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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 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: 16 hours ago

TLE from 16 hours ago
0 ESSA 1 (OT-3)
1 01982U 66008A   26106.08983398  .00000069  00000-0  28889-4 0  9997
2 01982  97.8178 142.6058 0078498 296.5566  62.7598 14.48317986148958
Epoch: 2026-04-16T02:09Z
TLE epoch observation values (Epoch: 2026-04-16T02:09:21.655Z)
Latitude
-0.00004°
Longitude
-93.9768°
Altitude
708.927 km
Speed
7.515 km/s
True Right ascension
09h 30m 25s
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
00:50:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
784.01 km
Perigee altitude
672.443 km
Semi-major axis
7,106.364 km
Eccentricity
0.00785
Inclination
97.8178°
RAAN
142.6058°
Arg. of periapsis
296.5566°
True anomaly
63.56314°
Mean anomaly
62.7598°
Eccentric anomaly
63.16111°
Mean motion
3.62303 °/min
Orbital period
99.36 mins
BSTAR
0.000028889
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Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

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