WESTFORD NEEDLES, 18962

Orbit data source: Space-Track

WESTFORD NEEDLES, 18962 is space debris in LEO originally from a launch on Thu, 09 May 1963 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
18962, 1963-014DN
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1963-05-09 (63 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 weeks ago

TLE from 2 weeks ago
0 WESTFORD NEEDLES
1 18962U 63014DN  26022.34956586 -.00000645  00000-0 -10141+0 0  9991
2 18962  86.5011 171.6860 1395009  48.8188 322.4859  8.76592273189754
Epoch: 2026-01-22T08:23Z
TLE epoch observation values (Epoch: 2026-01-22T08:23:22.490Z)
Latitude
-0°
Longitude
-75.86171°
Altitude
2,545.4 km
Speed
7.017 km/s
True Right ascension
11h 26m 44s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
17:43:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,941.166 km
Perigee altitude
2,169.685 km
Semi-major axis
9,933.563 km
Eccentricity
0.1395
Inclination
86.5011°
RAAN
171.686°
Arg. of periapsis
48.8188°
True anomaly
311.27378°
Mean anomaly
322.4859°
Eccentric anomaly
317.03877°
Mean motion
2.19223 °/min
Orbital period
164.22 mins
BSTAR
-0.10141
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