STARLINK-34546, 64718
Orbit data source: Space-Track
STARLINK-34546, 64718 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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64718 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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-34546
1 64718U 25142Y 26145.32125892 .00002307 00000-0 20107-3 0 9995
2 64718 70.0002 121.0713 0003597 267.9826 92.0921 14.98336275 51137Epoch: 2026-05-25T07:42Z
TLE epoch observation values (Epoch: 2026-05-25T07:42:36.770Z)
Latitude
-0.00005°
Longitude
122.50735°
Altitude
574.553 km
Speed
7.574 km/s
True Right ascension
08h 04m 17s
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
03:10:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.484 km
Perigee altitude
567.485 km
Semi-major axis
6,948.122 km
Eccentricity
0.00036
Inclination
70.0002°
RAAN
121.0713°
Arg. of periapsis
267.9826°
True anomaly
92.13329°
Mean anomaly
92.0921°
Eccentric anomaly
92.1127°
Mean motion
3.7475 °/min
Orbital period
96.06 mins
BSTAR
0.00020107
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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-34546 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 | 2026-05-25 23:51:41.037Z | 204.115° SW | 2026-05-25 23:55:41.037Z | 12.264° NNE | 44.487° | 2026-05-25 23:58:41.037Z | 23.621° NE |
| 4 mins | 2026-05-26 08:17:41.037Z | 24.123° NE | 2026-05-26 08:19:41.037Z | 59.189° ENE | 17.364° | 2026-05-26 08:21:41.037Z | 91.424° ESE |
| 6 mins | 2026-05-26 09:55:41.037Z | 307.3° NW | 2026-05-26 09:57:41.037Z | 258.974° W | 32.382° | 2026-05-26 10:01:41.037Z | 182.482° SSW |
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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