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: 2 days ago

TLE from 2 days ago
0 DELTA 1 DEB (YO)
1 00312U 62025C   26110.62830024  .00000952  00000-0  18185-3 0  9998
2 00312  58.2468 235.8246 0185612 227.4736 131.0495 14.61745325350509
Epoch: 2026-04-20T15:04Z
TLE epoch observation values (Epoch: 2026-04-20T15:04:45.140Z)
Latitude
0.00003°
Longitude
160.92083°
Altitude
776.419 km
Speed
7.42 km/s
True Right ascension
15h 43m 17s
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
11:25:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
818.159 km
Perigee altitude
555.883 km
Semi-major axis
7,065.158 km
Eccentricity
0.01856
Inclination
58.2468°
RAAN
235.8246°
Arg. of periapsis
227.4736°
True anomaly
132.62924°
Mean anomaly
131.0495°
Eccentric anomaly
131.84178°
Mean motion
3.65477 °/min
Orbital period
98.5 mins
BSTAR
0.00018185
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Other satellites on launch #25 in the year 1962 (1962-06-19 UTC)

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