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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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 26068.58575256 .00073856 00000-0 57319-3 0 9995
2 62886 42.9993 181.7792 0001911 281.1969 78.8684 15.70871886 63451Epoch: 2026-03-09T14:03Z
TLE epoch observation values (Epoch: 2026-03-09T14:03:29.021Z)
Latitude
0.00001°
Longitude
163.63171°
Altitude
355.927 km
Speed
7.698 km/s
True Right ascension
12h 07m 07s
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
14:17:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.673 km
Perigee altitude
357.098 km
Semi-major axis
6,736.523 km
Eccentricity
0.00019
Inclination
42.9993°
RAAN
181.7792°
Arg. of periapsis
281.1969°
True anomaly
78.88989°
Mean anomaly
78.8684°
Eccentric anomaly
78.87914°
Mean motion
3.92545 °/min
Orbital period
91.71 mins
BSTAR
0.00057319
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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 | 2026-03-10 11:41:32.538Z | 247.321° WSW | 2026-03-10 11:42:32.538Z | 236.005° WSW | 43.416° | 2026-03-10 11:45:32.538Z | 72.547° E |
| 4 mins | 2026-03-10 13:17:32.538Z | 296.32° NW | 2026-03-10 13:19:32.538Z | 28.546° NE | 32.118° | 2026-03-10 13:21:32.538Z | 69.956° E |
| 4 mins | 2026-03-10 14:53:32.538Z | 293.792° NW | 2026-03-10 14:55:32.538Z | 49° ENE | 42.617° | 2026-03-10 14:57:32.538Z | 98.224° 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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