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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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: 1 day ago
TLE from 1 day ago
0 STARLINK-11415
1 62592U 25008F 26030.05283371 .00242253 00000-0 18379-2 0 9997
2 62592 42.9992 359.4138 0001405 258.0359 102.0351 15.70827064 61140Epoch: 2026-01-30T01:16Z
TLE epoch observation values (Epoch: 2026-01-30T01:16:04.832Z)
Latitude
-0.00003°
Longitude
-148.90307°
Altitude
356.5 km
Speed
7.697 km/s
True Right ascension
23h 57m 39s
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
07:02:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.46 km
Perigee altitude
357.567 km
Semi-major axis
6,736.651 km
Eccentricity
0.00014
Inclination
42.9992°
RAAN
359.4138°
Arg. of periapsis
258.0359°
True anomaly
102.05085°
Mean anomaly
102.0351°
Eccentric anomaly
102.04297°
Mean motion
3.92534 °/min
Orbital period
91.71 mins
BSTAR
0.0018379
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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 | 2026-01-31 06:44:28.068Z | 265.577° W | 2026-01-31 06:46:28.068Z | 216.746° SW | 23.371° | 2026-01-31 06:48:28.068Z | 159.902° S |
| 4 mins | 2026-02-01 00:47:28.068Z | 213.013° SW | 2026-02-01 00:49:28.068Z | 131.943° SE | 31.054° | 2026-02-01 00:51:28.068Z | 85.171° E |
| 4 mins | 2026-02-01 02:23:28.068Z | 278.83° WNW | 2026-02-01 02:25:28.068Z | 21.406° NNE | 37.01° | 2026-02-01 02:27:28.068Z | 66.237° 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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