SATELIOT_4, 60537
Orbit data source: Space-Track
SATELIOT_4, 60537 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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60537 intel report (Beta)
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Edit Public Description
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: 6 hours ago
TLE from 6 hours ago
0 SATELIOT_4
1 60537U 24149BX 25289.58531603 .00002683 00000-0 24848-3 0 9996
2 60537 97.7002 3.5567 0003216 114.5705 245.5851 14.95331978 63558Epoch: 2025-10-16T14:02Z
TLE epoch observation values (Epoch: 2025-10-16T14:02:51.304Z)
Latitude
-0.00008°
Longitude
127.50002°
Altitude
585.317 km
Speed
7.567 km/s
True Right ascension
00h 14m 13s
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
14:42:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.591 km
Perigee altitude
576.117 km
Semi-major axis
6,956.491 km
Eccentricity
0.00032
Inclination
97.7002°
RAAN
3.5567°
Arg. of periapsis
114.5705°
True anomaly
245.55155°
Mean anomaly
245.5851°
Eccentric anomaly
245.56832°
Mean motion
3.74074 °/min
Orbital period
96.24 mins
BSTAR
0.00024848
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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_4 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 | 2025-10-17 04:38:08.990Z | 139.723° SSE | 2025-10-17 04:41:08.990Z | 75.374° E | 34.279° | 2025-10-17 04:44:08.990Z | 6.879° NNE |
| 6 mins | 2025-10-17 17:56:08.990Z | 13.631° NNE | 2025-10-17 17:58:08.990Z | 29.292° NE | 44.766° | 2025-10-17 18:02:08.990Z | 192.654° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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