 290 active payloads and 999 tracked debris or rocket body fragments. With an inclination of 52.0°, GLOBALSTAR DEB passes over latitudes between 52.0°N and 52.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Globalstar operates approximately 84 active satellites in total.
🔗 Globalstar Constellation
This satellite is part of the Globalstar constellation, a LEO mobile satellite communications system providing voice, data and IoT services. The second-generation constellation operates 24 satellites at approximately 1,414 km altitude with a 52° inclination. Globalstar also provides the backbone for Apple's Emergency SOS via satellite feature on iPhones.
❓ Frequently Asked Questions
GLOBALSTAR DEB orbits in Low Earth Orbit (LEO) at altitudes between 872 km (perigee) and 1,062 km (apogee), with an average altitude of approximately 967 km. It completes one orbit every 104 minutes, travelling at approximately 26,533 km/h (16,487 mph).
GLOBALSTAR DEB (NORAD ID 27772) is a piece of tracked orbital debris attributed to Globalstar. 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.
GLOBALSTAR DEB was launched on 1999-06-10 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. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks GLOBALSTAR DEB (NORAD ID 27772) 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.
GLOBALSTAR DEB travels at approximately 26,533 km/h (16,487 mph) — roughly 7.37 km/s. It completes 13.79 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.37 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 GLOBALSTAR DEB. Read more about debris statistics and the Kessler syndrome.