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: 6 hours ago
TLE from 6 hours ago
0 SATELIOT_3
1 60552U 24149CN 26219.76494256 .00001855 00000-0 16099-3 0 9998
2 60552 97.6805 295.6422 0002819 265.6144 94.4757 14.98245974107808Epoch: 2026-08-07T18:21Z
TLE epoch observation values (Epoch: 2026-08-07T18:21:31.037Z)
Latitude
0.00005°
Longitude
63.97692°
Altitude
575.522 km
Speed
7.573 km/s
True Right ascension
19h 42m 34s
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
14:36:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.281 km
Perigee altitude
567.364 km
Semi-major axis
6,947.46 km
Eccentricity
0.00028
Inclination
97.6805°
RAAN
295.6422°
Arg. of periapsis
265.6144°
True anomaly
94.5079°
Mean anomaly
94.4757°
Eccentric anomaly
94.4918°
Mean motion
3.74804 °/min
Orbital period
96.05 mins
BSTAR
0.00016099
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-08 04:08:24.325Z | 98.901° ESE | 2026-08-08 04:10:24.325Z | 64.477° ENE | 16.791° | 2026-08-08 04:12:24.325Z | 31.579° NE |
| 5 mins | 2026-08-08 05:43:24.325Z | 215.404° SW | 2026-08-08 05:45:24.325Z | 270.445° WNW | 29.585° | 2026-08-08 05:48:24.325Z | 325.897° NNW |
| 5 mins | 2026-08-08 17:23:24.325Z | 48.263° ENE | 2026-08-08 17:25:24.325Z | 92.442° ESE | 26.842° | 2026-08-08 17:28:24.325Z | 153.553° SSE |
| 4 mins | 2026-08-08 18:59:24.325Z | 313.992° NW | 2026-08-08 19:00:24.325Z | 294.418° NW | 18.693° | 2026-08-08 19:03:24.325Z | 245.834° WSW |
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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