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
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: 10 hours ago
TLE from 10 hours ago
0 SATORO-T3
1 64589U 25135BP 26062.41594299 .00003116 00000-0 29869-3 0 9995
2 64589 97.7589 178.1384 0004095 341.9511 18.1563 14.93859418 38112Epoch: 2026-03-03T09:58Z
TLE epoch observation values (Epoch: 2026-03-03T09:58:57.474Z)
Latitude
-0°
Longitude
-132.7964°
Altitude
586.25 km
Speed
7.569 km/s
True Right ascension
11h 52m 33s
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
23:43:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.782 km
Perigee altitude
580.081 km
Semi-major axis
6,961.068 km
Eccentricity
0.00041
Inclination
97.7589°
RAAN
178.1384°
Arg. of periapsis
341.9511°
True anomaly
18.17093°
Mean anomaly
18.1563°
Eccentric anomaly
18.16361°
Mean motion
3.73705 °/min
Orbital period
96.33 mins
BSTAR
0.00029869
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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 | 2026-03-03 20:11:40.755Z | 24.185° NE | 2026-03-03 20:15:40.755Z | 123.57° SE | 37.46° | 2026-03-03 20:18:40.755Z | 174.995° S |
| 6 mins | 2026-03-04 07:01:40.755Z | 123.95° SE | 2026-03-04 07:03:40.755Z | 85.656° E | 27.07° | 2026-03-04 07:07:40.755Z | 9.082° NNE |
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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