Showing default

SECOR 7 (EGRS 7), 2411

Orbit data source: Space-Track

SECOR 7 (EGRS 7), 2411 is an American payload satellite in LEO that was launched on Fri, 19 Aug 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
2411, 1966-077B
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)
1966-08-19 (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
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 SECOR 7 (EGRS 7)
1  2411U 66077B   26071.51365860  .00000003  00000-0  76474-3 0  9998
2  2411  90.3265 276.3232 0011619 151.7523 208.3961  8.59615459869073
Epoch: 2026-03-12T12:19Z
TLE epoch observation values (Epoch: 2026-03-12T12:19:40.103Z)
Latitude
0.00005°
Longitude
-78.75636°
Altitude
3,700.545 km
Speed
6.286 km/s
True Right ascension
18h 25m 17s
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
16:03:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,697.579 km
Perigee altitude
3,674.192 km
Semi-major axis
10,064.022 km
Eccentricity
0.00116
Inclination
90.3265°
RAAN
276.3232°
Arg. of periapsis
151.7523°
True anomaly
208.33286°
Mean anomaly
208.3961°
Eccentric anomaly
208.36447°
Mean motion
2.14974 °/min
Orbital period
167.46 mins
BSTAR
0.00076474
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...

Documentation

Showing up to 5 results
|