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: 19 hours ago
TLE from 19 hours ago
0 KINEIS-2C
1 62929U 25028B 25257.70864097 .00001011 00000-0 16766-3 0 9999
2 62929 98.0169 310.2129 0002377 132.8147 227.3260 14.72339622 32079Epoch: 2025-09-14T17:00Z
TLE epoch observation values (Epoch: 2025-09-14T17:00:26.579Z)
Latitude
-0.00009°
Longitude
61.1784°
Altitude
657.75 km
Speed
7.528 km/s
True Right ascension
20h 40m 51s
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
04:51:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.336 km
Perigee altitude
648.995 km
Semi-major axis
7,028.802 km
Eccentricity
0.00024
Inclination
98.0169°
RAAN
310.2129°
Arg. of periapsis
132.8147°
True anomaly
227.30598°
Mean anomaly
227.326°
Eccentric anomaly
227.31599°
Mean motion
3.68316 °/min
Orbital period
97.74 mins
BSTAR
0.00016766
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-15 16:24:32.206Z | 15.028° NNE | 2025-09-15 16:28:32.206Z | 118.182° SE | 44.667° | 2025-09-15 16:32:32.206Z | 190.389° SSW |
| 7 mins | 2025-09-16 03:23:32.206Z | 153.433° SSE | 2025-09-16 03:26:32.206Z | 85.958° E | 42.527° | 2025-09-16 03:30:32.206Z | 354.077° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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