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: 16 hours ago
TLE from 16 hours ago
0 STARLINK-32400
1 61669U 24193J 25291.53687913 .00001596 00000-0 66022-4 0 9999
2 61669 53.1618 29.0761 0001325 94.4044 265.7108 15.30187698 54797Epoch: 2025-10-18T12:53Z
TLE epoch observation values (Epoch: 2025-10-18T12:53:06.356Z)
Latitude
-0.00005°
Longitude
168.5331°
Altitude
476.22 km
Speed
7.629 km/s
True Right ascension
01h 56m 18s
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
23:54:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.416 km
Perigee altitude
474.6 km
Semi-major axis
6,853.645 km
Eccentricity
0.00013
Inclination
53.1618°
RAAN
29.0761°
Arg. of periapsis
94.4044°
True anomaly
265.69566°
Mean anomaly
265.7108°
Eccentric anomaly
265.70323°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
0.000066022
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-19 09:27:20.779Z | 234.958° WSW | 2025-10-19 09:30:20.779Z | 22.375° NNE | 42.567° | 2025-10-19 09:33:20.779Z | 47.585° ENE |
| 4 mins | 2025-10-19 14:24:20.779Z | 340.193° N | 2025-10-19 14:26:20.779Z | 15.188° NNE | 16.959° | 2025-10-19 14:28:20.779Z | 54.717° ENE |
| 5 mins | 2025-10-19 16:03:20.779Z | 312.507° NW | 2025-10-19 16:05:20.779Z | 117.283° SE | 43.586° | 2025-10-19 16:08:20.779Z | 129.353° 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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