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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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: 22 hours ago
TLE from 22 hours ago
0 KINEIS-2E
1 62931U 25028D 26008.11629216 .00001419 00000-0 21099-3 0 9991
2 62931 97.9185 63.0312 0001039 73.7174 286.4150 14.76482706 49159Epoch: 2026-01-08T02:47Z
TLE epoch observation values (Epoch: 2026-01-08T02:47:27.642Z)
Latitude
-0.00005°
Longitude
-86.50898°
Altitude
643.259 km
Speed
7.536 km/s
True Right ascension
04h 12m 07s
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
01:16:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
638.224 km
Perigee altitude
636.766 km
Semi-major axis
7,015.632 km
Eccentricity
0.0001
Inclination
97.9185°
RAAN
63.0312°
Arg. of periapsis
73.7174°
True anomaly
286.40358°
Mean anomaly
286.415°
Eccentric anomaly
286.40929°
Mean motion
3.69354 °/min
Orbital period
97.47 mins
BSTAR
0.00021099
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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
Loading observer location...
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 | 2026-01-09 03:18:44.071Z | 154.241° SSE | 2026-01-09 03:22:44.071Z | 44.684° NE | 41.331° | 2026-01-09 03:25:44.071Z | 355.988° N |
| 7 mins | 2026-01-09 16:46:44.071Z | 355.597° N | 2026-01-09 16:49:44.071Z | 274.932° WNW | 38.127° | 2026-01-09 16:53:44.071Z | 210.888° SW |
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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