STARLINK-34614, 65030
Orbit data source: Space-Track
STARLINK-34614, 65030 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 30 Jul 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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65030 intel report (Beta)
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Edit Public Description
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-34614
1 65030U 25161R 25342.43244493 .00028591 00000-0 97393-3 0 9997
2 65030 53.1614 358.3904 0001248 88.7933 271.3211 15.30193538 21357Epoch: 2025-12-08T10:22Z
TLE epoch observation values (Epoch: 2025-12-08T10:22:43.241Z)
Latitude
-0.00003°
Longitude
125.27865°
Altitude
476.115 km
Speed
7.629 km/s
True Right ascension
23h 53m 33s
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
22:40:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.346 km
Perigee altitude
474.635 km
Semi-major axis
6,853.628 km
Eccentricity
0.00012
Inclination
53.1614°
RAAN
358.3904°
Arg. of periapsis
88.7933°
True anomaly
271.3068°
Mean anomaly
271.3211°
Eccentric anomaly
271.31395°
Mean motion
3.82527 °/min
Orbital period
94.11 mins
BSTAR
0.00097393
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Other satellites on launch #161 in the year 2025 (2025-07-30 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-34614 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 | 2025-12-09 03:47:25.534Z | 220.211° SW | 2025-12-09 03:50:25.534Z | 174.032° S | 42.206° | 2025-12-09 03:53:25.534Z | 56.23° ENE |
| 4 mins | 2025-12-09 05:27:25.534Z | 302.545° NW | 2025-12-09 05:29:25.534Z | 347.121° N | 19.145° | 2025-12-09 05:31:25.534Z | 22.463° NNE |
| 5 mins | 2025-12-09 10:23:25.534Z | 322.38° NNW | 2025-12-09 10:25:25.534Z | 10.956° NNE | 39.367° | 2025-12-09 10:28:25.534Z | 113.555° SE |
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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