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
CABLE + BOX, 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   26257.45689260  .00000865  00000-0  16381-3 0  9994
2 00312  58.2450  57.3599 0195164  66.2629 295.8741 14.62040251371975
Epoch: 2026-09-14T10:57Z
TLE epoch observation values (Epoch: 2026-09-14T10:57:55.520Z)
Latitude
0.00002°
Longitude
-100.55834°
Altitude
630.015 km
Speed
7.575 km/s
True Right ascension
03h 49m 26s
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
02:45:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
823.939 km
Perigee altitude
548.203 km
Semi-major axis
7,064.208 km
Eccentricity
0.01952
Inclination
58.245°
RAAN
57.3599°
Arg. of periapsis
66.2629°
True anomaly
293.84066°
Mean anomaly
295.8741°
Eccentric anomaly
294.8595°
Mean motion
3.65551 °/min
Orbital period
98.48 mins
BSTAR
0.00016381
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Other satellites on launch #25 in the year 1962 (1962-06-19 UTC)

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