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
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   25257.24790318  .00013558  00000-0  41040-3 0  9991
2 00228  48.4346 324.6025 0010444 289.2787  70.7020 15.34317090400486
Epoch: 2025-09-14T05:56Z
TLE epoch observation values (Epoch: 2025-09-14T05:56:58.834Z)
Latitude
-0.00005°
Longitude
-118.11233°
Altitude
460.978 km
Speed
7.639 km/s
True Right ascension
21h 38m 24s
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
20:32:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.132 km
Perigee altitude
456.84 km
Semi-major axis
6,842.123 km
Eccentricity
0.00104
Inclination
48.4346°
RAAN
324.6025°
Arg. of periapsis
289.2787°
True anomaly
70.815°
Mean anomaly
70.702°
Eccentric anomaly
70.7585°
Mean motion
3.83492 °/min
Orbital period
93.87 mins
BSTAR
0.0004104
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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