STARLINK-34568, 64717
Orbit data source: Space-Track
STARLINK-34568, 64717 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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64717 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-34568
1 64717U 25142X 26145.35463479 .00003533 00000-0 30369-3 0 9996
2 64717 70.0001 121.1889 0003822 266.6623 93.4099 14.98339705 50975Epoch: 2026-05-25T08:30Z
TLE epoch observation values (Epoch: 2026-05-25T08:30:40.445Z)
Latitude
-0.00004°
Longitude
110.57674°
Altitude
574.609 km
Speed
7.574 km/s
True Right ascension
08h 04m 45s
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
03:58:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.63 km
Perigee altitude
567.319 km
Semi-major axis
6,948.111 km
Eccentricity
0.00038
Inclination
70.0001°
RAAN
121.1889°
Arg. of periapsis
266.6623°
True anomaly
93.45362°
Mean anomaly
93.4099°
Eccentric anomaly
93.43176°
Mean motion
3.74751 °/min
Orbital period
96.06 mins
BSTAR
0.00030369
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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-34568 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 | 2026-05-25 23:03:29.037Z | 157.819° S | 2026-05-25 23:06:29.037Z | 106.135° ESE | 23.018° | 2026-05-25 23:09:29.037Z | 54.287° ENE |
| 5 mins | 2026-05-26 00:42:29.037Z | 257.473° W | 2026-05-26 00:44:29.037Z | 297.099° NW | 24.131° | 2026-05-26 00:47:29.037Z | 354.132° N |
| 6 mins | 2026-05-26 09:06:29.037Z | 353.735° N | 2026-05-26 09:08:29.037Z | 43.285° NE | 38.545° | 2026-05-26 09:12:29.037Z | 139.993° 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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