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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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: 14 hours ago
TLE from 14 hours ago
0 SATELIOT_4
1 60537U 24149BX 26260.42452323 .00001954 00000-0 17509-3 0 9996
2 60537 97.6667 333.1414 0003744 89.9730 270.1920 14.96934565113779Epoch: 2026-09-17T10:11Z
TLE epoch observation values (Epoch: 2026-09-17T10:11:18.807Z)
Latitude
-0.00009°
Longitude
-176.04891°
Altitude
579.418 km
Speed
7.571 km/s
True Right ascension
22h 12m 33s
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
16:56:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.985 km
Perigee altitude
570.78 km
Semi-major axis
6,951.519 km
Eccentricity
0.00037
Inclination
97.6667°
RAAN
333.1414°
Arg. of periapsis
89.973°
True anomaly
270.1491°
Mean anomaly
270.192°
Eccentric anomaly
270.17055°
Mean motion
3.74476 °/min
Orbital period
96.13 mins
BSTAR
0.00017509
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-18 03:59:21.339Z | 107.26° ESE | 2026-09-18 04:01:21.339Z | 75.969° E | 18.187° | 2026-09-18 04:04:21.339Z | 26.144° NE |
| 6 mins | 2026-09-18 05:34:21.339Z | 207.853° SW | 2026-09-18 05:36:21.339Z | 248.36° W | 32.478° | 2026-09-18 05:40:21.339Z | 327.197° NNW |
| 6 mins | 2026-09-18 17:15:21.339Z | 42.786° NE | 2026-09-18 17:17:21.339Z | 82.92° E | 32.046° | 2026-09-18 17:21:21.339Z | 161.383° S |
| 4 mins | 2026-09-18 18:51:21.339Z | 319.381° NNW | 2026-09-18 18:52:21.339Z | 301.69° NW | 18.413° | 2026-09-18 18:55:21.339Z | 251.397° W |
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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