DELTA 1 DEB (YO), 227

Orbit data source: Space-Track

DELTA 1 DEB (YO), 227 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
227, 1962-002B
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: 9 hours ago

TLE from 9 hours ago
0 DELTA 1 DEB (YO)
1 00227U 62002B   25340.48171662  .00000559  00000-0  20780-3 0  9999
2 00227  48.1456 135.3488 0127526 345.0004  14.7125 14.40591476316519
Epoch: 2025-12-06T11:33Z
TLE epoch observation values (Epoch: 2025-12-06T11:33:40.315Z)
Latitude
-0.00001°
Longitude
-113.57802°
Altitude
668.961 km
Speed
7.57 km/s
True Right ascension
09h 01m 23s
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
18:57:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
848.585 km
Perigee altitude
666.587 km
Semi-major axis
7,135.723 km
Eccentricity
0.01275
Inclination
48.1456°
RAAN
135.3488°
Arg. of periapsis
345.0004°
True anomaly
15.08944°
Mean anomaly
14.7125°
Eccentric anomaly
14.90038°
Mean motion
3.60069 °/min
Orbital period
99.98 mins
BSTAR
0.0002078
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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