DMSP 5D-2 F13 DEB
NORAD 42276
Debris
LEO
1995-015GS
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LEO · NORAD 42276
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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
833 km
Apogee
1001 km
Inclination
99.1°
Period
103.3 min
Mean Motion
13.93322742 rev/day
TLE Epoch
2026-10-13 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude917 km
Orbital Velocity26,624 km/h
Velocity7.40 km/s
Orbital Period103 minutes
Orbits / Day13.93
Eccentricity0.0115
Semi-Major Axis7,288 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1995-03-24
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1995-015GS
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
DMSP 5D-2 F13 DEB is a tracked piece of space debris attributed to United States, launched on 1995-03-24 from Vandenberg Space Force Base, United States on the DMSP Block 5D-2 S-13 launch. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 833 km and 1,001 km with an inclination of 99.1°. It travels at approximately 26,624 km/h (7.40 km/s), completing one full orbit every 103 minutes — that’s roughly 13.93 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, DMSP 5D-2 F13 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
DMSP 5D-2 F13 DEB orbits at an average altitude of 917 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of DMSP 5D-2 F13 DEB’s average altitude, there are currently 327 active payloads and 1,423 tracked debris or rocket body fragments. With an inclination of 99.1°, DMSP 5D-2 F13 DEB passes over latitudes between 99.1°N and 99.1°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,201 active satellites in total, of which 156 share a similar altitude band with DMSP 5D-2 F13 DEB.
🔗 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
DMSP 5D-2 F13 DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 917 km altitude. Its 99.1° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 103 minutes, travelling at 26,624 km/h.
DMSP 5D-2 F13 DEB (NORAD ID 42276) 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.
DMSP 5D-2 F13 DEB was launched on 1995-03-24 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks DMSP 5D-2 F13 DEB (NORAD ID 42276) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
DMSP 5D-2 F13 DEB travels at approximately 26,624 km/h (16,543 mph) — roughly 7.40 km/s. It completes 13.93 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 7.40 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 DMSP 5D-2 F13 DEB. Read more about debris statistics and the Kessler syndrome.