STARLINK-32750, 62572
Orbit data source: Space-Track
STARLINK-32750, 62572 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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62572 intel report (Beta)
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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: 9 hours ago
TLE from 9 hours ago
0 STARLINK-32750
1 62572U 25006U 26171.45413833 .00006450 00000-0 24360-3 0 9996
2 62572 43.0041 71.8171 0001612 261.5686 98.4983 15.27592224 80586Epoch: 2026-06-20T10:53Z
TLE epoch observation values (Epoch: 2026-06-20T10:53:57.551Z)
Latitude
-0.00003°
Longitude
-0.34126°
Altitude
482.952 km
Speed
7.626 km/s
True Right ascension
04h 47m 16s
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
07:14:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.063 km
Perigee altitude
483.851 km
Semi-major axis
6,863.094 km
Eccentricity
0.00016
Inclination
43.0041°
RAAN
71.8171°
Arg. of periapsis
261.5686°
True anomaly
98.51657°
Mean anomaly
98.4983°
Eccentric anomaly
98.50743°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.0002436
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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-32750 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 | 2026-06-20 20:30:17.363Z | 208.62° SW | 2026-06-20 20:33:17.363Z | 152.532° SSE | 26.125° | 2026-06-20 20:36:17.363Z | 90.06° ESE |
| 5 mins | 2026-06-20 22:10:17.363Z | 261.882° W | 2026-06-20 22:12:17.363Z | 7.809° NNE | 44.079° | 2026-06-20 22:15:17.363Z | 70.145° E |
| 5 mins | 2026-06-20 23:49:17.363Z | 294.274° NW | 2026-06-20 23:51:17.363Z | 357.691° N | 38.114° | 2026-06-20 23:54:17.363Z | 76.682° E |
| 5 mins | 2026-06-21 01:28:17.363Z | 286.304° WNW | 2026-06-21 01:30:17.363Z | 255.41° W | 44.442° | 2026-06-21 01:33:17.363Z | 112.864° SE |
| 4 mins | 2026-06-21 03:07:17.363Z | 251.216° W | 2026-06-21 03:09:17.363Z | 210.334° SW | 18.97° | 2026-06-21 03:11:17.363Z | 173.429° S |
| 4 mins | 2026-06-21 20:04:17.363Z | 185.054° SSW | 2026-06-21 20:05:17.363Z | 159.726° S | 25.208° | 2026-06-21 20:08:17.363Z | 92.818° 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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