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: 20 hours ago
TLE from 20 hours ago
0 STARLINK-11260
1 60997U 24158H 25290.44040752 -.00001451 00000-0 -71178-5 0 9997
2 60997 53.1584 245.2743 0001127 117.5901 242.5232 15.69719798 65453Epoch: 2025-10-17T10:34Z
TLE epoch observation values (Epoch: 2025-10-17T10:34:11.209Z)
Latitude
0.00001°
Longitude
60.54186°
Altitude
360.964 km
Speed
7.694 km/s
True Right ascension
16h 21m 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
01:31:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.719 km
Perigee altitude
359.2 km
Semi-major axis
6,738.097 km
Eccentricity
0.00011
Inclination
53.1584°
RAAN
245.2743°
Arg. of periapsis
117.5901°
True anomaly
242.51174°
Mean anomaly
242.5232°
Eccentric anomaly
242.51747°
Mean motion
3.92408 °/min
Orbital period
91.74 mins
BSTAR
-0.0000071178
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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 | 2025-10-18 06:56:42.547Z | 299.03° NW | 2025-10-18 06:58:42.547Z | 245.954° WSW | 38.527° | 2025-10-18 07:01:42.547Z | 144.918° SSE |
| 4 mins | 2025-10-18 23:26:42.547Z | 216.258° SW | 2025-10-18 23:27:42.547Z | 167.19° S | 43.451° | 2025-10-18 23:30:42.547Z | 53.463° ENE |
| 5 mins | 2025-10-19 05:49:42.547Z | 321.172° NNW | 2025-10-19 05:52:42.547Z | 47.67° ENE | 34.564° | 2025-10-19 05:54:42.547Z | 105.93° 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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