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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-11507
1 62519U 25004J 26037.89309683 .00169466 00000-0 12959-2 0 9998
2 62519 42.9992 256.4810 0001416 259.6029 100.4679 15.70867714 62361Epoch: 2026-02-06T21:26Z
TLE epoch observation values (Epoch: 2026-02-06T21:26:03.566Z)
Latitude
-0.00001°
Longitude
157.94169°
Altitude
356.36 km
Speed
7.697 km/s
True Right ascension
17h 05m 55s
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
11:31:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.351 km
Perigee altitude
357.444 km
Semi-major axis
6,736.535 km
Eccentricity
0.00014
Inclination
42.9992°
RAAN
256.481°
Arg. of periapsis
259.6029°
True anomaly
100.48386°
Mean anomaly
100.4679°
Eccentric anomaly
100.47588°
Mean motion
3.92544 °/min
Orbital period
91.71 mins
BSTAR
0.0012959
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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 | 2026-02-07 17:28:37.026Z | 198.756° SSW | 2026-02-07 17:30:37.026Z | 145.627° SSE | 22.158° | 2026-02-07 17:32:37.026Z | 96.52° ESE |
| 4 mins | 2026-02-07 19:04:37.026Z | 263.047° W | 2026-02-07 19:06:37.026Z | 19.038° NNE | 42.694° | 2026-02-07 19:08:37.026Z | 67.902° E |
| 4 mins | 2026-02-07 22:17:37.026Z | 286.465° WNW | 2026-02-07 22:18:37.026Z | 278.989° WNW | 42.663° | 2026-02-07 22:21:37.026Z | 110.944° 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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