STARLINK-32914, 63086
Orbit data source: Space-Track
STARLINK-32914, 63086 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 23 Feb 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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63086 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: 16 hours ago
TLE from 16 hours ago
0 STARLINK-32914
1 63086U 25037K 26171.17869045 .00003846 00000-0 32986-3 0 9999
2 63086 70.0011 96.0497 0002651 268.3561 91.7294 14.98338828 73954Epoch: 2026-06-20T04:17Z
TLE epoch observation values (Epoch: 2026-06-20T04:17:18.854Z)
Latitude
-0.00009°
Longitude
123.32407°
Altitude
574.509 km
Speed
7.574 km/s
True Right ascension
06h 24m 11s
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
07:17:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.819 km
Perigee altitude
568.135 km
Semi-major axis
6,948.114 km
Eccentricity
0.00027
Inclination
70.0011°
RAAN
96.0497°
Arg. of periapsis
268.3561°
True anomaly
91.75976°
Mean anomaly
91.7294°
Eccentric anomaly
91.74458°
Mean motion
3.74751 °/min
Orbital period
96.06 mins
BSTAR
0.00032986
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Other satellites on launch #37 in the year 2025 (2025-02-23 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-32914 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-20 20:26:33.827Z | 201.145° SSW | 2026-06-20 20:30:33.827Z | 35.7° NE | 42.953° | 2026-06-20 20:33:33.827Z | 25.711° NE |
| 4 mins | 2026-06-21 04:52:33.827Z | 28.868° NE | 2026-06-21 04:53:33.827Z | 45.547° ENE | 16.173° | 2026-06-21 04:56:33.827Z | 93.035° ESE |
| 5 mins | 2026-06-21 06:30:33.827Z | 306.737° NW | 2026-06-21 06:32:33.827Z | 248.818° W | 34.416° | 2026-06-21 06:35:33.827Z | 184.106° SSW |
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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