STARLINK-34548, 64716
Orbit data source: Space-Track
STARLINK-34548, 64716 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 28 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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64716 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-34548
1 64716U 25142W 26199.80572939 .00002480 00000-0 21554-3 0 9992
2 64716 70.0021 343.7449 0003210 263.4147 96.6647 14.98335831 59101Epoch: 2026-07-18T19:20Z
TLE epoch observation values (Epoch: 2026-07-18T19:20:15.019Z)
Latitude
0.00001°
Longitude
117.06912°
Altitude
574.722 km
Speed
7.574 km/s
True Right ascension
22h 54m 58s
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
18:58:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.216 km
Perigee altitude
567.756 km
Semi-major axis
6,948.123 km
Eccentricity
0.00032
Inclination
70.0021°
RAAN
343.7449°
Arg. of periapsis
263.4147°
True anomaly
96.70123°
Mean anomaly
96.6647°
Eccentric anomaly
96.68297°
Mean motion
3.7475 °/min
Orbital period
96.06 mins
BSTAR
0.00021554
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Other satellites on launch #142 in the year 2025 (2025-06-28 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-34548 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-19 11:30:44.187Z | 227.767° WSW | 2026-07-19 11:33:44.187Z | 306.034° NW | 37.086° | 2026-07-19 11:36:44.187Z | 9.587° NNE |
| 5 mins | 2026-07-19 19:55:44.187Z | 14.587° NNE | 2026-07-19 19:57:44.187Z | 59.074° ENE | 25.833° | 2026-07-19 20:00:44.187Z | 114.502° SE |
| 5 mins | 2026-07-19 21:33:44.187Z | 294.348° NW | 2026-07-19 21:35:44.187Z | 257.293° W | 21.274° | 2026-07-19 21:38:44.187Z | 206.067° SW |
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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