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: 21 hours ago

TLE from 21 hours ago
0 DELTA 1 DEB (YO)
1 00228U 62002C   25291.02599633  .00040693  00000-0  11345-2 0  9996
2 00228  48.4312 149.6246 0006937  94.9581 265.2149 15.36254042405672
Epoch: 2025-10-18T00:37Z
TLE epoch observation values (Epoch: 2025-10-18T00:37:26.082Z)
Latitude
-0.00004°
Longitude
113.50296°
Altitude
457.98 km
Speed
7.639 km/s
True Right ascension
09h 58m 29s
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
16:31:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.978 km
Perigee altitude
453.493 km
Semi-major axis
6,836.373 km
Eccentricity
0.00069
Inclination
48.4312°
RAAN
149.6246°
Arg. of periapsis
94.9581°
True anomaly
265.13569°
Mean anomaly
265.2149°
Eccentric anomaly
265.17529°
Mean motion
3.83976 °/min
Orbital period
93.76 mins
BSTAR
0.0011345
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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