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: 8 hours ago
TLE from 8 hours ago
0 KINEIS-2E
1 62931U 25028D 26278.16624744 .00000821 00000-0 12297-3 0 9992
2 62931 97.8840 327.4090 0001587 118.3851 241.7520 14.77242277 89014Epoch: 2026-10-05T03:59Z
TLE epoch observation values (Epoch: 2026-10-05T03:59:23.778Z)
Latitude
-0°
Longitude
-106.28912°
Altitude
641.588 km
Speed
7.537 km/s
True Right ascension
21h 49m 38s
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
05:57:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
636.199 km
Perigee altitude
633.973 km
Semi-major axis
7,013.223 km
Eccentricity
0.00016
Inclination
97.884°
RAAN
327.409°
Arg. of periapsis
118.3851°
True anomaly
241.73598°
Mean anomaly
241.752°
Eccentric anomaly
241.74399°
Mean motion
3.69544 °/min
Orbital period
97.42 mins
BSTAR
0.00012297
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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 | 2026-10-05 15:56:46.546Z | 26.404° NE | 2026-10-05 15:59:46.546Z | 78.331° E | 49.943° | 2026-10-05 16:03:46.546Z | 174.047° S |
| 6 mins | 2026-10-06 02:53:46.546Z | 128.871° SE | 2026-10-06 02:55:46.546Z | 88.639° E | 38.169° | 2026-10-06 02:59:46.546Z | 6.341° NNE |
| 4 mins | 2026-10-06 04:31:46.546Z | 248.461° W | 2026-10-06 04:32:46.546Z | 265.268° W | 17.708° | 2026-10-06 04:35:46.546Z | 308.939° NW |
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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