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: 2 days ago

TLE from 2 days ago
0 VANGUARD R/B
1 00016U 58002A   25285.44442524 -.00000019  00000-0 -24316-4 0  9995
2 00016  34.2644 301.4946 2023945 154.3873 217.2692 10.49570126662889
Epoch: 2025-10-12T10:39Z
TLE epoch observation values (Epoch: 2025-10-12T10:39:58.340Z)
Latitude
-0.00003°
Longitude
120.24001°
Altitude
3,957.112 km
Speed
5.65 km/s
True Right ascension
20h 05m 58s
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
22:13:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,220.395 km
Perigee altitude
652.373 km
Semi-major axis
8,814.521 km
Eccentricity
0.20239
Inclination
34.2644°
RAAN
301.4946°
Arg. of periapsis
154.3873°
True anomaly
205.6667°
Mean anomaly
217.2692°
Eccentric anomaly
211.25283°
Mean motion
2.62268 °/min
Orbital period
137.26 mins
BSTAR
-0.000024316
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Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)

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