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: 18 hours ago
TLE from 18 hours ago
0 KINEIS-5C
1 62081U 24219A 25257.61362581 .00000704 00000-0 11926-3 0 9991
2 62081 97.9813 57.1646 0002141 137.7779 222.3594 14.72291040 43200Epoch: 2025-09-14T14:43Z
TLE epoch observation values (Epoch: 2025-09-14T14:43:37.269Z)
Latitude
-0.00002°
Longitude
-157.5708°
Altitude
657.885 km
Speed
7.528 km/s
True Right ascension
03h 48m 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
01:32:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.323 km
Perigee altitude
649.314 km
Semi-major axis
7,028.955 km
Eccentricity
0.00021
Inclination
97.9813°
RAAN
57.1646°
Arg. of periapsis
137.7779°
True anomaly
222.34287°
Mean anomaly
222.3594°
Eccentric anomaly
222.35114°
Mean motion
3.68304 °/min
Orbital period
97.75 mins
BSTAR
0.00011926
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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 | 2025-09-15 10:24:49.831Z | 151.944° SSE | 2025-09-15 10:28:49.831Z | 95.92° ESE | 39.485° | 2025-09-15 10:32:49.831Z | 358.026° N |
| 7 mins | 2025-09-15 23:55:49.831Z | 357.913° N | 2025-09-15 23:58:49.831Z | 272.729° WNW | 39.796° | 2025-09-16 00:02:49.831Z | 208.607° SW |
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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