SATELIOT_3, 60552
Orbit data source: Space-Track
SATELIOT_3, 60552 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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60552 intel report (Beta)
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Identifier
Orbit
Country
ES / SPNRelated 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)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 SATELIOT_3
1 60552U 24149CN 26256.69661531 .00002213 00000-0 19056-3 0 9998
2 60552 97.6764 331.9811 0006551 132.3235 227.8544 14.98350996113338Epoch: 2026-09-13T16:43Z
TLE epoch observation values (Epoch: 2026-09-13T16:43:07.562Z)
Latitude
0°
Longitude
88.51204°
Altitude
578.102 km
Speed
7.57 km/s
True Right ascension
22h 07m 55s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
03:56:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.548 km
Perigee altitude
564.446 km
Semi-major axis
6,947.134 km
Eccentricity
0.00066
Inclination
97.6764°
RAAN
331.9811°
Arg. of periapsis
132.3235°
True anomaly
227.79877°
Mean anomaly
227.8544°
Eccentric anomaly
227.82658°
Mean motion
3.7483 °/min
Orbital period
96.04 mins
BSTAR
0.00019056
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SATELIOT_3 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-14 17:20:27.336Z | 41.961° NE | 2026-09-14 17:23:27.336Z | 102.891° ESE | 28.683° | 2026-09-14 17:26:27.336Z | 155.258° SSE |
| 4 mins | 2026-09-14 18:56:27.336Z | 325.113° NNW | 2026-09-14 18:58:27.336Z | 286.627° WNW | 20.561° | 2026-09-14 19:00:27.336Z | 251.799° W |
| 5 mins | 2026-09-15 05:43:27.336Z | 213.707° SW | 2026-09-15 05:45:27.336Z | 266.009° W | 34.6° | 2026-09-15 05:48:27.336Z | 324.679° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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