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
Medium (>0.1 m² and <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   26177.03562037  .00000304  00000-0  80840-4 0  9991
2 00312  58.2478 352.3269 0185802 319.2067  39.5176 14.61872513360215
Epoch: 2026-06-26T00:51Z
TLE epoch observation values (Epoch: 2026-06-26T00:51:17.599Z)
Latitude
-0.00005°
Longitude
65.33363°
Altitude
588.26 km
Speed
7.62 km/s
True Right ascension
23h 29m 18s
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
08:23:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
817.875 km
Perigee altitude
555.347 km
Semi-major axis
7,064.748 km
Eccentricity
0.01858
Inclination
58.2478°
RAAN
352.3269°
Arg. of periapsis
319.2067°
True anomaly
40.89696°
Mean anomaly
39.5176°
Eccentric anomaly
40.2048°
Mean motion
3.65509 °/min
Orbital period
98.49 mins
BSTAR
0.00008084
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Other satellites on launch #25 in the year 1962 (1962-06-19 UTC)

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