STARLINK-32804, 62846
Orbit data source: Space-Track
STARLINK-32804, 62846 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 27 Jan 2025 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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62846 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: 8 hours ago
TLE from 8 hours ago
0 STARLINK-32804
1 62846U 25019T 26069.10239543 .00024154 00000-0 88410-3 0 9993
2 62846 43.0009 86.6828 0001171 196.3825 163.6989 15.27590591 62314Epoch: 2026-03-10T02:27Z
TLE epoch observation values (Epoch: 2026-03-10T02:27:26.965Z)
Latitude
-0°
Longitude
-117.96536°
Altitude
483.564 km
Speed
7.625 km/s
True Right ascension
05h 46m 43s
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
14:52:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.766 km
Perigee altitude
484.159 km
Semi-major axis
6,863.099 km
Eccentricity
0.00012
Inclination
43.0009°
RAAN
86.6828°
Arg. of periapsis
196.3825°
True anomaly
163.70267°
Mean anomaly
163.6989°
Eccentric anomaly
163.70078°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.0008841
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Other satellites on launch #19 in the year 2025 (2025-01-27 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-32804 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-10 10:49:23.093Z | 256.415° W | 2026-03-10 10:51:23.093Z | 214.262° SW | 21.536° | 2026-03-10 10:54:23.093Z | 160.391° S |
| 4 mins | 2026-03-11 03:46:23.093Z | 183.999° SSW | 2026-03-11 03:48:23.093Z | 135.424° SSE | 22.45° | 2026-03-11 03:50:23.093Z | 97.337° ESE |
| 6 mins | 2026-03-11 05:24:23.093Z | 254.582° W | 2026-03-11 05:26:23.093Z | 272.64° WNW | 44.043° | 2026-03-11 05:30:23.093Z | 71.567° E |
| 6 mins | 2026-03-11 07:03:23.093Z | 289.385° WNW | 2026-03-11 07:05:23.093Z | 334.19° NNW | 36.695° | 2026-03-11 07:09:23.093Z | 77.481° E |
| 6 mins | 2026-03-11 08:42:23.093Z | 288.861° WNW | 2026-03-11 08:45:23.093Z | 100.667° ESE | 42.883° | 2026-03-11 08:48:23.093Z | 107.657° ESE |
| 4 mins | 2026-03-11 10:22:23.093Z | 243.505° WSW | 2026-03-11 10:23:23.093Z | 219.874° SW | 21.905° | 2026-03-11 10:26:23.093Z | 161.658° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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