KINEIS-2B, 62934
Orbit data source: Space-Track
KINEIS-2B, 62934 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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62934 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-2B
1 62934U 25028G 25260.93687090 .00001298 00000-0 21286-3 0 9990
2 62934 98.0068 313.3370 0002364 318.2723 41.8304 14.72360250 32586Epoch: 2025-09-17T22:29Z
TLE epoch observation values (Epoch: 2025-09-17T22:29:05.645Z)
Latitude
-0.00003°
Longitude
-21.04218°
Altitude
655.312 km
Speed
7.531 km/s
True Right ascension
20h 53m 20s
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
22:05:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.261 km
Perigee altitude
648.938 km
Semi-major axis
7,028.736 km
Eccentricity
0.00024
Inclination
98.0068°
RAAN
313.337°
Arg. of periapsis
318.2723°
True anomaly
41.84847°
Mean anomaly
41.8304°
Eccentric anomaly
41.83943°
Mean motion
3.68322 °/min
Orbital period
97.74 mins
BSTAR
0.00021286
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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-2B 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 | 2025-09-19 15:50:48.085Z | 38.924° NE | 2025-09-19 15:53:48.085Z | 94.289° ESE | 29.027° | 2025-09-19 15:57:48.085Z | 161.517° S |
| 5 mins | 2025-09-19 17:28:48.085Z | 322.928° NNW | 2025-09-19 17:30:48.085Z | 286.178° WNW | 20.453° | 2025-09-19 17:33:48.085Z | 243.476° WSW |
| 6 mins | 2025-09-20 02:49:48.085Z | 116.529° SE | 2025-09-20 02:51:48.085Z | 81.283° E | 25.201° | 2025-09-20 02:55:48.085Z | 12.389° NNE |
| 5 mins | 2025-09-20 04:26:48.085Z | 223.596° SW | 2025-09-20 04:28:48.085Z | 259.804° W | 22.998° | 2025-09-20 04:31:48.085Z | 312.296° NW |
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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