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ESSA 3 (TOS-A), 2435

Orbit data source: Space-Track

ESSA 3 (TOS-A), 2435 is a payload satellite owned by ESSA (US) in SSO that was launched on Sun, 02 Oct 1966 UTC via a THOR DELTA E 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.

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Identifier
2435, 1966-087A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational spacecraft
Bus & Motor
TIROS I, Unknown motor
Mass
148 kg wet, 148 kg dry
Launch date (UTC)
1966-10-02 (60 years ago)
Launch vehicle
THOR DELTA E
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: 6 hours ago

TLE from 6 hours ago
0 ESSA 3 (TOS-A)
1  2435U 66087A   26099.16920078 -.00000035  00000-0  39270-4 0  9994
2  2435 101.0825   6.1136 0063917 175.5053 358.3174 12.56879393730332
Epoch: 2026-04-09T04:03Z
TLE epoch observation values (Epoch: 2026-04-09T04:03:38.947Z)
Latitude
6.01123°
Longitude
-71.04374°
Altitude
1,387.951 km
Speed
7.189 km/s
True Right ascension
12h 29m 09s
True Declination
5° 58' 42"
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
16:16:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,483.28 km
Perigee altitude
1,383.422 km
Semi-major axis
7,811.488 km
Eccentricity
0.00639
Inclination
101.0825°
RAAN
6.1136°
Arg. of periapsis
175.5053°
True anomaly
358.29572°
Mean anomaly
358.3174°
Eccentric anomaly
358.30658°
Mean motion
3.14371 °/min
Orbital period
114.51 mins
BSTAR
0.00003927
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Other satellites on launch #87 in the year 1966 (1966-10-02 UTC)

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