STARLINK-11547, 62587
Orbit data source: Space-Track
STARLINK-11547, 62587 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 13 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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62587 intel report (Beta)
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Edit Public Description
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-11547
1 62587U 25008A 25290.00282043 .00414835 00000-0 30706-2 0 9993
2 62587 42.9987 272.4770 0000953 275.6104 84.4655 15.70894305 43517Epoch: 2025-10-17T00:04Z
TLE epoch observation values (Epoch: 2025-10-17T00:04:03.685Z)
Latitude
0°
Longitude
-114.29279°
Altitude
356.049 km
Speed
7.697 km/s
True Right ascension
18h 09m 54s
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
05:34:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
358.964 km
Perigee altitude
357.68 km
Semi-major axis
6,736.459 km
Eccentricity
0.0001
Inclination
42.9987°
RAAN
272.477°
Arg. of periapsis
275.6104°
True anomaly
84.47637°
Mean anomaly
84.4655°
Eccentric anomaly
84.47093°
Mean motion
3.92551 °/min
Orbital period
91.71 mins
BSTAR
0.0030706
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Other satellites on launch #8 in the year 2025 (2025-01-13 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-11547 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 | 2025-10-18 02:13:15.629Z | 215.677° SW | 2025-10-18 02:15:15.629Z | 158.586° S | 30.157° | 2025-10-18 02:17:15.629Z | 91.893° ESE |
| 4 mins | 2025-10-18 05:26:15.629Z | 304.521° NW | 2025-10-18 05:27:15.629Z | 339.607° N | 34.239° | 2025-10-18 05:30:15.629Z | 80.878° E |
| 4 mins | 2025-10-18 07:02:15.629Z | 275.482° WNW | 2025-10-18 07:03:15.629Z | 248.964° W | 37.318° | 2025-10-18 07:06:15.629Z | 123.699° 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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