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: 17 hours ago
TLE from 17 hours ago
0 STARLINK-1728
1 46582U 20070BC 26038.92416816 .00116961 00000-0 22985-2 0 9992
2 46582 53.0449 268.1347 0010617 104.3021 255.9165 15.46375604295616Epoch: 2026-02-07T22:10Z
TLE epoch observation values (Epoch: 2026-02-07T22:10:48.129Z)
Latitude
0.00001°
Longitude
157.39346°
Altitude
429.998 km
Speed
7.654 km/s
True Right ascension
17h 52m 32s
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
17:25:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.842 km
Perigee altitude
420.39 km
Semi-major axis
6,805.753 km
Eccentricity
0.00106
Inclination
53.0449°
RAAN
268.1347°
Arg. of periapsis
104.3021°
True anomaly
255.79853°
Mean anomaly
255.9165°
Eccentric anomaly
255.85751°
Mean motion
3.86571 °/min
Orbital period
93.13 mins
BSTAR
0.0022985
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-08 16:57:35.431Z | 168.937° S | 2026-02-08 16:59:35.431Z | 120.749° SE | 19.817° | 2026-02-08 17:01:35.431Z | 81.727° E |
| 4 mins | 2026-02-08 18:34:35.431Z | 277.537° WNW | 2026-02-08 18:35:35.431Z | 310.946° NW | 31.017° | 2026-02-08 18:38:35.431Z | 33.657° NE |
| 5 mins | 2026-02-09 01:04:35.431Z | 288.91° WNW | 2026-02-09 01:06:35.431Z | 217.467° SW | 35.375° | 2026-02-09 01:09:35.431Z | 151.113° 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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