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: 8 hours ago
TLE from 8 hours ago
0 KINEIS-2C
1 62929U 25028B 25305.61981917 .00002011 00000-0 32557-3 0 9991
2 62929 98.0163 357.4593 0002057 54.0180 306.1218 14.72364265 39121Epoch: 2025-11-01T14:52Z
TLE epoch observation values (Epoch: 2025-11-01T14:52:32.376Z)
Latitude
-0°
Longitude
93.17711°
Altitude
655.685 km
Speed
7.53 km/s
True Right ascension
23h 49m 50s
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
18:28:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.033 km
Perigee altitude
649.141 km
Semi-major axis
7,028.724 km
Eccentricity
0.00021
Inclination
98.0163°
RAAN
357.4593°
Arg. of periapsis
54.018°
True anomaly
306.10276°
Mean anomaly
306.1218°
Eccentric anomaly
306.11228°
Mean motion
3.68323 °/min
Orbital period
97.74 mins
BSTAR
0.00032557
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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 | 2025-11-02 02:27:11.716Z | 101.595° ESE | 2025-11-02 02:29:11.716Z | 73.396° E | 16.287° | 2025-11-02 02:32:11.716Z | 28.579° NE |
| 7 mins | 2025-11-02 04:03:11.716Z | 196.053° SSW | 2025-11-02 04:06:11.716Z | 265.23° W | 34.94° | 2025-11-02 04:10:11.716Z | 333.203° NNW |
| 6 mins | 2025-11-02 15:56:11.716Z | 42.384° NE | 2025-11-02 15:58:11.716Z | 82.174° E | 30.658° | 2025-11-02 16:02:11.716Z | 162.487° S |
| 5 mins | 2025-11-02 17:33:11.716Z | 326.546° NNW | 2025-11-02 17:35:11.716Z | 293.466° NW | 18.899° | 2025-11-02 17:38:11.716Z | 249.177° W |
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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