STARLINK-32915, 63152
Orbit data source: Space-Track
STARLINK-32915, 63152 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 03 Mar 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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63152 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-32915
1 63152U 25043W 25291.21672592 .00034326 00000-0 12501-2 0 9993
2 63152 43.0028 107.6621 0001442 277.2307 82.8381 15.27606182 35497Epoch: 2025-10-18T05:12Z
TLE epoch observation values (Epoch: 2025-10-18T05:12:05.119Z)
Latitude
-0°
Longitude
2.68985°
Altitude
482.623 km
Speed
7.626 km/s
True Right ascension
07h 10m 38s
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
11:00:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.905 km
Perigee altitude
483.926 km
Semi-major axis
6,863.052 km
Eccentricity
0.00014
Inclination
43.0028°
RAAN
107.6621°
Arg. of periapsis
277.2307°
True anomaly
82.8545°
Mean anomaly
82.8381°
Eccentric anomaly
82.8463°
Mean motion
3.8174 °/min
Orbital period
94.31 mins
BSTAR
0.0012501
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Other satellites on launch #43 in the year 2025 (2025-03-03 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-32915 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 | 2025-10-18 16:26:39.951Z | 253.123° W | 2025-10-18 16:29:39.951Z | 335.141° NNW | 44.931° | 2025-10-18 16:32:39.951Z | 71.232° E |
| 5 mins | 2025-10-18 18:06:39.951Z | 291.389° WNW | 2025-10-18 18:08:39.951Z | 349.679° N | 37.802° | 2025-10-18 18:11:39.951Z | 73.658° E |
| 6 mins | 2025-10-18 19:45:39.951Z | 289.399° WNW | 2025-10-18 19:47:39.951Z | 302.71° NW | 43.868° | 2025-10-18 19:51:39.951Z | 107.116° ESE |
| 5 mins | 2025-10-18 21:24:39.951Z | 256.762° W | 2025-10-18 21:26:39.951Z | 213.055° SW | 22.516° | 2025-10-18 21:29:39.951Z | 158.52° S |
| 4 mins | 2025-10-19 14:21:39.951Z | 181.139° SSW | 2025-10-19 14:23:39.951Z | 133.694° SE | 21.386° | 2025-10-19 14:25:39.951Z | 97.294° ESE |
| 5 mins | 2025-10-19 15:59:39.951Z | 252.783° W | 2025-10-19 16:01:39.951Z | 266.96° W | 44.598° | 2025-10-19 16:04:39.951Z | 71.367° 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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