DELTA 1 DEB (YO), 228

Orbit data source: Space-Track

DELTA 1 DEB (YO), 228 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
228, 1962-002C
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
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 DELTA 1 DEB (YO)
1 00228U 62002C   26035.09783861  .00030009  00000-0  66093-3 0  9999
2 00228  48.4319 300.5773 0007355 209.0937 150.9595 15.43569253422485
Epoch: 2026-02-04T02:20Z
TLE epoch observation values (Epoch: 2026-02-04T02:20:53.255Z)
Latitude
-0.00003°
Longitude
131.08607°
Altitude
440.351 km
Speed
7.647 km/s
True Right ascension
20h 02m 18s
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
00:59:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.638 km
Perigee altitude
431.614 km
Semi-major axis
6,814.763 km
Eccentricity
0.00074
Inclination
48.4319°
RAAN
300.5773°
Arg. of periapsis
209.0937°
True anomaly
151.00038°
Mean anomaly
150.9595°
Eccentric anomaly
150.97994°
Mean motion
3.85804 °/min
Orbital period
93.31 mins
BSTAR
0.00066093
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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