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: 12 hours ago
TLE from 12 hours ago
0 KINEIS-2E
1 62931U 25028D 26090.85403039 .00002039 00000-0 29793-3 0 9994
2 62931 97.9037 144.1172 0001976 90.4101 269.7335 14.76791587 61362Epoch: 2026-03-31T20:29Z
TLE epoch observation values (Epoch: 2026-03-31T20:29:48.225Z)
Latitude
-0.00009°
Longitude
7.44103°
Altitude
642.494 km
Speed
7.537 km/s
True Right ascension
09h 36m 28s
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
13:52:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
637.901 km
Perigee altitude
635.129 km
Semi-major axis
7,014.652 km
Eccentricity
0.0002
Inclination
97.9037°
RAAN
144.1172°
Arg. of periapsis
90.4101°
True anomaly
269.71086°
Mean anomaly
269.7335°
Eccentric anomaly
269.72218°
Mean motion
3.69432 °/min
Orbital period
97.45 mins
BSTAR
0.00029793
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-01 16:35:44.509Z | 1.685° NNE | 2026-04-01 16:38:44.509Z | 246.119° WSW | 41.262° | 2026-04-01 16:41:44.509Z | 204.999° SW |
| 7 mins | 2026-04-02 03:31:44.509Z | 167.689° S | 2026-04-02 03:34:44.509Z | 334.752° NNW | 44.507° | 2026-04-02 03:38:44.509Z | 346.979° N |
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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