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: 6 hours ago
TLE from 6 hours ago
0 KINEIS-5C
1 62081U 24219A 25312.18569476 .00001421 00000-0 23229-3 0 9993
2 62081 97.9850 110.7668 0001860 39.8993 320.2351 14.72363565 51231Epoch: 2025-11-08T04:27Z
TLE epoch observation values (Epoch: 2025-11-08T04:27:24.027Z)
Latitude
-0.00001°
Longitude
-3.70224°
Altitude
655.536 km
Speed
7.53 km/s
True Right ascension
07h 23m 04s
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
06:52:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.895 km
Perigee altitude
649.28 km
Semi-major axis
7,028.725 km
Eccentricity
0.00019
Inclination
97.985°
RAAN
110.7668°
Arg. of periapsis
39.8993°
True anomaly
320.22146°
Mean anomaly
320.2351°
Eccentric anomaly
320.22828°
Mean motion
3.68323 °/min
Orbital period
97.74 mins
BSTAR
0.00023229
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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 | 2025-11-08 11:05:45.833Z | 187.023° SSW | 2025-11-08 11:09:45.833Z | 270.869° WNW | 36.947° | 2025-11-08 11:13:45.833Z | 335.636° NNW |
| 6 mins | 2025-11-08 22:59:45.833Z | 46.071° ENE | 2025-11-08 23:01:45.833Z | 86.464° E | 29.001° | 2025-11-08 23:05:45.833Z | 160.23° S |
| 5 mins | 2025-11-09 00:36:45.833Z | 326.515° NNW | 2025-11-09 00:38:45.833Z | 291.478° WNW | 20.312° | 2025-11-09 00:41:45.833Z | 246.206° WSW |
| 6 mins | 2025-11-09 09:57:45.833Z | 119.927° SE | 2025-11-09 10:00:45.833Z | 63.463° ENE | 25.784° | 2025-11-09 10:03:45.833Z | 14.388° NNE |
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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