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 4 days

TLE from in 4 days
0 OPS 6679 (VELA 8)
1  2766U 67040B   26148.52225105 -.00001179  00000-0  00000+0 0  9999
2  2766  36.4866   5.2796 4640335 121.7860 358.7111  0.21294873  5451
Epoch: 2026-05-28T12:32Z
TLE epoch observation values (Epoch: 2026-05-28T12:32:02.490Z)
Latitude
30.58036°
Longitude
58.26687°
Altitude
57,912.786 km
Speed
3.006 km/s
True Right ascension
08h 49m 22s
True Declination
30° 33' 49"
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
07:43:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167,043.79 km
Perigee altitude
57,109.716 km
Semi-major axis
118,454.89 km
Eccentricity
0.46403
Inclination
36.4866°
RAAN
5.2796°
Arg. of periapsis
121.786°
True anomaly
356.02747°
Mean anomaly
358.7111°
Eccentric anomaly
357.5958°
Mean motion
0.05324 °/min
Orbital period
6,762.21 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
|