STARLINK-11613, 63136
Orbit data source: Space-Track
STARLINK-11613, 63136 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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63136 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-11613
1 63136U 25043E 25305.47575880 .00276821 00000-0 20802-2 0 9992
2 63136 42.9988 303.8862 0000750 317.1913 42.8896 15.70949161 39303Epoch: 2025-11-01T11:25Z
TLE epoch observation values (Epoch: 2025-11-01T11:25:05.560Z)
Latitude
-0.00002°
Longitude
91.60771°
Altitude
355.584 km
Speed
7.698 km/s
True Right ascension
20h 15m 32s
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
18:38:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
358.67 km
Perigee altitude
357.66 km
Semi-major axis
6,736.302 km
Eccentricity
0.00008
Inclination
42.9988°
RAAN
303.8862°
Arg. of periapsis
317.1913°
True anomaly
42.89545°
Mean anomaly
42.8896°
Eccentric anomaly
42.89252°
Mean motion
3.92564 °/min
Orbital period
91.7 mins
BSTAR
0.0020802
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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-11613 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 | 2025-11-03 03:18:09.006Z | 230.166° WSW | 2025-11-03 03:21:09.006Z | 128.998° SE | 35.307° | 2025-11-03 03:23:09.006Z | 81.874° E |
| 4 mins | 2025-11-03 04:55:09.006Z | 282.83° WNW | 2025-11-03 04:57:09.006Z | 14.585° NNE | 36.103° | 2025-11-03 04:59:09.006Z | 65.703° ENE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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