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: 15 hours ago

TLE from 15 hours ago
0 WESTFORD NEEDLES
1 18962U 63014DN  26289.01410763  .00000097  00000-0  12585-1 0  9997
2 18962  86.4989 135.7095 1449058 110.5552 265.6503  8.76932905213127
Epoch: 2026-10-16T00:20Z
TLE epoch observation values (Epoch: 2026-10-16T00:20:18.899Z)
Latitude
0.00003°
Longitude
106.08955°
Altitude
3,867.933 km
Speed
6.14 km/s
True Right ascension
09h 02m 50s
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
10:28:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,991.904 km
Perigee altitude
2,113.789 km
Semi-major axis
9,930.984 km
Eccentricity
0.14491
Inclination
86.4989°
RAAN
135.7095°
Arg. of periapsis
110.5552°
True anomaly
249.53235°
Mean anomaly
265.6503°
Eccentric anomaly
257.54326°
Mean motion
2.19308 °/min
Orbital period
164.15 mins
BSTAR
0.012585
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