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 (63 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
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   25255.47813435  .00000594  00000-0  12824-3 0  9993
2 00312  58.2486 322.5452 0187238 295.0438  63.1257 14.60815838318329
Epoch: 2025-09-12T11:28Z
TLE epoch observation values (Epoch: 2025-09-12T11:28:30.807Z)
Latitude
-0.00002°
Longitude
158.69155°
Altitude
634.095 km
Speed
7.573 km/s
True Right ascension
21h 30m 10s
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
19:09:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
822.361 km
Perigee altitude
557.675 km
Semi-major axis
7,068.155 km
Eccentricity
0.01872
Inclination
58.2486°
RAAN
322.5452°
Arg. of periapsis
295.0438°
True anomaly
65.05965°
Mean anomaly
63.1257°
Eccentric anomaly
64.09066°
Mean motion
3.65245 °/min
Orbital period
98.56 mins
BSTAR
0.00012824
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Other satellites on launch #25 in the year 1962 (1962-06-19 UTC)

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