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: 8 hours ago
TLE from 8 hours ago
0 STARLINK-32400
1 61669U 24193J 25290.68778606 .00000174 00000-0 18004-4 0 9992
2 61669 53.1604 33.0197 0001302 80.3597 279.7551 15.30195822 54663Epoch: 2025-10-17T16:30Z
TLE epoch observation values (Epoch: 2025-10-17T16:30:24.715Z)
Latitude
-0.00001°
Longitude
118.98714°
Altitude
475.976 km
Speed
7.629 km/s
True Right ascension
02h 12m 04s
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
19:43:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.376 km
Perigee altitude
474.592 km
Semi-major axis
6,853.621 km
Eccentricity
0.00013
Inclination
53.1604°
RAAN
33.0197°
Arg. of periapsis
80.3597°
True anomaly
279.7404°
Mean anomaly
279.7551°
Eccentric anomaly
279.74775°
Mean motion
3.82528 °/min
Orbital period
94.11 mins
BSTAR
0.000018004
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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 | 2025-10-18 09:57:44.945Z | 246.608° WSW | 2025-10-18 09:59:44.945Z | 357.639° N | 41.574° | 2025-10-18 10:02:44.945Z | 44.839° NE |
| 5 mins | 2025-10-18 14:53:44.945Z | 338.32° N | 2025-10-18 14:55:44.945Z | 13.074° NNE | 17.986° | 2025-10-18 14:58:44.945Z | 69.388° E |
| 5 mins | 2025-10-18 16:32:44.945Z | 305.649° NW | 2025-10-18 16:34:44.945Z | 163.334° S | 43.829° | 2025-10-18 16:37:44.945Z | 134.73° SE |
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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