STARLINK-11546, 62835
Orbit data source: Space-Track
STARLINK-11546, 62835 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 27 Jan 2025 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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62835 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 V2MD, Unknown motor
Mass
960 kg wet, ~910 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 18.1 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 STARLINK-11546
1 62835U 25019G 25342.44040704 .00378103 00000-0 27951-2 0 9998
2 62835 43.0000 136.5369 0002498 263.9290 96.1294 15.71035628 49529Epoch: 2025-12-08T10:34Z
TLE epoch observation values (Epoch: 2025-12-08T10:34:11.168Z)
Latitude
0.00005°
Longitude
-99.44898°
Altitude
355.887 km
Speed
7.697 km/s
True Right ascension
09h 06m 08s
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
03:42:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.6 km
Perigee altitude
356.235 km
Semi-major axis
6,736.055 km
Eccentricity
0.00025
Inclination
43°
RAAN
136.5369°
Arg. of periapsis
263.929°
True anomaly
96.15786°
Mean anomaly
96.1294°
Eccentric anomaly
96.14363°
Mean motion
3.92586 °/min
Orbital period
91.7 mins
BSTAR
0.0027951
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Other satellites on launch #19 in the year 2025 (2025-01-27 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-11546 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-09 14:17:08.258Z | 233.64° WSW | 2025-12-09 14:18:08.258Z | 202.06° SSW | 40.728° | 2025-12-09 14:21:08.258Z | 75.62° E |
| 4 mins | 2025-12-09 15:53:08.258Z | 292.904° NW | 2025-12-09 15:54:08.258Z | 324.621° NNW | 33.059° | 2025-12-09 15:57:08.258Z | 68.483° E |
| 4 mins | 2025-12-09 17:29:08.258Z | 297.335° NW | 2025-12-09 17:31:08.258Z | 43.168° NE | 39.501° | 2025-12-09 17:33:08.258Z | 91.335° ESE |
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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