STARLINK-34896, 66288
Orbit data source: Space-Track
STARLINK-34896, 66288 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 31 Oct 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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66288 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: 22 hours ago
TLE from 22 hours ago
0 STARLINK-34896
1 66288U 25247Z 26170.93949451 .00028241 00000-0 84293-3 0 9996
2 66288 53.1589 74.7226 0001303 116.2328 243.8809 15.34433595 36714Epoch: 2026-06-19T22:32Z
TLE epoch observation values (Epoch: 2026-06-19T22:32:52.325Z)
Latitude
-0°
Longitude
-171.6567°
Altitude
463.897 km
Speed
7.636 km/s
True Right ascension
04h 58m 53s
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
07:15:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.752 km
Perigee altitude
461.969 km
Semi-major axis
6,840.997 km
Eccentricity
0.00013
Inclination
53.1589°
RAAN
74.7226°
Arg. of periapsis
116.2328°
True anomaly
243.86749°
Mean anomaly
243.8809°
Eccentric anomaly
243.8742°
Mean motion
3.83587 °/min
Orbital period
93.85 mins
BSTAR
0.00084293
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Other satellites on launch #247 in the year 2025 (2025-10-31 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-34896 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 | 2026-06-20 20:37:27.858Z | 243.577° WSW | 2026-06-20 20:40:27.858Z | 313.115° NW | 40.463° | 2026-06-20 20:43:27.858Z | 41.321° NE |
| 5 mins | 2026-06-21 03:12:27.858Z | 302.815° NW | 2026-06-21 03:14:27.858Z | 222.573° SW | 43.724° | 2026-06-21 03:17:27.858Z | 138.551° SSE |
| 6 mins | 2026-06-21 20:04:27.858Z | 236.649° WSW | 2026-06-21 20:06:27.858Z | 260.333° W | 41.504° | 2026-06-21 20:10:27.858Z | 47.211° ENE |
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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