STARLINK-32400, 61669
Orbit data source: Space-Track
STARLINK-32400, 61669 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 26 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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61669 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: 9 hours ago
TLE from 9 hours ago
0 STARLINK-32400
1 61669U 24193J 25352.60619208 .00000199 00000-0 18850-4 0 9991
2 61669 53.1610 105.4168 0001101 82.4760 277.6366 15.30197674 64146Epoch: 2025-12-18T14:32Z
TLE epoch observation values (Epoch: 2025-12-18T14:32:54.995Z)
Latitude
-0.00002°
Longitude
159.72835°
Altitude
476.022 km
Speed
7.629 km/s
True Right ascension
07h 01m 40s
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
22:03:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.233 km
Perigee altitude
474.724 km
Semi-major axis
6,853.615 km
Eccentricity
0.00011
Inclination
53.161°
RAAN
105.4168°
Arg. of periapsis
82.476°
True anomaly
277.6241°
Mean anomaly
277.6366°
Eccentric anomaly
277.63035°
Mean motion
3.82528 °/min
Orbital period
94.11 mins
BSTAR
0.00001885
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Other satellites on launch #193 in the year 2024 (2024-10-26 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-32400 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 | 2025-12-19 09:30:57.317Z | 182.372° SSW | 2025-12-19 09:33:57.317Z | 116.464° SE | 22.763° | 2025-12-19 09:35:57.317Z | 78.984° E |
| 5 mins | 2025-12-19 11:08:57.317Z | 266.294° W | 2025-12-19 11:10:57.317Z | 314.981° NW | 31.321° | 2025-12-19 11:13:57.317Z | 32.126° NE |
| 4 mins | 2025-12-19 16:06:57.317Z | 356.009° N | 2025-12-19 16:07:57.317Z | 22.866° NE | 24.646° | 2025-12-19 16:10:57.317Z | 86.022° E |
| 5 mins | 2025-12-19 17:43:57.317Z | 287.721° WNW | 2025-12-19 17:45:57.317Z | 235.336° WSW | 33.191° | 2025-12-19 17:48:57.317Z | 158.89° S |
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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