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, 1.0 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 KINEIS-2A
1 62932U 25028E 26008.39348977 .00002691 00000-0 43744-3 0 9998
2 62932 98.0266 64.4767 0003983 340.3749 19.7304 14.71908291 49090Epoch: 2026-01-08T09:26Z
TLE epoch observation values (Epoch: 2026-01-08T09:26:37.516Z)
Latitude
-0.00002°
Longitude
174.87215°
Altitude
655.352 km
Speed
7.531 km/s
True Right ascension
04h 17m 54s
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
01:15:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
654.84 km
Perigee altitude
649.24 km
Semi-major axis
7,030.177 km
Eccentricity
0.0004
Inclination
98.0266°
RAAN
64.4767°
Arg. of periapsis
340.3749°
True anomaly
19.74582°
Mean anomaly
19.7304°
Eccentric anomaly
19.73811°
Mean motion
3.68208 °/min
Orbital period
97.77 mins
BSTAR
0.00043744
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Other satellites on launch #28 in the year 2025 (2025-02-08 UTC)
Did you know?
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
Loading observer location...
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 | 2026-01-09 03:30:42.500Z | 161.352° S | 2026-01-09 03:34:42.500Z | 29.201° NE | 44.032° | 2026-01-09 03:38:42.500Z | 349.941° N |
| 4 mins | 2026-01-09 15:25:42.500Z | 70.708° E | 2026-01-09 15:26:42.500Z | 86.532° E | 16.54° | 2026-01-09 15:29:42.500Z | 131.032° SE |
| 6 mins | 2026-01-09 17:01:42.500Z | 345.049° N | 2026-01-09 17:03:42.500Z | 300.876° NW | 33.284° | 2026-01-09 17:07:42.500Z | 221.051° SW |
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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