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: 1 day ago
TLE from 1 day ago
0 STARLINK-11415
1 62592U 25008F 26197.34014037 .00116192 00000-0 89581-3 0 9990
2 62592 43.0000 71.0589 0001161 275.9727 84.1008 15.70855951 87452Epoch: 2026-07-16T08:09Z
TLE epoch observation values (Epoch: 2026-07-16T08:09:48.127Z)
Latitude
-0.00006°
Longitude
14.4253°
Altitude
356.14 km
Speed
7.697 km/s
True Right ascension
04h 44m 14s
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
21:11:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.213 km
Perigee altitude
357.649 km
Semi-major axis
6,736.568 km
Eccentricity
0.00012
Inclination
43°
RAAN
71.0589°
Arg. of periapsis
275.9727°
True anomaly
84.11403°
Mean anomaly
84.1008°
Eccentric anomaly
84.10742°
Mean motion
3.92541 °/min
Orbital period
91.71 mins
BSTAR
0.00089581
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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 | 2026-07-17 19:31:24.417Z | 244.851° WSW | 2026-07-17 19:32:24.417Z | 233.572° WSW | 41.18° | 2026-07-17 19:35:24.417Z | 73.264° E |
| 4 mins | 2026-07-17 21:07:24.417Z | 293.459° NW | 2026-07-17 21:09:24.417Z | 20.799° NNE | 33.254° | 2026-07-17 21:11:24.417Z | 68.498° E |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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