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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
Civil Science
Bus & Motor
OV3, Unknown motor
Mass
69 kg wet, 69 kg dry
Launch date (UTC)
1966-04-22 (59 years ago)
Launch vehicle
SCOUT B
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Oct Cyl, 0.4 m
Radar Cross Section
0.613 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 OPS 1527 (OV3-1)
1 02150U 66034A   25242.06864256  .00011430  00000-0  61487-3 0  9997
2 02150  82.3705  14.3858 1427053 345.2517  11.0695 12.54061723365268
Epoch: 2025-08-30T01:38Z
TLE epoch observation values (Epoch: 2025-08-30T01:38:50.717Z)
Latitude
-0.00001°
Longitude
11.16624°
Altitude
361.577 km
Speed
8.21 km/s
True Right ascension
00h 57m 32s
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
16:00:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,561.184 km
Perigee altitude
328.433 km
Semi-major axis
7,822.946 km
Eccentricity
0.14271
Inclination
82.3705°
RAAN
14.3858°
Arg. of periapsis
345.2517°
True anomaly
14.86566°
Mean anomaly
11.0695°
Eccentric anomaly
12.89406°
Mean motion
3.13681 °/min
Orbital period
114.77 mins
BSTAR
0.00061487
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Other satellites on launch #34 in the year 1966 (1966-04-22 UTC)

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