DELTA 1 DEB (YO), 228

Orbit data source: Space-Track

DELTA 1 DEB (YO), 228 is space debris in LEO originally from a launch on Thu, 08 Feb 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
228, 1962-002C
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)
1962-02-08 (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
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 00228U 62002C   25340.14072250  .00030540  00000-0  76946-3 0  9994
2 00228  48.4327 254.1341 0005046 298.7143  61.3289 15.39523808413237
Epoch: 2025-12-06T03:22Z
TLE epoch observation values (Epoch: 2025-12-06T03:22:38.423Z)
Latitude
0.00001°
Longitude
128.30128°
Altitude
446.249 km
Speed
7.647 km/s
True Right ascension
16h 56m 32s
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
14:37:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
452 km
Perigee altitude
445.111 km
Semi-major axis
6,826.692 km
Eccentricity
0.0005
Inclination
48.4327°
RAAN
254.1341°
Arg. of periapsis
298.7143°
True anomaly
61.37965°
Mean anomaly
61.3289°
Eccentric anomaly
61.35427°
Mean motion
3.84793 °/min
Orbital period
93.56 mins
BSTAR
0.00076946
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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