STARLINK-34262, 64688
Orbit data source: Space-Track
STARLINK-34262, 64688 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 Eastern Test Range (AFETR). 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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64688 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: 14 hours ago
TLE from 14 hours ago
0 STARLINK-34262
1 64688U 25139AA 26171.27939010 .00012845 00000-0 39080-3 0 9993
2 64688 53.1607 8.9115 0001729 99.4565 260.6633 15.34387805 56075Epoch: 2026-06-20T06:42Z
TLE epoch observation values (Epoch: 2026-06-20T06:42:19.304Z)
Latitude
-0.00004°
Longitude
-0.16525°
Altitude
463.833 km
Speed
7.636 km/s
True Right ascension
00h 35m 38s
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
07:20:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.179 km
Perigee altitude
461.813 km
Semi-major axis
6,841.133 km
Eccentricity
0.00017
Inclination
53.1607°
RAAN
8.9115°
Arg. of periapsis
99.4565°
True anomaly
260.64375°
Mean anomaly
260.6633°
Eccentric anomaly
260.65353°
Mean motion
3.83576 °/min
Orbital period
93.85 mins
BSTAR
0.0003908
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Other satellites on launch #139 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-34262 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-20 21:13:11.954Z | 343.094° N | 2026-06-20 21:15:11.954Z | 20.809° NNE | 17.242° | 2026-06-20 21:17:11.954Z | 59.765° ENE |
| 5 mins | 2026-06-20 22:51:11.954Z | 309.284° NW | 2026-06-20 22:53:11.954Z | 291.642° WNW | 44.797° | 2026-06-20 22:56:11.954Z | 131.987° SE |
| 5 mins | 2026-06-21 15:44:11.954Z | 229.36° WSW | 2026-06-21 15:46:11.954Z | 48.892° ENE | 43.54° | 2026-06-21 15:49:11.954Z | 50.002° ENE |
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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