STARLINK-32095, 59692 (Decayed)
Orbit data source: Space-Track
STARLINK-32095, 59692 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 08 May 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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59692 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Decayed 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: 1 year ago
TLE from 1 year ago
0 STARLINK-32095
1 59692U 24086L 25104.33335648 .07851965 89135-5 24176-2 0 9992
2 59692 42.9690 82.1567 0010574 235.7889 293.6918 16.25565097 54082Epoch: 2025-04-14T08:00Z
TLE epoch observation values (Epoch: 2025-04-14T08:00:01.999Z)
Latitude
7.2086°
Longitude
-68.3603°
Altitude
200.807 km
Speed
7.79 km/s
True Right ascension
16h 57m 35s
True Declination
7° 09' 44"
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
23:07:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
213.48 km
Perigee altitude
199.555 km
Semi-major axis
6,584.655 km
Eccentricity
0.00106
Inclination
42.969°
RAAN
82.1567°
Arg. of periapsis
235.7889°
True anomaly
293.58078°
Mean anomaly
293.6918°
Eccentric anomaly
293.6363°
Mean motion
4.06203 °/min
Orbital period
88.63 mins
BSTAR
0.0024176
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Other satellites on launch #86 in the year 2024 (2024-05-08 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-32095 Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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