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: 10 hours ago
TLE from 10 hours ago
0 SATELIOT_1
1 60550U 24149CL 26131.95576395 .00002291 00000-0 19929-3 0 9995
2 60550 97.6747 208.4590 0006726 179.8157 180.3069 14.97917651 94645Epoch: 2026-05-11T22:56Z
TLE epoch observation values (Epoch: 2026-05-11T22:56:18.005Z)
Latitude
-0.00001°
Longitude
-5.35308°
Altitude
581.06 km
Speed
7.567 km/s
True Right ascension
13h 53m 50s
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
17:35:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.012 km
Perigee altitude
565.665 km
Semi-major axis
6,948.475 km
Eccentricity
0.00067
Inclination
97.6747°
RAAN
208.459°
Arg. of periapsis
179.8157°
True anomaly
180.30649°
Mean anomaly
180.3069°
Eccentric anomaly
180.30669°
Mean motion
3.74722 °/min
Orbital period
96.07 mins
BSTAR
0.00019929
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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 | 2026-05-12 17:09:47.482Z | 51.409° ENE | 2026-05-12 17:11:47.482Z | 87.647° E | 21.096° | 2026-05-12 17:14:47.482Z | 143.067° SSE |
| 4 mins | 2026-05-12 18:45:47.482Z | 323.029° NNW | 2026-05-12 18:46:47.482Z | 301.585° NW | 22.814° | 2026-05-12 18:49:47.482Z | 241.827° WSW |
| 6 mins | 2026-05-13 05:31:47.482Z | 195.433° SSW | 2026-05-13 05:34:47.482Z | 274.567° WNW | 34.307° | 2026-05-13 05:37:47.482Z | 331.024° 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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