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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 SATORO-T3
1 64589U 25135BP 26120.21556435 .00001953 00000-0 18782-3 0 9997
2 64589 97.7659 235.2539 0006314 124.5265 235.6552 14.94142146 46740Epoch: 2026-04-30T05:10Z
TLE epoch observation values (Epoch: 2026-04-30T05:10:24.759Z)
Latitude
-0.00004°
Longitude
-60.51462°
Altitude
590.564 km
Speed
7.563 km/s
True Right ascension
15h 41m 00s
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
16:37:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.447 km
Perigee altitude
577.658 km
Semi-major axis
6,960.19 km
Eccentricity
0.00063
Inclination
97.7659°
RAAN
235.2539°
Arg. of periapsis
124.5265°
True anomaly
235.59549°
Mean anomaly
235.6552°
Eccentric anomaly
235.62534°
Mean motion
3.73776 °/min
Orbital period
96.31 mins
BSTAR
0.00018782
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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 | 2026-04-30 20:11:59.044Z | 22.879° NE | 2026-04-30 20:15:59.044Z | 105.945° ESE | 38.269° | 2026-04-30 20:18:59.044Z | 173.447° S |
| 5 mins | 2026-05-01 07:02:59.044Z | 113.453° SE | 2026-05-01 07:04:59.044Z | 62.519° ENE | 27.52° | 2026-05-01 07:07:59.044Z | 10.72° NNE |
| 4 mins | 2026-05-01 08:38:59.044Z | 243.703° WSW | 2026-05-01 08:39:59.044Z | 262.411° W | 18.049° | 2026-05-01 08:42:59.044Z | 310.848° NW |
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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