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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.

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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: 6 hours ago

TLE from 6 hours ago
0 SATELIOT_1
1 60550U 24149CL  25289.59365879  .00003020  00000-0  26981-3 0  9998
2 60550  97.7001   4.4555 0006945 162.1674 197.9792 14.96644542 63611
Epoch: 2025-10-16T14:14Z
TLE epoch observation values (Epoch: 2025-10-16T14:14:52.119Z)
Latitude
-0.00008°
Longitude
125.3872°
Altitude
584.919 km
Speed
7.565 km/s
True Right ascension
00h 17m 49s
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
14:42:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.111 km
Perigee altitude
569.454 km
Semi-major axis
6,952.42 km
Eccentricity
0.00069
Inclination
97.7001°
RAAN
4.4555°
Arg. of periapsis
162.1674°
True anomaly
197.95465°
Mean anomaly
197.9792°
Eccentric anomaly
197.96693°
Mean motion
3.74403 °/min
Orbital period
96.15 mins
BSTAR
0.00026981
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