KINEIS-1C, 60081
Orbit data source: Space-Track
KINEIS-1C, 60081 is a French payload satellite in SSO that was launched on Thu, 20 Jun 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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60081 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: 15 hours ago
TLE from 15 hours ago
0 KINEIS-1C
1 60081U 24114C 25315.30578413 .00001895 00000-0 25711-3 0 9996
2 60081 98.0031 335.2118 0001869 125.1812 234.9575 14.80059818 75141Epoch: 2025-11-11T07:20Z
TLE epoch observation values (Epoch: 2025-11-11T07:20:19.748Z)
Latitude
-0.00004°
Longitude
174.43528°
Altitude
632.906 km
Speed
7.541 km/s
True Right ascension
22h 20m 50s
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
19:07:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.49 km
Perigee altitude
624.872 km
Semi-major axis
7,004.318 km
Eccentricity
0.00019
Inclination
98.0031°
RAAN
335.2118°
Arg. of periapsis
125.1812°
True anomaly
234.93997°
Mean anomaly
234.9575°
Eccentric anomaly
234.94873°
Mean motion
3.70249 °/min
Orbital period
97.23 mins
BSTAR
0.00025711
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Other satellites on launch #114 in the year 2024 (2024-06-20 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-1C 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 | 2025-11-12 01:18:34.891Z | 157.346° SSE | 2025-11-12 01:22:34.891Z | 37.411° NE | 42.48° | 2025-11-12 01:25:34.891Z | 353.621° N |
| 7 mins | 2025-11-12 14:44:34.891Z | 355.649° N | 2025-11-12 14:47:34.891Z | 279.639° WNW | 37.6° | 2025-11-12 14:51:34.891Z | 211.912° 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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