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OPS 6911 (VELA 10), 3955

Orbit data source: Space-Track

OPS 6911 (VELA 10), 3955 is a payload satellite owned by SAMSO (US) in HEO that was launched on Fri, 23 May 1969 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.

Not visible in the next 10 days
Identifier
3955, 1969-046E
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
TRW
Mission
Spacecraft
Bus & Motor
VELA, BE-3A7
Mass
~365 kg wet, 250 kg dry
Launch date (UTC)
1969-05-23 (57 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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 10 months ago

TLE from 10 months ago
0 OPS 6911 (VELA 10)
1 03955U 69046E   25220.60555884  .00000590  00000-0  00000-0 0  9993
2 03955  62.5463  63.7142 8192423 138.0677   0.4662  0.21421919  6344
Epoch: 2025-08-08T14:32Z
TLE epoch observation values (Epoch: 2025-08-08T14:32:00.283Z)
Latitude
22.80579°
Longitude
56.11098°
Altitude
15,777.682 km
Speed
5.71 km/s
True Right ascension
15h 25m 51s
True Declination
22° 45' 59"
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
01:06:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
208,266.027 km
Perigee altitude
14,948.646 km
Semi-major axis
117,985.473 km
Eccentricity
0.81924
Inclination
62.5463°
RAAN
63.7142°
Arg. of periapsis
138.0677°
True anomaly
8.15735°
Mean anomaly
0.4662°
Eccentric anomaly
2.57521°
Mean motion
0.05356 °/min
Orbital period
6,722.06 mins
BSTAR
0
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