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
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 DELTA 1 DEB (YO)
1 00227U 62002B   25259.39583808  .00000354  00000-0  15045-3 0  9998
2 00227  48.1463 139.6296 0128030  10.8360 349.5248 14.40467422304823
Epoch: 2025-09-16T09:30Z
TLE epoch observation values (Epoch: 2025-09-16T09:30:00.41Z)
Latitude
-0°
Longitude
1.54114°
Altitude
667.508 km
Speed
7.572 km/s
True Right ascension
09h 18m 31s
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
18:23:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
849.359 km
Perigee altitude
666.631 km
Semi-major axis
7,136.132 km
Eccentricity
0.0128
Inclination
48.1463°
RAAN
139.6296°
Arg. of periapsis
10.836°
True anomaly
349.2538°
Mean anomaly
349.5248°
Eccentric anomaly
349.38973°
Mean motion
3.60038 °/min
Orbital period
99.99 mins
BSTAR
0.00015045
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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