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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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-2C
1 62929U 25028B 25304.73635211 .00002307 00000-0 37237-3 0 9994
2 62929 98.0163 356.5881 0002092 55.1107 305.0297 14.72360729 38991Epoch: 2025-10-31T17:40Z
TLE epoch observation values (Epoch: 2025-10-31T17:40:20.822Z)
Latitude
0.00001°
Longitude
51.22484°
Altitude
655.705 km
Speed
7.53 km/s
True Right ascension
23h 46m 21s
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
01:55:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.069 km
Perigee altitude
649.128 km
Semi-major axis
7,028.735 km
Eccentricity
0.00021
Inclination
98.0163°
RAAN
356.5881°
Arg. of periapsis
55.1107°
True anomaly
305.01007°
Mean anomaly
305.0297°
Eccentric anomaly
305.01988°
Mean motion
3.68322 °/min
Orbital period
97.74 mins
BSTAR
0.00037237
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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 | 2025-11-01 15:28:03.272Z | 50.766° ENE | 2025-11-01 15:31:03.272Z | 95.992° ESE | 18.345° | 2025-11-01 15:34:03.272Z | 139.103° SSE |
| 6 mins | 2025-11-01 17:05:03.272Z | 346.307° N | 2025-11-01 17:08:03.272Z | 280.702° WNW | 30.947° | 2025-11-01 17:11:03.272Z | 227.406° WSW |
| 4 mins | 2025-11-02 02:28:03.272Z | 90.903° ESE | 2025-11-02 02:30:03.272Z | 58.939° ENE | 16.389° | 2025-11-02 02:32:03.272Z | 30.149° NE |
| 7 mins | 2025-11-02 04:03:03.272Z | 194.969° SSW | 2025-11-02 04:06:03.272Z | 259.482° W | 34.977° | 2025-11-02 04:10:03.272Z | 332.543° 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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