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: 15 hours ago
TLE from 15 hours ago
0 KINEIS-5C
1 62081U 24219A 26306.90403314 .00000383 00000-0 68233-4 0 9996
2 62081 97.9192 102.0530 0003967 180.3061 179.8145 14.72366234104166Epoch: 2026-11-02T21:41Z
TLE epoch observation values (Epoch: 2026-11-02T21:41:48.463Z)
Latitude
-0.00001°
Longitude
94.42671°
Altitude
659.325 km
Speed
7.526 km/s
True Right ascension
06h 48m 12s
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
09:01:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.364 km
Perigee altitude
647.788 km
Semi-major axis
7,028.713 km
Eccentricity
0.0004
Inclination
97.9192°
RAAN
102.053°
Arg. of periapsis
180.3061°
True anomaly
179.81465°
Mean anomaly
179.8145°
Eccentric anomaly
179.81457°
Mean motion
3.68324 °/min
Orbital period
97.74 mins
BSTAR
0.000068233
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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 | 2026-11-03 22:44:11.107Z | 33.279° NE | 2026-11-03 22:48:11.107Z | 101.671° ESE | 33.599° | 2026-11-03 22:51:11.107Z | 155.95° SSE |
| 5 mins | 2026-11-04 00:22:11.107Z | 332.797° NNW | 2026-11-04 00:24:11.107Z | 300.948° NW | 21.832° | 2026-11-04 00:27:11.107Z | 250.715° W |
| 6 mins | 2026-11-04 09:44:11.107Z | 112.466° ESE | 2026-11-04 09:46:11.107Z | 74.211° E | 28.336° | 2026-11-04 09:50:11.107Z | 10.842° NNE |
| 5 mins | 2026-11-04 11:21:11.107Z | 227.192° WSW | 2026-11-04 11:23:11.107Z | 266.217° W | 25.891° | 2026-11-04 11:26:11.107Z | 315.604° 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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