STARLINK-34559, 64706
Orbit data source: Space-Track
STARLINK-34559, 64706 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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64706 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: 8 hours ago
TLE from 8 hours ago
0 STARLINK-34559
1 64706U 25142L 26207.62499491 .00004472 00000-0 38222-3 0 9995
2 64706 70.0022 324.0804 0002929 269.5600 90.5224 14.98339887 60308Epoch: 2026-07-26T14:59Z
TLE epoch observation values (Epoch: 2026-07-26T14:59:59.560Z)
Latitude
0.00004°
Longitude
154.76201°
Altitude
574.468 km
Speed
7.574 km/s
True Right ascension
21h 36m 19s
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
12:19:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.008 km
Perigee altitude
567.938 km
Semi-major axis
6,948.11 km
Eccentricity
0.00029
Inclination
70.0022°
RAAN
324.0804°
Arg. of periapsis
269.56°
True anomaly
90.55596°
Mean anomaly
90.5224°
Eccentric anomaly
90.53918°
Mean motion
3.74751 °/min
Orbital period
96.06 mins
BSTAR
0.00038222
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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-34559 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 | 2026-07-27 08:44:56.645Z | 174.766° S | 2026-07-27 08:47:56.645Z | 123.641° SE | 31.562° | 2026-07-27 08:51:56.645Z | 41.575° NE |
| 4 mins | 2026-07-27 10:24:56.645Z | 273.625° WNW | 2026-07-27 10:26:56.645Z | 308.422° NW | 17.622° | 2026-07-27 10:28:56.645Z | 341.578° N |
| 7 mins | 2026-07-27 18:47:56.645Z | 337.102° NNW | 2026-07-27 18:50:56.645Z | 129.699° SE | 44.713° | 2026-07-27 18:54:56.645Z | 155.486° 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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