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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-1728
1 46582U 20070BC 25326.66514507 .00074128 00000-0 23975-2 0 9996
2 46582 53.0512 272.2815 0005888 90.6660 269.5015 15.31407530283725Epoch: 2025-11-22T15:57Z
TLE epoch observation values (Epoch: 2025-11-22T15:57:48.534Z)
Latitude
0.00004°
Longitude
-29.06126°
Altitude
472.538 km
Speed
7.631 km/s
True Right ascension
18h 09m 07s
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
04:10:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.919 km
Perigee altitude
467.853 km
Semi-major axis
6,850.023 km
Eccentricity
0.00059
Inclination
53.0512°
RAAN
272.2815°
Arg. of periapsis
90.666°
True anomaly
269.43403°
Mean anomaly
269.5015°
Eccentric anomaly
269.46777°
Mean motion
3.82829 °/min
Orbital period
94.04 mins
BSTAR
0.0023975
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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 | 2025-11-23 23:30:08.433Z | 254.448° W | 2025-11-23 23:32:08.433Z | 327.364° NNW | 39.036° | 2025-11-23 23:35:08.433Z | 40.641° NE |
| 4 mins | 2025-11-24 04:27:08.433Z | 351.564° N | 2025-11-24 04:28:08.433Z | 12.94° NNE | 19.796° | 2025-11-24 04:31:08.433Z | 73.866° E |
| 5 mins | 2025-11-24 06:05:08.433Z | 293.993° NW | 2025-11-24 06:07:08.433Z | 184.798° SSW | 39.909° | 2025-11-24 06:10:08.433Z | 142.27° SSE |
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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