Showing default

SECOR 8 (EGRS 8), 2520

Orbit data source: Space-Track

SECOR 8 (EGRS 8), 2520 is an American payload satellite in LEO that was launched on Wed, 05 Oct 1966 UTC via an ATLAS SLV-3 AGENA D 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.

Loading next visibility...
Identifier
2520, 1966-089B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
ITT
Mission
Spacecraft
Bus & Motor
SECOR, Unknown motor
Mass
18 kg wet, 18 kg dry
Launch date (UTC)
1966-10-05 (60 years ago)
Launch vehicle
ATLAS SLV-3 AGENA D
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
BOX, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 SECOR 8 (EGRS 8)
1 02520U 66089B   26251.33205373 -.00000006  00000-0 -38891-2 0  9999
2 02520  89.8548  31.0075 0014305 224.2583 135.7125  8.58893946389091
Epoch: 2026-09-08T07:58Z
TLE epoch observation values (Epoch: 2026-09-08T07:58:09.442Z)
Latitude
0.00004°
Longitude
-75.93183°
Altitude
3,706.213 km
Speed
6.284 km/s
True Right ascension
02h 04m 01s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
14:40:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,705.928 km
Perigee altitude
3,677.118 km
Semi-major axis
10,069.66 km
Eccentricity
0.00143
Inclination
89.8548°
RAAN
31.0075°
Arg. of periapsis
224.2583°
True anomaly
135.82681°
Mean anomaly
135.7125°
Eccentric anomaly
135.76967°
Mean motion
2.14793 °/min
Orbital period
167.6 mins
BSTAR
-0.0038891
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 #89 in the year 1966 (1966-10-05 UTC)

Documentation

Showing up to 5 results
|