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: 17 hours ago
TLE from 17 hours ago
0 KINEIS-1C
1 60081U 24114C 25260.27111081 .00000861 00000-0 12115-3 0 9991
2 60081 98.0092 280.3540 0001679 54.0194 306.1174 14.79867084 67002Epoch: 2025-09-17T06:30Z
TLE epoch observation values (Epoch: 2025-09-17T06:30:23.973Z)
Latitude
0.00004°
Longitude
-173.69535°
Altitude
632.068 km
Speed
7.543 km/s
True Right ascension
18h 41m 24s
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
16:40:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.966 km
Perigee altitude
625.614 km
Semi-major axis
7,004.927 km
Eccentricity
0.00017
Inclination
98.0092°
RAAN
280.354°
Arg. of periapsis
54.0194°
True anomaly
306.10186°
Mean anomaly
306.1174°
Eccentric anomaly
306.10963°
Mean motion
3.70201 °/min
Orbital period
97.24 mins
BSTAR
0.00012115
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-18 00:30:00.130Z | 116.819° SE | 2025-09-18 00:33:00.130Z | 71.499° E | 20.669° | 2025-09-18 00:36:00.130Z | 21.921° NNE |
| 6 mins | 2025-09-18 02:07:00.130Z | 214.139° SW | 2025-09-18 02:09:00.130Z | 254.69° W | 27.257° | 2025-09-18 02:13:00.130Z | 325.085° NNW |
| 6 mins | 2025-09-18 13:56:00.130Z | 37.614° NE | 2025-09-18 13:58:00.130Z | 85.796° E | 35.562° | 2025-09-18 14:02:00.130Z | 171.44° S |
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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