STARLINK-32748, 62524
Orbit data source: Space-Track
STARLINK-32748, 62524 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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62524 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 V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 STARLINK-32748
1 62524U 25004P 25287.83197513 .00020692 00000-0 75960-3 0 9990
2 62524 42.9975 323.4263 0001541 74.0013 286.1008 15.27567898 44153Epoch: 2025-10-14T19:58Z
TLE epoch observation values (Epoch: 2025-10-14T19:58:02.651Z)
Latitude
-0.00003°
Longitude
0.30048°
Altitude
482.567 km
Speed
7.626 km/s
True Right ascension
21h 33m 42s
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
01:40:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.089 km
Perigee altitude
483.973 km
Semi-major axis
6,863.168 km
Eccentricity
0.00015
Inclination
42.9975°
RAAN
323.4263°
Arg. of periapsis
74.0013°
True anomaly
286.08383°
Mean anomaly
286.1008°
Eccentric anomaly
286.09232°
Mean motion
3.8173 °/min
Orbital period
94.31 mins
BSTAR
0.0007596
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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-32748 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-15 07:13:23.524Z | 258.033° W | 2025-10-15 07:16:23.524Z | 33.569° NE | 43.665° | 2025-10-15 07:19:23.524Z | 70.6° E |
| 5 mins | 2025-10-15 08:53:23.524Z | 295.526° NW | 2025-10-15 08:55:23.524Z | 7.674° NNE | 38.007° | 2025-10-15 08:58:23.524Z | 76.978° E |
| 5 mins | 2025-10-15 10:32:23.524Z | 286.863° WNW | 2025-10-15 10:34:23.524Z | 220.505° SW | 44.912° | 2025-10-15 10:37:23.524Z | 111.468° ESE |
| 4 mins | 2025-10-15 12:11:23.524Z | 249.546° W | 2025-10-15 12:13:23.524Z | 206.596° SW | 19.458° | 2025-10-15 12:15:23.524Z | 170.448° S |
| 4 mins | 2025-10-16 05:08:23.524Z | 180.939° SSW | 2025-10-16 05:09:23.524Z | 155.061° SSE | 24.577° | 2025-10-16 05:12:23.524Z | 92.149° ESE |
| 5 mins | 2025-10-16 06:46:23.524Z | 258.972° W | 2025-10-16 06:48:23.524Z | 351.921° N | 44.534° | 2025-10-16 06:51:23.524Z | 70.413° E |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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