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
Last TLE update
3 days ago
Origin
Manufacturer
RCA/East Windsor
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~1 kg wet, ~1 kg dry
Launch date (UTC)
1961-07-12 (64 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history

TLE from 3 days ago
0 DELTA 1 DEB (YO)
1   167U 61017D   25195.96745802  .00000157  00000-0  12858-3 0  9992
2   167  47.8457  91.2478 0090093 170.3146 189.9499 14.23947544317110
Epoch: 2025-07-14T23:13Z
TLE epoch observation values (Epoch: 2025-07-14T23:13:08.372Z)
Latitude
-0.00007°
Longitude
169.89412°
Altitude
876.152 km
Speed
7.383 km/s
True Right ascension
06h 04m 59s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
39.57876°
Longitude
-72.82468°
Altitude
785.032 km
Speed
7.482 km/s
Apparent Right ascension
11h 02m 20s
Apparent Declination
3° 45' 23"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
19:41:22
Azimuth
300.935° NW
Elevation
-26.579°
Doppler factor
1
Orbital elements
Apogee altitude
877.902 km
Perigee altitude
748.326 km
Semi-major axis
7,191.251 km
Eccentricity
0.00901
Inclination
47.8457°
RAAN
91.2478°
Arg. of periapsis
170.3146°
True anomaly
189.77347°
Mean anomaly
189.9499°
Eccentric anomaly
189.86149°
Mean motion
3.55907 °/min
Orbital period
101.15 mins
BSTAR
0.00012858
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Other satellites on launch #17 in the year 1961 (1961-07-12 UTC)
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