STARLINK-32414, 61667
Orbit data source: Space-Track
STARLINK-32414, 61667 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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61667 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: 22 hours ago
TLE from 22 hours ago
0 STARLINK-32414
1 61667U 24193G 25336.89225235 -.00002072 00000-0 -57865-4 0 9998
2 61667 53.1607 180.8290 0001486 80.1971 279.9197 15.30191417 61703Epoch: 2025-12-02T21:24Z
TLE epoch observation values (Epoch: 2025-12-02T21:24:50.603Z)
Latitude
-0.00004°
Longitude
147.64724°
Altitude
475.965 km
Speed
7.629 km/s
True Right ascension
12h 03m 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
17:31:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.515 km
Perigee altitude
474.479 km
Semi-major axis
6,853.634 km
Eccentricity
0.00015
Inclination
53.1607°
RAAN
180.829°
Arg. of periapsis
80.1971°
True anomaly
279.90293°
Mean anomaly
279.9197°
Eccentric anomaly
279.91131°
Mean motion
3.82527 °/min
Orbital period
94.11 mins
BSTAR
-0.000057865
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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-32414 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 | 2025-12-03 23:00:26.435Z | 322.601° NNW | 2025-12-03 23:02:26.435Z | 64.465° ENE | 41.898° | 2025-12-03 23:05:26.435Z | 120.368° SE |
| 5 mins | 2025-12-04 15:55:26.435Z | 216.02° SW | 2025-12-04 15:57:26.435Z | 165.628° S | 42.214° | 2025-12-04 16:00:26.435Z | 56.63° ENE |
| 4 mins | 2025-12-04 17:34:26.435Z | 303.283° NW | 2025-12-04 17:35:26.435Z | 324.413° NNW | 19.432° | 2025-12-04 17:38:26.435Z | 23.327° NE |
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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