Showing default

OPS 0340, 2125

Orbit data source: Space-Track

OPS 0340, 2125 is a payload satellite owned by USAF SSD (US) in SSO that was launched on Thu, 31 Mar 1966 UTC via a THOR BURNER 1 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
2125, 1966-026A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Defense Weather
Bus & Motor
P35?, Unknown motor
Mass
72 kg wet, 72 kg dry
Launch date (UTC)
1966-03-31 (59 years ago)
Launch vehicle
THOR BURNER 1
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.3 m
Radar Cross Section
0.377 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 OPS 0340
1 02125U 66026A   25242.73524924  .00001125  00000-0  20891-3 0  9993
2 02125  98.0103  55.1204 0149004  76.0478 285.7242 14.60173833117151
Epoch: 2025-08-30T17:38Z
TLE epoch observation values (Epoch: 2025-08-30T17:38:45.534Z)
Latitude
-0.00006°
Longitude
171.2654°
Altitude
668.51 km
Speed
7.537 km/s
True Right ascension
03h 40m 28s
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
19:56:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
794.997 km
Perigee altitude
584.371 km
Semi-major axis
7,067.821 km
Eccentricity
0.0149
Inclination
98.0103°
RAAN
55.1204°
Arg. of periapsis
76.0478°
True anomaly
284.07253°
Mean anomaly
285.7242°
Eccentric anomaly
284.89917°
Mean motion
3.65271 °/min
Orbital period
98.56 mins
BSTAR
0.00020891
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...

Documentation

Showing up to 5 results
|