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: 1 day ago
TLE from 1 day ago
0 SATELIOT_3
1 60552U 24149CN 26311.92194642 .00001705 00000-0 14736-3 0 9995
2 60552 97.6713 26.2982 0004612 335.5354 24.5649 14.98525663121602Epoch: 2026-11-07T22:07Z
TLE epoch observation values (Epoch: 2026-11-07T22:07:36.170Z)
Latitude
-0.00005°
Longitude
7.27724°
Altitude
571.589 km
Speed
7.577 km/s
True Right ascension
01h 45m 11s
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
23:36:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.661 km
Perigee altitude
565.253 km
Semi-major axis
6,946.594 km
Eccentricity
0.00046
Inclination
97.6713°
RAAN
26.2982°
Arg. of periapsis
335.5354°
True anomaly
24.58688°
Mean anomaly
24.5649°
Eccentric anomaly
24.57589°
Mean motion
3.74874 °/min
Orbital period
96.03 mins
BSTAR
0.00014736
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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 | 2026-11-09 04:42:26.005Z | 140.752° SSE | 2026-11-09 04:45:26.005Z | 79.846° E | 42.89° | 2026-11-09 04:49:26.005Z | 1.685° NNE |
| 6 mins | 2026-11-09 17:58:26.005Z | 14.094° NNE | 2026-11-09 18:01:26.005Z | 178.139° S | 73.805° | 2026-11-09 18:04:26.005Z | 191.535° SSW |
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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