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: 19 hours ago
TLE from 19 hours ago
0 SATELIOT_2
1 60534U 24149BU 26304.48995027 .00001659 00000-0 15008-3 0 9995
2 60534 97.6712 16.9002 0001676 83.6315 276.5097 14.96761910120357Epoch: 2026-10-31T11:45Z
TLE epoch observation values (Epoch: 2026-10-31T11:45:31.703Z)
Latitude
-0.00007°
Longitude
160.72318°
Altitude
579.828 km
Speed
7.571 km/s
True Right ascension
01h 07m 36s
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
02:18:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.083 km
Perigee altitude
572.752 km
Semi-major axis
6,952.055 km
Eccentricity
0.00017
Inclination
97.6712°
RAAN
16.9002°
Arg. of periapsis
83.6315°
True anomaly
276.49062°
Mean anomaly
276.5097°
Eccentric anomaly
276.50016°
Mean motion
3.74432 °/min
Orbital period
96.15 mins
BSTAR
0.00015008
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-01 17:12:40.331Z | 36.215° NE | 2026-11-01 17:15:40.331Z | 87.023° E | 30.033° | 2026-11-01 17:18:40.331Z | 151.256° SSE |
| 4 mins | 2026-11-01 18:49:40.331Z | 318.879° NNW | 2026-11-01 18:50:40.331Z | 300.191° NW | 19.946° | 2026-11-01 18:53:40.331Z | 248.644° W |
| 4 mins | 2026-11-02 04:02:40.331Z | 89.913° E | 2026-11-02 04:03:40.331Z | 71.31° E | 18.842° | 2026-11-02 04:06:40.331Z | 23.238° NE |
| 5 mins | 2026-11-02 05:36:40.331Z | 211.422° SW | 2026-11-02 05:38:40.331Z | 255.874° W | 32.559° | 2026-11-02 05:41:40.331Z | 320.468° NNW |
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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