KINEIS-2C, 62929
Orbit data source: Space-Track
KINEIS-2C, 62929 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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62929 intel report (Beta)
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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: 18 hours ago
TLE from 18 hours ago
0 KINEIS-2C
1 62929U 25028B 26171.10515420 .00001045 00000-0 16921-3 0 9992
2 62929 98.1241 225.5020 0002343 248.6652 111.4305 14.73359912 73049Epoch: 2026-06-20T02:31Z
TLE epoch observation values (Epoch: 2026-06-20T02:31:25.322Z)
Latitude
-0.00011°
Longitude
-80.67805°
Altitude
653.97 km
Speed
7.53 km/s
True Right ascension
15h 02m 00s
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
07:22:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
649.068 km
Perigee altitude
645.776 km
Semi-major axis
7,025.559 km
Eccentricity
0.00023
Inclination
98.1241°
RAAN
225.502°
Arg. of periapsis
248.6652°
True anomaly
111.45549°
Mean anomaly
111.4305°
Eccentric anomaly
111.443°
Mean motion
3.68572 °/min
Orbital period
97.67 mins
BSTAR
0.00016921
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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-2C 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 | 2026-06-21 03:06:13.697Z | 136.69° SSE | 2026-06-21 03:10:13.697Z | 54.804° ENE | 31.93° | 2026-06-21 03:13:13.697Z | 6.308° NNE |
| 4 mins | 2026-06-21 04:45:13.697Z | 244.201° WSW | 2026-06-21 04:46:13.697Z | 260.493° W | 17.077° | 2026-06-21 04:49:13.697Z | 305.843° NW |
| 7 mins | 2026-06-21 16:35:13.697Z | 11.594° NNE | 2026-06-21 16:38:13.697Z | 358.052° N | 44.11° | 2026-06-21 16:42:13.697Z | 195.852° 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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