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  26127.21285950  .00002376  00000-0  20668-3 0  9999
2 60550  97.6738 203.7961 0006373 199.3570 160.7411 14.97894360 93934
Epoch: 2026-05-07T05:06Z
TLE epoch observation values (Epoch: 2026-05-07T05:06:31.060Z)
Latitude
-0.00007°
Longitude
-97.89554°
Altitude
580.639 km
Speed
7.568 km/s
True Right ascension
13h 35m 11s
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
00:28:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.839 km
Perigee altitude
565.982 km
Semi-major axis
6,948.547 km
Eccentricity
0.00064
Inclination
97.6738°
RAAN
203.7961°
Arg. of periapsis
199.357°
True anomaly
160.76517°
Mean anomaly
160.7411°
Eccentric anomaly
160.75314°
Mean motion
3.74716 °/min
Orbital period
96.07 mins
BSTAR
0.00020668
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
|