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: 19 hours ago

TLE from 19 hours ago
0 VANGUARD 1
1 00005U 58002B   26067.66433402  .00000224  00000-0  31278-3 0  9991
2 00005  34.2419 264.5468 1837399  45.2139 328.3992 10.85956128432357
Epoch: 2026-03-08T15:56Z
TLE epoch observation values (Epoch: 2026-03-08T15:56:38.459Z)
Latitude
-0.00002°
Longitude
-140.98185°
Altitude
989.199 km
Speed
7.872 km/s
True Right ascension
17h 38m 11s
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
15:07:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,821.688 km
Perigee altitude
655.258 km
Semi-major axis
8,616.61 km
Eccentricity
0.18374
Inclination
34.2419°
RAAN
264.5468°
Arg. of periapsis
45.2139°
True anomaly
314.8465°
Mean anomaly
328.3992°
Eccentric anomaly
321.90391°
Mean motion
2.71355 °/min
Orbital period
132.67 mins
BSTAR
0.00031278
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
|