KINEIS-2C, 62929
Orbit data source: Space-Track
KINEIS-2C, 62929 is a French payload satellite in SSO that was launched on Sat, 08 Feb 2025 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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62929 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-2C
1 62929U 25028B 26008.64930817 .00001708 00000-0 27825-3 0 9992
2 62929 98.0254 64.5794 0002325 128.5164 231.6252 14.72278798 49135Epoch: 2026-01-08T15:35Z
TLE epoch observation values (Epoch: 2026-01-08T15:35:00.225Z)
Latitude
-0.00005°
Longitude
82.62809°
Altitude
657.825 km
Speed
7.528 km/s
True Right ascension
04h 18m 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
01:15:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.494 km
Perigee altitude
649.225 km
Semi-major axis
7,028.996 km
Eccentricity
0.00023
Inclination
98.0254°
RAAN
64.5794°
Arg. of periapsis
128.5164°
True anomaly
231.60432°
Mean anomaly
231.6252°
Eccentric anomaly
231.61476°
Mean motion
3.68301 °/min
Orbital period
97.75 mins
BSTAR
0.00027825
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Other satellites on launch #28 in the year 2025 (2025-02-08 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-2C 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 | 2026-01-09 03:07:42.232Z | 141.543° SSE | 2026-01-09 03:11:42.232Z | 59.992° ENE | 34.785° | 2026-01-09 03:14:42.232Z | 5.154° NNE |
| 4 mins | 2026-01-09 04:46:42.232Z | 241.989° WSW | 2026-01-09 04:48:42.232Z | 272.739° WNW | 15.448° | 2026-01-09 04:50:42.232Z | 301.143° NW |
| 7 mins | 2026-01-09 16:37:42.232Z | 6.964° NNE | 2026-01-09 16:40:42.232Z | 300.293° NW | 43.863° | 2026-01-09 16:44:42.232Z | 200.85° SSW |
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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