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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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: 13 hours ago
TLE from 13 hours ago
0 KINEIS-2C
1 62929U 25028B 26044.73692626 .00001331 00000-0 21830-3 0 9997
2 62929 98.0258 100.2050 0002343 69.9572 290.1888 14.72315227 54447Epoch: 2026-02-13T17:41Z
TLE epoch observation values (Epoch: 2026-02-13T17:41:10.428Z)
Latitude
0.00001°
Longitude
51.1415°
Altitude
656.126 km
Speed
7.53 km/s
True Right ascension
06h 40m 49s
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
09:34:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.39 km
Perigee altitude
649.097 km
Semi-major axis
7,028.88 km
Eccentricity
0.00023
Inclination
98.0258°
RAAN
100.205°
Arg. of periapsis
69.9572°
True anomaly
290.1636°
Mean anomaly
290.1888°
Eccentric anomaly
290.1762°
Mean motion
3.6831 °/min
Orbital period
97.74 mins
BSTAR
0.0002183
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-14 15:29:30.229Z | 57.262° ENE | 2026-02-14 15:31:30.229Z | 88.479° E | 18.39° | 2026-02-14 15:34:30.229Z | 135.098° SSE |
| 6 mins | 2026-02-14 17:06:30.229Z | 339.612° N | 2026-02-14 17:08:30.229Z | 294.126° NW | 30.894° | 2026-02-14 17:12:30.229Z | 223.887° SW |
| 6 mins | 2026-02-15 04:04:30.229Z | 200.281° SSW | 2026-02-15 04:06:30.229Z | 242.432° WSW | 33.93° | 2026-02-15 04:10:30.229Z | 329.945° NNW |
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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