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 (69 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.1 m
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 00016U 58002A   26305.20639632  .00000307  00000-0  43378-3 0  9997
2 00016  34.2662 268.9544 2017860 339.1111  13.7295 10.49646508703317
Epoch: 2026-11-01T04:57Z
TLE epoch observation values (Epoch: 2026-11-01T04:57:12.642Z)
Latitude
0.00002°
Longitude
154.15067°
Altitude
733.468 km
Speed
8.179 km/s
True Right ascension
17h 55m 49s
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
11:00:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,214.516 km
Perigee altitude
657.395 km
Semi-major axis
8,814.092 km
Eccentricity
0.20179
Inclination
34.2662°
RAAN
268.9544°
Arg. of periapsis
339.1111°
True anomaly
20.94794°
Mean anomaly
13.7295°
Eccentric anomaly
17.13598°
Mean motion
2.62287 °/min
Orbital period
137.25 mins
BSTAR
0.00043378
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Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)

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