DECAYED
Showing default

KSF3-B, 55019 (Decayed)

Orbit data source: Space-Track

KSF3-B, 55019 was a payload satellite owned by Kleos Space (LU) 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
55019, 2023-001L
Orbit
Decayed
Country
Flag of UnknownUnknown / LUXE
Related business
Manufacturer
ISIS BV
Mission
Decayed Commercial Sigint
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 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
0.080 m², Medium (>0.1 m² and < 1m²)

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

TLE from 2 months ago
0 KSF3-B
1 55019U 23001L   25341.61621245  .12892631  24942-5  46037-3 0  9999
2 55019  97.3197  60.0279 0011713 286.9588  73.0429 16.43288850163977
Epoch: 2025-12-07T14:47Z
TLE epoch observation values (Epoch: 2025-12-07T14:47:20.755Z)
Latitude
-0.00006°
Longitude
121.56439°
Altitude
158.101 km
Speed
7.813 km/s
True Right ascension
04h 00m 06s
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
13:32:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
161.519 km
Perigee altitude
146.217 km
Semi-major axis
6,532.005 km
Eccentricity
0.00117
Inclination
97.3197°
RAAN
60.0279°
Arg. of periapsis
286.9588°
True anomaly
73.17134°
Mean anomaly
73.0429°
Eccentric anomaly
73.10711°
Mean motion
4.11125 °/min
Orbital period
87.56 mins
BSTAR
0.00046037
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|