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VELA 1, 692

Orbit data source: Space-Track

VELA 1, 692 is a payload satellite owned by USAF SSD (US) in HEO that was launched on Thu, 17 Oct 1963 UTC via an ATLAS AGENA D 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.

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Identifier
692, 1963-039C
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
TRW
Mission
Spacecraft
Bus & Motor
VELA, BE3A
Mass
~207 kg wet, 115 kg dry
Launch date (UTC)
1963-10-17 (63 years ago)
Launch vehicle
ATLAS AGENA D
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
POLY, 1.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 weeks ago

TLE from 2 weeks ago
0 VELA 1
1 00692U 63039C   26246.64073463 -.00000560  00000-0  00000-0 0  9993
2 00692  33.7681  45.3484 5262132 227.7809   0.9690  0.21985686 13341
Epoch: 2026-09-03T15:22Z
TLE epoch observation values (Epoch: 2026-09-03T15:22:39.472Z)
Latitude
-24.48264°
Longitude
54.89587°
Altitude
49,328.861 km
Speed
3.298 km/s
True Right ascension
17h 53m 20s
True Declination
-24° 27' 58"
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
02:45:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
170,602.277 km
Perigee altitude
48,562.407 km
Semi-major axis
115,960.479 km
Eccentricity
0.52621
Inclination
33.7681°
RAAN
45.3484°
Arg. of periapsis
227.7809°
True anomaly
3.66904°
Mean anomaly
0.969°
Eccentric anomaly
2.04474°
Mean motion
0.05496 °/min
Orbital period
6,549.74 mins
BSTAR
0
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Other satellites on launch #39 in the year 1963 (1963-10-17 UTC)

Documentation

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