STARLINK-11415, 62592
Orbit data source: Space-Track
STARLINK-11415, 62592 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 13 Jan 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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62592 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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-11415
1 62592U 25008F 26300.75002315 .01240687 00000-0 87091-2 0 9998
2 62592 42.9997 167.7352 0001489 255.0260 239.0092 15.70736521 5961Epoch: 2026-10-27T18:00Z
TLE epoch observation values (Epoch: 2026-10-27T18:00:02.000Z)
Latitude
29.48015°
Longitude
4.54542°
Altitude
357.781 km
Speed
7.699 km/s
True Right ascension
20h 42m 38s
True Declination
29° 19' 28"
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
01:27:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.776 km
Perigee altitude
357.769 km
Semi-major axis
6,736.909 km
Eccentricity
0.00015
Inclination
42.9997°
RAAN
167.7352°
Arg. of periapsis
255.026°
True anomaly
238.99457°
Mean anomaly
239.0092°
Eccentric anomaly
239.00189°
Mean motion
3.92511 °/min
Orbital period
91.72 mins
BSTAR
0.0087091
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Other satellites on launch #8 in the year 2025 (2025-01-13 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-11415 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 | 2026-10-28 18:01:36.237Z | 197.245° SSW | 2026-10-28 18:03:36.237Z | 153.723° SSE | 20.021° | 2026-10-28 18:05:36.237Z | 103.432° ESE |
| 4 mins | 2026-10-28 19:37:36.237Z | 256.987° W | 2026-10-28 19:39:36.237Z | 7.847° NNE | 78.202° | 2026-10-28 19:41:36.237Z | 69.021° E |
| 4 mins | 2026-10-28 22:50:36.237Z | 293.603° NW | 2026-10-28 22:51:36.237Z | 323.143° NNW | 73.987° | 2026-10-28 22:54:36.237Z | 105.131° 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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