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OPS 1527 (OV3-1), 2150

Orbit data source: Space-Track

OPS 1527 (OV3-1), 2150 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Fri, 22 Apr 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.

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Identifier
2150, 1966-034A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Space General
Mission
Spacecraft
Bus & Motor
OV3, Unknown motor
Mass
69 kg wet, 69 kg dry
Launch date (UTC)
1966-04-22 (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: 18 hours ago

TLE from 18 hours ago
0 OPS 1527 (OV3-1)
1 02150U 66034A   26067.88465693  .00012281  00000-0  65231-3 0  9991
2 02150  82.3683 245.3788 1401909 261.8984  82.1242 12.59625826389239
Epoch: 2026-03-08T21:13Z
TLE epoch observation values (Epoch: 2026-03-08T21:13:54.358Z)
Latitude
-0.00006°
Longitude
120.31676°
Altitude
1,430.24 km
Speed
7.145 km/s
True Right ascension
16h 21m 30s
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
19:39:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,515.213 km
Perigee altitude
328.269 km
Semi-major axis
7,799.878 km
Eccentricity
0.14019
Inclination
82.3683°
RAAN
245.3788°
Arg. of periapsis
261.8984°
True anomaly
98.21383°
Mean anomaly
82.1242°
Eccentric anomaly
90.15652°
Mean motion
3.15073 °/min
Orbital period
114.26 mins
BSTAR
0.00065231
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Other satellites on launch #34 in the year 1966 (1966-04-22 UTC)

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