STARLINK-32572, 61952
Orbit data source: Space-Track
STARLINK-32572, 61952 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 14 Nov 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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61952 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: 14 hours ago
TLE from 14 hours ago
0 STARLINK-32572
1 61952U 24209P 26171.32467471 .00023510 00000-0 80325-3 0 9993
2 61952 53.1606 25.4727 0001868 72.5043 287.6162 15.30205573 90616Epoch: 2026-06-20T07:47Z
TLE epoch observation values (Epoch: 2026-06-20T07:47:31.894Z)
Latitude
-0.00003°
Longitude
0.04886°
Altitude
475.711 km
Speed
7.629 km/s
True Right ascension
01h 41m 53s
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
08:33:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.735 km
Perigee altitude
474.175 km
Semi-major axis
6,853.592 km
Eccentricity
0.00019
Inclination
53.1606°
RAAN
25.4727°
Arg. of periapsis
72.5043°
True anomaly
287.5958°
Mean anomaly
287.6162°
Eccentric anomaly
287.606°
Mean motion
3.8253 °/min
Orbital period
94.11 mins
BSTAR
0.00080325
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Other satellites on launch #209 in the year 2024 (2024-11-14 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-32572 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 22:20:27.012Z | 337.833° N | 2026-06-20 22:22:27.012Z | 11.867° NNE | 17.58° | 2026-06-20 22:25:27.012Z | 68.047° E |
| 5 mins | 2026-06-20 23:59:27.012Z | 307.546° NW | 2026-06-21 00:01:27.012Z | 157.218° SSE | 44.364° | 2026-06-21 00:04:27.012Z | 133.314° SE |
| 5 mins | 2026-06-21 16:54:27.012Z | 233.893° WSW | 2026-06-21 16:56:27.012Z | 267.903° W | 44.231° | 2026-06-21 16:59:27.012Z | 47.633° ENE |
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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