STARLINK-32440, 61714
Orbit data source: Space-Track
STARLINK-32440, 61714 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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61714 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: 4 hours ago
TLE from 4 hours ago
0 STARLINK-32440
1 61714U 24196H 25299.18976281 .00000957 00000-0 44429-4 0 9998
2 61714 53.1622 6.1100 0001275 84.9608 275.1539 15.30191802 56562Epoch: 2025-10-26T04:33Z
TLE epoch observation values (Epoch: 2025-10-26T04:33:15.506Z)
Latitude
0.00002°
Longitude
-97.01412°
Altitude
476.061 km
Speed
7.629 km/s
True Right ascension
00h 24m 26s
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
04:12:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.369 km
Perigee altitude
474.622 km
Semi-major axis
6,853.633 km
Eccentricity
0.00013
Inclination
53.1622°
RAAN
6.11°
Arg. of periapsis
84.9608°
True anomaly
275.13935°
Mean anomaly
275.1539°
Eccentric anomaly
275.14662°
Mean motion
3.82527 °/min
Orbital period
94.11 mins
BSTAR
0.000044429
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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-32440 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-26 12:50:50.481Z | 345.004° N | 2025-10-26 12:52:50.481Z | 25.623° NE | 19.115° | 2025-10-26 12:54:50.481Z | 65.048° ENE |
| 5 mins | 2025-10-26 14:28:50.481Z | 303.604° NW | 2025-10-26 14:30:50.481Z | 251.963° W | 43.452° | 2025-10-26 14:33:50.481Z | 138.815° SSE |
| 6 mins | 2025-10-27 07:23:50.481Z | 238.628° WSW | 2025-10-27 07:26:50.481Z | 6.908° NNE | 42.042° | 2025-10-27 07:29:50.481Z | 45.95° 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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