Showing default

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.

Loading next visibility...
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
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   26134.89553612  .00000102  00000-0  13755-3 0  9992
2 00005  34.2482  57.0677 1836008 348.3595   7.9502 10.85981134439666
Epoch: 2026-05-14T21:29Z
TLE epoch observation values (Epoch: 2026-05-14T21:29:34.320Z)
Latitude
-0.00005°
Longitude
-137.96002°
Altitude
676.08 km
Speed
8.171 km/s
True Right ascension
03h 48m 16s
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
17:03:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,820.332 km
Perigee altitude
656.348 km
Semi-major axis
8,616.477 km
Eccentricity
0.1836
Inclination
34.2482°
RAAN
57.0677°
Arg. of periapsis
348.3595°
True anomaly
11.70013°
Mean anomaly
7.9502°
Eccentric anomaly
9.72763°
Mean motion
2.71362 °/min
Orbital period
132.66 mins
BSTAR
0.00013755
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)

Documentation

Showing up to 5 results
|