KINEIS-1D, 60082
Orbit data source: Space-Track
KINEIS-1D, 60082 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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60082 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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 KINEIS-1D
1 60082U 24114D 25258.28876815 .00000862 00000-0 13349-3 0 9994
2 60082 98.0092 276.2423 0002022 47.0171 313.1207 14.75731051 66573Epoch: 2025-09-15T06:55Z
TLE epoch observation values (Epoch: 2025-09-15T06:55:49.568Z)
Latitude
-0.00006°
Longitude
177.79021°
Altitude
644.874 km
Speed
7.536 km/s
True Right ascension
18h 24m 58s
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
12:30:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
641.302 km
Perigee altitude
638.464 km
Semi-major axis
7,018.02 km
Eccentricity
0.0002
Inclination
98.0092°
RAAN
276.2423°
Arg. of periapsis
47.0171°
True anomaly
313.10378°
Mean anomaly
313.1207°
Eccentric anomaly
313.11224°
Mean motion
3.69166 °/min
Orbital period
97.52 mins
BSTAR
0.00013349
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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-1D 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-16 00:57:10.495Z | 148.983° SSE | 2025-09-16 01:01:10.495Z | 64.515° ENE | 39.03° | 2025-09-16 01:05:10.495Z | 357.196° N |
| 6 mins | 2025-09-16 14:26:10.495Z | 358.865° N | 2025-09-16 14:28:10.495Z | 315.26° NNW | 40.729° | 2025-09-16 14:32:10.495Z | 207.128° 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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