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
CABLE + BOX, 0.054 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 DELTA 1 DEB (YO)
1 00167U 61017D   26271.17457766  .00000103  00000-0  10579-3 0  9999
2 00167  47.8457 314.8102 0090138 174.5841 185.6038 14.24205903379359
Epoch: 2026-09-28T04:11Z
TLE epoch observation values (Epoch: 2026-09-28T04:11:23.509Z)
Latitude
-0.00001°
Longitude
-114.99548°
Altitude
875.96 km
Speed
7.382 km/s
True Right ascension
20h 59m 14s
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
06:34:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
877.057 km
Perigee altitude
747.432 km
Semi-major axis
7,190.381 km
Eccentricity
0.00901
Inclination
47.8457°
RAAN
314.8102°
Arg. of periapsis
174.5841°
True anomaly
185.50406°
Mean anomaly
185.6038°
Eccentric anomaly
185.55382°
Mean motion
3.55972 °/min
Orbital period
101.13 mins
BSTAR
0.00010579
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Other satellites on launch #17 in the year 1961 (1961-07-12 UTC)

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