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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Edit Public Description
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: 1 day ago
TLE from 1 day ago
0 SATELIOT_3
1 60552U 24149CN 25338.43796625 .00007016 00000-0 61354-3 0 9997
2 60552 97.7039 53.1374 0006069 35.4793 324.6831 14.97043652 70937Epoch: 2025-12-04T10:30Z
TLE epoch observation values (Epoch: 2025-12-04T10:30:40.283Z)
Latitude
-0.0001°
Longitude
-178.02484°
Altitude
575.644 km
Speed
7.575 km/s
True Right ascension
03h 32m 32s
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
09:18:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.265 km
Perigee altitude
568.827 km
Semi-major axis
6,951.183 km
Eccentricity
0.00061
Inclination
97.7039°
RAAN
53.1374°
Arg. of periapsis
35.4793°
True anomaly
324.64287°
Mean anomaly
324.6831°
Eccentric anomaly
324.66299°
Mean motion
3.74503 °/min
Orbital period
96.13 mins
BSTAR
0.00061354
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-05 17:33:27.309Z | 29.655° NE | 2025-12-05 17:36:27.309Z | 79.452° E | 31.94° | 2025-12-05 17:40:27.309Z | 167.452° S |
| 5 mins | 2025-12-06 04:22:27.309Z | 111.252° ESE | 2025-12-06 04:24:27.309Z | 72.6° E | 22.13° | 2025-12-06 04:27:27.309Z | 18.905° NNE |
| 5 mins | 2025-12-06 05:57:27.309Z | 219.725° SW | 2025-12-06 05:59:27.309Z | 257.501° W | 22.35° | 2025-12-06 06:02:27.309Z | 314.217° NW |
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
Authenticating...
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