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STARLINK-1928, 46758

Orbit data source: Space-Track

STARLINK-1928, 46758 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 24 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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https://www.satcat.com/sats-embedded/46758?theme=dark&initialShowStats=false

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Identifier

46758, 2020-074V

Orbit

LEO

Country

US

Related business

Manufacturer

SpaceX/Seattle

Mission

Partially operational Commercial Communications

Bus & Motor

STARLINK, Unknown motor

Mass

260 kg wet, ~248 kg dry

Launch date (UTC)

2020-10-24 (6 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 1 Pan, 10.1 m

Radar Cross Section

13.562 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago

0 STARLINK-1928
1 46758U 20074V   26126.33335648  .00102114  00000-0  51154-3 0  9993
2 46758  53.0417 358.2171 0006881 180.0927 227.5659 15.80978273  6001

Epoch: 2026-05-06T08:00Z

TLE epoch observation values (Epoch: 2026-05-06T08:00:01.999Z)

Latitude

36.28308°

Longitude

47.32898°

Altitude

333.598 km

Speed

7.711 km/s

True Right ascension

02h 06m 07s

True Declination

36° 06' 32"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

22:28:35

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

332.569 km

Perigee altitude

323.34 km

Semi-major axis

6,706.091 km

Eccentricity

0.00069

Inclination

53.0417°

RAAN

358.2171°

Arg. of periapsis

180.0927°

True anomaly

227.50774°

Mean anomaly

227.5659°

Eccentric anomaly

227.53682°

Mean motion

3.9522 °/min

Orbital period

91.09 mins

BSTAR

0.00051154

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Other satellites on launch #74 in the year 2020 (2020-10-24 UTC)

STARLINK-1833, 46759 (Decayed)

STARLINK-1917, 46767 (Decayed)

STARLINK-1933, 46791 (Decayed)

STARLINK-1883, 46785 (Decayed)

STARLINK-1851, 46783 (Decayed)

STARLINK-1930, 46789 (Decayed)

STARLINK-1908, 46747 (Decayed)

STARLINK-1925, 46756 (Decayed)

STARLINK-1937, 46773 (Decayed)

STARLINK-1910, 46748 (Decayed)

STARLINK-1902, 46763 (Decayed)

STARLINK-1947, 46797 (Decayed)

STARLINK-1948, 46798 (Decayed)

STARLINK-1946, 46776 (Decayed)

STARLINK-1798, 46779 (Decayed)

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

STARLINK-1928 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	2026-05-06 18:37:12.215Z	246.528° WSW	2026-05-06 18:39:12.215Z	307.627° NW	38.376°	2026-05-06 18:41:12.215Z	36.811° NE

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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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Check out STARLINK-1928, 46758 on other resources

View STARLINK-1928, 46758 on NASA - NSSDCA Website

View STARLINK-1928, 46758 on Heavens-Above

View STARLINK-1928, 46758 on Keep Track

View STARLINK-1928, 46758 on Celestrak

View STARLINK-1928, 46758 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

Go to standalone docs website

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