STARLINK-32854, 62816
Orbit data source: Space-Track
STARLINK-32854, 62816 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 24 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62816 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-32854
1 62816U 25018L 25300.94181994 .00033111 00000-0 11250-2 0 9994
2 62816 53.1585 206.2341 0001085 90.5585 269.5540 15.30202098 42834Epoch: 2025-10-27T22:36Z
TLE epoch observation values (Epoch: 2025-10-27T22:36:13.242Z)
Latitude
-0.00005°
Longitude
-169.35754°
Altitude
476.114 km
Speed
7.629 km/s
True Right ascension
13h 44m 56s
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
00:29:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.209 km
Perigee altitude
474.722 km
Semi-major axis
6,853.602 km
Eccentricity
0.00011
Inclination
53.1585°
RAAN
206.2341°
Arg. of periapsis
90.5585°
True anomaly
269.54157°
Mean anomaly
269.554°
Eccentric anomaly
269.54778°
Mean motion
3.82529 °/min
Orbital period
94.11 mins
BSTAR
0.001125
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Other satellites on launch #18 in the year 2025 (2025-01-24 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-32854 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 | 2025-10-28 20:45:32.975Z | 245.421° WSW | 2025-10-28 20:47:32.975Z | 345.047° N | 42.301° | 2025-10-28 20:50:32.975Z | 44.531° NE |
| 4 mins | 2025-10-29 01:42:32.975Z | 350.966° N | 2025-10-29 01:44:32.975Z | 33.115° NE | 17.983° | 2025-10-29 01:46:32.975Z | 67.958° E |
| 5 mins | 2025-10-29 03:20:32.975Z | 306.035° NW | 2025-10-29 03:22:32.975Z | 178.178° S | 44.394° | 2025-10-29 03:25:32.975Z | 134.749° 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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