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: 6 hours ago
TLE from 6 hours ago
0 SATELIOT_3
1 60552U 24149CN 25289.57287232 .00004371 00000-0 38739-3 0 9998
2 60552 97.7079 4.9971 0005818 167.3694 192.7675 14.96731013 63626Epoch: 2025-10-16T13:44Z
TLE epoch observation values (Epoch: 2025-10-16T13:44:56.168Z)
Latitude
0.00003°
Longitude
133.4324°
Altitude
584.002 km
Speed
7.566 km/s
True Right ascension
00h 19m 59s
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
14:42:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.06 km
Perigee altitude
569.97 km
Semi-major axis
6,952.152 km
Eccentricity
0.00058
Inclination
97.7079°
RAAN
4.9971°
Arg. of periapsis
167.3694°
True anomaly
192.75278°
Mean anomaly
192.7675°
Eccentric anomaly
192.76014°
Mean motion
3.74425 °/min
Orbital period
96.15 mins
BSTAR
0.00038739
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-17 04:20:09.052Z | 116.88° SE | 2025-10-17 04:23:09.052Z | 62.704° ENE | 21.464° | 2025-10-17 04:25:09.052Z | 26.271° NE |
| 5 mins | 2025-10-17 05:56:09.052Z | 224.194° SW | 2025-10-17 05:58:09.052Z | 267.428° W | 23.591° | 2025-10-17 06:01:09.052Z | 319.077° NNW |
| 5 mins | 2025-10-17 17:37:09.052Z | 42.586° NE | 2025-10-17 17:39:09.052Z | 102.035° ESE | 34.002° | 2025-10-17 17:42:09.052Z | 166.487° S |
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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