STARLINK-11157, 60122
Orbit data source: Space-Track
STARLINK-11157, 60122 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 24 Jun 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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60122 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, 14.5 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-11157
1 60122U 24118K 25260.49432642 -.00001507 00000-0 -75812-5 0 9999
2 60122 53.1588 354.8567 0001063 92.6874 267.4266 15.69709846 70798Epoch: 2025-09-17T11:51Z
TLE epoch observation values (Epoch: 2025-09-17T11:51:49.802Z)
Latitude
0°
Longitude
-179.77028°
Altitude
360.674 km
Speed
7.694 km/s
True Right ascension
23h 39m 25s
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
08:54:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.704 km
Perigee altitude
359.272 km
Semi-major axis
6,738.125 km
Eccentricity
0.00011
Inclination
53.1588°
RAAN
354.8567°
Arg. of periapsis
92.6874°
True anomaly
267.41443°
Mean anomaly
267.4266°
Eccentric anomaly
267.42052°
Mean motion
3.92405 °/min
Orbital period
91.74 mins
BSTAR
-0.0000075812
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Other satellites on launch #118 in the year 2024 (2024-06-24 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-11157 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 | 2025-09-19 08:21:11.566Z | 209.153° SW | 2025-09-19 08:23:11.566Z | 156.213° SSE | 36.411° | 2025-09-19 08:26:11.566Z | 60.278° 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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