STARLINK-11515, 62556
Orbit data source: Space-Track
STARLINK-11515, 62556 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 10 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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62556 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: 9 hours ago
TLE from 9 hours ago
0 STARLINK-11515
1 62556U 25006C 26171.47012101 .00135045 00000-0 10389-2 0 9991
2 62556 42.9994 240.6795 0000324 269.4106 90.6724 15.70841119 82761Epoch: 2026-06-20T11:16Z
TLE epoch observation values (Epoch: 2026-06-20T11:16:58.455Z)
Latitude
-0.00004°
Longitude
162.75161°
Altitude
356.266 km
Speed
7.697 km/s
True Right ascension
16h 02m 43s
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
07:23:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
358.692 km
Perigee altitude
358.255 km
Semi-major axis
6,736.611 km
Eccentricity
0.00003
Inclination
42.9994°
RAAN
240.6795°
Arg. of periapsis
269.4106°
True anomaly
90.67611°
Mean anomaly
90.6724°
Eccentric anomaly
90.67426°
Mean motion
3.92537 °/min
Orbital period
91.71 mins
BSTAR
0.0010389
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Other satellites on launch #6 in the year 2025 (2025-01-10 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-11515 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 | 2026-06-21 08:54:41.394Z | 250.632° W | 2026-06-21 08:56:41.394Z | 73.868° E | 43.743° | 2026-06-21 08:58:41.394Z | 71.919° E |
| 4 mins | 2026-06-21 12:07:41.394Z | 295.977° NW | 2026-06-21 12:08:41.394Z | 324.882° NNW | 42.156° | 2026-06-21 12:11:41.394Z | 101.346° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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