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: 12 hours ago

TLE from 12 hours ago
0 VANGUARD R/B
1 00016U 58002A   26035.11580513  .00000032  00000-0  19925-4 0  9997
2 00016  34.2814 329.8451 2022467 278.5942  59.2012 10.49576543674935
Epoch: 2026-02-04T02:46Z
TLE epoch observation values (Epoch: 2026-02-04T02:46:45.563Z)
Latitude
0.00001°
Longitude
153.86826°
Altitude
1,826.016 km
Speed
7.208 km/s
True Right ascension
21h 59m 22s
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
16:54:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,219.046 km
Perigee altitude
653.646 km
Semi-major axis
8,814.483 km
Eccentricity
0.20225
Inclination
34.2814°
RAAN
329.8451°
Arg. of periapsis
278.5942°
True anomaly
81.46575°
Mean anomaly
59.2012°
Eccentric anomaly
70.09694°
Mean motion
2.6227 °/min
Orbital period
137.26 mins
BSTAR
0.000019925
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Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)

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