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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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: 7 hours ago
TLE from 7 hours ago
0 KINEIS-5C
1 62081U 24219A 26186.61352235 .00000722 00000-0 12195-3 0 9997
2 62081 97.9058 344.9554 0003357 204.5608 155.5440 14.72305808 86460Epoch: 2026-07-05T14:43Z
TLE epoch observation values (Epoch: 2026-07-05T14:43:28.331Z)
Latitude
-0.00003°
Longitude
-159.52298°
Altitude
658.877 km
Speed
7.527 km/s
True Right ascension
22h 59m 49s
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
10:04:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.128 km
Perigee altitude
648.408 km
Semi-major axis
7,028.905 km
Eccentricity
0.00034
Inclination
97.9058°
RAAN
344.9554°
Arg. of periapsis
204.5608°
True anomaly
155.55992°
Mean anomaly
155.544°
Eccentric anomaly
155.55196°
Mean motion
3.68308 °/min
Orbital period
97.74 mins
BSTAR
0.00012195
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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 | 2026-07-05 23:27:07.807Z | 13.673° NNE | 2026-07-05 23:31:07.807Z | 180.08° SSW | 43.989° | 2026-07-05 23:35:07.807Z | 192.483° SSW |
| 7 mins | 2026-07-06 10:26:07.807Z | 154.333° SSE | 2026-07-06 10:29:07.807Z | 54.277° ENE | 42.982° | 2026-07-06 10:33:07.807Z | 352.757° N |
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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