GLOBALSTAR M004 DEB
NORAD 43357
Debris
LEO
1998-008H
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LEO · NORAD 43357
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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
1349 km
Apogee
1491 km
Inclination
52.0°
Period
114.2 min
Mean Motion
12.60688509 rev/day
TLE Epoch
2026-06-20 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,420 km
Orbital Velocity25,750 km/h
Velocity7.15 km/s
Orbital Period114 minutes
Orbits / Day12.61
Eccentricity0.0091
Semi-Major Axis7,791 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 Globalstar (United States)
Launch Date
1998-02-14
Launch Site
Cape Canaveral, Florida
Int'l Designator
1998-008H
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
GLOBALSTAR M004 DEB is a tracked piece of space debris attributed to United States, launched on 1998-02-14 from Cape Canaveral, Florida on the Globalstar D-1 launch. With over 28 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,349 km and 1,491 km with an inclination of 52.0°. It travels at approximately 25,750 km/h (7.15 km/s), completing one full orbit every 114 minutes — that’s roughly 12.61 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, GLOBALSTAR M004 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 M004 DEB orbits at an average altitude of 1,420 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of GLOBALSTAR M004 DEB’s average altitude, there are currently 308 active payloads and 153 tracked debris or rocket body fragments. With an inclination of 52.0°, GLOBALSTAR M004 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. United States operates approximately 12,358 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 M004 DEB orbits in Low Earth Orbit (LEO) at altitudes between 1,349 km (perigee) and 1,491 km (apogee), with an average altitude of approximately 1,420 km. It completes one orbit every 114 minutes, travelling at approximately 25,750 km/h (16,000 mph).
GLOBALSTAR M004 DEB (NORAD ID 43357) 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.
GLOBALSTAR M004 DEB was launched on 1998-02-14 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks GLOBALSTAR M004 DEB (NORAD ID 43357) 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 M004 DEB travels at approximately 25,750 km/h (16,000 mph) — roughly 7.15 km/s. It completes 12.61 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 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 7.15 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 M004 DEB. Read more about debris statistics and the Kessler syndrome.