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 (65 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CABLE + BOX, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <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   26253.20791440  .00039033  00000-0  49843-3 0  9996
2 00228  48.4271 223.1743 0001832 164.5240 195.5763 15.58775008456342
Epoch: 2026-09-10T04:59Z
TLE epoch observation values (Epoch: 2026-09-10T04:59:23.804Z)
Latitude
-0.00003°
Longitude
159.07617°
Altitude
392.782 km
Speed
7.675 km/s
True Right ascension
14h 52m 41s
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
14:38:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
393.49 km
Perigee altitude
391.009 km
Semi-major axis
6,770.387 km
Eccentricity
0.00018
Inclination
48.4271°
RAAN
223.1743°
Arg. of periapsis
164.524°
True anomaly
195.57066°
Mean anomaly
195.5763°
Eccentric anomaly
195.57348°
Mean motion
3.89604 °/min
Orbital period
92.4 mins
BSTAR
0.00049843
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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