STARLINK-34485, 64684
Orbit data source: Space-Track
STARLINK-34485, 64684 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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64684 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-34485
1 64684U 25139W 26170.96422421 .00023928 00000-0 71654-3 0 9994
2 64684 53.1595 10.5066 0000783 61.4152 298.6930 15.34422628 55962Epoch: 2026-06-19T23:08Z
TLE epoch observation values (Epoch: 2026-06-19T23:08:28.971Z)
Latitude
0.00002°
Longitude
115.20025°
Altitude
463.28 km
Speed
7.636 km/s
True Right ascension
00h 42m 01s
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
07:19:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.429 km
Perigee altitude
462.357 km
Semi-major axis
6,841.03 km
Eccentricity
0.00008
Inclination
53.1595°
RAAN
10.5066°
Arg. of periapsis
61.4152°
True anomaly
298.68513°
Mean anomaly
298.693°
Eccentric anomaly
298.68906°
Mean motion
3.83584 °/min
Orbital period
93.85 mins
BSTAR
0.00071654
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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-34485 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 21:28:28.087Z | 335.504° NNW | 2026-06-20 21:31:28.087Z | 34.967° NE | 19.855° | 2026-06-20 21:33:28.087Z | 72.605° E |
| 6 mins | 2026-06-20 23:06:28.087Z | 300.476° NW | 2026-06-20 23:09:28.087Z | 182.267° SSW | 39.09° | 2026-06-20 23:12:28.087Z | 142.702° SSE |
| 5 mins | 2026-06-21 15:59:28.087Z | 245.287° WSW | 2026-06-21 16:01:28.087Z | 318.857° NNW | 42.121° | 2026-06-21 16:04:28.087Z | 43.364° 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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