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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 KINEIS-2D
1 62930U 25028C 25257.38230381 .00001367 00000-0 21383-3 0 9993
2 62930 97.9693 309.7743 0003661 36.3511 323.7946 14.74350361 32051Epoch: 2025-09-14T09:10Z
TLE epoch observation values (Epoch: 2025-09-14T09:10:31.049Z)
Latitude
0.00002°
Longitude
178.54281°
Altitude
648.15 km
Speed
7.535 km/s
True Right ascension
20h 39m 05s
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
02:47:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
646.837 km
Perigee altitude
641.695 km
Semi-major axis
7,022.403 km
Eccentricity
0.00037
Inclination
97.9693°
RAAN
309.7743°
Arg. of periapsis
36.3511°
True anomaly
323.76981°
Mean anomaly
323.7946°
Eccentric anomaly
323.78221°
Mean motion
3.6882 °/min
Orbital period
97.61 mins
BSTAR
0.00021383
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-15 16:41:40.616Z | 3.932° NNE | 2025-09-15 16:44:40.616Z | 315.057° NNW | 41.323° | 2025-09-15 16:48:40.616Z | 206.045° SW |
| 7 mins | 2025-09-16 03:39:40.616Z | 171.281° S | 2025-09-16 03:42:40.616Z | 315.459° NNW | 43.954° | 2025-09-16 03:46:40.616Z | 345.455° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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