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: 17 hours ago

TLE from 17 hours ago
0 DELTA 1 DEB (YO)
1 00312U 62025C   25242.68014258  .00001523  00000-0  27600-3 0  9999
2 00312  58.2490   9.3932 0186761 277.3445  80.6395 14.60779898316452
Epoch: 2025-08-30T16:19Z
TLE epoch observation values (Epoch: 2025-08-30T16:19:24.318Z)
Latitude
-0.0001°
Longitude
145.43085°
Altitude
672.982 km
Speed
7.531 km/s
True Right ascension
00h 37m 34s
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
01:26:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
822.141 km
Perigee altitude
558.126 km
Semi-major axis
7,068.271 km
Eccentricity
0.01868
Inclination
58.249°
RAAN
9.3932°
Arg. of periapsis
277.3445°
True anomaly
82.75869°
Mean anomaly
80.6395°
Eccentric anomaly
81.69835°
Mean motion
3.65236 °/min
Orbital period
98.57 mins
BSTAR
0.000276
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Other satellites on launch #25 in the year 1962 (1962-06-19 UTC)

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