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ORBCOMM FM 5 DEB

NORAD 51448 Debris LEO 1997-084X
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
756 km
Apogee
808 km
Inclination
45.0°
Period
100.5 min
Mean Motion
14.32948329 rev/day
TLE Epoch
2026-06-19 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude782 km
Orbital Velocity26,874 km/h
Velocity7.46 km/s
Orbital Period100 minutes
Orbits / Day14.33
Eccentricity0.0036
Semi-Major Axis7,153 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
ORBCOMM (ORBCOMM)
Launch Date
1997-12-23
Launch Site
Esrange, Sweden
Int'l Designator
1997-084X
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
🔗 Constellation / Groups
orbcomm
📖 About This Object
ORBCOMM FM 5 DEB is a tracked piece of space debris attributed to ORBCOMM, launched on 1997-12-23 from Esrange, Sweden. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 756 km and 808 km with an inclination of 45.0°. It travels at approximately 26,874 km/h (7.46 km/s), completing one full orbit every 100 minutes — that’s roughly 14.33 orbits per day. It is part of the Orbcomm constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, ORBCOMM FM 5 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
ORBCOMM FM 5 DEB orbits at an average altitude of 782 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of ORBCOMM FM 5 DEB’s average altitude, there are currently 402 active payloads and 2,206 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 45.0°, ORBCOMM FM 5 DEB passes over latitudes between 45.0°N and 45.0°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. ORBCOMM operates approximately 58 active satellites in total, of which 34 share a similar altitude band with ORBCOMM FM 5 DEB.
🔗 ORBCOMM Constellation

This satellite is part of the ORBCOMM constellation, providing machine-to-machine (M2M) and Internet of Things (IoT) connectivity. The OG2 (second-generation) constellation operates in LEO and supports asset tracking, fleet management and industrial monitoring for transportation, heavy equipment, maritime and energy sectors.

❓ Frequently Asked Questions
ORBCOMM FM 5 DEB orbits in Low Earth Orbit (LEO) at altitudes between 756 km (perigee) and 808 km (apogee), with an average altitude of approximately 782 km. It completes one orbit every 100 minutes, travelling at approximately 26,874 km/h (16,699 mph).
ORBCOMM FM 5 DEB (NORAD ID 51448) is a piece of tracked orbital debris attributed to ORBCOMM. 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.
ORBCOMM FM 5 DEB was launched on 1997-12-23 from Esrange, Sweden. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks ORBCOMM FM 5 DEB (NORAD ID 51448) 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.
ORBCOMM FM 5 DEB travels at approximately 26,874 km/h (16,699 mph) — roughly 7.46 km/s. It completes 14.33 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.46 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 ORBCOMM FM 5 DEB. Read more about debris statistics and the Kessler syndrome.