STARLINK-11527, 62523
Orbit data source: Space-Track
STARLINK-11527, 62523 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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62523 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: 16 hours ago
TLE from 16 hours ago
0 STARLINK-11527
1 62523U 25004N 26125.61130149 .00180259 00000-0 13737-2 0 9998
2 62523 43.0001 87.3683 0000472 25.5647 334.5244 15.70915091 76168Epoch: 2026-05-05T14:40Z
TLE epoch observation values (Epoch: 2026-05-05T14:40:16.448Z)
Latitude
-0.00003°
Longitude
3.81608°
Altitude
355.765 km
Speed
7.698 km/s
True Right ascension
05h 49m 28s
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
14:51:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
358.58 km
Perigee altitude
357.944 km
Semi-major axis
6,736.399 km
Eccentricity
0.00005
Inclination
43.0001°
RAAN
87.3683°
Arg. of periapsis
25.5647°
True anomaly
334.52207°
Mean anomaly
334.5244°
Eccentric anomaly
334.52324°
Mean motion
3.92556 °/min
Orbital period
91.71 mins
BSTAR
0.0013737
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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-11527 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 | 2026-05-07 00:27:06.873Z | 211.551° SW | 2026-05-07 00:29:06.873Z | 155.411° SSE | 28.003° | 2026-05-07 00:31:06.873Z | 93.536° ESE |
| 4 mins | 2026-05-07 03:40:06.873Z | 304.764° NW | 2026-05-07 03:41:06.873Z | 340.654° N | 33.95° | 2026-05-07 03:44:06.873Z | 79.374° E |
| 4 mins | 2026-05-07 05:16:06.873Z | 278.705° WNW | 2026-05-07 05:18:06.873Z | 147.726° SSE | 38.406° | 2026-05-07 05:20:06.873Z | 120.434° 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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