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: 12 hours ago
TLE from 12 hours ago
0 SATELIOT_1
1 60550U 24149CL 26219.78886545 .00000438 00000-0 41767-4 0 9991
2 60550 97.6721 294.8279 0005251 261.7468 98.3159 14.98244050107794Epoch: 2026-08-07T18:55Z
TLE epoch observation values (Epoch: 2026-08-07T18:55:57.974Z)
Latitude
-0.00006°
Longitude
54.52682°
Altitude
575.905 km
Speed
7.572 km/s
True Right ascension
19h 39m 18s
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
20:36:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.976 km
Perigee altitude
565.68 km
Semi-major axis
6,947.465 km
Eccentricity
0.00053
Inclination
97.6721°
RAAN
294.8279°
Arg. of periapsis
261.7468°
True anomaly
98.37543°
Mean anomaly
98.3159°
Eccentric anomaly
98.34567°
Mean motion
3.74803 °/min
Orbital period
96.05 mins
BSTAR
0.000041767
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-08 17:56:19.627Z | 12.75° NNE | 2026-08-08 17:59:19.627Z | 17.95° NNE | 43.824° | 2026-08-08 18:03:19.627Z | 192.787° SSW |
| 6 mins | 2026-08-09 04:44:19.627Z | 137.941° SSE | 2026-08-09 04:46:19.627Z | 88.757° E | 36.122° | 2026-08-09 04:50:19.627Z | 0.389° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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