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: 8 hours ago
TLE from 8 hours ago
0 KINEIS-2C
1 62929U 25028B 26091.15416192 .00001544 00000-0 25222-3 0 9992
2 62929 98.0293 146.0401 0000812 167.6292 192.4935 14.72293730 61278Epoch: 2026-04-01T03:41Z
TLE epoch observation values (Epoch: 2026-04-01T03:41:59.589Z)
Latitude
-0.00009°
Longitude
-98.97925°
Altitude
657.32 km
Speed
7.528 km/s
True Right ascension
09h 44m 09s
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
17:41:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.383 km
Perigee altitude
650.241 km
Semi-major axis
7,028.949 km
Eccentricity
0.00008
Inclination
98.0293°
RAAN
146.0401°
Arg. of periapsis
167.6292°
True anomaly
192.49149°
Mean anomaly
192.4935°
Eccentric anomaly
192.49249°
Mean motion
3.68305 °/min
Orbital period
97.75 mins
BSTAR
0.00025222
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-01 15:42:13.270Z | 42.894° NE | 2026-04-01 15:45:13.270Z | 91.816° ESE | 24.119° | 2026-04-01 15:48:13.270Z | 145.374° SSE |
| 5 mins | 2026-04-01 17:20:13.270Z | 328.985° NNW | 2026-04-01 17:22:13.270Z | 288.051° WNW | 24.58° | 2026-04-01 17:25:13.270Z | 238.762° WSW |
| 5 mins | 2026-04-02 02:42:13.270Z | 99.674° ESE | 2026-04-02 02:44:13.270Z | 61.884° ENE | 21.493° | 2026-04-02 02:47:13.270Z | 17.528° NNE |
| 6 mins | 2026-04-02 04:18:13.270Z | 214.672° SW | 2026-04-02 04:20:13.270Z | 254.275° W | 27.459° | 2026-04-02 04:24:13.270Z | 324.319° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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