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: 22 hours ago
TLE from 22 hours ago
0 KINEIS-2D
1 62930U 25028C 25288.39563707 .00002844 00000-0 43463-3 0 9993
2 62930 97.9643 340.2691 0001803 266.9106 93.1896 14.74559621 36624Epoch: 2025-10-15T09:29Z
TLE epoch observation values (Epoch: 2025-10-15T09:29:43.042Z)
Latitude
-0.00009°
Longitude
173.66945°
Altitude
649.632 km
Speed
7.533 km/s
True Right ascension
22h 41m 04s
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
02:14:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
644.867 km
Perigee altitude
642.335 km
Semi-major axis
7,021.738 km
Eccentricity
0.00018
Inclination
97.9643°
RAAN
340.2691°
Arg. of periapsis
266.9106°
True anomaly
93.21023°
Mean anomaly
93.1896°
Eccentric anomaly
93.19991°
Mean motion
3.68873 °/min
Orbital period
97.59 mins
BSTAR
0.00043463
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-16 15:24:09.280Z | 52.33° ENE | 2025-10-16 15:27:09.280Z | 96.708° ESE | 17.023° | 2025-10-16 15:29:09.280Z | 127.234° SE |
| 6 mins | 2025-10-16 17:01:09.280Z | 346.34° N | 2025-10-16 17:04:09.280Z | 273.404° WNW | 31.974° | 2025-10-16 17:07:09.280Z | 223.601° SW |
| 7 mins | 2025-10-17 03:58:09.280Z | 192.075° SSW | 2025-10-17 04:01:09.280Z | 267.838° W | 37.189° | 2025-10-17 04:05:09.280Z | 335.612° 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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