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: 1 day ago
TLE from 1 day ago
0 STARLINK-11260
1 60997U 24158H 26036.09771318 -.00000079 00000-0 42058-5 0 9995
2 60997 53.1587 59.7721 0001148 64.1324 295.9812 15.69709204 82837Epoch: 2026-02-05T02:20Z
TLE epoch observation values (Epoch: 2026-02-05T02:20:42.418Z)
Latitude
-0.00005°
Longitude
-110.65951°
Altitude
360.305 km
Speed
7.695 km/s
True Right ascension
03h 59m 05s
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
06:31:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.763 km
Perigee altitude
359.216 km
Semi-major axis
6,738.127 km
Eccentricity
0.00011
Inclination
53.1587°
RAAN
59.7721°
Arg. of periapsis
64.1324°
True anomaly
295.96937°
Mean anomaly
295.9812°
Eccentric anomaly
295.97529°
Mean motion
3.92405 °/min
Orbital period
91.74 mins
BSTAR
0.0000042058
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-06 04:31:58.224Z | 256.371° W | 2026-02-06 04:33:58.224Z | 331.127° NNW | 34.967° | 2026-02-06 04:35:58.224Z | 33.702° NE |
| 4 mins | 2026-02-06 10:56:58.224Z | 303.416° NW | 2026-02-06 10:58:58.224Z | 161.311° S | 40.983° | 2026-02-06 11:00:58.224Z | 137.338° SSE |
| 4 mins | 2026-02-07 03:25:58.224Z | 205.839° SW | 2026-02-07 03:27:58.224Z | 95.851° ESE | 35.858° | 2026-02-07 03:29:58.224Z | 59.812° ENE |
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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