SATELIOT_2, 60534
Orbit data source: Space-Track
SATELIOT_2, 60534 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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60534 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: 9 hours ago
TLE from 9 hours ago
0 SATELIOT_2
1 60534U 24149BU 26133.45270543 .00000571 00000-0 55614-4 0 9991
2 60534 97.6833 209.0446 0001340 109.4874 250.6492 14.96227877 94770Epoch: 2026-05-13T10:51Z
TLE epoch observation values (Epoch: 2026-05-13T10:51:53.749Z)
Latitude
-0.00003°
Longitude
174.85813°
Altitude
581.923 km
Speed
7.569 km/s
True Right ascension
13h 56m 10s
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
04:02:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.506 km
Perigee altitude
574.642 km
Semi-major axis
6,953.711 km
Eccentricity
0.00013
Inclination
97.6833°
RAAN
209.0446°
Arg. of periapsis
109.4874°
True anomaly
250.63471°
Mean anomaly
250.6492°
Eccentric anomaly
250.64196°
Mean motion
3.74299 °/min
Orbital period
96.18 mins
BSTAR
0.000055614
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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_2 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 | 2026-05-14 04:38:36.837Z | 145.418° SSE | 2026-05-14 04:42:36.837Z | 57.746° ENE | 35.206° | 2026-05-14 04:45:36.837Z | 2.99° NNE |
| 6 mins | 2026-05-14 17:56:36.837Z | 11.123° NNE | 2026-05-14 17:58:36.837Z | 1.588° NNE | 44.071° | 2026-05-14 18:02:36.837Z | 194.625° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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