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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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: 11 hours ago
TLE from 11 hours ago
0 KINEIS-2E
1 62931U 25028D 26171.40903878 .00001088 00000-0 16143-3 0 9999
2 62931 97.8953 222.9740 0001879 114.1277 246.0130 14.77021772 73259Epoch: 2026-06-20T09:49Z
TLE epoch observation values (Epoch: 2026-06-20T09:49:00.950Z)
Latitude
-0.00002°
Longitude
167.09597°
Altitude
642.295 km
Speed
7.537 km/s
True Right ascension
14h 51m 53s
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
07:24:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
637.103 km
Perigee altitude
634.467 km
Semi-major axis
7,013.922 km
Eccentricity
0.00019
Inclination
97.8953°
RAAN
222.974°
Arg. of periapsis
114.1277°
True anomaly
245.99333°
Mean anomaly
246.013°
Eccentric anomaly
246.00316°
Mean motion
3.69489 °/min
Orbital period
97.43 mins
BSTAR
0.00016143
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 02:14:28.951Z | 96.28° ESE | 2026-06-21 02:16:28.951Z | 68.394° E | 14.296° | 2026-06-21 02:18:28.951Z | 38.721° NE |
| 6 mins | 2026-06-21 03:50:28.951Z | 195.191° SSW | 2026-06-21 03:52:28.951Z | 244.963° WSW | 37.511° | 2026-06-21 03:56:28.951Z | 334.608° NNW |
| 6 mins | 2026-06-21 15:40:28.951Z | 44.61° NE | 2026-06-21 15:43:28.951Z | 106.229° ESE | 26.834° | 2026-06-21 15:46:28.951Z | 155.404° SSE |
| 5 mins | 2026-06-21 17:17:28.951Z | 328.001° NNW | 2026-06-21 17:19:28.951Z | 291.354° WNW | 21.343° | 2026-06-21 17:22:28.951Z | 243.906° WSW |
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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