STARLINK-1728, 46582
Orbit data source: Space-Track
STARLINK-1728, 46582 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 06 Oct 2020 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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46582 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Partially operational Commercial Communications
Bus & Motor
STARLINK, Unknown motor
Mass
260 kg wet, ~248 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 STARLINK-1728
1 46582U 20070BC 25356.77483619 .00103120 00000-0 28725-2 0 9993
2 46582 53.0499 131.3577 0005267 203.9689 156.1069 15.35974869288341Epoch: 2025-12-22T18:35Z
TLE epoch observation values (Epoch: 2025-12-22T18:35:45.846Z)
Latitude
0.00001°
Longitude
120.84858°
Altitude
462.209 km
Speed
7.635 km/s
True Right ascension
08h 45m 25s
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
15:08:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.902 km
Perigee altitude
454.701 km
Semi-major axis
6,836.438 km
Eccentricity
0.00053
Inclination
53.0499°
RAAN
131.3577°
Arg. of periapsis
203.9689°
True anomaly
156.13133°
Mean anomaly
156.1069°
Eccentric anomaly
156.11912°
Mean motion
3.83971 °/min
Orbital period
93.76 mins
BSTAR
0.0028725
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Other satellites on launch #70 in the year 2020 (2020-10-06 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-1728 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 | 2025-12-23 18:31:22.583Z | 314.257° NW | 2025-12-23 18:33:22.583Z | 337.965° N | 41.985° | 2025-12-23 18:36:22.583Z | 124.147° SE |
| 5 mins | 2025-12-24 11:23:22.583Z | 215.149° SW | 2025-12-24 11:25:22.583Z | 99.766° ESE | 42.243° | 2025-12-24 11:28:22.583Z | 54.751° ENE |
| 4 mins | 2025-12-24 13:01:22.583Z | 302.231° NW | 2025-12-24 13:03:22.583Z | 346.919° N | 18.708° | 2025-12-24 13:05:22.583Z | 22.629° NE |
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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