Showing default

OPS 6679 (VELA 8), 2766

Orbit data source: Space-Track

OPS 6679 (VELA 8), 2766 is a payload satellite owned by USAF SSD (US) in HEO that was launched on Fri, 28 Apr 1967 UTC via a TITAN IIIC launch vehicle from the Air Force Eastern Test Range (AFETR). 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
2766, 1967-040B
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
TRW
Mission
Spacecraft
Bus & Motor
VELA, BE-3
Mass
~348 kg wet, 221 kg dry
Launch date (UTC)
1967-04-28 (59 years ago)
Launch vehicle
TITAN IIIC
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: in 3 days

TLE from in 3 days
0 OPS 6679 (VELA 8)
1 02766U 67040B   26077.99047656 -.00000716  00000-0  00000-0 0  9991
2 02766  36.0453   6.6849 4644594 119.1395 359.8489  0.21266075  5305
Epoch: 2026-03-18T23:46Z
TLE epoch observation values (Epoch: 2026-03-18T23:46:17.174Z)
Latitude
32.38925°
Longitude
-46.85989°
Altitude
57,515.032 km
Speed
3.019 km/s
True Right ascension
08h 25m 01s
True Declination
32° 22' 19"
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
20:59:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167,250.821 km
Perigee altitude
57,116.526 km
Semi-major axis
118,561.81 km
Eccentricity
0.46446
Inclination
36.0453°
RAAN
6.6849°
Arg. of periapsis
119.1395°
True anomaly
359.53344°
Mean anomaly
359.8489°
Eccentric anomaly
359.71786°
Mean motion
0.05317 °/min
Orbital period
6,771.37 mins
BSTAR
0
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
|