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: 11 hours ago
TLE from 11 hours ago
0 KINEIS-5C
1 62081U 24219A 25304.84606976 .00001240 00000-0 20381-3 0 9999
2 62081 97.9853 103.5555 0002221 53.7258 306.4154 14.72342679 50150Epoch: 2025-10-31T20:18Z
TLE epoch observation values (Epoch: 2025-10-31T20:18:20.427Z)
Latitude
-0.00005°
Longitude
118.58575°
Altitude
655.681 km
Speed
7.53 km/s
True Right ascension
06h 54m 13s
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
03:17:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.215 km
Perigee altitude
649.093 km
Semi-major axis
7,028.791 km
Eccentricity
0.00022
Inclination
97.9853°
RAAN
103.5555°
Arg. of periapsis
53.7258°
True anomaly
306.39492°
Mean anomaly
306.4154°
Eccentric anomaly
306.40516°
Mean motion
3.68317 °/min
Orbital period
97.74 mins
BSTAR
0.00020381
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-01 09:31:39.515Z | 91.155° ESE | 2025-11-01 09:33:39.515Z | 61.041° ENE | 15.233° | 2025-11-01 09:35:39.515Z | 32.606° NE |
| 7 mins | 2025-11-01 11:06:39.515Z | 190.627° SSW | 2025-11-01 11:09:39.515Z | 253.748° W | 36.981° | 2025-11-01 11:13:39.515Z | 334.048° NNW |
| 6 mins | 2025-11-01 22:59:39.515Z | 41.867° NE | 2025-11-01 23:02:39.515Z | 105.117° ESE | 29.268° | 2025-11-01 23:05:39.515Z | 157.64° S |
| 5 mins | 2025-11-02 00:36:39.515Z | 331.226° NNW | 2025-11-02 00:38:39.515Z | 298.709° NW | 20.128° | 2025-11-02 00:41:39.515Z | 249.983° W |
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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