STARLINK-11352, 62880
Orbit data source: Space-Track
STARLINK-11352, 62880 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 04 Feb 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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62880 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK V2MD, Unknown motor
Mass
960 kg wet, ~910 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 18.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 STARLINK-11352
1 62880U 25024B 26035.01914358 .00279872 00000-0 20936-2 0 9991
2 62880 42.9989 24.1847 0003207 285.4535 74.5979 15.71046702 58172Epoch: 2026-02-04T00:27Z
TLE epoch observation values (Epoch: 2026-02-04T00:27:34.005Z)
Latitude
0.00003°
Longitude
-116.89869°
Altitude
355.102 km
Speed
7.698 km/s
True Right ascension
01h 36m 44s
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
20:15:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.047 km
Perigee altitude
355.726 km
Semi-major axis
6,736.023 km
Eccentricity
0.00032
Inclination
42.9989°
RAAN
24.1847°
Arg. of periapsis
285.4535°
True anomaly
74.63333°
Mean anomaly
74.5979°
Eccentric anomaly
74.61562°
Mean motion
3.92589 °/min
Orbital period
91.7 mins
BSTAR
0.0020936
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Other satellites on launch #24 in the year 2025 (2025-02-04 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-11352 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 | 2026-02-05 02:37:17.549Z | 222.111° SW | 2026-02-05 02:39:17.549Z | 157.499° SSE | 34.513° | 2026-02-05 02:41:17.549Z | 87.131° E |
| 4 mins | 2026-02-05 05:50:17.549Z | 304.076° NW | 2026-02-05 05:51:17.549Z | 338.53° N | 35.269° | 2026-02-05 05:54:17.549Z | 84.093° E |
| 4 mins | 2026-02-05 07:26:17.549Z | 269.693° W | 2026-02-05 07:27:17.549Z | 238.812° WSW | 34.604° | 2026-02-05 07:30:17.549Z | 129.972° 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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