KINEIS-1A, 60084
Orbit data source: Space-Track
KINEIS-1A, 60084 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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60084 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: 9 hours ago
TLE from 9 hours ago
0 KINEIS-1A
1 60084U 24114F 25289.59729485 .00001724 00000-0 23523-3 0 9997
2 60084 98.0059 309.8005 0003272 173.5494 186.5760 14.79947980 71350Epoch: 2025-10-16T14:20Z
TLE epoch observation values (Epoch: 2025-10-16T14:20:06.275Z)
Latitude
-0.00002°
Longitude
69.41962°
Altitude
634.785 km
Speed
7.54 km/s
True Right ascension
20h 39m 12s
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
17:34:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
628.826 km
Perigee altitude
624.242 km
Semi-major axis
7,004.671 km
Eccentricity
0.00033
Inclination
98.0059°
RAAN
309.8005°
Arg. of periapsis
173.5494°
True anomaly
186.57171°
Mean anomaly
186.576°
Eccentric anomaly
186.57385°
Mean motion
3.70221 °/min
Orbital period
97.24 mins
BSTAR
0.00023523
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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-1A 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 | 2025-10-17 01:49:54.280Z | 193.467° SSW | 2025-10-17 01:51:54.280Z | 239.659° WSW | 37.354° | 2025-10-17 01:55:54.280Z | 334.363° NNW |
| 6 mins | 2025-10-17 13:38:54.280Z | 49.453° ENE | 2025-10-17 13:40:54.280Z | 87.323° E | 25.211° | 2025-10-17 13:44:54.280Z | 155.793° SSE |
| 4 mins | 2025-10-17 15:15:54.280Z | 322.216° NNW | 2025-10-17 15:17:54.280Z | 281.027° WNW | 21.871° | 2025-10-17 15:19:54.280Z | 247.716° W |
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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