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: 9 hours ago
TLE from 9 hours ago
0 KINEIS-2B
1 62934U 25028G 25258.15053700 .00001782 00000-0 28943-3 0 9991
2 62934 98.0072 310.5926 0002547 330.7824 29.3241 14.72356219 32177Epoch: 2025-09-15T03:36Z
TLE epoch observation values (Epoch: 2025-09-15T03:36:46.396Z)
Latitude
-0°
Longitude
-97.96003°
Altitude
655.002 km
Speed
7.531 km/s
True Right ascension
20h 42m 22s
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
04:51:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.402 km
Perigee altitude
648.822 km
Semi-major axis
7,028.749 km
Eccentricity
0.00025
Inclination
98.0072°
RAAN
310.5926°
Arg. of periapsis
330.7824°
True anomaly
29.3384°
Mean anomaly
29.3241°
Eccentric anomaly
29.33125°
Mean motion
3.68321 °/min
Orbital period
97.74 mins
BSTAR
0.00028943
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-15 15:37:15.202Z | 47.038° ENE | 2025-09-15 15:40:15.202Z | 97.064° ESE | 22.391° | 2025-09-15 15:43:15.202Z | 145.024° SSE |
| 6 mins | 2025-09-15 17:14:15.202Z | 340.658° N | 2025-09-15 17:17:15.202Z | 281.756° WNW | 26.233° | 2025-09-15 17:20:15.202Z | 234.119° WSW |
| 4 mins | 2025-09-16 02:37:15.202Z | 93.742° ESE | 2025-09-16 02:38:15.202Z | 76.363° E | 19.611° | 2025-09-16 02:41:15.202Z | 26.441° NE |
| 7 mins | 2025-09-16 04:12:15.202Z | 203.577° SW | 2025-09-16 04:15:15.202Z | 261.459° W | 29.839° | 2025-09-16 04:19:15.202Z | 328.112° 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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