LARES-2, 53105
Orbit data source: Space-Track
LARES-2, 53105 is a payload satellite owned by ASI (IT) that was launched on Wed, 13 Jul 2022 UTC via a VEGA C launch vehicle from the French Guiana (FRGUI). 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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53105 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ITRelated business
Manufacturer
OHB-I
Mission
Operational Civil Technology
Bus & Motor
LARES, Unknown motor
Mass
295 kg wet, 295 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Sphere, 0.2 m
Radar Cross Section
0.139 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 LARES-2
1 53105U 22080A 25365.53869689 -.00000012 00000-0 00000-0 0 9995
2 53105 70.1804 2.8119 0005290 11.5829 348.4948 6.38964836 80954Epoch: 2025-12-31T12:55Z
TLE epoch observation values (Epoch: 2025-12-31T12:55:43.411Z)
Latitude
0.00005°
Longitude
68.67463°
Altitude
5,884.233 km
Speed
5.703 km/s
True Right ascension
00h 11m 14s
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
10:38:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
5,894.527 km
Perigee altitude
5,881.55 km
Semi-major axis
12,266.175 km
Eccentricity
0.00053
Inclination
70.1804°
RAAN
2.8119°
Arg. of periapsis
11.5829°
True anomaly
348.4827°
Mean anomaly
348.4948°
Eccentric anomaly
348.48875°
Mean motion
1.59764 °/min
Orbital period
225.33 mins
BSTAR
0
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Other satellites on launch #80 in the year 2022 (2022-07-13 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.LARES-2 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2026-01-08 10:27:09.658Z | 148.034° SSE | 2026-01-08 10:27:09.658Z | 148.034° SSE | 32.004° | 2026-01-08 10:41:09.658Z | 154.511° SSE |
| 40 mins | 2026-01-08 13:38:09.658Z | 324.331° NNW | 2026-01-08 13:57:09.658Z | 283.77° WNW | 22.375° | 2026-01-08 14:18:09.658Z | 238.681° WSW |
| 61 mins | 2026-01-08 23:42:09.658Z | 181.957° SSW | 2026-01-09 00:12:09.658Z | 99.898° ESE | 43.841° | 2026-01-09 00:43:09.658Z | 26.141° NE |
| 60 mins | 2026-01-09 03:46:09.658Z | 263.294° W | 2026-01-09 04:15:09.658Z | 332.569° NNW | 32.524° | 2026-01-09 04:46:09.658Z | 45.719° ENE |
| 62 mins | 2026-01-09 08:04:09.658Z | 327.174° NNW | 2026-01-09 08:35:09.658Z | 46.187° ENE | 38.955° | 2026-01-09 09:06:09.658Z | 125.505° 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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