STARLINK-32417, 61673
Orbit data source: Space-Track
STARLINK-32417, 61673 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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61673 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: 6 hours ago
TLE from 6 hours ago
0 STARLINK-32417
1 61673U 24193N 25290.68092824 .00000405 00000-0 25831-4 0 9991
2 61673 53.1606 35.1015 0001607 98.9734 261.1448 15.30190456 54633Epoch: 2025-10-17T16:20Z
TLE epoch observation values (Epoch: 2025-10-17T16:20:32.199Z)
Latitude
-0.0001°
Longitude
123.54445°
Altitude
476.313 km
Speed
7.629 km/s
True Right ascension
02h 20m 24s
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
17:10:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.601 km
Perigee altitude
474.399 km
Semi-major axis
6,853.637 km
Eccentricity
0.00016
Inclination
53.1606°
RAAN
35.1015°
Arg. of periapsis
98.9734°
True anomaly
261.12661°
Mean anomaly
261.1448°
Eccentric anomaly
261.1357°
Mean motion
3.82527 °/min
Orbital period
94.11 mins
BSTAR
0.000025831
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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-32417 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 | 2025-10-18 09:45:41.436Z | 225.374° WSW | 2025-10-18 09:48:41.436Z | 178.813° S | 44.489° | 2025-10-18 09:51:41.436Z | 52.249° ENE |
| 4 mins | 2025-10-18 11:25:41.436Z | 307.059° NW | 2025-10-18 11:26:41.436Z | 327.232° NNW | 17.968° | 2025-10-18 11:29:41.436Z | 23.219° NE |
| 5 mins | 2025-10-18 16:21:41.436Z | 319.149° NNW | 2025-10-18 16:23:41.436Z | 14.756° NNE | 42.352° | 2025-10-18 16:26:41.436Z | 119.772° 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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