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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.

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Identifier
1982, 1966-008A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational Civil Weather
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
Cyl, 0.5 m
Radar Cross Section
0.920 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 ESSA 1 (OT-3)
1 01982U 66008A   25242.12579982  .00000200  00000-0  62984-4 0  9993
2 01982  97.8549 290.1562 0078636 283.8547  75.3908 14.48164643115815
Epoch: 2025-08-30T03:01Z
TLE epoch observation values (Epoch: 2025-08-30T03:01:09.104Z)
Latitude
-0.00002°
Longitude
-93.69631°
Altitude
720.937 km
Speed
7.502 km/s
True Right ascension
19h 20m 37s
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
15:31:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
784.616 km
Perigee altitude
672.845 km
Semi-major axis
7,106.868 km
Eccentricity
0.00786
Inclination
97.8549°
RAAN
290.1562°
Arg. of periapsis
283.8547°
True anomaly
76.2649°
Mean anomaly
75.3908°
Eccentric anomaly
75.82764°
Mean motion
3.62265 °/min
Orbital period
99.37 mins
BSTAR
0.000062984
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Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

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