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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 DELTA 1 DEB (YO)
1 00227U 62002B   26178.07036941  .00000173  00000-0  99021-4 0  9991
2 00227  48.1473 304.9806 0126798 100.5675 260.9532 14.40792247345725
Epoch: 2026-06-27T01:41Z
TLE epoch observation values (Epoch: 2026-06-27T01:41:19.917Z)
Latitude
0.00005°
Longitude
4.45785°
Altitude
771.556 km
Speed
7.462 km/s
True Right ascension
20h 19m 55s
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
02:19:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
847.394 km
Perigee altitude
666.451 km
Semi-major axis
7,135.06 km
Eccentricity
0.01268
Inclination
48.1473°
RAAN
304.9806°
Arg. of periapsis
100.5675°
True anomaly
259.52199°
Mean anomaly
260.9532°
Eccentric anomaly
260.23722°
Mean motion
3.6012 °/min
Orbital period
99.97 mins
BSTAR
0.000099021
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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