STARLINK-35226, 65492
Orbit data source: Space-Track
STARLINK-35226, 65492 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 05 Sep 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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65492 intel report (Beta)
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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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-35226
1 65492U 25198A 26171.22053320 .00023623 00000-0 70842-3 0 9995
2 65492 53.1592 152.9363 0000692 50.4272 309.6792 15.34385267 44344Epoch: 2026-06-20T05:17Z
TLE epoch observation values (Epoch: 2026-06-20T05:17:34.068Z)
Latitude
0.00001°
Longitude
165.10608°
Altitude
463.346 km
Speed
7.636 km/s
True Right ascension
10h 11m 44s
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
07:17:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.477 km
Perigee altitude
462.531 km
Semi-major axis
6,841.141 km
Eccentricity
0.00007
Inclination
53.1592°
RAAN
152.9363°
Arg. of periapsis
50.4272°
True anomaly
309.6731°
Mean anomaly
309.6792°
Eccentric anomaly
309.67615°
Mean motion
3.83575 °/min
Orbital period
93.85 mins
BSTAR
0.00070842
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Other satellites on launch #198 in the year 2025 (2025-09-05 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-35226 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 | 2026-06-21 01:49:22.547Z | 247.141° WSW | 2026-06-21 01:51:22.547Z | 317.547° NNW | 41.414° | 2026-06-21 01:54:22.547Z | 42.489° NE |
| 5 mins | 2026-06-21 08:23:22.547Z | 304.501° NW | 2026-06-21 08:25:22.547Z | 214.097° SW | 44.254° | 2026-06-21 08:28:22.547Z | 136.656° SSE |
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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