SATORO-T3, 64589
Orbit data source: Space-Track
SATORO-T3, 64589 is a payload satellite owned by Satoro (SG) in SSO that was launched on Mon, 23 Jun 2025 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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64589 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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 SATORO-T3
1 64589U 25135BP 25312.04010689 .00003995 00000-0 38990-3 0 9997
2 64589 97.7570 64.2850 0004694 4.6682 355.4580 14.92978999 20899Epoch: 2025-11-08T00:57Z
TLE epoch observation values (Epoch: 2025-11-08T00:57:45.235Z)
Latitude
-0.00005°
Longitude
2.3711°
Altitude
588.436 km
Speed
7.568 km/s
True Right ascension
04h 17m 08s
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
05:40:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.939 km
Perigee altitude
582.401 km
Semi-major axis
6,963.807 km
Eccentricity
0.00047
Inclination
97.757°
RAAN
64.285°
Arg. of periapsis
4.6682°
True anomaly
355.45374°
Mean anomaly
355.458°
Eccentric anomaly
355.45587°
Mean motion
3.73485 °/min
Orbital period
96.39 mins
BSTAR
0.0003899
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-T3 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 | 2025-11-08 20:50:46.549Z | 352.862° N | 2025-11-08 20:52:46.549Z | 300.882° NW | 38.166° | 2025-11-08 20:56:46.549Z | 210.652° SW |
| 6 mins | 2025-11-09 07:39:46.549Z | 167.464° S | 2025-11-09 07:41:46.549Z | 171.012° S | 43.288° | 2025-11-09 07:45:46.549Z | 347.22° N |
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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