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NOAA 17 DEB

NORAD 48713 Debris LEO 2002-032AW
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🛰️ Orbital Parameters
Perigee
456 km
Apogee
481 km
Inclination
99.0°
Period
94.0 min
Mean Motion
15.32894725 rev/day
TLE Epoch
2026-11-01 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude469 km
Orbital Velocity27,483 km/h
Velocity7.63 km/s
Orbital Period94 minutes
Orbits / Day15.33
Eccentricity0.0018
Semi-Major Axis6,840 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇺🇸 NOAA (United States)
Launch Date
2002-06-24
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2002-032AW
Object Type
Debris
RCS Size
Small (<0.1 m²)
🔗 Constellation / Groups
weather
📖 About This Object
NOAA 17 DEB is a tracked piece of space debris attributed to United States, launched on 2002-06-24 from Vandenberg Space Force Base, United States on the NOAA M launch. With over 24 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 456 km and 481 km with an inclination of 99.0°. It travels at approximately 27,483 km/h (7.63 km/s), completing one full orbit every 94 minutes — that’s roughly 15.33 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 ~1–3 years. As orbital debris, NOAA 17 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 17 DEB orbits at an average altitude of 469 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 17 DEB’s average altitude, there are currently 10,784 active payloads and 186 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1017, STARLINK-1039. This makes it one of the more crowded altitude bands, containing roughly 56.9% of all active satellites. With an inclination of 99.0°, NOAA 17 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 13,340 active satellites in total, of which 10,159 share a similar altitude band with NOAA 17 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 17 DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 469 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 94 minutes, travelling at 27,483 km/h.
NOAA 17 DEB (NORAD ID 48713) 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 17 DEB was launched on 2002-06-24 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks NOAA 17 DEB (NORAD ID 48713) 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.
NOAA 17 DEB travels at approximately 27,483 km/h (17,077 mph) — roughly 7.63 km/s. It completes 15.33 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 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 7.63 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 17 DEB. Read more about debris statistics and the Kessler syndrome.