STARLINK-34048, 63816
Orbit data source: Space-Track
STARLINK-34048, 63816 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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63816 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 STARLINK-34048
1 63816U 25092N 25291.29569885 .00035534 00000-0 12925-2 0 9994
2 63816 43.0042 257.0361 0001703 270.9154 89.1503 15.27633740 26880Epoch: 2025-10-18T07:05Z
TLE epoch observation values (Epoch: 2025-10-18T07:05:48.380Z)
Latitude
0°
Longitude
123.55576°
Altitude
482.647 km
Speed
7.626 km/s
True Right ascension
17h 08m 08s
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
09:21:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.001 km
Perigee altitude
483.664 km
Semi-major axis
6,862.97 km
Eccentricity
0.00017
Inclination
43.0042°
RAAN
257.0361°
Arg. of periapsis
270.9154°
True anomaly
89.16981°
Mean anomaly
89.1503°
Eccentric anomaly
89.16006°
Mean motion
3.81746 °/min
Orbital period
94.3 mins
BSTAR
0.0012925
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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-34048 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 | 2025-10-19 00:33:01.679Z | 191.041° SSW | 2025-10-19 00:35:01.679Z | 152.374° SSE | 21.081° | 2025-10-19 00:38:01.679Z | 94.96° ESE |
| 5 mins | 2025-10-19 02:12:01.679Z | 251.45° W | 2025-10-19 02:14:01.679Z | 65.403° ENE | 44.891° | 2025-10-19 02:17:01.679Z | 71.79° E |
| 5 mins | 2025-10-19 03:51:01.679Z | 291.79° WNW | 2025-10-19 03:53:01.679Z | 356.785° N | 37.992° | 2025-10-19 03:56:01.679Z | 73.595° E |
| 5 mins | 2025-10-19 05:30:01.679Z | 290.465° WNW | 2025-10-19 05:32:01.679Z | 324.189° NNW | 44.329° | 2025-10-19 05:35:01.679Z | 104.553° ESE |
| 5 mins | 2025-10-19 07:09:01.679Z | 256.425° W | 2025-10-19 07:11:01.679Z | 209.814° SW | 23.712° | 2025-10-19 07:14:01.679Z | 155.636° SSE |
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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