STARLINK-32379, 61851
Orbit data source: Space-Track
STARLINK-32379, 61851 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 07 Nov 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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61851 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: 1 day ago
TLE from 1 day ago
0 STARLINK-32379
1 61851U 24202G 26266.18800629 .00000749 00000-0 36738-4 0 9998
2 61851 43.0026 191.2762 0001227 270.7909 89.2802 15.27585293105666Epoch: 2026-09-23T04:30Z
TLE epoch observation values (Epoch: 2026-09-23T04:30:43.743Z)
Latitude
-0.00002°
Longitude
121.55119°
Altitude
482.798 km
Speed
7.626 km/s
True Right ascension
12h 45m 06s
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
21:45:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.82 km
Perigee altitude
484.136 km
Semi-major axis
6,863.115 km
Eccentricity
0.00012
Inclination
43.0026°
RAAN
191.2762°
Arg. of periapsis
270.7909°
True anomaly
89.29426°
Mean anomaly
89.2802°
Eccentric anomaly
89.28723°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
0.000036738
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Other satellites on launch #202 in the year 2024 (2024-11-07 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-32379 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 | 2026-09-24 04:33:37.342Z | 264.562° W | 2026-09-24 04:36:37.342Z | 205.534° SW | 23.068° | 2026-09-24 04:38:37.342Z | 167.567° S |
| 4 mins | 2026-09-24 21:31:37.342Z | 178.131° S | 2026-09-24 21:32:37.342Z | 153.496° SSE | 25.529° | 2026-09-24 21:35:37.342Z | 93.082° ESE |
| 5 mins | 2026-09-24 23:09:37.342Z | 256.323° W | 2026-09-24 23:11:37.342Z | 6.484° NNE | 82.317° | 2026-09-24 23:14:37.342Z | 70.565° E |
| 5 mins | 2026-09-25 00:48:37.342Z | 292.907° NW | 2026-09-25 00:50:37.342Z | 353.736° N | 50.65° | 2026-09-25 00:53:37.342Z | 73.985° E |
| 6 mins | 2026-09-25 02:27:37.342Z | 289.479° WNW | 2026-09-25 02:29:37.342Z | 302.501° NW | 76.623° | 2026-09-25 02:33:37.342Z | 107.8° ESE |
| 5 mins | 2026-09-25 04:06:37.342Z | 255.67° W | 2026-09-25 04:08:37.342Z | 211.99° SW | 23.986° | 2026-09-25 04:11:37.342Z | 159.014° S |
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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