STARLINK-33542, 62105 (Decayed)
Orbit data source: Space-Track
STARLINK-33542, 62105 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 25 Nov 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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62105 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Decayed Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
530 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 STARLINK-33542
1 62105U 24220T 25227.55376212 .01880513 37636-2 10928-2 0 9998
2 62105 42.9060 157.2174 0004173 230.1523 298.6811 16.18820999 43156Epoch: 2025-08-15T13:17Z
TLE epoch observation values (Epoch: 2025-08-15T13:17:25.047Z)
Latitude
7.59241°
Longitude
165.46354°
Altitude
220.521 km
Speed
7.778 km/s
True Right ascension
21h 56m 04s
True Declination
7° 32' 38"
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
08:33:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
227.548 km
Perigee altitude
222.037 km
Semi-major axis
6,602.93 km
Eccentricity
0.00042
Inclination
42.906°
RAAN
157.2174°
Arg. of periapsis
230.1523°
True anomaly
298.63914°
Mean anomaly
298.6811°
Eccentric anomaly
298.66012°
Mean motion
4.04518 °/min
Orbital period
88.99 mins
BSTAR
0.0010928
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Other satellites on launch #220 in the year 2024 (2024-11-25 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-33542 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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