STARLINK-34283, 64214
Orbit data source: Space-Track
STARLINK-34283, 64214 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 31 May 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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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: 1 day ago
TLE from 1 day ago
0 STARLINK-34283
1 64214U 25117M 26170.58696867 .00027992 00000-0 83638-3 0 9994
2 64214 53.1609 284.3926 0000765 61.8005 298.3075 15.34404820 60152Epoch: 2026-06-19T14:05Z
TLE epoch observation values (Epoch: 2026-06-19T14:05:14.093Z)
Latitude
0.00002°
Longitude
165.27008°
Altitude
463.342 km
Speed
7.636 km/s
True Right ascension
18h 57m 34s
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
07:22:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.469 km
Perigee altitude
462.422 km
Semi-major axis
6,841.083 km
Eccentricity
0.00008
Inclination
53.1609°
RAAN
284.3926°
Arg. of periapsis
61.8005°
True anomaly
298.29978°
Mean anomaly
298.3075°
Eccentric anomaly
298.30364°
Mean motion
3.8358 °/min
Orbital period
93.85 mins
BSTAR
0.00083638
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Other satellites on launch #117 in the year 2025 (2025-05-31 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-34283 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 | 2026-06-21 10:02:57.464Z | 233.925° WSW | 2026-06-21 10:04:57.464Z | 249.776° W | 41.806° | 2026-06-21 10:08:57.464Z | 48.207° ENE |
| 5 mins | 2026-06-21 16:36:57.464Z | 313.03° NW | 2026-06-21 16:38:57.464Z | 331.047° NNW | 42.718° | 2026-06-21 16:41:57.464Z | 126.669° SE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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