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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Identifier
Orbit
Country
SG / 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, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 SATORO-T3
1 64589U 25135BP 26224.53997168 .00001144 00000-0 11124-3 0 9994
2 64589 97.7758 338.5113 0006076 134.1435 226.0286 14.94518674 62329Epoch: 2026-08-12T12:57Z
TLE epoch observation values (Epoch: 2026-08-12T12:57:33.553Z)
Latitude
0.00002°
Longitude
-176.87095°
Altitude
589.851 km
Speed
7.564 km/s
True Right ascension
22h 34m 02s
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
18:26:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.111 km
Perigee altitude
576.655 km
Semi-major axis
6,959.02 km
Eccentricity
0.00061
Inclination
97.7758°
RAAN
338.5113°
Arg. of periapsis
134.1435°
True anomaly
225.97852°
Mean anomaly
226.0286°
Eccentric anomaly
226.00356°
Mean motion
3.7387 °/min
Orbital period
96.29 mins
BSTAR
0.00011124
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-13 06:47:36.061Z | 106.381° ESE | 2026-08-13 06:49:36.061Z | 70.431° E | 19.868° | 2026-08-13 06:52:36.061Z | 20.784° NNE |
| 5 mins | 2026-08-13 08:22:36.061Z | 214.224° SW | 2026-08-13 08:24:36.061Z | 254.348° W | 25.714° | 2026-08-13 08:27:36.061Z | 316.597° NNW |
| 6 mins | 2026-08-13 20:04:36.061Z | 39.635° NE | 2026-08-13 20:06:36.061Z | 82.964° E | 31.299° | 2026-08-13 20:10:36.061Z | 166.554° S |
| 4 mins | 2026-08-13 21:40:36.061Z | 318.855° NNW | 2026-08-13 21:41:36.061Z | 302.43° NW | 15.464° | 2026-08-13 21:44:36.061Z | 255.228° W |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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