STARLINK-34489, 64679
Orbit data source: Space-Track
STARLINK-34489, 64679 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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64679 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: 21 hours ago
TLE from 21 hours ago
0 STARLINK-34489
1 64679U 25139R 26170.97053786 .00021397 00000-0 64235-3 0 9998
2 64679 53.1590 10.5474 0000776 90.6714 269.4378 15.34411840 55960Epoch: 2026-06-19T23:17Z
TLE epoch observation values (Epoch: 2026-06-19T23:17:34.471Z)
Latitude
0.00004°
Longitude
112.96193°
Altitude
463.575 km
Speed
7.636 km/s
True Right ascension
00h 42m 11s
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
07:19:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.456 km
Perigee altitude
462.394 km
Semi-major axis
6,841.062 km
Eccentricity
0.00008
Inclination
53.159°
RAAN
10.5474°
Arg. of periapsis
90.6714°
True anomaly
269.42891°
Mean anomaly
269.4378°
Eccentric anomaly
269.43335°
Mean motion
3.83582 °/min
Orbital period
93.85 mins
BSTAR
0.00064235
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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-34489 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 | 2026-06-20 21:38:30.396Z | 340.857° N | 2026-06-20 21:40:30.396Z | 23.975° NE | 22.201° | 2026-06-20 21:43:30.396Z | 82.75° E |
| 5 mins | 2026-06-20 23:16:30.396Z | 289.908° WNW | 2026-06-20 23:18:30.396Z | 219.27° SW | 37.083° | 2026-06-20 23:21:30.396Z | 150.902° SSE |
| 5 mins | 2026-06-21 16:08:30.396Z | 250.477° W | 2026-06-21 16:10:30.396Z | 291.796° WNW | 36.774° | 2026-06-21 16:13:30.396Z | 37.263° NE |
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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