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VANGUARD 3, 20

Orbit data source: Space-Track

VANGUARD 3, 20 is a payload satellite owned by GSFC (US) in LEO that was launched on Fri, 18 Sep 1959 UTC via a VANGUARD 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
20, 1959-007A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NRL
Mission
Civil Science
Bus & Motor
NRL 20", Unknown motor
Mass
47 kg wet, 23 kg dry
Launch date (UTC)
1959-09-18 (66 years ago)
Launch vehicle
VANGUARD
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Sphere + Cyl, 1.3 m
Radar Cross Section
1.104 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 VANGUARD 3
1 00020U 59007A   25245.58991874  .00004503  00000-0  18195-2 0  9990
2 00020  33.3477 221.9252 1640593 312.4297  34.8463 11.60936777451162
Epoch: 2025-09-02T14:09Z
TLE epoch observation values (Epoch: 2025-09-02T14:09:28.979Z)
Latitude
Longitude
27.57548°
Altitude
839.939 km
Speed
7.88 km/s
True Right ascension
14h 47m 42s
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
23:37:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,215.84 km
Perigee altitude
511.543 km
Semi-major axis
8,241.828 km
Eccentricity
0.16406
Inclination
33.3477°
RAAN
221.9252°
Arg. of periapsis
312.4297°
True anomaly
47.63129°
Mean anomaly
34.8463°
Eccentric anomaly
41.01506°
Mean motion
2.90073 °/min
Orbital period
124.11 mins
BSTAR
0.0018195
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Other satellites on launch #7 in the year 1959 (1959-09-18 UTC)

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