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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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: 9 hours ago
TLE from 9 hours ago
0 KINEIS-2A
1 62932U 25028E 26091.11764338 .00001675 00000-0 27374-3 0 9995
2 62932 98.0934 146.5062 0001330 130.4711 229.6612 14.72164480 61265Epoch: 2026-04-01T02:49Z
TLE epoch observation values (Epoch: 2026-04-01T02:49:24.388Z)
Latitude
-0.00001°
Longitude
-85.33049°
Altitude
657.777 km
Speed
7.528 km/s
True Right ascension
09h 46m 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
17:41:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.162 km
Perigee altitude
650.292 km
Semi-major axis
7,029.364 km
Eccentricity
0.00013
Inclination
98.0934°
RAAN
146.5062°
Arg. of periapsis
130.4711°
True anomaly
229.64958°
Mean anomaly
229.6612°
Eccentric anomaly
229.65539°
Mean motion
3.68272 °/min
Orbital period
97.75 mins
BSTAR
0.00027374
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-01 16:26:13.404Z | 15.613° NNE | 2026-04-01 16:30:13.404Z | 73.27° E | 44.307° | 2026-04-01 16:34:13.404Z | 189.117° SSW |
| 8 mins | 2026-04-02 03:24:13.404Z | 155.82° SSE | 2026-04-02 03:28:13.404Z | 106.993° ESE | 41.372° | 2026-04-02 03:32:13.404Z | 355.072° N |
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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