STARLINK-11260, 60997
Orbit data source: Space-Track
STARLINK-11260, 60997 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 05 Sep 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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60997 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: 9 hours ago
TLE from 9 hours ago
0 STARLINK-11260
1 60997U 24158H 26001.90728235 -.00001732 00000-0 -94465-5 0 9994
2 60997 53.1600 228.3144 0000819 94.9721 265.1391 15.69714408 77468Epoch: 2026-01-01T21:46Z
TLE epoch observation values (Epoch: 2026-01-01T21:46:29.195Z)
Latitude
0.00005°
Longitude
160.13767°
Altitude
360.676 km
Speed
7.694 km/s
True Right ascension
15h 13m 15s
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
06:10:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.527 km
Perigee altitude
359.423 km
Semi-major axis
6,738.112 km
Eccentricity
0.00008
Inclination
53.16°
RAAN
228.3144°
Arg. of periapsis
94.9721°
True anomaly
265.12975°
Mean anomaly
265.1391°
Eccentric anomaly
265.13442°
Mean motion
3.92406 °/min
Orbital period
91.74 mins
BSTAR
-0.0000094465
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Other satellites on launch #158 in the year 2024 (2024-09-05 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-11260 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 | 2026-01-02 17:49:26.424Z | 236.789° WSW | 2026-01-02 17:52:26.424Z | 350.474° N | 42.519° | 2026-01-02 17:54:26.424Z | 43.589° NE |
| 4 mins | 2026-01-03 00:15:26.424Z | 319.41° NNW | 2026-01-03 00:17:26.424Z | 94.793° ESE | 39.768° | 2026-01-03 00:19:26.424Z | 122.352° SE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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