DELTA 1 DEB (YO), 312

Orbit data source: Space-Track

DELTA 1 DEB (YO), 312 is space debris in LEO originally from a launch on Tue, 19 Jun 1962 UTC launched from the Air Force Eastern Test Range (AFETR). 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
312, 1962-025C
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~1 kg wet, ~1 kg dry
Launch date (UTC)
1962-06-19 (64 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 DELTA 1 DEB (YO)
1   312U 62025C   26036.69061185  .00003304  00000-0  53632-3 0  9996
2   312  58.2457 146.8867 0195539 128.7342 233.1351 14.61564774339691
Epoch: 2026-02-05T16:34Z
TLE epoch observation values (Epoch: 2026-02-05T16:34:28.863Z)
Latitude
-0.00001°
Longitude
122.42721°
Altitude
774.112 km
Speed
7.423 km/s
True Right ascension
09h 47m 32s
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
14:20:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
825.766 km
Perigee altitude
549.44 km
Semi-major axis
7,065.74 km
Eccentricity
0.01955
Inclination
58.2457°
RAAN
146.8867°
Arg. of periapsis
128.7342°
True anomaly
231.36861°
Mean anomaly
233.1351°
Eccentric anomaly
232.24926°
Mean motion
3.65432 °/min
Orbital period
98.51 mins
BSTAR
0.00053632
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Other satellites on launch #25 in the year 1962 (1962-06-19 UTC)

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