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: 14 hours ago
TLE from 14 hours ago
0 KINEIS-2B
1 62934U 25028G 25305.37854658 .00002229 00000-0 35807-3 0 9993
2 62934 98.0001 357.0962 0004358 146.0184 214.1303 14.72591017 39126Epoch: 2025-11-01T09:05Z
TLE epoch observation values (Epoch: 2025-11-01T09:05:06.424Z)
Latitude
-0.00007°
Longitude
179.90996°
Altitude
658.354 km
Speed
7.527 km/s
True Right ascension
23h 48m 23s
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
18:28:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.927 km
Perigee altitude
646.801 km
Semi-major axis
7,028.001 km
Eccentricity
0.00044
Inclination
98.0001°
RAAN
357.0962°
Arg. of periapsis
146.0184°
True anomaly
214.10229°
Mean anomaly
214.1303°
Eccentric anomaly
214.1163°
Mean motion
3.68379 °/min
Orbital period
97.73 mins
BSTAR
0.00035807
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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 | 2025-11-02 03:09:10.671Z | 142.415° SSE | 2025-11-02 03:13:10.671Z | 52.72° ENE | 35.317° | 2025-11-02 03:16:10.671Z | 3.147° NNE |
| 4 mins | 2025-11-02 04:48:10.671Z | 245.044° WSW | 2025-11-02 04:50:10.671Z | 275.363° WNW | 14.642° | 2025-11-02 04:52:10.671Z | 302.504° NW |
| 7 mins | 2025-11-02 16:39:10.671Z | 4.438° NNE | 2025-11-02 16:42:10.671Z | 260.767° W | 43.033° | 2025-11-02 16:46:10.671Z | 202.037° SSW |
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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