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 (62 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: 3 days ago

TLE from 3 days ago
0 WESTFORD NEEDLES
1 18962U 63014DN  25285.43805140  .00000804  00000-0  12714+0 0  9993
2 18962  86.4816 185.3926 1378522 162.2792 203.1538  8.76472533180828
Epoch: 2025-10-12T10:30Z
TLE epoch observation values (Epoch: 2025-10-12T10:30:47.640Z)
Latitude
-0.00004°
Longitude
6.43891°
Altitude
4,844.907 km
Speed
5.562 km/s
True Right ascension
12h 21m 34s
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
10:23:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,925.821 km
Perigee altitude
2,186.844 km
Semi-major axis
9,934.47 km
Eccentricity
0.13785
Inclination
86.4816°
RAAN
185.3926°
Arg. of periapsis
162.2792°
True anomaly
197.80323°
Mean anomaly
203.1538°
Eccentric anomaly
200.40058°
Mean motion
2.19193 °/min
Orbital period
164.24 mins
BSTAR
0.12714
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