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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 KINEIS-2C
1 62929U 25028B 25260.08723775 .00001230 00000-0 20216-3 0 9999
2 62929 98.0166 312.5589 0002471 130.3941 229.7483 14.72346562 32424Epoch: 2025-09-17T02:05Z
TLE epoch observation values (Epoch: 2025-09-17T02:05:37.341Z)
Latitude
0.00003°
Longitude
-75.11492°
Altitude
657.718 km
Speed
7.528 km/s
True Right ascension
20h 50m 14s
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
18:08:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.38 km
Perigee altitude
648.906 km
Semi-major axis
7,028.78 km
Eccentricity
0.00025
Inclination
98.0166°
RAAN
312.5589°
Arg. of periapsis
130.3941°
True anomaly
229.72669°
Mean anomaly
229.7483°
Eccentric anomaly
229.7375°
Mean motion
3.68318 °/min
Orbital period
97.74 mins
BSTAR
0.00020216
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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 | 2025-09-18 02:41:51.894Z | 120.836° SE | 2025-09-18 02:44:51.894Z | 78.221° E | 22.155° | 2025-09-18 02:48:51.894Z | 14.771° NNE |
| 6 mins | 2025-09-18 04:19:51.894Z | 219.518° SW | 2025-09-18 04:21:51.894Z | 260.727° W | 26.504° | 2025-09-18 04:25:51.894Z | 324.869° NNW |
| 7 mins | 2025-09-18 16:11:51.894Z | 28.858° NE | 2025-09-18 16:14:51.894Z | 119.233° SE | 39.394° | 2025-09-18 16:18:51.894Z | 179.356° 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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