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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: 5 hours ago

TLE from 5 hours ago
0 OPS 1527 (OV3-1)
1 02150U 66034A   25323.93657096  .00011322  00000-0  59789-3 0  9997
2 02150  82.3677 319.1681 1417055 155.4712 212.1145 12.56474644375532
Epoch: 2025-11-19T22:28Z
TLE epoch observation values (Epoch: 2025-11-19T22:28:39.730Z)
Latitude
-0.00006°
Longitude
-77.1986°
Altitude
2,415.986 km
Speed
6.299 km/s
True Right ascension
21h 16m 40s
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
00:23:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,541.918 km
Perigee altitude
327.65 km
Semi-major axis
7,812.921 km
Eccentricity
0.14171
Inclination
82.3677°
RAAN
319.1681°
Arg. of periapsis
155.4712°
True anomaly
204.63364°
Mean anomaly
212.1145°
Eccentric anomaly
208.26917°
Mean motion
3.14285 °/min
Orbital period
114.55 mins
BSTAR
0.00059789
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Other satellites on launch #34 in the year 1966 (1966-04-22 UTC)

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