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: 20 hours ago

TLE from 20 hours ago
0 VANGUARD R/B
1 00012U 59001B   26061.46412065  .00000644  00000-0  35242-3 0  9994
2 00012  32.9082 241.3617 1647324 259.9593  81.1890 11.48553360519055
Epoch: 2026-03-02T11:08Z
TLE epoch observation values (Epoch: 2026-03-02T11:08:20.024Z)
Latitude
0.00002°
Longitude
-85.97887°
Altitude
1,933.544 km
Speed
6.922 km/s
True Right ascension
16h 05m 26s
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
10:44:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,290.282 km
Perigee altitude
555.402 km
Semi-major axis
8,300.979 km
Eccentricity
0.16473
Inclination
32.9082°
RAAN
241.3617°
Arg. of periapsis
259.9593°
True anomaly
100.09947°
Mean anomaly
81.189°
Eccentric anomaly
90.62691°
Mean motion
2.86978 °/min
Orbital period
125.44 mins
BSTAR
0.00035242
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Other satellites on launch #1 in the year 1959 (1959-02-17 UTC)

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