STARLINK-32136, 61515
Orbit data source: Space-Track
STARLINK-32136, 61515 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 15 Oct 2024 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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61515 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 STARLINK-32136
1 61515U 24183G 26170.88310575 .00000464 00000-0 26726-4 0 9990
2 61515 53.1622 27.4331 0001202 99.2845 260.8292 15.31705751 95302Epoch: 2026-06-19T21:11Z
TLE epoch observation values (Epoch: 2026-06-19T21:11:40.336Z)
Latitude
-0.00007°
Longitude
161.40928°
Altitude
471.755 km
Speed
7.631 km/s
True Right ascension
01h 49m 43s
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
07:24:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.802 km
Perigee altitude
470.156 km
Semi-major axis
6,849.116 km
Eccentricity
0.00012
Inclination
53.1622°
RAAN
27.4331°
Arg. of periapsis
99.2845°
True anomaly
260.8156°
Mean anomaly
260.8292°
Eccentric anomaly
260.8224°
Mean motion
3.82905 °/min
Orbital period
94.02 mins
BSTAR
0.000026726
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Other satellites on launch #183 in the year 2024 (2024-10-15 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-32136 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 | 2026-06-20 22:43:46.240Z | 356.081° N | 2026-06-20 22:44:46.240Z | 20.633° NNE | 22.248° | 2026-06-20 22:47:46.240Z | 81.215° E |
| 5 mins | 2026-06-21 00:20:46.240Z | 293.176° NW | 2026-06-21 00:22:46.240Z | 238.965° WSW | 37.156° | 2026-06-21 00:25:46.240Z | 152.216° SSE |
| 5 mins | 2026-06-21 17:15:46.240Z | 259.456° W | 2026-06-21 17:17:46.240Z | 344.894° N | 37.464° | 2026-06-21 17:20:46.240Z | 40.893° NE |
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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