STARLINK-34592, 64746
Orbit data source: Space-Track
STARLINK-34592, 64746 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 02 Jul 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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64746 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 STARLINK-34592
1 64746U 25144Y 26171.39648282 .00015847 00000-0 54604-3 0 9999
2 64746 53.1610 51.4161 0001289 89.7965 270.3184 15.30200046 55610Epoch: 2026-06-20T09:30Z
TLE epoch observation values (Epoch: 2026-06-20T09:30:56.115Z)
Latitude
0.00001°
Longitude
0.07059°
Altitude
476.11 km
Speed
7.629 km/s
True Right ascension
03h 25m 39s
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
07:21:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.355 km
Perigee altitude
474.588 km
Semi-major axis
6,853.608 km
Eccentricity
0.00013
Inclination
53.161°
RAAN
51.4161°
Arg. of periapsis
89.7965°
True anomaly
270.30363°
Mean anomaly
270.3184°
Eccentric anomaly
270.31101°
Mean motion
3.82529 °/min
Orbital period
94.11 mins
BSTAR
0.00054604
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Other satellites on launch #144 in the year 2025 (2025-07-02 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.STARLINK-34592 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 | 2026-06-21 00:04:29.330Z | 346.274° N | 2026-06-21 00:06:29.330Z | 25.955° NE | 17.935° | 2026-06-21 00:08:29.330Z | 63.32° ENE |
| 5 mins | 2026-06-21 01:42:29.330Z | 308.094° NW | 2026-06-21 01:44:29.330Z | 280.619° WNW | 44.541° | 2026-06-21 01:47:29.330Z | 133.433° SE |
| 6 mins | 2026-06-21 18:37:29.330Z | 233.177° WSW | 2026-06-21 18:40:29.330Z | 30.221° NE | 42.745° | 2026-06-21 18:43:29.330Z | 48.34° ENE |
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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