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: 6 hours ago
TLE from 6 hours ago
0 STARLINK-34548
1 64716U 25142W 26207.61664780 .00007022 00000-0 59561-3 0 9993
2 64716 70.0024 324.0509 0003236 269.2339 90.8449 14.98337382 60277Epoch: 2026-07-26T14:47Z
TLE epoch observation values (Epoch: 2026-07-26T14:47:58.369Z)
Latitude
-0.00008°
Longitude
157.74565°
Altitude
574.491 km
Speed
7.574 km/s
True Right ascension
21h 36m 12s
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
09:50:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.229 km
Perigee altitude
567.733 km
Semi-major axis
6,948.118 km
Eccentricity
0.00032
Inclination
70.0024°
RAAN
324.0509°
Arg. of periapsis
269.2339°
True anomaly
90.88198°
Mean anomaly
90.8449°
Eccentric anomaly
90.86344°
Mean motion
3.74751 °/min
Orbital period
96.06 mins
BSTAR
0.00059561
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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 | 2026-07-27 08:33:09.487Z | 161.72° S | 2026-07-27 08:36:09.487Z | 106.226° ESE | 25.684° | 2026-07-27 08:39:09.487Z | 51.579° ENE |
| 5 mins | 2026-07-27 10:12:09.487Z | 260.739° W | 2026-07-27 10:14:09.487Z | 297.488° NW | 21.839° | 2026-07-27 10:17:09.487Z | 351.764° N |
| 6 mins | 2026-07-27 18:36:09.487Z | 348.939° N | 2026-07-27 18:38:09.487Z | 36.395° NE | 40.954° | 2026-07-27 18:42:09.487Z | 144.643° SSE |
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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