STARLINK-32844, 62820
Orbit data source: Space-Track
STARLINK-32844, 62820 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 24 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62820 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 STARLINK-32844
1 62820U 25018Q 26255.12927036 .00013566 00000-0 44787-3 0 9998
2 62820 53.1598 162.1472 0001203 78.0498 282.0638 15.31718987 91735Epoch: 2026-09-12T03:06Z
TLE epoch observation values (Epoch: 2026-09-12T03:06:08.959Z)
Latitude
-0.00002°
Longitude
124.46715°
Altitude
471.412 km
Speed
7.632 km/s
True Right ascension
10h 48m 35s
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
00:48:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.764 km
Perigee altitude
470.116 km
Semi-major axis
6,849.077 km
Eccentricity
0.00012
Inclination
53.1598°
RAAN
162.1472°
Arg. of periapsis
78.0498°
True anomaly
282.05032°
Mean anomaly
282.0638°
Eccentric anomaly
282.05706°
Mean motion
3.82909 °/min
Orbital period
94.02 mins
BSTAR
0.00044787
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Other satellites on launch #18 in the year 2025 (2025-01-24 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-32844 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-12 20:29:53.014Z | 222.213° SW | 2026-09-12 20:32:53.014Z | 182.394° SSW | 68.321° | 2026-09-12 20:35:53.014Z | 54.636° ENE |
| 4 mins | 2026-09-12 22:09:53.014Z | 304.898° NW | 2026-09-12 22:10:53.014Z | 325.476° NNW | 19.769° | 2026-09-12 22:13:53.014Z | 22.935° NE |
| 5 mins | 2026-09-13 03:05:53.014Z | 324.518° NNW | 2026-09-13 03:07:53.014Z | 40.88° NE | 59.568° | 2026-09-13 03:10:53.014Z | 116.281° 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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