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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 KINEIS-1C
1 60081U 24114C 25258.31028109 .00001119 00000-0 15540-3 0 9993
2 60081 98.0093 278.3989 0001777 55.8227 304.3153 14.79865496 66711Epoch: 2025-09-15T07:26Z
TLE epoch observation values (Epoch: 2025-09-15T07:26:48.286Z)
Latitude
0.00002°
Longitude
172.18094°
Altitude
632.065 km
Speed
7.543 km/s
True Right ascension
18h 33m 35s
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
12:30:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
628.039 km
Perigee altitude
625.55 km
Semi-major axis
7,004.932 km
Eccentricity
0.00018
Inclination
98.0093°
RAAN
278.3989°
Arg. of periapsis
55.8227°
True anomaly
304.29848°
Mean anomaly
304.3153°
Eccentric anomaly
304.30689°
Mean motion
3.70201 °/min
Orbital period
97.24 mins
BSTAR
0.0001554
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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 | 2025-09-16 01:25:09.555Z | 165.801° S | 2025-09-16 01:29:09.555Z | 348.903° N | 43.558° | 2025-09-16 01:32:09.555Z | 347.478° N |
| 4 mins | 2025-09-16 13:16:09.555Z | 69.761° E | 2025-09-16 13:17:09.555Z | 85.8° E | 16.139° | 2025-09-16 13:20:09.555Z | 131.325° SE |
| 6 mins | 2025-09-16 14:51:09.555Z | 349.81° N | 2025-09-16 14:54:09.555Z | 283.212° WNW | 32.69° | 2025-09-16 14:57:09.555Z | 224.648° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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