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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.

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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 (59 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: 17 hours ago

TLE from 17 hours ago
0 SECOR 9 (EGRS 9)
1 02861U 67065A   26111.99057788 -.00000022  00000-0 -15126-1 0  9997
2 02861  89.9776 314.1381 0072578 155.8824 204.5436  8.36661323796350
Epoch: 2026-04-21T23:46Z
TLE epoch observation values (Epoch: 2026-04-21T23:46:25.928Z)
Latitude
-0.00002°
Longitude
107.47164°
Altitude
3,941.262 km
Speed
6.195 km/s
True Right ascension
20h 56m 33s
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
00:17:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,943.579 km
Perigee altitude
3,794.833 km
Semi-major axis
10,247.343 km
Eccentricity
0.00726
Inclination
89.9776°
RAAN
314.1381°
Arg. of periapsis
155.8824°
True anomaly
204.20096°
Mean anomaly
204.5436°
Eccentric anomaly
204.372°
Mean motion
2.09231 °/min
Orbital period
172.06 mins
BSTAR
-0.015126
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Other satellites on launch #65 in the year 1967 (1967-06-29 UTC)

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