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: 8 hours ago
TLE from 8 hours ago
0 SATELIOT_3
1 60552U 24149CN 26084.43228682 .00003102 00000-0 26969-3 0 9994
2 60552 97.6862 162.4477 0005307 27.2856 332.8645 14.97689955 87542Epoch: 2026-03-25T10:22Z
TLE epoch observation values (Epoch: 2026-03-25T10:22:29.581Z)
Latitude
0.00008°
Longitude
-176.07124°
Altitude
573.804 km
Speed
7.576 km/s
True Right ascension
10h 49m 47s
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
23:33:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.732 km
Perigee altitude
567.356 km
Semi-major axis
6,949.181 km
Eccentricity
0.00053
Inclination
97.6862°
RAAN
162.4477°
Arg. of periapsis
27.2856°
True anomaly
332.83675°
Mean anomaly
332.8645°
Eccentric anomaly
332.85062°
Mean motion
3.74665 °/min
Orbital period
96.09 mins
BSTAR
0.00026969
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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 | 2026-03-25 18:57:56.529Z | 328.531° NNW | 2026-03-25 18:59:56.529Z | 292.08° WNW | 19.319° | 2026-03-25 19:02:56.529Z | 243.952° WSW |
| 4 mins | 2026-03-26 04:10:56.529Z | 94.627° ESE | 2026-03-26 04:12:56.529Z | 57.933° ENE | 16.942° | 2026-03-26 04:14:56.529Z | 26.954° NE |
| 6 mins | 2026-03-26 05:44:56.529Z | 207.185° SW | 2026-03-26 05:46:56.529Z | 247.43° WSW | 28.133° | 2026-03-26 05:50:56.529Z | 327.246° NNW |
| 5 mins | 2026-03-26 17:25:56.529Z | 48.086° ENE | 2026-03-26 17:27:56.529Z | 94.372° ESE | 27.878° | 2026-03-26 17:30:56.529Z | 155.55° SSE |
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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