KINEIS-2D, 62930
Orbit data source: Space-Track
KINEIS-2D, 62930 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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62930 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: 13 hours ago
TLE from 13 hours ago
0 KINEIS-2D
1 62930U 25028C 25338.67277763 .00004928 00000-0 74161-3 0 9998
2 62930 97.9566 29.6852 0004562 106.7559 253.4151 14.74887342 44036Epoch: 2025-12-04T16:08Z
TLE epoch observation values (Epoch: 2025-12-04T16:08:47.987Z)
Latitude
0.00001°
Longitude
73.7594°
Altitude
649.438 km
Speed
7.532 km/s
True Right ascension
01h 58m 44s
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
03:01:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
645.762 km
Perigee altitude
639.356 km
Semi-major axis
7,020.696 km
Eccentricity
0.00046
Inclination
97.9566°
RAAN
29.6852°
Arg. of periapsis
106.7559°
True anomaly
253.36501°
Mean anomaly
253.4151°
Eccentric anomaly
253.39005°
Mean motion
3.68955 °/min
Orbital period
97.57 mins
BSTAR
0.00074161
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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-2D 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 | 2025-12-05 15:32:05.347Z | 50.588° ENE | 2025-12-05 15:35:05.347Z | 100.319° ESE | 20.172° | 2025-12-05 15:38:05.347Z | 144.156° SSE |
| 6 mins | 2025-12-05 17:09:05.347Z | 339.193° N | 2025-12-05 17:11:05.347Z | 299.608° NW | 27.884° | 2025-12-05 17:15:05.347Z | 228.63° WSW |
| 4 mins | 2025-12-06 02:31:05.347Z | 87.721° E | 2025-12-06 02:32:05.347Z | 70.899° E | 17.567° | 2025-12-06 02:35:05.347Z | 25.495° NE |
| 6 mins | 2025-12-06 04:06:05.347Z | 202.694° SW | 2025-12-06 04:09:05.347Z | 276.437° WNW | 32.123° | 2025-12-06 04:12:05.347Z | 327.546° 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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