Showing default

ESSA 1 (OT-3), 1982

Orbit data source: Space-Track

ESSA 1 (OT-3), 1982 is a payload satellite owned by ESSA (US) in SSO that was launched on Thu, 03 Feb 1966 UTC via a THOR DELTA C launch vehicle from the Air Force Eastern Test Range (AFETR). 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
1982, 1966-008A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational spacecraft
Bus & Motor
TIROS I, Unknown motor
Mass
138 kg wet, 138 kg dry
Launch date (UTC)
1966-02-03 (60 years ago)
Launch vehicle
THOR DELTA C
Launch site
Air Force Eastern Test Range (AFETR)
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: 3 hours ago

TLE from 3 hours ago
0 ESSA 1 (OT-3)
1 01982U 66008A   26120.59798558  .00000163  00000-0  53052-4 0  9996
2 01982  97.8154 156.0390 0078448 250.9030 108.3658 14.48322755151054
Epoch: 2026-04-30T14:21Z
TLE epoch observation values (Epoch: 2026-04-30T14:21:05.954Z)
Latitude
-0.00002°
Longitude
82.2219°
Altitude
752.081 km
Speed
7.469 km/s
True Right ascension
10h 24m 09s
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
01:20:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
783.959 km
Perigee altitude
672.463 km
Semi-major axis
7,106.348 km
Eccentricity
0.00784
Inclination
97.8154°
RAAN
156.039°
Arg. of periapsis
250.903°
True anomaly
109.2163°
Mean anomaly
108.3658°
Eccentric anomaly
108.79132°
Mean motion
3.62304 °/min
Orbital period
99.36 mins
BSTAR
0.000053052
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 #8 in the year 1966 (1966-02-03 UTC)

Documentation

Showing up to 5 results
|