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 (63 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: 12 hours ago

TLE from 12 hours ago
0 WESTFORD NEEDLES
1 00602U 63014E   26079.77347261  .00000001  00000-0 -75652-3 0  9993
2 00602  87.3665 198.0215 0019331 134.1575 226.0873  8.67238502990179
Epoch: 2026-03-20T18:33Z
TLE epoch observation values (Epoch: 2026-03-20T18:33:48.033Z)
Latitude
-0.00004°
Longitude
101.26764°
Altitude
3,644.619 km
Speed
6.303 km/s
True Right ascension
13h 12m 05s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
11:17:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,646.152 km
Perigee altitude
3,607.471 km
Semi-major axis
10,004.948 km
Eccentricity
0.00193
Inclination
87.3665°
RAAN
198.0215°
Arg. of periapsis
134.1575°
True anomaly
225.92799°
Mean anomaly
226.0873°
Eccentric anomaly
226.00762°
Mean motion
2.16881 °/min
Orbital period
165.99 mins
BSTAR
-0.00075652
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