KINEIS-5A, 62084
Orbit data source: Space-Track
KINEIS-5A, 62084 is a French payload satellite in SSO that was launched on Mon, 25 Nov 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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62084 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: 4 hours ago
TLE from 4 hours ago
0 KINEIS-5A
1 62084U 24219D 25358.27961966 .00000833 00000-0 13953-3 0 9995
2 62084 97.9837 156.3316 0003440 129.5066 230.6446 14.72323961 58039Epoch: 2025-12-24T06:42Z
TLE epoch observation values (Epoch: 2025-12-24T06:42:39.138Z)
Latitude
-0.00004°
Longitude
-37.38276°
Altitude
658.202 km
Speed
7.527 km/s
True Right ascension
10h 25m 19s
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
10:16:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.132 km
Perigee altitude
648.296 km
Semi-major axis
7,028.851 km
Eccentricity
0.00034
Inclination
97.9837°
RAAN
156.3316°
Arg. of periapsis
129.5066°
True anomaly
230.61413°
Mean anomaly
230.6446°
Eccentric anomaly
230.62936°
Mean motion
3.68313 °/min
Orbital period
97.74 mins
BSTAR
0.00013953
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Other satellites on launch #219 in the year 2024 (2024-11-25 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-5A Visibility forecast
Loading observer location...
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 | 2025-12-24 11:43:34.668Z | 219.697° SW | 2025-12-24 11:46:34.668Z | 263.445° W | 19.043° | 2025-12-24 11:49:34.668Z | 309.685° NW |
| 7 mins | 2025-12-24 23:36:34.668Z | 14.06° NNE | 2025-12-24 23:39:34.668Z | 183.254° SSW | 44.062° | 2025-12-24 23:43:34.668Z | 192.936° SSW |
| 7 mins | 2025-12-25 10:34:34.668Z | 155.415° SSE | 2025-12-25 10:37:34.668Z | 54.343° ENE | 43.317° | 2025-12-25 10:41:34.668Z | 352.19° N |
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
Authenticating...
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