Showing default

OPS 1427 (OV3-4), 2201

Orbit data source: Space-Track

OPS 1427 (OV3-4), 2201 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Fri, 10 Jun 1966 UTC via an SCOUT B launch vehicle from the Wallops Island (WLPIS). 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
2201, 1966-052A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Space General
Mission
Defense Technology
Bus & Motor
OV3, Unknown motor
Mass
78 kg wet, 78 kg dry
Launch date (UTC)
1966-06-10 (59 years ago)
Launch vehicle
SCOUT B
Launch site
Wallops Island (WLPIS)
Object type
Payload
Rocket body
Debris
Shape & HBR
Oct Cyl, 0.3 m
Radar Cross Section
0.548 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 OPS 1427 (OV3-4)
1 02201U 66052A   25243.39563424  .00000238  00000-0  35677-3 0  9990
2 02201  40.9018 273.4369 2236770 278.5510  56.9819 10.10051052168028
Epoch: 2025-08-31T09:29Z
TLE epoch observation values (Epoch: 2025-08-31T09:29:42.798Z)
Latitude
-0°
Longitude
151.19239°
Altitude
1,935.139 km
Speed
7.199 km/s
True Right ascension
18h 13m 44s
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
16:14:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,686.324 km
Perigee altitude
641.359 km
Semi-major axis
9,041.978 km
Eccentricity
0.22368
Inclination
40.9018°
RAAN
273.4369°
Arg. of periapsis
278.551°
True anomaly
81.51827°
Mean anomaly
56.9819°
Eccentric anomaly
68.94176°
Mean motion
2.52434 °/min
Orbital period
142.61 mins
BSTAR
0.00035677
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 #52 in the year 1966 (1966-06-10 UTC)

Documentation

Showing up to 5 results
|