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NOAA 16 DEB

NORAD 42428 Debris LEO 2000-055TY
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
780 km
Apogee
814 km
Inclination
99.0°
Period
100.8 min
Mean Motion
14.28502097 rev/day
TLE Epoch
2026-06-18 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude797 km
Orbital Velocity26,846 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.29
Eccentricity0.0024
Semi-Major Axis7,168 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 NOAA (United States)
Launch Date
2000-09-21
Launch Site
Vandenberg SFB, California
Int'l Designator
2000-055TY
Object Type
Debris
RCS Size
Small (<0.1 m²)
🔗 Constellation / Groups
weather
📖 About This Object
NOAA 16 DEB is a tracked piece of space debris attributed to United States, launched on 2000-09-21 from Vandenberg SFB, California. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 780 km and 814 km with an inclination of 99.0°. It travels at approximately 26,846 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.29 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. It is part of the Weather constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, NOAA 16 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
NOAA 16 DEB orbits at an average altitude of 797 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 NOAA 16 DEB’s average altitude, there are currently 432 active payloads and 2,267 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 99.0°, NOAA 16 DEB passes over latitudes between 99.0°N and 99.0°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 12,339 active satellites in total, of which 162 share a similar altitude band with NOAA 16 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
NOAA 16 DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 797 km altitude. Its 99.0° 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 101 minutes, travelling at 26,846 km/h.
NOAA 16 DEB (NORAD ID 42428) 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.
NOAA 16 DEB was launched on 2000-09-21 from Vandenberg SFB, California, 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks NOAA 16 DEB (NORAD ID 42428) 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.
NOAA 16 DEB travels at approximately 26,846 km/h (16,681 mph) — roughly 7.46 km/s. It completes 14.29 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 NOAA 16 DEB. Read more about debris statistics and the Kessler syndrome.