KINEIS-5C, 62081
Orbit data source: Space-Track
KINEIS-5C, 62081 is a French payload satellite in SSO that was launched on Mon, 25 Nov 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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62081 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
KINEIS
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
28 kg wet, 28 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan + 1 Ant, 1.0 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 KINEIS-5C
1 62081U 24219A 25288.67135462 .00001404 00000-0 22949-3 0 9992
2 62081 97.9839 87.6661 0002695 83.2696 276.8818 14.72395463 47773Epoch: 2025-10-15T16:06Z
TLE epoch observation values (Epoch: 2025-10-15T16:06:45.039Z)
Latitude
-0.00002°
Longitude
-178.46364°
Altitude
656.213 km
Speed
7.529 km/s
True Right ascension
05h 50m 39s
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
18:10:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.38 km
Perigee altitude
648.592 km
Semi-major axis
7,028.623 km
Eccentricity
0.00027
Inclination
97.9839°
RAAN
87.6661°
Arg. of periapsis
83.2696°
True anomaly
276.85114°
Mean anomaly
276.8818°
Eccentric anomaly
276.86647°
Mean motion
3.68331 °/min
Orbital period
97.74 mins
BSTAR
0.00022949
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Other satellites on launch #219 in the year 2024 (2024-11-25 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.KINEIS-5C 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-18 00:07:27.790Z | 356.499° N | 2025-10-18 00:11:27.790Z | 286.174° WNW | 33.159° | 2025-10-18 00:15:27.790Z | 219.508° SW |
| 7 mins | 2025-10-18 11:06:27.790Z | 189.996° SSW | 2025-10-18 11:09:27.790Z | 251.214° W | 37.083° | 2025-10-18 11:13:27.790Z | 334° NNW |
| 6 mins | 2025-10-18 22:59:27.790Z | 41.885° NE | 2025-10-18 23:02:27.790Z | 104.5° ESE | 29.082° | 2025-10-18 23:05:27.790Z | 157.216° SSE |
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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