STARLINK-11365, 62886
Orbit data source: Space-Track
STARLINK-11365, 62886 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 04 Feb 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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62886 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MD, Unknown motor
Mass
960 kg wet, ~910 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 18.1 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 STARLINK-11365
1 62886U 25024H 26008.49965060 .00312142 00000-0 23370-2 0 9998
2 62886 42.9997 183.9594 0001971 259.1040 100.9606 15.70930776 54006Epoch: 2026-01-08T11:59Z
TLE epoch observation values (Epoch: 2026-01-08T11:59:29.811Z)
Latitude
-0.00003°
Longitude
-103.96771°
Altitude
356.259 km
Speed
7.697 km/s
True Right ascension
12h 15m 50s
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
08:15:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.545 km
Perigee altitude
356.89 km
Semi-major axis
6,736.354 km
Eccentricity
0.0002
Inclination
42.9997°
RAAN
183.9594°
Arg. of periapsis
259.104°
True anomaly
100.98277°
Mean anomaly
100.9606°
Eccentric anomaly
100.97169°
Mean motion
3.9256 °/min
Orbital period
91.71 mins
BSTAR
0.002337
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Other satellites on launch #24 in the year 2025 (2025-02-04 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-11365 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-01-09 15:43:26.831Z | 250.508° W | 2026-01-09 15:44:26.831Z | 249.34° W | 41.951° | 2026-01-09 15:47:26.831Z | 71.96° E |
| 4 mins | 2026-01-09 17:19:26.831Z | 295.677° NW | 2026-01-09 17:21:26.831Z | 24.113° NE | 32.705° | 2026-01-09 17:23:26.831Z | 69.799° E |
| 4 mins | 2026-01-09 18:55:26.831Z | 292.815° NW | 2026-01-09 18:57:26.831Z | 47.817° ENE | 43.325° | 2026-01-09 18:59:26.831Z | 99.859° ESE |
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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