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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
Civil Technology
Bus & Motor
NRL 6", Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
1958-03-17 (67 years ago)
Launch vehicle
VANGUARD
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Sphere, 0.1 m
Radar Cross Section
0.020 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 VANGUARD 1
1 00005U 58002B   25239.40453637  .00000003  00000-0 -21059-4 0  9998
2 00005  34.2562 141.0512 1842667 253.9336  85.1474 10.85924434411340
Epoch: 2025-08-27T09:42Z
TLE epoch observation values (Epoch: 2025-08-27T09:42:31.942Z)
Latitude
0.00004°
Longitude
19.5358°
Altitude
2,391.106 km
Speed
6.683 km/s
True Right ascension
09h 24m 12s
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
10:59:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,826.425 km
Perigee altitude
650.855 km
Semi-major axis
8,616.777 km
Eccentricity
0.18427
Inclination
34.2562°
RAAN
141.0512°
Arg. of periapsis
253.9336°
True anomaly
106.12544°
Mean anomaly
85.1474°
Eccentric anomaly
95.65375°
Mean motion
2.71348 °/min
Orbital period
132.67 mins
BSTAR
-0.000021059
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Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)

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