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, 0.065 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 DELTA 1 DEB (YO)
1   227U 62002B   26305.46518140  .00000120  00000-0  82805-4 0  9996
2   227  48.1466  92.3898 0127537 265.7878  92.8433 14.40851562364096
Epoch: 2026-11-01T11:09Z
TLE epoch observation values (Epoch: 2026-11-01T11:09:51.672Z)
Latitude
-0.00005°
Longitude
-115.83171°
Altitude
761.692 km
Speed
7.472 km/s
True Right ascension
06h 09m 33s
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
18:16:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
847.723 km
Perigee altitude
665.731 km
Semi-major axis
7,134.864 km
Eccentricity
0.01275
Inclination
48.1466°
RAAN
92.3898°
Arg. of periapsis
265.7878°
True anomaly
94.30166°
Mean anomaly
92.8433°
Eccentric anomaly
93.57261°
Mean motion
3.60134 °/min
Orbital period
99.96 mins
BSTAR
0.000082805
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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