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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 KINEIS-5C
1 62081U 24219A 25259.31268278 .00000844 00000-0 14133-3 0 9996
2 62081 97.9814 58.8327 0002221 134.8407 225.2981 14.72294673 43454Epoch: 2025-09-16T07:30Z
TLE epoch observation values (Epoch: 2025-09-16T07:30:15.792Z)
Latitude
-0.00003°
Longitude
-49.23788°
Altitude
657.86 km
Speed
7.528 km/s
True Right ascension
03h 55m 19s
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
07:11:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.368 km
Perigee altitude
649.246 km
Semi-major axis
7,028.944 km
Eccentricity
0.00022
Inclination
97.9814°
RAAN
58.8327°
Arg. of periapsis
134.8407°
True anomaly
225.28001°
Mean anomaly
225.2981°
Eccentric anomaly
225.28906°
Mean motion
3.68305 °/min
Orbital period
97.74 mins
BSTAR
0.00014133
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-16 22:45:51.188Z | 40.787° NE | 2025-09-16 22:49:51.188Z | 105.065° ESE | 22.417° | 2025-09-16 22:52:51.188Z | 148.922° SSE |
| 6 mins | 2025-09-17 00:23:51.188Z | 335.98° NNW | 2025-09-17 00:25:51.188Z | 297.945° NW | 25.783° | 2025-09-17 00:29:51.188Z | 232.033° WSW |
| 5 mins | 2025-09-17 09:45:51.188Z | 103.663° ESE | 2025-09-17 09:47:51.188Z | 70.185° E | 20.231° | 2025-09-17 09:50:51.188Z | 22.672° NE |
| 6 mins | 2025-09-17 11:21:51.188Z | 207.343° SW | 2025-09-17 11:24:51.188Z | 270.981° WNW | 29.213° | 2025-09-17 11:27:51.188Z | 323.014° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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