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
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, 4.4 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 STARLINK-1728
1 46582U 20070BC 25259.57657033 -.00001164 00000-0 -59232-4 0 9992
2 46582 53.0536 218.2403 0001920 93.3490 266.7719 15.06394738273544Epoch: 2025-09-16T13:50Z
TLE epoch observation values (Epoch: 2025-09-16T13:50:15.676Z)
Latitude
0.00001°
Longitude
14.9101°
Altitude
548.182 km
Speed
7.589 km/s
True Right ascension
14h 32m 57s
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
01:51:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
548.828 km
Perigee altitude
546.169 km
Semi-major axis
6,925.636 km
Eccentricity
0.00019
Inclination
53.0536°
RAAN
218.2403°
Arg. of periapsis
93.349°
True anomaly
266.74993°
Mean anomaly
266.7719°
Eccentric anomaly
266.76092°
Mean motion
3.76577 °/min
Orbital period
95.6 mins
BSTAR
-0.000059232
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-17 23:26:28.081Z | 210.421° SW | 2025-09-17 23:29:28.081Z | 154.436° SSE | 38.56° | 2025-09-17 23:33:28.081Z | 59.123° ENE |
| 5 mins | 2025-09-18 01:07:28.081Z | 289.396° WNW | 2025-09-18 01:09:28.081Z | 332.787° NNW | 24.752° | 2025-09-18 01:12:28.081Z | 28.487° NE |
| 4 mins | 2025-09-18 04:29:28.081Z | 349.393° N | 2025-09-18 04:31:28.081Z | 24.5° NE | 16.066° | 2025-09-18 04:33:28.081Z | 55.06° ENE |
| 6 mins | 2025-09-18 06:08:28.081Z | 321.914° NNW | 2025-09-18 06:11:28.081Z | 49.878° ENE | 39.227° | 2025-09-18 06:14:28.081Z | 111.835° ESE |
| 5 mins | 2025-09-18 07:48:28.081Z | 268.376° W | 2025-09-18 07:50:28.081Z | 231.953° WSW | 19.268° | 2025-09-18 07:53:28.081Z | 183.87° SSW |
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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