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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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: 7 hours ago
TLE from 7 hours ago
0 KINEIS-2D
1 62930U 25028C 26304.12347351 .00000820 00000-0 12630-3 0 9993
2 62930 97.9124 353.8653 0004482 119.0765 241.0894 14.76008008 92760Epoch: 2026-10-31T02:57Z
TLE epoch observation values (Epoch: 2026-10-31T02:57:48.111Z)
Latitude
-0.00001°
Longitude
-90.01887°
Altitude
646.492 km
Speed
7.534 km/s
True Right ascension
23h 35m 27s
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
05:20:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
642.145 km
Perigee altitude
635.855 km
Semi-major axis
7,017.137 km
Eccentricity
0.00045
Inclination
97.9124°
RAAN
353.8653°
Arg. of periapsis
119.0765°
True anomaly
241.04445°
Mean anomaly
241.0894°
Eccentric anomaly
241.06693°
Mean motion
3.69235 °/min
Orbital period
97.5 mins
BSTAR
0.0001263
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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 | 2026-10-31 16:33:36.075Z | 2.996° NNE | 2026-10-31 16:36:36.075Z | 270.2° WNW | 66.372° | 2026-10-31 16:40:36.075Z | 203.57° SW |
| 7 mins | 2026-11-01 03:29:36.075Z | 167.656° S | 2026-11-01 03:32:36.075Z | 177.471° S | 74.967° | 2026-11-01 03:36:36.075Z | 346.552° 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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