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VZLUSAT-2, 51085

Orbit data source: Space-Track

VZLUSAT-2, 51085 is a payload satellite owned by VZLU (CZ) in LEO that was launched on Thu, 13 Jan 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Not visible in the next 10 days
Identifier
51085, 2022-002DF
Orbit
LEO
Country
Flag of CZCZ / CZE
Related business
Manufacturer
VZLU
Mission
Operational Civil EO-Sci/Ast
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
2022-01-13 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 weeks ago

TLE from 2 weeks ago
0 VZLUSAT-2
1 51085U 22002DF  25333.89742664  .08514901  24879-5  47783-3 0  9992
2 51085  97.2881  55.3308 0009599 266.9747  93.0455 16.41514709216501
Epoch: 2025-11-29T21:32Z
TLE epoch observation values (Epoch: 2025-11-29T21:32:17.661Z)
Latitude
-0.00006°
Longitude
23.23818°
Altitude
165.373 km
Speed
7.807 km/s
True Right ascension
03h 41m 19s
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
12:55:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
164.851 km
Perigee altitude
152.302 km
Semi-major axis
6,536.714 km
Eccentricity
0.00096
Inclination
97.2881°
RAAN
55.3308°
Arg. of periapsis
266.9747°
True anomaly
93.15533°
Mean anomaly
93.0455°
Eccentric anomaly
93.10042°
Mean motion
4.1068 °/min
Orbital period
87.66 mins
BSTAR
0.00047783
Loading maneuver chart data...
Computing Atmospheric mass density...

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