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: 23 hours ago
TLE from 23 hours ago
0 STARLINK-11610
1 63135U 25043D 26306.41668981 -.00066323 00000-0 -49988-3 0 9995
2 63135 43.0000 257.9257 0001568 254.9179 289.8960 15.71658226 6013Epoch: 2026-11-02T10:00Z
TLE epoch observation values (Epoch: 2026-11-02T10:00:01.999Z)
Latitude
-3.34861°
Longitude
-110.19948°
Altitude
354.065 km
Speed
7.699 km/s
True Right ascension
05h 26m 00s
True Declination
-3° 19' 39"
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
04:55:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
357.196 km
Perigee altitude
355.084 km
Semi-major axis
6,734.277 km
Eccentricity
0.00016
Inclination
43°
RAAN
257.9257°
Arg. of periapsis
254.9179°
True anomaly
289.8791°
Mean anomaly
289.896°
Eccentric anomaly
289.88755°
Mean motion
3.92741 °/min
Orbital period
91.66 mins
BSTAR
-0.00049988
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-03 23:33:30.059Z | 195.249° SSW | 2026-11-03 23:35:30.059Z | 139.282° SSE | 23.482° | 2026-11-03 23:37:30.059Z | 94.454° ESE |
| 4 mins | 2026-11-04 01:09:30.059Z | 263.768° W | 2026-11-04 01:11:30.059Z | 39.106° NE | 59.456° | 2026-11-04 01:13:30.059Z | 68.238° E |
| 4 mins | 2026-11-04 04:22:30.059Z | 288.424° WNW | 2026-11-04 04:23:30.059Z | 285.85° WNW | 81.739° | 2026-11-04 04:26:30.059Z | 109.505° 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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