Showing default

SECOR 5 (EGRS 5), 1506

Orbit data source: Space-Track

SECOR 5 (EGRS 5), 1506 is an American payload satellite in LEO that was launched on Tue, 10 Aug 1965 UTC via an SCOUT B launch vehicle from the Wallops Island (WLPIS). 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
1506, 1965-063A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Cubic
Mission
Spacecraft
Bus & Motor
NRL 20", Unknown motor
Mass
18 kg wet, 18 kg dry
Launch date (UTC)
1965-08-10 (61 years ago)
Launch vehicle
SCOUT B
Launch site
Wallops Island (WLPIS)
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: 7 hours ago

TLE from 7 hours ago
0 SECOR 5 (EGRS 5)
1 01506U 65063A   26111.92720181 -.00000014  00000-0  13248-3 0  9990
2 01506  69.2350 333.2314 0788864 208.1262 161.0253 11.78686633611623
Epoch: 2026-04-21T22:15Z
TLE epoch observation values (Epoch: 2026-04-21T22:15:10.236Z)
Latitude
11.02487°
Longitude
153.66072°
Altitude
2,392.295 km
Speed
6.485 km/s
True Right ascension
22h 29m 47s
True Declination
10° 58' 21"
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
11:58:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,419.28 km
Perigee altitude
1,132.775 km
Semi-major axis
8,154.165 km
Eccentricity
0.07889
Inclination
69.235°
RAAN
333.2314°
Arg. of periapsis
208.1262°
True anomaly
163.71215°
Mean anomaly
161.0253°
Eccentric anomaly
162.39253°
Mean motion
2.94764 °/min
Orbital period
122.13 mins
BSTAR
0.00013248
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
|