Showing default

OV3-3, 2389

Orbit data source: Space-Track

OV3-3, 2389 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Thu, 04 Aug 1966 UTC via an SCOUT B launch vehicle from the Air Force Western Test Range (AFWTR). 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
2389, 1966-070A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Space General
Mission
Spacecraft
Bus & Motor
OV3, Unknown motor
Mass
77 kg wet, 77 kg dry
Launch date (UTC)
1966-08-04 (60 years ago)
Launch vehicle
SCOUT B
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 OV3-3
1 02389U 66070A   26120.59271304  .00007042  00000-0  32090-3 0  9993
2 02389  81.3312  12.9794 1014683 281.1397  67.7466 13.44406710592572
Epoch: 2026-04-30T14:13Z
TLE epoch observation values (Epoch: 2026-04-30T14:13:30.406Z)
Latitude
-0.00002°
Longitude
-58.9344°
Altitude
878.086 km
Speed
7.52 km/s
True Right ascension
00h 51m 55s
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
07:31:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,847.916 km
Perigee altitude
332.333 km
Semi-major axis
7,468.262 km
Eccentricity
0.10147
Inclination
81.3312°
RAAN
12.9794°
Arg. of periapsis
281.1397°
True anomaly
78.97704°
Mean anomaly
67.7466°
Eccentric anomaly
73.31555°
Mean motion
3.3629 °/min
Orbital period
107.05 mins
BSTAR
0.0003209
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #70 in the year 1966 (1966-08-04 UTC)

Documentation

Showing up to 5 results
|