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: 1 day ago
TLE from 1 day ago
0 KINEIS-2C
1 62929U 25028B 26134.22745224 .00000724 00000-0 11965-3 0 9997
2 62929 98.0769 188.6844 0001520 72.8024 287.3350 14.73335840 67615Epoch: 2026-05-14T05:27Z
TLE epoch observation values (Epoch: 2026-05-14T05:27:31.873Z)
Latitude
-0.00003°
Longitude
-125.17455°
Altitude
653.128 km
Speed
7.531 km/s
True Right ascension
12h 34m 44s
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
15:25:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
648.565 km
Perigee altitude
646.429 km
Semi-major axis
7,025.634 km
Eccentricity
0.00015
Inclination
98.0769°
RAAN
188.6844°
Arg. of periapsis
72.8024°
True anomaly
287.31837°
Mean anomaly
287.335°
Eccentric anomaly
287.32669°
Mean motion
3.68566 °/min
Orbital period
97.68 mins
BSTAR
0.00011965
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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 | 2026-05-15 16:15:50.040Z | 22.89° NE | 2026-05-15 16:18:50.040Z | 69.868° E | 40.003° | 2026-05-15 16:22:50.040Z | 179.338° S |
| 7 mins | 2026-05-16 03:13:50.040Z | 143.008° SSE | 2026-05-16 03:16:50.040Z | 84.867° E | 37.147° | 2026-05-16 03:20:50.040Z | 0.343° NNE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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