STARLINK-34572, 64720
Orbit data source: Space-Track
STARLINK-34572, 64720 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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64720 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-34572
1 64720U 25142AA 26145.35046156 .00003336 00000-0 28720-3 0 9998
2 64720 70.0000 121.1728 0003931 265.8593 94.2116 14.98338174 51135Epoch: 2026-05-25T08:24Z
TLE epoch observation values (Epoch: 2026-05-25T08:24:39.878Z)
Latitude
-0.00012°
Longitude
112.06709°
Altitude
574.656 km
Speed
7.574 km/s
True Right ascension
08h 04m 41s
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
03:09:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.71 km
Perigee altitude
567.248 km
Semi-major axis
6,948.116 km
Eccentricity
0.00039
Inclination
70°
RAAN
121.1728°
Arg. of periapsis
265.8593°
True anomaly
94.25652°
Mean anomaly
94.2116°
Eccentric anomaly
94.23406°
Mean motion
3.74751 °/min
Orbital period
96.06 mins
BSTAR
0.0002872
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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-34572 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-25 22:57:56.283Z | 147.826° SSE | 2026-05-25 22:59:56.283Z | 114.85° SE | 19.992° | 2026-05-25 23:02:56.283Z | 61.376° ENE |
| 6 mins | 2026-05-26 00:35:56.283Z | 248.304° W | 2026-05-26 00:38:56.283Z | 313.324° NW | 26.441° | 2026-05-26 00:41:56.283Z | 2.016° NNE |
| 6 mins | 2026-05-26 08:59:56.283Z | 354.799° N | 2026-05-26 09:02:56.283Z | 75.481° E | 35.629° | 2026-05-26 09:05:56.283Z | 132.944° SE |
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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