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STARLINK-1882, 46784

Orbit data source: Space-Track

STARLINK-1882, 46784 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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Iframe URL

https://www.satcat.com/sats-embedded/46784?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

46784, 2020-074AX

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: 3 hours ago

TLE from 3 hours ago

0 STARLINK-1882
1 46784U 20074AX  26127.91668980  .00019598  00000-0  13153-3 0  9995
2 46784  53.0478 342.5810 0000722 239.8581 328.8352 15.75269316  5975

Epoch: 2026-05-07T22:00Z

TLE epoch observation values (Epoch: 2026-05-07T22:00:01.998Z)

Latitude

-22.75284°

Longitude

-14.90008°

Altitude

349.925 km

Speed

7.699 km/s

True Right ascension

12h 03m 27s

True Declination

-22° 37' 23"

Sunlit

Object was in full shadow 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

09:10:36

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

344.63 km

Perigee altitude

343.659 km

Semi-major axis

6,722.282 km

Eccentricity

0.00007

Inclination

53.0478°

RAAN

342.581°

Arg. of periapsis

239.8581°

True anomaly

328.83092°

Mean anomaly

328.8352°

Eccentric anomaly

328.83306°

Mean motion

3.93793 °/min

Orbital period

91.42 mins

BSTAR

0.00013153

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

STARLINK-1946, 46776 (Decayed)

STARLINK-1916, 46766 (Decayed)

FALCON 9 DEB, 46799 (Decayed)

STARLINK-1943, 46795 (Decayed)

STARLINK-1926, 46757 (Decayed)

STARLINK-1935, 46771 (Decayed)

STARLINK-1945, 46775 (Decayed)

STARLINK-1933, 46791 (Decayed)

STARLINK-1925, 46756 (Decayed)

STARLINK-1948, 46798 (Decayed)

STARLINK-1922, 46753

STARLINK-1847, 46739 (Decayed)

STARLINK-1798, 46779 (Decayed)

STARLINK-1942, 46794

FALCON 9 R/B, 46803 (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-1882 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	2026-05-08 17:06:32.239Z	234.02° WSW	2026-05-08 17:08:32.239Z	2.135° NNE	44.292°	2026-05-08 17:10:32.239Z	47.286° ENE

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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-1882, 46784 on other resources

View STARLINK-1882, 46784 on NASA - NSSDCA Website

View STARLINK-1882, 46784 on Heavens-Above

View STARLINK-1882, 46784 on Keep Track

View STARLINK-1882, 46784 on Celestrak

View STARLINK-1882, 46784 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

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