Showing default

SATELIOT_1, 60550

Orbit data source: Space-Track

SATELIOT_1, 60550 is a payload satellite owned by Sateliot (ES) in SSO that was launched on Fri, 16 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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.

Loading next visibility...
Identifier
60550, 2024-149CL
Orbit
SSO
Country
Flag of ESES / SPN
Related business
Manufacturer
Endurosat
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
7.407 kg wet, 7.407 kg dry
Launch date (UTC)
2024-08-16 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.092 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 SATELIOT_1
1 60550U 24149CL  26219.78886545  .00000438  00000-0  41767-4 0  9991
2 60550  97.6721 294.8279 0005251 261.7468  98.3159 14.98244050107794
Epoch: 2026-08-07T18:55Z
TLE epoch observation values (Epoch: 2026-08-07T18:55:57.974Z)
Latitude
-0.00006°
Longitude
54.52682°
Altitude
575.905 km
Speed
7.572 km/s
True Right ascension
19h 39m 18s
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
19:35:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.976 km
Perigee altitude
565.68 km
Semi-major axis
6,947.465 km
Eccentricity
0.00053
Inclination
97.6721°
RAAN
294.8279°
Arg. of periapsis
261.7468°
True anomaly
98.37543°
Mean anomaly
98.3159°
Eccentric anomaly
98.34567°
Mean motion
3.74803 °/min
Orbital period
96.05 mins
BSTAR
0.000041767
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
|