STARLINK-1705, 46579
Orbit data source: Space-Track
STARLINK-1705, 46579 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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46579 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: 5 hours ago
TLE from 5 hours ago
0 STARLINK-1705
1 46579U 20070AZ 25286.66667824 .00188943 00000-0 30021-2 0 9999
2 46579 53.0502 81.8775 0008684 223.2329 230.4573 15.52142695 5901Epoch: 2025-10-13T16:00Z
TLE epoch observation values (Epoch: 2025-10-13T16:00:00.999Z)
Latitude
53.0525°
Longitude
-84.58875°
Altitude
420.72 km
Speed
7.663 km/s
True Right ascension
11h 51m 31s
True Declination
52° 52' 44"
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
15:16:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
416.643 km
Perigee altitude
404.852 km
Semi-major axis
6,788.885 km
Eccentricity
0.00087
Inclination
53.0502°
RAAN
81.8775°
Arg. of periapsis
223.2329°
True anomaly
230.38061°
Mean anomaly
230.4573°
Eccentric anomaly
230.41895°
Mean motion
3.88012 °/min
Orbital period
92.78 mins
BSTAR
0.0030021
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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-1705 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 | 2025-10-13 20:46:42.922Z | 271.648° WNW | 2025-10-13 20:47:42.922Z | 228.38° WSW | 33.632° | 2025-10-13 20:50:42.922Z | 154.084° SSE |
| 4 mins | 2025-10-14 13:26:42.922Z | 250.009° W | 2025-10-14 13:27:42.922Z | 277.97° WNW | 39.075° | 2025-10-14 13:30:42.922Z | 42.162° NE |
| 4 mins | 2025-10-14 19:55:42.922Z | 308.323° NW | 2025-10-14 19:57:42.922Z | 139.769° SSE | 42.89° | 2025-10-14 19:59:42.922Z | 132.382° SE |
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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