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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.

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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, 1.1 m
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 SECOR 8 (EGRS 8)
1 02520U 66089B   26306.65380399 -.00000018  00000-0 -98578-2 0  9998
2 02520  89.8649  30.7312 0014892 168.1088 192.0117  8.58893610393843
Epoch: 2026-11-02T15:41Z
TLE epoch observation values (Epoch: 2026-11-02T15:41:28.664Z)
Latitude
-0.00002°
Longitude
113.43404°
Altitude
3,710.564 km
Speed
6.282 km/s
True Right ascension
02h 02m 55s
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
09:49:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,706.521 km
Perigee altitude
3,676.53 km
Semi-major axis
10,069.663 km
Eccentricity
0.00149
Inclination
89.8649°
RAAN
30.7312°
Arg. of periapsis
168.1088°
True anomaly
191.97625°
Mean anomaly
192.0117°
Eccentric anomaly
191.99397°
Mean motion
2.14793 °/min
Orbital period
167.6 mins
BSTAR
-0.0098578
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Other satellites on launch #89 in the year 1966 (1966-10-05 UTC)

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