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: 5 hours ago
TLE from 5 hours ago
0 SATELIOT_4
1 60537U 24149BX 26035.16905112 .00002819 00000-0 25584-3 0 9999
2 60537 97.6868 112.1579 0003579 107.6721 252.4891 14.96085368 80088Epoch: 2026-02-04T04:03Z
TLE epoch observation values (Epoch: 2026-02-04T04:03:26.016Z)
Latitude
-0.00007°
Longitude
-83.03998°
Altitude
582.806 km
Speed
7.569 km/s
True Right ascension
07h 28m 37s
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
10:42:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.505 km
Perigee altitude
573.527 km
Semi-major axis
6,954.153 km
Eccentricity
0.00036
Inclination
97.6868°
RAAN
112.1579°
Arg. of periapsis
107.6721°
True anomaly
252.44999°
Mean anomaly
252.4891°
Eccentric anomaly
252.46955°
Mean motion
3.74263 °/min
Orbital period
96.19 mins
BSTAR
0.00025584
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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
Loading observer location...
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 | 2026-02-04 17:28:07.183Z | 29.282° NE | 2026-02-04 17:31:07.183Z | 83.239° E | 33.451° | 2026-02-04 17:35:07.183Z | 169.748° S |
| 4 mins | 2026-02-05 04:18:07.183Z | 101.528° ESE | 2026-02-05 04:19:07.183Z | 80.002° E | 22.999° | 2026-02-05 04:22:07.183Z | 20.96° NNE |
| 4 mins | 2026-02-05 05:53:07.183Z | 230.707° WSW | 2026-02-05 05:55:07.183Z | 272.848° WNW | 21.398° | 2026-02-05 05:57:07.183Z | 308.874° NW |
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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