WESTFORD NEEDLES
NORAD 2367
Debris
MEO
1963-014S
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MEO · NORAD 2367
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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
456 km
Apogee
6020 km
Inclination
84.1°
Period
156.4 min
Mean Motion
9.20992705 rev/day
TLE Epoch
2026-11-03 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude3,238 km
Orbital Velocity23,186 km/h
Velocity6.44 km/s
Orbital Period2 hours 36 minutes
Orbits / Day9.21
Eccentricity0.2895
Semi-Major Axis9,609 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1963-05-09
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1963-014S
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
WESTFORD NEEDLES is a tracked piece of space debris attributed to United States, launched on 1963-05-09 from Vandenberg Space Force Base, United States on the Midas ETS-III F2 launch. After more than 63 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 456 km and 6,020 km with an inclination of 84.1°. It travels at approximately 23,186 km/h (6.44 km/s), completing one full orbit every 2 hours 36 minutes — that’s roughly 9.21 orbits per day. Its orbital eccentricity of 0.2895 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, WESTFORD NEEDLES 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
WESTFORD NEEDLES orbits at an average altitude of 3,238 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of WESTFORD NEEDLES’s average altitude, there are currently 1 active payload and 7 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 84.1°, WESTFORD NEEDLES passes over latitudes between 84.1°N and 84.1°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 13,342 active satellites in total.
🔗 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
WESTFORD NEEDLES orbits in Medium Earth Orbit (MEO) at altitudes between 456 km (perigee) and 6,020 km (apogee), with an average altitude of approximately 3,238 km. It completes one orbit every 2 hours 36 minutes, travelling at approximately 23,186 km/h (14,407 mph).
WESTFORD NEEDLES (NORAD ID 2367) 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.
WESTFORD NEEDLES was launched on 1963-05-09 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks WESTFORD NEEDLES (NORAD ID 2367) 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.
WESTFORD NEEDLES travels at approximately 23,186 km/h (14,407 mph) — roughly 6.44 km/s. It completes 9.21 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 18 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 6.44 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 WESTFORD NEEDLES. Read more about debris statistics and the Kessler syndrome.