VANGUARD R/B, 12

Orbit data source: Space-Track

VANGUARD R/B, 12 is space debris in LEO originally from a launch on Tue, 17 Feb 1959 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
12, 1959-001B
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)
1959-02-17 (67 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: 1 day ago

TLE from 1 day ago
0 VANGUARD R/B
1    12U 59001B   26001.29008782  .00001990  00000-0  11391-2 0  9999
2    12  32.9086  93.4321 1648086 301.3029  43.6395 11.48449649512138
Epoch: 2026-01-01T06:57Z
TLE epoch observation values (Epoch: 2026-01-01T06:57:43.587Z)
Latitude
-0.00003°
Longitude
-111.94634°
Altitude
1,058.208 km
Speed
7.694 km/s
True Right ascension
06h 13m 43s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
06:16:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,291.497 km
Perigee altitude
555.187 km
Semi-major axis
8,301.479 km
Eccentricity
0.16481
Inclination
32.9086°
RAAN
93.4321°
Arg. of periapsis
301.3029°
True anomaly
58.75701°
Mean anomaly
43.6395°
Eccentric anomaly
50.97541°
Mean motion
2.86952 °/min
Orbital period
125.46 mins
BSTAR
0.0011391
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Other satellites on launch #1 in the year 1959 (1959-02-17 UTC)

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