OV1-5 R/B, 2123

Orbit data source: Space-Track

OV1-5 R/B, 2123 is space debris in LEO originally from a launch on Wed, 30 Mar 1966 UTC launched from the Air Force Western Test Range (AFWTR). 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
2123, 1966-025C
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
~125 kg wet, ~125 kg dry
Launch date (UTC)
1966-03-30 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.1 m
Radar Cross Section
1.347 m², Medium (>0.1 m² and < 1m²)

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

TLE from 11 hours ago
0 OV1-5 R/B
1 02123U 66025C   25242.83199906  .00000331  00000-0  87293-4 0  9997
2 02123 144.6411 314.6473 0046151  63.5373 297.0026 13.65861282965078
Epoch: 2025-08-30T19:58Z
TLE epoch observation values (Epoch: 2025-08-30T19:58:04.718Z)
Latitude
-0.00001°
Longitude
35.86701°
Altitude
998.124 km
Speed
7.362 km/s
True Right ascension
20h 58m 35s
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
22:19:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,051.569 km
Perigee altitude
983.306 km
Semi-major axis
7,395.574 km
Eccentricity
0.00462
Inclination
144.6411°
RAAN
314.6473°
Arg. of periapsis
63.5373°
True anomaly
296.53017°
Mean anomaly
297.0026°
Eccentric anomaly
296.76651°
Mean motion
3.4126 °/min
Orbital period
105.49 mins
BSTAR
0.000087293
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