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: 18 hours ago
TLE from 18 hours ago
0 SATORO-T2
1 60477U 24149K 25286.91710069 .00073978 00000-0 14398-2 0 9991
2 60477 97.3963 8.2987 0000548 32.6745 327.4539 15.47314042 64724Epoch: 2025-10-13T22:00Z
TLE epoch observation values (Epoch: 2025-10-13T22:00:37.499Z)
Latitude
-0.00001°
Longitude
15.42945°
Altitude
427.4 km
Speed
7.655 km/s
True Right ascension
00h 33m 11s
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
10:41:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
421.889 km
Perigee altitude
421.144 km
Semi-major axis
6,799.653 km
Eccentricity
0.00005
Inclination
97.3963°
RAAN
8.2987°
Arg. of periapsis
32.6745°
True anomaly
327.45052°
Mean anomaly
327.4539°
Eccentric anomaly
327.45221°
Mean motion
3.87091 °/min
Orbital period
93 mins
BSTAR
0.0014398
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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 | 2025-10-14 18:44:07.290Z | 357.799° N | 2025-10-14 18:47:07.290Z | 282.463° WNW | 34.646° | 2025-10-14 18:50:07.290Z | 212.626° SW |
| 4 mins | 2025-10-15 05:12:07.290Z | 127.211° SE | 2025-10-15 05:14:07.290Z | 54.555° ENE | 29.716° | 2025-10-15 05:16:07.290Z | 9.801° NNE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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