SATELIOT_1, 60550
Orbit data source: Space-Track
SATELIOT_1, 60550 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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60550 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_1
1 60550U 24149CL 26173.63724485 .00001749 00000-0 15265-3 0 9997
2 60550 97.6760 249.4448 0008299 64.4468 295.7611 14.98091637100884Epoch: 2026-06-22T15:17Z
TLE epoch observation values (Epoch: 2026-06-22T15:17:37.955Z)
Latitude
-0.00005°
Longitude
109.21636°
Altitude
573.342 km
Speed
7.576 km/s
True Right ascension
16h 37m 46s
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
10:52:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.566 km
Perigee altitude
564.034 km
Semi-major axis
6,947.937 km
Eccentricity
0.00083
Inclination
97.676°
RAAN
249.4448°
Arg. of periapsis
64.4468°
True anomaly
295.67541°
Mean anomaly
295.7611°
Eccentric anomaly
295.71826°
Mean motion
3.74765 °/min
Orbital period
96.06 mins
BSTAR
0.00015265
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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_1 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 | 2026-06-24 04:18:59.238Z | 113.462° SE | 2026-06-24 04:20:59.238Z | 75.901° E | 22.171° | 2026-06-24 04:23:59.238Z | 19.955° NNE |
| 4 mins | 2026-06-24 05:54:59.238Z | 234.576° WSW | 2026-06-24 05:55:59.238Z | 255.925° W | 21.834° | 2026-06-24 05:58:59.238Z | 313.189° NW |
| 6 mins | 2026-06-24 17:33:59.238Z | 32.173° NE | 2026-06-24 17:36:59.238Z | 110.795° ESE | 34.887° | 2026-06-24 17:39:59.238Z | 169.423° 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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