KINEIS-2D, 62930
Orbit data source: Space-Track
KINEIS-2D, 62930 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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62930 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: 15 hours ago
TLE from 15 hours ago
0 KINEIS-2D
1 62930U 25028C 26123.70472100 .00001802 00000-0 27192-3 0 9997
2 62930 97.9316 177.0053 0003070 17.3073 342.8241 14.75543322 66159Epoch: 2026-05-03T16:54Z
TLE epoch observation values (Epoch: 2026-05-03T16:54:47.894Z)
Latitude
0.00003°
Longitude
61.70129°
Altitude
644.382 km
Speed
7.537 km/s
True Right ascension
11h 48m 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
16:12:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
642.63 km
Perigee altitude
638.321 km
Semi-major axis
7,018.612 km
Eccentricity
0.00031
Inclination
97.9316°
RAAN
177.0053°
Arg. of periapsis
17.3073°
True anomaly
342.81371°
Mean anomaly
342.8241°
Eccentric anomaly
342.8189°
Mean motion
3.69119 °/min
Orbital period
97.53 mins
BSTAR
0.00027192
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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-2D 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 | 2026-05-04 16:16:15.731Z | 18.361° NNE | 2026-05-04 16:20:15.731Z | 145.395° SSE | 42.401° | 2026-05-04 16:23:15.731Z | 184.926° SSW |
| 6 mins | 2026-05-05 03:14:15.731Z | 141.74° SSE | 2026-05-05 03:16:15.731Z | 94.141° ESE | 38.892° | 2026-05-05 03:20:15.731Z | 358.585° 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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