STARLINK-11512, 62517
Orbit data source: Space-Track
STARLINK-11512, 62517 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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62517 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: 7 hours ago
TLE from 7 hours ago
0 STARLINK-11512
1 62517U 25004G 26095.52585265 .00300797 00000-0 22561-2 0 9996
2 62517 42.9994 268.5665 0002178 261.2921 98.7700 15.70921863 71437Epoch: 2026-04-05T12:37Z
TLE epoch observation values (Epoch: 2026-04-05T12:37:13.668Z)
Latitude
-0.00004°
Longitude
-114.57051°
Altitude
356.256 km
Speed
7.697 km/s
True Right ascension
17h 54m 15s
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
01:44:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.71 km
Perigee altitude
356.776 km
Semi-major axis
6,736.38 km
Eccentricity
0.00022
Inclination
42.9994°
RAAN
268.5665°
Arg. of periapsis
261.2921°
True anomaly
98.79467°
Mean anomaly
98.77°
Eccentric anomaly
98.78233°
Mean motion
3.92558 °/min
Orbital period
91.71 mins
BSTAR
0.0022561
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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-11512 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 | 2026-04-05 20:43:56.225Z | 266.049° W | 2026-04-05 20:45:56.225Z | 214.272° SW | 24.885° | 2026-04-05 20:47:56.225Z | 156.566° SSE |
| 4 mins | 2026-04-06 16:22:56.225Z | 275.899° WNW | 2026-04-06 16:24:56.225Z | 13.192° NNE | 38.552° | 2026-04-06 16:26:56.225Z | 65.69° ENE |
| 4 mins | 2026-04-06 19:35:56.225Z | 270.377° WNW | 2026-04-06 19:36:56.225Z | 221.773° SW | 40.001° | 2026-04-06 19:39:56.225Z | 123.298° 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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