Showing default

ESSA 2 (OT-2), 2091

Orbit data source: Space-Track

ESSA 2 (OT-2), 2091 is a payload satellite owned by ESSA (US) in SSO that was launched on Mon, 28 Feb 1966 UTC via a THOR DELTA E 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
2091, 1966-016A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational spacecraft
Bus & Motor
TIROS I, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
1966-02-28 (60 years ago)
Launch vehicle
THOR DELTA E
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: 2 days ago

TLE from 2 days ago
0 ESSA 2 (OT-2)
1 02091U 66016A   26174.50884197 -.00000051  00000-0 -33352-4 0  9991
2 02091 101.2322  83.5823 0038334 243.4790 290.3900 12.69431154794429
Epoch: 2026-06-23T12:12Z
TLE epoch observation values (Epoch: 2026-06-23T12:12:43.946Z)
Latitude
6.34758°
Longitude
169.97937°
Altitude
1,376.011 km
Speed
7.176 km/s
True Right ascension
17h 39m 22s
True Declination
6° 18' 46"
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
22:44:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,411.496 km
Perigee altitude
1,352.003 km
Semi-major axis
7,759.886 km
Eccentricity
0.00383
Inclination
101.2322°
RAAN
83.5823°
Arg. of periapsis
243.479°
True anomaly
289.97756°
Mean anomaly
290.39°
Eccentric anomaly
290.18385°
Mean motion
3.17512 °/min
Orbital period
113.38 mins
BSTAR
-0.000033352
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 #16 in the year 1966 (1966-02-28 UTC)

Documentation

Showing up to 5 results
|