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.

Loading next visibility...
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: 4 days ago

TLE from 4 days ago
0 WESTFORD NEEDLES
1 00602U 63014E   26171.01230868 -.00000016  00000-0 -84747-2 0  9998
2 00602  87.3592 189.4145 0015021  50.5943 309.6241  8.67238574998080
Epoch: 2026-06-20T00:17Z
TLE epoch observation values (Epoch: 2026-06-20T00:17:43.469Z)
Latitude
0.00002°
Longitude
-83.24966°
Altitude
3,621.607 km
Speed
6.317 km/s
True Right ascension
12h 37m 39s
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
12:58:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,641.839 km
Perigee altitude
3,611.782 km
Semi-major axis
10,004.948 km
Eccentricity
0.0015
Inclination
87.3592°
RAAN
189.4145°
Arg. of periapsis
50.5943°
True anomaly
309.49136°
Mean anomaly
309.6241°
Eccentric anomaly
309.55775°
Mean motion
2.16881 °/min
Orbital period
165.99 mins
BSTAR
-0.0084747

Documentation

Showing up to 5 results
|