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 (1 year 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: 17 hours ago

TLE from 17 hours ago
0 SATELIOT_1
1 60550U 24149CL  25338.66079941  .00005291  00000-0  46417-3 0  9991
2 60550  97.6960  52.7487 0006958  15.8772 344.2666 14.97026061 70954
Epoch: 2025-12-04T15:51Z
TLE epoch observation values (Epoch: 2025-12-04T15:51:33.069Z)
Latitude
-0.00006°
Longitude
101.14687°
Altitude
574.484 km
Speed
7.576 km/s
True Right ascension
03h 30m 59s
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
07:18:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.937 km
Perigee altitude
568.264 km
Semi-major axis
6,951.237 km
Eccentricity
0.0007
Inclination
97.696°
RAAN
52.7487°
Arg. of periapsis
15.8772°
True anomaly
344.24496°
Mean anomaly
344.2666°
Eccentric anomaly
344.25578°
Mean motion
3.74498 °/min
Orbital period
96.13 mins
BSTAR
0.00046417
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
|