STARLINK-11507, 62519
Orbit data source: Space-Track
STARLINK-11507, 62519 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 08 Jan 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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62519 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 V2MD, Unknown motor
Mass
960 kg wet, ~910 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 STARLINK-11507
1 62519U 25004J 25255.82521728 .00136297 00000-0 10470-2 0 9990
2 62519 42.9994 62.9644 0001765 276.9523 83.1144 15.70869677 39230Epoch: 2025-09-12T19:48Z
TLE epoch observation values (Epoch: 2025-09-12T19:48:18.772Z)
Latitude
-0.00003°
Longitude
133.81878°
Altitude
356.039 km
Speed
7.697 km/s
True Right ascension
04h 11m 51s
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
08:48:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.581 km
Perigee altitude
357.203 km
Semi-major axis
6,736.529 km
Eccentricity
0.00018
Inclination
42.9994°
RAAN
62.9644°
Arg. of periapsis
276.9523°
True anomaly
83.13448°
Mean anomaly
83.1144°
Eccentric anomaly
83.12444°
Mean motion
3.92545 °/min
Orbital period
91.71 mins
BSTAR
0.001047
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Other satellites on launch #4 in the year 2025 (2025-01-08 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-11507 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 | 2025-09-13 17:31:46.649Z | 296.398° NW | 2025-09-13 17:33:46.649Z | 13.578° NNE | 34.324° | 2025-09-13 17:35:46.649Z | 72.277° E |
| 4 mins | 2025-09-13 19:08:46.649Z | 283.528° WNW | 2025-09-13 19:09:46.649Z | 230.386° WSW | 44.615° | 2025-09-13 19:12:46.649Z | 112.479° ESE |
| 4 mins | 2025-09-14 14:46:46.649Z | 236.673° WSW | 2025-09-14 14:48:46.649Z | 110.077° ESE | 40.422° | 2025-09-14 14:50:46.649Z | 76.355° E |
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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