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: 9 hours ago
TLE from 9 hours ago
0 KINEIS-2D
1 62930U 25028C 25305.56306152 .00002660 00000-0 40597-3 0 9992
2 62930 97.9618 357.1448 0002844 189.8255 170.2899 14.74664989 39152Epoch: 2025-11-01T13:30Z
TLE epoch observation values (Epoch: 2025-11-01T13:30:48.515Z)
Latitude
0.00002°
Longitude
113.3513°
Altitude
651.197 km
Speed
7.531 km/s
True Right ascension
23h 48m 34s
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
18:33:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
645.263 km
Perigee altitude
641.269 km
Semi-major axis
7,021.403 km
Eccentricity
0.00028
Inclination
97.9618°
RAAN
357.1448°
Arg. of periapsis
189.8255°
True anomaly
170.29539°
Mean anomaly
170.2899°
Eccentric anomaly
170.29265°
Mean motion
3.68899 °/min
Orbital period
97.59 mins
BSTAR
0.00040597
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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 | 2025-11-02 02:41:11.169Z | 117.167° SE | 2025-11-02 02:44:11.169Z | 69.444° E | 22.223° | 2025-11-02 02:47:11.169Z | 20.097° NNE |
| 6 mins | 2025-11-02 04:18:11.169Z | 213.616° SW | 2025-11-02 04:21:11.169Z | 275.217° WNW | 26.162° | 2025-11-02 04:24:11.169Z | 321.965° NNW |
| 7 mins | 2025-11-02 16:09:11.169Z | 27.529° NE | 2025-11-02 16:12:11.169Z | 98.635° ESE | 39.198° | 2025-11-02 16:16:11.169Z | 177.229° S |
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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