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 (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: 20 hours ago

TLE from 20 hours ago
0 DELTA 1 DEB (YO)
1 00227U 62002B   26233.55024111  .00000031  00000-0  58224-4 0  9995
2 00227  48.1476  55.6277 0127273 329.1101  30.2351 14.40819025353722
Epoch: 2026-08-21T13:12Z
TLE epoch observation values (Epoch: 2026-08-21T13:12:20.831Z)
Latitude
-0.00002°
Longitude
-112.3325°
Altitude
677.99 km
Speed
7.56 km/s
True Right ascension
03h 42m 30s
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
00:36:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
847.643 km
Perigee altitude
666.025 km
Semi-major axis
7,134.971 km
Eccentricity
0.01273
Inclination
48.1476°
RAAN
55.6277°
Arg. of periapsis
329.1101°
True anomaly
30.97971°
Mean anomaly
30.2351°
Eccentric anomaly
30.60637°
Mean motion
3.60126 °/min
Orbital period
99.96 mins
BSTAR
0.000058224
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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