DECAYED
Showing default

BDSAT-2, 55098 (Decayed)

Orbit data source: Space-Track

BDSAT-2, 55098 was a Czech payload satellite in LEO that was launched on Tue, 03 Jan 2023 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
55098, 2023-001CT
Orbit
Decayed
Country
Flag of CZCZ / CZE
Related business
Flag of CZCentral European Institute of Technology (CZ)
Manufacturer
CEITEC
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1.172 kg wet, 1.172 kg dry
Launch date (UTC)
2023-01-03 (3 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
0.015 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 8 months ago

TLE from 8 months ago
0 BDSAT-2
1 55098U 23001CT  25043.17195676  .04841583  24403-5  13946-2 0  9995
2 55098  97.3601 120.6613 0008975 287.7661  72.2652 16.27416800118122
Epoch: 2025-02-12T04:07Z
TLE epoch observation values (Epoch: 2025-02-12T04:07:37.064Z)
Latitude
-0.00001°
Longitude
-83.70938°
Altitude
200.933 km
Speed
7.787 km/s
True Right ascension
08h 02m 38s
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
23:23:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
202.214 km
Perigee altitude
190.413 km
Semi-major axis
6,574.45 km
Eccentricity
0.0009
Inclination
97.3601°
RAAN
120.6613°
Arg. of periapsis
287.7661°
True anomaly
72.36319°
Mean anomaly
72.2652°
Eccentric anomaly
72.31419°
Mean motion
4.0715 °/min
Orbital period
88.42 mins
BSTAR
0.0013946
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|