WESTFORD NEEDLES, 2796

Orbit data source: Space-Track

WESTFORD NEEDLES, 2796 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
2796, 1963-014AQ
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
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 week ago

TLE from 1 week ago
0 WESTFORD NEEDLES
1 02796U 63014AQ  25252.05845508  .00000109  00000-0  42061-1 0  9993
2 02796  87.2213 115.0393 0497237 104.9466 260.6972  8.68183305900657
Epoch: 2025-09-09T01:24Z
TLE epoch observation values (Epoch: 2025-09-09T01:24:10.518Z)
Latitude
-0.00004°
Longitude
105.6408°
Altitude
3,728.076 km
Speed
6.248 km/s
True Right ascension
07h 40m 09s
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
17:38:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,116.663 km
Perigee altitude
3,122.42 km
Semi-major axis
9,997.679 km
Eccentricity
0.04972
Inclination
87.2213°
RAAN
115.0393°
Arg. of periapsis
104.9466°
True anomaly
255.1389°
Mean anomaly
260.6972°
Eccentric anomaly
257.91142°
Mean motion
2.17117 °/min
Orbital period
165.81 mins
BSTAR
0.042061
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