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, 1.0 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 KINEIS-2B
1 62934U 25028G 25311.15412500 .00002179 00000-0 35002-3 0 9993
2 62934 97.9983 2.7813 0004646 131.7592 228.4014 14.72615913 39978Epoch: 2025-11-07T03:41Z
TLE epoch observation values (Epoch: 2025-11-07T03:41:56.399Z)
Latitude
0.00001°
Longitude
-99.30586°
Altitude
657.908 km
Speed
7.527 km/s
True Right ascension
00h 11m 07s
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
12:29:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.05 km
Perigee altitude
646.519 km
Semi-major axis
7,027.922 km
Eccentricity
0.00046
Inclination
97.9983°
RAAN
2.7813°
Arg. of periapsis
131.7592°
True anomaly
228.3616°
Mean anomaly
228.4014°
Eccentric anomaly
228.3815°
Mean motion
3.68386 °/min
Orbital period
97.72 mins
BSTAR
0.00035002
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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 | 2025-11-07 17:18:51.795Z | 341.607° N | 2025-11-07 17:21:51.795Z | 290.422° WNW | 23.966° | 2025-11-07 17:24:51.795Z | 240.396° WSW |
| 5 mins | 2025-11-08 02:41:51.795Z | 100.03° ESE | 2025-11-08 02:43:51.795Z | 61.651° ENE | 21.792° | 2025-11-08 02:46:51.795Z | 17.14° NNE |
| 6 mins | 2025-11-08 04:17:51.795Z | 215.733° SW | 2025-11-08 04:19:51.795Z | 255.197° W | 27.009° | 2025-11-08 04:23:51.795Z | 324.13° NNW |
| 7 mins | 2025-11-08 16:09:51.795Z | 29.523° NE | 2025-11-08 16:12:51.795Z | 114.355° SE | 38.843° | 2025-11-08 16:16:51.795Z | 178.016° S |
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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