KINEIS-2E, 62931
Orbit data source: Space-Track
KINEIS-2E, 62931 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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62931 intel report (Beta)
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KINEIS-2E radio frequencies
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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: 10 hours ago
TLE from 10 hours ago
0 KINEIS-2E
1 62931U 25028D 25258.08858121 .00001193 00000-0 18117-3 0 9998
2 62931 97.9357 310.1825 0001277 77.3740 282.7612 14.75870896 32185Epoch: 2025-09-15T02:07Z
TLE epoch observation values (Epoch: 2025-09-15T02:07:33.416Z)
Latitude
-0.00006°
Longitude
-76.00498°
Altitude
645.205 km
Speed
7.535 km/s
True Right ascension
20h 40m 43s
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
04:51:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.332 km
Perigee altitude
638.54 km
Semi-major axis
7,017.573 km
Eccentricity
0.00013
Inclination
97.9357°
RAAN
310.1825°
Arg. of periapsis
77.374°
True anomaly
282.74693°
Mean anomaly
282.7612°
Eccentric anomaly
282.75406°
Mean motion
3.69201 °/min
Orbital period
97.51 mins
BSTAR
0.00018117
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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-2E 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 | 2025-09-15 15:43:14.703Z | 37.653° NE | 2025-09-15 15:47:14.703Z | 107.609° ESE | 25.508° | 2025-09-15 15:50:14.703Z | 154.161° SSE |
| 5 mins | 2025-09-15 17:21:14.703Z | 329.008° NNW | 2025-09-15 17:23:14.703Z | 291.191° WNW | 22.534° | 2025-09-15 17:26:14.703Z | 242.378° WSW |
| 6 mins | 2025-09-16 02:41:14.703Z | 111.39° ESE | 2025-09-16 02:43:14.703Z | 78.665° E | 21.687° | 2025-09-16 02:47:14.703Z | 15.054° NNE |
| 5 mins | 2025-09-16 04:18:14.703Z | 222.157° SW | 2025-09-16 04:20:14.703Z | 266.075° W | 26.407° | 2025-09-16 04:23:14.703Z | 319.014° 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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