SATORO-T2, 60477
Orbit data source: Space-Track
SATORO-T2, 60477 is a payload satellite owned by Satoro (SG) 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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60477 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SINGRelated business
Manufacturer
Satoro
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SATORO-T2
1 60477U 24149K 25312.81304906 .00113121 00000-0 18648-2 0 9996
2 60477 97.3929 34.8437 0001341 249.3389 110.7720 15.51898758 68730Epoch: 2025-11-08T19:30Z
TLE epoch observation values (Epoch: 2025-11-08T19:30:47.438Z)
Latitude
-0.00001°
Longitude
53.90876°
Altitude
414.639 km
Speed
7.662 km/s
True Right ascension
02h 19m 22s
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
18:58:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
409.015 km
Perigee altitude
407.195 km
Semi-major axis
6,786.242 km
Eccentricity
0.00013
Inclination
97.3929°
RAAN
34.8437°
Arg. of periapsis
249.3389°
True anomaly
110.78637°
Mean anomaly
110.772°
Eccentric anomaly
110.77918°
Mean motion
3.88239 °/min
Orbital period
92.73 mins
BSTAR
0.0018648
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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.SATORO-T2 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 | 2025-11-10 05:40:42.127Z | 168.634° S | 2025-11-10 05:43:42.127Z | 298.193° NW | 44.864° | 2025-11-10 05:46:42.127Z | 347.103° N |
| 4 mins | 2025-11-10 18:30:42.127Z | 12.625° NNE | 2025-11-10 18:31:42.127Z | 14.873° NNE | 44.215° | 2025-11-10 18:34:42.127Z | 192.615° 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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