WESTFORD NEEDLES, 602

Orbit data source: Space-Track

WESTFORD NEEDLES, 602 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
602, 1963-014E
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~10 kg wet, ~10 kg dry
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: 14 hours ago

TLE from 14 hours ago
0 WESTFORD NEEDLES
1 00602U 63014E   25286.74897163 -.00000007  00000-0 -42957-2 0  9998
2 00602  87.3556 212.9758 0025099 288.8613  70.9522  8.67236685976478
Epoch: 2025-10-13T17:58Z
TLE epoch observation values (Epoch: 2025-10-13T17:58:31.148Z)
Latitude
0.00002°
Longitude
-79.20127°
Altitude
3,623.054 km
Speed
6.316 km/s
True Right ascension
14h 11m 54s
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
02:42:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,651.937 km
Perigee altitude
3,601.714 km
Semi-major axis
10,004.962 km
Eccentricity
0.00251
Inclination
87.3556°
RAAN
212.9758°
Arg. of periapsis
288.8613°
True anomaly
71.22434°
Mean anomaly
70.9522°
Eccentric anomaly
71.08824°
Mean motion
2.1688 °/min
Orbital period
165.99 mins
BSTAR
-0.0042957

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