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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 SATORO-T3
1 64589U 25135BP 26197.82517757 .00000604 00000-0 61349-4 0 9992
2 64589 97.7740 312.0547 0003896 219.7413 140.3522 14.94439412 58330Epoch: 2026-07-16T19:48Z
TLE epoch observation values (Epoch: 2026-07-16T19:48:15.342Z)
Latitude
-0.00002°
Longitude
80.3297°
Altitude
589.248 km
Speed
7.564 km/s
True Right ascension
20h 48m 13s
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
20:56:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.841 km
Perigee altitude
578.418 km
Semi-major axis
6,959.266 km
Eccentricity
0.00039
Inclination
97.774°
RAAN
312.0547°
Arg. of periapsis
219.7413°
True anomaly
140.38068°
Mean anomaly
140.3522°
Eccentric anomaly
140.36644°
Mean motion
3.73851 °/min
Orbital period
96.3 mins
BSTAR
0.000061349
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-17 08:47:30.501Z | 231.112° WSW | 2026-07-17 08:49:30.501Z | 260.457° W | 14.729° | 2026-07-17 08:51:30.501Z | 293.205° NW |
| 6 mins | 2026-07-17 20:29:30.501Z | 16.943° NNE | 2026-07-17 20:31:30.501Z | 38.685° NE | 43.053° | 2026-07-17 20:35:30.501Z | 189.464° SSW |
| 5 mins | 2026-07-18 07:18:30.501Z | 133.111° SE | 2026-07-18 07:20:30.501Z | 73.82° E | 36.081° | 2026-07-18 07:23:30.501Z | 4.712° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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