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: 9 hours ago

TLE from 9 hours ago
0 SATELIOT_1
1 60550U 24149CL  26087.19604316  .00002007  00000-0  17624-3 0  9991
2 60550  97.6775 164.4526 0006334 355.1872   4.9288 14.97691299 87940
Epoch: 2026-03-28T04:42Z
TLE epoch observation values (Epoch: 2026-03-28T04:42:18.129Z)
Latitude
-0.00002°
Longitude
-91.7427°
Altitude
572.696 km
Speed
7.577 km/s
True Right ascension
10h 57m 48s
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
19:22:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.441 km
Perigee altitude
566.637 km
Semi-major axis
6,949.176 km
Eccentricity
0.00063
Inclination
97.6775°
RAAN
164.4526°
Arg. of periapsis
355.1872°
True anomaly
4.93504°
Mean anomaly
4.9288°
Eccentric anomaly
4.93192°
Mean motion
3.74665 °/min
Orbital period
96.09 mins
BSTAR
0.00017624
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
|