VANGUARD R/B, 16

Orbit data source: Space-Track

VANGUARD R/B, 16 is space debris in LEO originally from a launch on Mon, 17 Mar 1958 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
16, 1958-002A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
GCR/Redlands
Mission
Spacecraft
Bus & Motor
33-KS-2800, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
1958-03-17 (68 years ago)
Launch vehicle
Unknown
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: 10 hours ago

TLE from 10 hours ago
0 VANGUARD R/B
1    16U 58002A   26111.63243060  .00000091  00000-0  98075-4 0  9990
2    16  34.2714 108.5664 2019353 241.7385  96.5036 10.49585498682977
Epoch: 2026-04-21T15:10Z
TLE epoch observation values (Epoch: 2026-04-21T15:10:42.003Z)
Latitude
-0°
Longitude
31.18596°
Altitude
2,968.462 km
Speed
6.331 km/s
True Right ascension
07h 14m 15s
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
08:29:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,216.242 km
Perigee altitude
656.351 km
Semi-major axis
8,814.433 km
Eccentricity
0.20194
Inclination
34.2714°
RAAN
108.5664°
Arg. of periapsis
241.7385°
True anomaly
118.31877°
Mean anomaly
96.5036°
Eccentric anomaly
107.53596°
Mean motion
2.62272 °/min
Orbital period
137.26 mins
BSTAR
0.000098075
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Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)

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