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 shape, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

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

TLE from 2 days ago
0 WESTFORD NEEDLES
1 02796U 63014AQ  25291.92461158  .00000102  00000-0  38901-1 0  9998
2 02796  87.2159 111.0205 0510340  64.0722 301.1815  8.68189176904110
Epoch: 2025-10-18T22:11Z
TLE epoch observation values (Epoch: 2025-10-18T22:11:26.440Z)
Latitude
-0.00007°
Longitude
110.51168°
Altitude
3,379.442 km
Speed
6.47 km/s
True Right ascension
07h 24m 04s
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
04:43:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,129.715 km
Perigee altitude
3,109.277 km
Semi-major axis
9,997.633 km
Eccentricity
0.05103
Inclination
87.2159°
RAAN
111.0205°
Arg. of periapsis
64.0722°
True anomaly
296.01469°
Mean anomaly
301.1815°
Eccentric anomaly
298.61461°
Mean motion
2.17119 °/min
Orbital period
165.81 mins
BSTAR
0.038901
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