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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-11512
1 62517U 25004G 26254.73809557 .00131890 00000-0 10143-2 0 9998
2 62517 42.9996 28.8828 0001616 275.1000 84.9683 15.70859061 96473Epoch: 2026-09-11T17:42Z
TLE epoch observation values (Epoch: 2026-09-11T17:42:51.457Z)
Latitude
-0.00002°
Longitude
132.41123°
Altitude
356.116 km
Speed
7.697 km/s
True Right ascension
01h 55m 31s
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
20:52:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.511 km
Perigee altitude
357.334 km
Semi-major axis
6,736.559 km
Eccentricity
0.00016
Inclination
42.9996°
RAAN
28.8828°
Arg. of periapsis
275.1°
True anomaly
84.98675°
Mean anomaly
84.9683°
Eccentric anomaly
84.97752°
Mean motion
3.92542 °/min
Orbital period
91.71 mins
BSTAR
0.0010143
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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 | 2026-09-12 12:14:07.332Z | 206.813° SW | 2026-09-12 12:16:07.332Z | 152.86° SSE | 28.882° | 2026-09-12 12:18:07.332Z | 95.441° ESE |
| 4 mins | 2026-09-12 15:27:07.332Z | 305.213° NW | 2026-09-12 15:28:07.332Z | 341.161° N | 41.333° | 2026-09-12 15:31:07.332Z | 76.962° E |
| 4 mins | 2026-09-12 17:03:07.332Z | 283.542° WNW | 2026-09-12 17:05:07.332Z | 134.429° SE | 59.233° | 2026-09-12 17:07:07.332Z | 115.634° 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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