STARLINK-35157, 65814
Orbit data source: Space-Track
STARLINK-35157, 65814 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Fri, 26 Sep 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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65814 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
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STARLINK-35157
1 65814U 25218Z 26062.50013755 .00005269 00000-0 36905-3 0 9992
2 65814 97.6019 286.9363 0001968 80.4735 279.6714 15.05655077 24043Epoch: 2026-03-03T12:00Z
TLE epoch observation values (Epoch: 2026-03-03T12:00:11.884Z)
Latitude
-0.00003°
Longitude
-54.39152°
Altitude
552.332 km
Speed
7.586 km/s
True Right ascension
19h 07m 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
00:36:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
547.852 km
Perigee altitude
545.126 km
Semi-major axis
6,924.626 km
Eccentricity
0.0002
Inclination
97.6019°
RAAN
286.9363°
Arg. of periapsis
80.4735°
True anomaly
279.64917°
Mean anomaly
279.6714°
Eccentric anomaly
279.66028°
Mean motion
3.76659 °/min
Orbital period
95.58 mins
BSTAR
0.00036905
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Other satellites on launch #218 in the year 2025 (2025-09-26 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-35157 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 | 2026-03-04 02:56:05.982Z | 45.264° ENE | 2026-03-04 02:59:05.982Z | 98.03° ESE | 20.284° | 2026-03-04 03:01:05.982Z | 135.938° SSE |
| 4 mins | 2026-03-04 04:32:05.982Z | 324.856° NNW | 2026-03-04 04:34:05.982Z | 277.898° WNW | 22.587° | 2026-03-04 04:36:05.982Z | 241.636° WSW |
| 6 mins | 2026-03-04 15:15:05.982Z | 191.924° SSW | 2026-03-04 15:17:05.982Z | 235.036° WSW | 35.826° | 2026-03-04 15:21:05.982Z | 335.372° NNW |
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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