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VANGUARD 1, 5

Orbit data source: Space-Track

VANGUARD 1, 5 is a payload satellite owned by NRL (US) in LEO that was launched on Mon, 17 Mar 1958 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
5, 1958-002B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
NRL 6", Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
1958-03-17 (68 years ago)
Launch vehicle
VANGUARD
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: 1 day ago

TLE from 1 day ago
0 VANGUARD 1
1 00005U 58002B   26201.29754256  .00000153  00000-0  17727-3 0  9997
2 00005  34.2522 212.1525 1837022 287.7762  53.1395 10.86017563446888
Epoch: 2026-07-20T07:08Z
TLE epoch observation values (Epoch: 2026-07-20T07:08:27.677Z)
Latitude
-0.00001°
Longitude
166.95355°
Altitude
1,503.225 km
Speed
7.41 km/s
True Right ascension
14h 08m 36s
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
20:12:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,820.977 km
Perigee altitude
655.317 km
Semi-major axis
8,616.284 km
Eccentricity
0.1837
Inclination
34.2522°
RAAN
212.1525°
Arg. of periapsis
287.7762°
True anomaly
72.28434°
Mean anomaly
53.1395°
Eccentric anomaly
62.47335°
Mean motion
2.71371 °/min
Orbital period
132.66 mins
BSTAR
0.00017727
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Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)

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