WESTFORD NEEDLES, 2378

Orbit data source: Space-Track

WESTFORD NEEDLES, 2378 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
2378, 1963-014Y
Orbit
LEO
Last TLE update
6 days ago
Origin
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

TLE from 6 days ago
0 WESTFORD NEEDLES
1  2378U 63014Y   25194.94369189 -.00000004  00000-0 -32400-2 0  9991
2  2378  87.3718 190.1925 0099282 150.2055 210.4501  8.66593827966447
Epoch: 2025-07-13T22:38Z
TLE epoch observation values (Epoch: 2025-07-13T22:38:54.979Z)
Latitude
-0.00004°
Longitude
-81.59624°
Altitude
3,722.095 km
Speed
6.256 km/s
True Right ascension
12h 40m 46s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-71.68489°
Longitude
105.82481°
Altitude
3,688.953 km
Speed
6.285 km/s
Apparent Right ascension
09h 26m 32s
Apparent Declination
-80° 09' 15"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
23:36:15
Azimuth
172.126° S
Elevation
-47.98°
Doppler factor
1
Orbital elements
Apogee altitude
3,731.155 km
Perigee altitude
3,532.394 km
Semi-major axis
10,009.911 km
Eccentricity
0.00993
Inclination
87.3718°
RAAN
190.1925°
Arg. of periapsis
150.2055°
True anomaly
209.87965°
Mean anomaly
210.4501°
Eccentric anomaly
210.16427°
Mean motion
2.16719 °/min
Orbital period
166.11 mins
BSTAR
-0.00324
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