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: 1 day ago
TLE from 1 day ago
0 SATORO-T3
1 64589U 25135BP 25268.80584102 .00005230 00000-0 51370-3 0 9998
2 64589 97.7534 21.6866 0006252 126.6895 233.4900 14.92576230 14443Epoch: 2025-09-25T19:20Z
TLE epoch observation values (Epoch: 2025-09-25T19:20:24.664Z)
Latitude
0.00005°
Longitude
86.72214°
Altitude
595.543 km
Speed
7.561 km/s
True Right ascension
01h 26m 44s
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
13:02:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.278 km
Perigee altitude
582.569 km
Semi-major axis
6,965.061 km
Eccentricity
0.00063
Inclination
97.7534°
RAAN
21.6866°
Arg. of periapsis
126.6895°
True anomaly
233.43244°
Mean anomaly
233.49°
Eccentric anomaly
233.46122°
Mean motion
3.73384 °/min
Orbital period
96.42 mins
BSTAR
0.0005137
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-26 20:02:27.052Z | 28.519° NE | 2025-09-26 20:06:27.052Z | 111.821° ESE | 32.841° | 2025-09-26 20:09:27.052Z | 166.601° S |
| 5 mins | 2025-09-27 06:53:27.052Z | 114.268° SE | 2025-09-27 06:55:27.052Z | 75.583° E | 23.761° | 2025-09-27 06:58:27.052Z | 18.879° NNE |
| 5 mins | 2025-09-27 08:29:27.052Z | 230.426° WSW | 2025-09-27 08:31:27.052Z | 271.84° WNW | 21.541° | 2025-09-27 08:34:27.052Z | 318.574° NNW |
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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