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, 18.1 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STARLINK-11507
1 62519U 25004J 25308.78999407 .00238834 00000-0 18039-2 0 9996
2 62519 42.9988 103.7082 0002746 261.3151 98.7406 15.70943475 47565Epoch: 2025-11-04T18:57Z
TLE epoch observation values (Epoch: 2025-11-04T18:57:35.487Z)
Latitude
-0°
Longitude
135.03837°
Altitude
356.252 km
Speed
7.697 km/s
True Right ascension
06h 54m 49s
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
00:17:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.031 km
Perigee altitude
356.331 km
Semi-major axis
6,736.318 km
Eccentricity
0.00027
Inclination
42.9988°
RAAN
103.7082°
Arg. of periapsis
261.3151°
True anomaly
98.7717°
Mean anomaly
98.7406°
Eccentric anomaly
98.75615°
Mean motion
3.92563 °/min
Orbital period
91.71 mins
BSTAR
0.0018039
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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 | 2025-11-05 13:28:27.955Z | 197.272° SSW | 2025-11-05 13:30:27.955Z | 144.564° SSE | 21.553° | 2025-11-05 13:32:27.955Z | 96.71° ESE |
| 4 mins | 2025-11-05 15:04:27.955Z | 262.166° W | 2025-11-05 15:06:27.955Z | 27.294° NE | 42.585° | 2025-11-05 15:08:27.955Z | 68.351° E |
| 4 mins | 2025-11-05 18:17:27.955Z | 287.397° WNW | 2025-11-05 18:18:27.955Z | 282.658° WNW | 43.465° | 2025-11-05 18:21:27.955Z | 109.972° ESE |
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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