STARLINK-32438, 61722
Orbit data source: Space-Track
STARLINK-32438, 61722 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 30 Oct 2024 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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61722 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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-32438
1 61722U 24196R 25294.70305905 .00006770 00000-0 24029-3 0 9991
2 61722 53.1601 27.1634 0002799 82.9069 277.2250 15.30229587 55872Epoch: 2025-10-21T16:52Z
TLE epoch observation values (Epoch: 2025-10-21T16:52:24.301Z)
Latitude
-0.00004°
Longitude
103.6749°
Altitude
475.786 km
Speed
7.629 km/s
True Right ascension
01h 48m 39s
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
00:21:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.301 km
Perigee altitude
473.465 km
Semi-major axis
6,853.52 km
Eccentricity
0.00028
Inclination
53.1601°
RAAN
27.1634°
Arg. of periapsis
82.9069°
True anomaly
277.19318°
Mean anomaly
277.225°
Eccentric anomaly
277.20909°
Mean motion
3.82536 °/min
Orbital period
94.11 mins
BSTAR
0.00024029
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Other satellites on launch #196 in the year 2024 (2024-10-30 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-32438 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 | 2025-10-22 08:42:54.113Z | 212.518° SW | 2025-10-22 08:45:54.113Z | 143.173° SSE | 39.444° | 2025-10-22 08:48:54.113Z | 60.243° ENE |
| 4 mins | 2025-10-22 10:22:54.113Z | 304.052° NW | 2025-10-22 10:23:54.113Z | 327.925° NNW | 21.441° | 2025-10-22 10:26:54.113Z | 26.513° NE |
| 5 mins | 2025-10-22 15:18:54.113Z | 329.285° NNW | 2025-10-22 15:20:54.113Z | 30.835° NE | 36.558° | 2025-10-22 15:23:54.113Z | 108.042° ESE |
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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