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: 4 days ago
TLE from 4 days ago
0 KINEIS-5C
1 62081U 24219A 25346.91348439 -.00000111 00000-0 -97545-5 0 9996
2 62081 97.9873 144.8904 0000684 207.5479 152.5693 14.72277460 56343Epoch: 2025-12-12T21:55Z
TLE epoch observation values (Epoch: 2025-12-12T21:55:25.051Z)
Latitude
0.00006°
Longitude
94.18773°
Altitude
657.242 km
Speed
7.529 km/s
True Right ascension
09h 39m 33s
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
16:20:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.343 km
Perigee altitude
650.381 km
Semi-major axis
7,028.999 km
Eccentricity
0.00007
Inclination
97.9873°
RAAN
144.8904°
Arg. of periapsis
207.5479°
True anomaly
152.57291°
Mean anomaly
152.5693°
Eccentric anomaly
152.57111°
Mean motion
3.68301 °/min
Orbital period
97.75 mins
BSTAR
-0.0000097545
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Other satellites on launch #219 in the year 2024 (2024-11-25 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-16 22:45:11.936Z | 48.822° ENE | 2025-12-16 22:48:11.936Z | 101.416° ESE | 22.505° | 2025-12-16 22:51:11.936Z | 147.266° SSE |
| 6 mins | 2025-12-17 00:22:11.936Z | 338.173° N | 2025-12-17 00:24:11.936Z | 302.161° NW | 25.705° | 2025-12-17 00:28:11.936Z | 233.038° WSW |
| 5 mins | 2025-12-17 09:44:11.936Z | 105.592° ESE | 2025-12-17 09:46:11.936Z | 73.428° E | 20.024° | 2025-12-17 09:49:11.936Z | 24.527° NE |
| 6 mins | 2025-12-17 11:20:11.936Z | 205.442° SW | 2025-12-17 11:23:11.936Z | 266.035° W | 29.546° | 2025-12-17 11:26:11.936Z | 321.768° 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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