Showing default

SECOR 9 (EGRS 9), 2861

Orbit data source: Space-Track

SECOR 9 (EGRS 9), 2861 is an American payload satellite in LEO that was launched on Thu, 29 Jun 1967 UTC via a THOR BURNER 2 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
2861, 1967-065A
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)
1967-06-29 (58 years ago)
Launch vehicle
THOR BURNER 2
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: 1 day ago

TLE from 1 day ago
0 SECOR 9 (EGRS 9)
1 02861U 67065A   25309.00803036  .00000001  00000-0 -38343-3 0  9996
2 02861  89.9880 314.2253 0072456 315.7721  43.7340  8.36660789782305
Epoch: 2025-11-05T00:11Z
TLE epoch observation values (Epoch: 2025-11-05T00:11:33.823Z)
Latitude
-0°
Longitude
-93.1525°
Altitude
3,820.094 km
Speed
6.269 km/s
True Right ascension
20h 56m 54s
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
04:28:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,943.459 km
Perigee altitude
3,794.962 km
Semi-major axis
10,247.347 km
Eccentricity
0.00725
Inclination
89.988°
RAAN
314.2253°
Arg. of periapsis
315.7721°
True anomaly
44.31176°
Mean anomaly
43.734°
Eccentric anomaly
44.0225°
Mean motion
2.09231 °/min
Orbital period
172.06 mins
BSTAR
-0.00038343
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 #65 in the year 1967 (1967-06-29 UTC)

Documentation

Showing up to 5 results
|