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: 1 day ago

TLE from 1 day ago
0 DELTA 1 DEB (YO)
1 00227U 62002B   25258.07784209  .00000292  00000-0  13276-3 0  9995
2 00227  48.1466 145.5502 0128084   5.3719 354.8517 14.40465666304633
Epoch: 2025-09-15T01:52Z
TLE epoch observation values (Epoch: 2025-09-15T01:52:05.556Z)
Latitude
-0.00006°
Longitude
123.23933°
Altitude
666.292 km
Speed
7.573 km/s
True Right ascension
09h 42m 12s
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
23:30:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
849.403 km
Perigee altitude
666.598 km
Semi-major axis
7,136.138 km
Eccentricity
0.01281
Inclination
48.1466°
RAAN
145.5502°
Arg. of periapsis
5.3719°
True anomaly
354.71786°
Mean anomaly
354.8517°
Eccentric anomaly
354.785°
Mean motion
3.60038 °/min
Orbital period
99.99 mins
BSTAR
0.00013276
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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