ATLAS D DEB, 2327

Orbit data source: Space-Track

ATLAS D DEB, 2327 is space debris in LEO originally from a launch on Thu, 14 Jul 1966 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
2327, 1966-063B
Orbit
LEO
Last TLE update
21 hours ago
Origin
Manufacturer
Goodyear
Mission
Spacecraft
Bus & Motor
CONTAINER, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
1966-07-14 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Half Cyl, 0.3 m
Radar Cross Section
0.210 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 21 hours ago
0 ATLAS D DEB
1 02327U 66063B   25199.69974038  .00001495  00000-0  75039-3 0  9993
2 02327 144.1971   4.7542 0030821 255.6006 104.1261 14.04786878991189
Epoch: 2025-07-18T16:47Z
TLE epoch observation values (Epoch: 2025-07-18T16:47:37.568Z)
Latitude
-0.00006°
Longitude
176.1003°
Altitude
881.832 km
Speed
7.41 km/s
True Right ascension
00h 19m 01s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-10.22062°
Longitude
-13.69823°
Altitude
868.548 km
Speed
7.424 km/s
Apparent Right ascension
13h 00m 59s
Apparent Declination
-26° 06' 08"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
03:02:17
Azimuth
70.573° E
Elevation
-61.262°
Doppler factor
1
Orbital elements
Apogee altitude
902.597 km
Perigee altitude
857.855 km
Semi-major axis
7,258.363 km
Eccentricity
0.00308
Inclination
144.1971°
RAAN
4.7542°
Arg. of periapsis
255.6006°
True anomaly
104.46828°
Mean anomaly
104.1261°
Eccentric anomaly
104.29722°
Mean motion
3.50982 °/min
Orbital period
102.57 mins
BSTAR
0.00075039
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