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, 14.5 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 STARLINK-11546
1 62835U 25019G 25256.79388020 .00186117 00000-0 14186-2 0 9994
2 62835 42.9987 292.7877 0001824 278.4774 81.5887 15.70891216 36052Epoch: 2025-09-13T19:03Z
TLE epoch observation values (Epoch: 2025-09-13T19:03:11.249Z)
Latitude
-0°
Longitude
13.9687°
Altitude
355.94 km
Speed
7.698 km/s
True Right ascension
19h 31m 09s
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
00:17:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.559 km
Perigee altitude
357.102 km
Semi-major axis
6,736.468 km
Eccentricity
0.00018
Inclination
42.9987°
RAAN
292.7877°
Arg. of periapsis
278.4774°
True anomaly
81.60938°
Mean anomaly
81.5887°
Eccentric anomaly
81.59904°
Mean motion
3.9255 °/min
Orbital period
91.71 mins
BSTAR
0.0014186
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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 | 2025-09-14 09:09:18.632Z | 295.152° NW | 2025-09-14 09:11:18.632Z | 359.017° N | 35.318° | 2025-09-14 09:13:18.632Z | 73.378° E |
| 4 mins | 2025-09-14 10:46:18.632Z | 276.488° WNW | 2025-09-14 10:47:18.632Z | 239.129° WSW | 41.29° | 2025-09-14 10:50:18.632Z | 119.578° SE |
| 4 mins | 2025-09-15 06:24:18.632Z | 247.021° WSW | 2025-09-15 06:26:18.632Z | 96.355° ESE | 43.948° | 2025-09-15 06:28:18.632Z | 73.242° E |
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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