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 shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DELTA 1 DEB (YO)
1 00312U 62025C   25286.13642022  .00003848  00000-0  63623-3 0  9990
2 00312  58.2461 210.2862 0189904 337.0442  22.2182 14.61039728322802
Epoch: 2025-10-13T03:16Z
TLE epoch observation values (Epoch: 2025-10-13T03:16:26.707Z)
Latitude
-0.00001°
Longitude
139.23138°
Altitude
567.319 km
Speed
7.644 km/s
True Right ascension
14h 01m 08s
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
04:43:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
823.509 km
Perigee altitude
555.083 km
Semi-major axis
7,067.433 km
Eccentricity
0.01899
Inclination
58.2461°
RAAN
210.2862°
Arg. of periapsis
337.0442°
True anomaly
23.05952°
Mean anomaly
22.2182°
Eccentric anomaly
22.63699°
Mean motion
3.65301 °/min
Orbital period
98.55 mins
BSTAR
0.00063623
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Other satellites on launch #25 in the year 1962 (1962-06-19 UTC)

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