KINEIS-2A, 62932
Orbit data source: Space-Track
KINEIS-2A, 62932 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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62932 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, 0.8 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-2A
1 62932U 25028E 25260.10322433 .00001226 00000-0 20198-3 0 9996
2 62932 98.0211 312.7581 0001611 335.8739 24.2393 14.72270572 32420Epoch: 2025-09-17T02:28Z
TLE epoch observation values (Epoch: 2025-09-17T02:28:38.582Z)
Latitude
0.00003°
Longitude
-80.68664°
Altitude
655.803 km
Speed
7.53 km/s
True Right ascension
20h 51m 01s
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
12:46:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.018 km
Perigee altitude
649.753 km
Semi-major axis
7,029.022 km
Eccentricity
0.00016
Inclination
98.0211°
RAAN
312.7581°
Arg. of periapsis
335.8739°
True anomaly
24.24688°
Mean anomaly
24.2393°
Eccentric anomaly
24.24309°
Mean motion
3.68299 °/min
Orbital period
97.75 mins
BSTAR
0.00020198
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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-2A 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 | 2025-09-18 03:04:27.067Z | 137.861° SSE | 2025-09-18 03:08:27.067Z | 56.925° ENE | 32.558° | 2025-09-18 03:11:27.067Z | 6.471° NNE |
| 4 mins | 2025-09-18 04:43:27.067Z | 242.411° WSW | 2025-09-18 04:45:27.067Z | 275.174° WNW | 16.672° | 2025-09-18 04:47:27.067Z | 303.925° NW |
| 7 mins | 2025-09-18 16:34:27.067Z | 9.635° NNE | 2025-09-18 16:37:27.067Z | 284.977° WNW | 44.708° | 2025-09-18 16:41:27.067Z | 197.489° 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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