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: 15 hours ago
TLE from 15 hours ago
0 SATELIOT_1
1 60550U 24149CL 26264.73432925 .00000863 00000-0 77229-4 0 9999
2 60550 97.6664 339.0065 0007330 109.5979 250.6036 14.98359745114525Epoch: 2026-09-21T17:37Z
TLE epoch observation values (Epoch: 2026-09-21T17:37:26.047Z)
Latitude
0.00004°
Longitude
74.03806°
Altitude
576.713 km
Speed
7.571 km/s
True Right ascension
22h 36m 01s
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
02:00:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.062 km
Perigee altitude
563.878 km
Semi-major axis
6,947.107 km
Eccentricity
0.00073
Inclination
97.6664°
RAAN
339.0065°
Arg. of periapsis
109.5979°
True anomaly
250.5244°
Mean anomaly
250.6036°
Eccentric anomaly
250.564°
Mean motion
3.74832 °/min
Orbital period
96.04 mins
BSTAR
0.000077229
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-22 18:14:25.541Z | 356.685° N | 2026-09-22 18:17:25.541Z | 256.668° W | 51.233° | 2026-09-22 18:20:25.541Z | 209.681° SW |
| 6 mins | 2026-09-23 05:01:25.541Z | 160.801° S | 2026-09-23 05:03:25.541Z | 137.726° SSE | 69.437° | 2026-09-23 05:07:25.541Z | 350.559° N |
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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