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: 18 hours ago
TLE from 18 hours ago
0 SATELIOT_3
1 60552U 24149CN 26083.96460949 .00003176 00000-0 27604-3 0 9993
2 60552 97.6860 161.9873 0005335 28.5899 331.5614 14.97686771 87473Epoch: 2026-03-24T23:09Z
TLE epoch observation values (Epoch: 2026-03-24T23:09:02.259Z)
Latitude
-0.00013°
Longitude
-7.7068°
Altitude
573.836 km
Speed
7.576 km/s
True Right ascension
10h 47m 56s
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
21:57:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.761 km
Perigee altitude
567.346 km
Semi-major axis
6,949.19 km
Eccentricity
0.00053
Inclination
97.686°
RAAN
161.9873°
Arg. of periapsis
28.5899°
True anomaly
331.53227°
Mean anomaly
331.5614°
Eccentric anomaly
331.54684°
Mean motion
3.74664 °/min
Orbital period
96.09 mins
BSTAR
0.00027604
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-25 17:21:51.487Z | 38.843° NE | 2026-03-25 17:24:51.487Z | 94.404° ESE | 26.185° | 2026-03-25 17:27:51.487Z | 153.018° SSE |
| 4 mins | 2026-03-25 18:58:51.487Z | 313.905° NW | 2026-03-25 18:59:51.487Z | 293.868° NW | 19.306° | 2026-03-25 19:02:51.487Z | 244.777° WSW |
| 4 mins | 2026-03-26 04:10:51.487Z | 95.917° ESE | 2026-03-26 04:12:51.487Z | 59.548° ENE | 17.038° | 2026-03-26 04:14:51.487Z | 27.935° NE |
| 6 mins | 2026-03-26 05:44:51.487Z | 206.257° SW | 2026-03-26 05:47:51.487Z | 276.975° WNW | 28.199° | 2026-03-26 05:50:51.487Z | 326.661° NNW |
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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