STARLINK-11610, 63135
Orbit data source: Space-Track
STARLINK-11610, 63135 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 03 Mar 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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63135 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-11610
1 63135U 25043D 26170.66668981 -.00202548 00000-0 -16073-2 0 9990
2 63135 43.0004 356.2925 0001557 260.1888 242.4881 15.70933169 6003Epoch: 2026-06-19T16:00Z
TLE epoch observation values (Epoch: 2026-06-19T16:00:01.999Z)
Latitude
24.52259°
Longitude
-0.71657°
Altitude
356.5 km
Speed
7.699 km/s
True Right ascension
09h 48m 44s
True Declination
24° 23' 07"
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
07:21:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.259 km
Perigee altitude
357.162 km
Semi-major axis
6,736.347 km
Eccentricity
0.00016
Inclination
43.0004°
RAAN
356.2925°
Arg. of periapsis
260.1888°
True anomaly
242.47228°
Mean anomaly
242.4881°
Eccentric anomaly
242.48019°
Mean motion
3.9256 °/min
Orbital period
91.71 mins
BSTAR
-0.0016073
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Other satellites on launch #43 in the year 2025 (2025-03-03 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-11610 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 20:51:22.221Z | 274.954° WNW | 2026-06-20 20:53:22.221Z | 223.956° SW | 32.773° | 2026-06-20 20:56:22.221Z | 134.549° SE |
| 4 mins | 2026-06-21 16:31:22.221Z | 265.118° W | 2026-06-21 16:33:22.221Z | 31.936° NE | 41.176° | 2026-06-21 16:35:22.221Z | 68.034° E |
| 4 mins | 2026-06-21 19:44:22.221Z | 285.233° WNW | 2026-06-21 19:45:22.221Z | 273.293° WNW | 42.546° | 2026-06-21 19:48:22.221Z | 112.16° 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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