Showing default

OSCAR 3, 1293

Orbit data source: Space-Track

OSCAR 3, 1293 is a payload satellite owned by OSCAR (US) in LEO that was launched on Tue, 09 Mar 1965 UTC via a THOR SLV-2 AGENA D 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
1293, 1965-016F
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
OSCAR
Mission
Non-operational spacecraft
Bus & Motor
OSCAR, Unknown motor
Mass
15 kg wet, 15 kg dry
Launch date (UTC)
1965-03-09 (61 years ago)
Launch vehicle
THOR SLV-2 AGENA D
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: 17 hours ago

TLE from 17 hours ago
0 OSCAR 3
1  1293U 65016F   25355.53830617  .00000316  00000-0  21608-3 0  9996
2  1293  70.0746  65.5625 0016147  14.7411 345.4169 14.08314119107076
Epoch: 2025-12-21T12:55Z
TLE epoch observation values (Epoch: 2025-12-21T12:55:09.653Z)
Latitude
-0.00001°
Longitude
141.42296°
Altitude
856.158 km
Speed
7.431 km/s
True Right ascension
04h 22m 14s
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
04:34:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
874.863 km
Perigee altitude
851.478 km
Semi-major axis
7,241.307 km
Eccentricity
0.00161
Inclination
70.0746°
RAAN
65.5625°
Arg. of periapsis
14.7411°
True anomaly
345.37022°
Mean anomaly
345.4169°
Eccentric anomaly
345.39357°
Mean motion
3.52223 °/min
Orbital period
102.21 mins
BSTAR
0.00021608
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
|