DELTA 1 DEB (YO), 167

Orbit data source: Space-Track

DELTA 1 DEB (YO), 167 is space debris in LEO originally from a launch on Wed, 12 Jul 1961 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
167, 1961-017D
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)
1961-07-12 (65 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: 3 days ago

TLE from 3 days ago
0 DELTA 1 DEB (YO)
1 00167U 61017D   26076.41005421 -.00000076  00000-0  32343-4 0  9990
2 00167  47.8437  91.6636 0089511  95.9328 265.1766 14.24132197351590
Epoch: 2026-03-17T09:50Z
TLE epoch observation values (Epoch: 2026-03-17T09:50:28.683Z)
Latitude
-0.00004°
Longitude
129.05547°
Altitude
817.696 km
Speed
7.443 km/s
True Right ascension
06h 06m 39s
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
11:29:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
876.857 km
Perigee altitude
748.129 km
Semi-major axis
7,190.63 km
Eccentricity
0.00895
Inclination
47.8437°
RAAN
91.6636°
Arg. of periapsis
95.9328°
True anomaly
264.15553°
Mean anomaly
265.1766°
Eccentric anomaly
264.66596°
Mean motion
3.55953 °/min
Orbital period
101.14 mins
BSTAR
0.000032343
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Other satellites on launch #17 in the year 1961 (1961-07-12 UTC)

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