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: 8 hours ago
TLE from 8 hours ago
0 KINEIS-5C
1 62081U 24219A 26034.51553589 .00001082 00000-0 17877-3 0 9995
2 62081 97.9911 196.5914 0002677 86.6911 273.4603 14.72356438 64089Epoch: 2026-02-03T12:22Z
TLE epoch observation values (Epoch: 2026-02-03T12:22:22.300Z)
Latitude
-0.00002°
Longitude
-122.69687°
Altitude
656.451 km
Speed
7.529 km/s
True Right ascension
13h 06m 21s
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
21:55:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.492 km
Perigee altitude
648.729 km
Semi-major axis
7,028.748 km
Eccentricity
0.00027
Inclination
97.9911°
RAAN
196.5914°
Arg. of periapsis
86.6911°
True anomaly
273.42968°
Mean anomaly
273.4603°
Eccentric anomaly
273.44499°
Mean motion
3.68321 °/min
Orbital period
97.74 mins
BSTAR
0.00017877
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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 | 2026-02-03 22:44:23.121Z | 41.202° NE | 2026-02-03 22:47:23.121Z | 84.6° E | 22.435° | 2026-02-03 22:51:23.121Z | 149.515° SSE |
| 6 mins | 2026-02-04 00:22:23.121Z | 335.114° NNW | 2026-02-04 00:24:23.121Z | 296.372° NW | 25.784° | 2026-02-04 00:28:23.121Z | 231.721° WSW |
| 5 mins | 2026-02-04 09:44:23.121Z | 102.722° ESE | 2026-02-04 09:46:23.121Z | 68.593° E | 20.296° | 2026-02-04 09:49:23.121Z | 21.762° NNE |
| 6 mins | 2026-02-04 11:20:23.121Z | 208.379° SW | 2026-02-04 11:23:23.121Z | 273.392° WNW | 28.929° | 2026-02-04 11:26:23.121Z | 323.575° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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