STARLINK-34055, 63819
Orbit data source: Space-Track
STARLINK-34055, 63819 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 04 May 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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63819 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 17.7 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-34055
1 63819U 25092R 26087.01173984 .00039089 00000-0 14216-2 0 9996
2 63819 43.0028 69.3187 0001665 278.6037 81.4626 15.27598767 51416Epoch: 2026-03-28T00:16Z
TLE epoch observation values (Epoch: 2026-03-28T00:16:54.322Z)
Latitude
-0°
Longitude
-120.34575°
Altitude
482.599 km
Speed
7.626 km/s
True Right ascension
04h 37m 16s
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
06:58:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.08 km
Perigee altitude
483.795 km
Semi-major axis
6,863.075 km
Eccentricity
0.00017
Inclination
43.0028°
RAAN
69.3187°
Arg. of periapsis
278.6037°
True anomaly
81.48147°
Mean anomaly
81.4626°
Eccentric anomaly
81.47203°
Mean motion
3.81738 °/min
Orbital period
94.31 mins
BSTAR
0.0014216
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Other satellites on launch #92 in the year 2025 (2025-05-04 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-34055 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 | 2026-03-29 01:34:58.553Z | 205.609° SW | 2026-03-29 01:37:58.553Z | 143.297° SSE | 25.735° | 2026-03-29 01:40:58.553Z | 87.935° E |
| 6 mins | 2026-03-29 03:13:58.553Z | 259.071° W | 2026-03-29 03:16:58.553Z | 43.434° NE | 42.52° | 2026-03-29 03:19:58.553Z | 70.688° E |
| 5 mins | 2026-03-29 04:53:58.553Z | 297.614° NW | 2026-03-29 04:55:58.553Z | 17.605° NNE | 37.697° | 2026-03-29 04:58:58.553Z | 77.982° E |
| 5 mins | 2026-03-29 06:32:58.553Z | 286.222° WNW | 2026-03-29 06:34:58.553Z | 149.092° SSE | 44.684° | 2026-03-29 06:37:58.553Z | 112.099° ESE |
| 4 mins | 2026-03-29 08:11:58.553Z | 246.405° WSW | 2026-03-29 08:12:58.553Z | 226.216° WSW | 18.963° | 2026-03-29 08:15:58.553Z | 169.131° S |
| 5 mins | 2026-03-30 01:07:58.553Z | 194.629° SSW | 2026-03-30 01:09:58.553Z | 147.273° SSE | 25.235° | 2026-03-30 01:12:58.553Z | 89.416° E |
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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