STARLINK-11514, 62514
Orbit data source: Space-Track
STARLINK-11514, 62514 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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62514 intel report (Beta)
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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: 21 hours ago
TLE from 21 hours ago
0 STARLINK-11514
1 62514U 25004D 26140.62845401 .00139538 00000-0 10705-2 0 9996
2 62514 43.0002 357.0172 0001843 276.0535 84.0123 15.70890981 78526Epoch: 2026-05-20T15:04Z
TLE epoch observation values (Epoch: 2026-05-20T15:04:58.426Z)
Latitude
0.00001°
Longitude
-107.51151°
Altitude
355.991 km
Speed
7.698 km/s
True Right ascension
23h 48m 04s
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
20:42:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.572 km
Perigee altitude
357.089 km
Semi-major axis
6,736.468 km
Eccentricity
0.00018
Inclination
43.0002°
RAAN
357.0172°
Arg. of periapsis
276.0535°
True anomaly
84.0333°
Mean anomaly
84.0123°
Eccentric anomaly
84.0228°
Mean motion
3.9255 °/min
Orbital period
91.71 mins
BSTAR
0.0010705
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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-11514 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 | 2026-05-21 18:49:54.038Z | 262.309° W | 2026-05-21 18:50:54.038Z | 283.895° WNW | 41.569° | 2026-05-21 18:53:54.038Z | 69.774° E |
| 4 mins | 2026-05-21 20:25:54.038Z | 297.924° NW | 2026-05-21 20:27:54.038Z | 24.588° NE | 32.994° | 2026-05-21 20:29:54.038Z | 72.168° E |
| 4 mins | 2026-05-21 22:01:54.038Z | 288.716° WNW | 2026-05-21 22:03:54.038Z | 98.233° ESE | 44.683° | 2026-05-21 22:05:54.038Z | 108.158° 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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