Showing default

OV2-3, 13912

Orbit data source: Space-Track

OV2-3, 13912 is a payload satellite owned by USAF SSD (US) in HEO that was launched on Tue, 21 Dec 1965 UTC via a TITAN IIIC launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
13912, 1965-108V
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Northrop
Mission
Spacecraft
Bus & Motor
OV2, Unknown motor
Mass
2,144 kg wet, 194 kg dry
Launch date (UTC)
1965-12-21 (60 years ago)
Launch vehicle
TITAN IIIC
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 OV2-3
1 13912U 65108V   26032.47781727  .00016151  00000-0  10803-2 0  9990
2 13912  26.5876 215.3126 5249422 288.3983  22.9775  5.27151136563514
Epoch: 2026-02-01T11:28Z
TLE epoch observation values (Epoch: 2026-02-01T11:28:03.412Z)
Latitude
0.00004°
Longitude
-88.38731°
Altitude
2,289.302 km
Speed
7.962 km/s
True Right ascension
14h 21m 15s
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
21:44:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
14,893.96 km
Perigee altitude
248.656 km
Semi-major axis
13,949.445 km
Eccentricity
0.52494
Inclination
26.5876°
RAAN
215.3126°
Arg. of periapsis
288.3983°
True anomaly
71.51495°
Mean anomaly
22.9775°
Eccentric anomaly
43.79206°
Mean motion
1.31737 °/min
Orbital period
273.27 mins
BSTAR
0.0010803
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|