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: 5 hours ago

TLE from 5 hours ago
0 VANGUARD R/B
1 00016U 58002A   26101.26253796  .00000067  00000-0  74812-4 0  9991
2 00016  34.2621 138.5496 2019010 197.9472 153.8216 10.49583607681885
Epoch: 2026-04-11T06:18Z
TLE epoch observation values (Epoch: 2026-04-11T06:18:03.279Z)
Latitude
-0.00001°
Longitude
-155.44845°
Altitude
4,083.243 km
Speed
5.567 km/s
True Right ascension
09h 14m 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
17:29:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,215.953 km
Perigee altitude
656.663 km
Semi-major axis
8,814.445 km
Eccentricity
0.2019
Inclination
34.2621°
RAAN
138.5496°
Arg. of periapsis
197.9472°
True anomaly
162.10637°
Mean anomaly
153.8216°
Eccentric anomaly
158.13061°
Mean motion
2.62271 °/min
Orbital period
137.26 mins
BSTAR
0.000074812
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Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)

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