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: 17 hours ago

TLE from 17 hours ago
0 DELTA 1 DEB (YO)
1 00228U 62002C   26125.21426080  .00045876  00000-0  80966-3 0  9993
2 00228  48.4293 185.5568 0008129 309.8163  50.2064 15.49793415436437
Epoch: 2026-05-05T05:08Z
TLE epoch observation values (Epoch: 2026-05-05T05:08:32.133Z)
Latitude
-0.00003°
Longitude
-114.66943°
Altitude
414.182 km
Speed
7.666 km/s
True Right ascension
12h 22m 13s
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
05:47:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
423.899 km
Perigee altitude
412.849 km
Semi-major axis
6,796.511 km
Eccentricity
0.00081
Inclination
48.4293°
RAAN
185.5568°
Arg. of periapsis
309.8163°
True anomaly
50.27802°
Mean anomaly
50.2064°
Eccentric anomaly
50.24221°
Mean motion
3.87359 °/min
Orbital period
92.94 mins
BSTAR
0.00080966
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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