WESTFORD NEEDLES
NORAD 18615
Debris
MEO
1963-014DK
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MEO · NORAD 18615
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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
1729 km
Apogee
5390 km
Inclination
86.3°
Period
164.3 min
Mean Motion
8.76349535 rev/day
TLE Epoch
2026-06-18 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude3,560 km
Orbital Velocity22,808 km/h
Velocity6.34 km/s
Orbital Period2 hours 44 minutes
Orbits / Day8.76
Eccentricity0.1843
Semi-Major Axis9,931 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1963-05-09
Launch Site
Vandenberg SFB, California
Int'l Designator
1963-014DK
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 SFB, California 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 1,729 km and 5,390 km with an inclination of 86.3°. It travels at approximately 22,808 km/h (6.34 km/s), completing one full orbit every 2 hours 44 minutes — that’s roughly 8.76 orbits per day. Its orbital eccentricity of 0.1843 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 3,560 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 0 active payloads 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 86.3°, WESTFORD NEEDLES passes over latitudes between 86.3°N and 86.3°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 12,358 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 1,729 km (perigee) and 5,390 km (apogee), with an average altitude of approximately 3,560 km. It completes one orbit every 2 hours 44 minutes, travelling at approximately 22,808 km/h (14,172 mph).
WESTFORD NEEDLES (NORAD ID 18615) 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 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks WESTFORD NEEDLES (NORAD ID 18615) 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.
WESTFORD NEEDLES travels at approximately 22,808 km/h (14,172 mph) — roughly 6.34 km/s. It completes 8.76 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 6.34 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.