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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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: 11 hours ago
TLE from 11 hours ago
0 KINEIS-2D
1 62930U 25028C 26008.60955945 .00002324 00000-0 35223-3 0 9995
2 62930 97.9516 64.0129 0003262 22.6334 337.5018 14.75078491 49189Epoch: 2026-01-08T14:37Z
TLE epoch observation values (Epoch: 2026-01-08T14:37:45.936Z)
Latitude
-0.00006°
Longitude
96.41031°
Altitude
645.798 km
Speed
7.536 km/s
True Right ascension
04h 16m 03s
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
01:24:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
644.242 km
Perigee altitude
639.662 km
Semi-major axis
7,020.089 km
Eccentricity
0.00033
Inclination
97.9516°
RAAN
64.0129°
Arg. of periapsis
22.6334°
True anomaly
337.48749°
Mean anomaly
337.5018°
Eccentric anomaly
337.49465°
Mean motion
3.69002 °/min
Orbital period
97.56 mins
BSTAR
0.00035223
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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 | 2026-01-09 03:47:11.045Z | 181.366° SSW | 2026-01-09 03:50:11.045Z | 275.437° WNW | 41.917° | 2026-01-09 03:54:11.045Z | 340.811° N |
| 5 mins | 2026-01-09 15:39:11.045Z | 56.004° ENE | 2026-01-09 15:41:11.045Z | 94.264° ESE | 23.407° | 2026-01-09 15:44:11.045Z | 145.599° SSE |
| 6 mins | 2026-01-09 17:15:11.045Z | 338.837° N | 2026-01-09 17:18:11.045Z | 281.085° WNW | 24.692° | 2026-01-09 17:21:11.045Z | 235.389° WSW |
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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