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: 16 hours ago
TLE from 16 hours ago
0 KINEIS-2D
1 62930U 25028C 25308.61643211 .00002193 00000-0 33584-3 0 9990
2 62930 97.9611 0.1463 0003085 180.9868 179.1336 14.74680713 39604Epoch: 2025-11-04T14:47Z
TLE epoch observation values (Epoch: 2025-11-04T14:47:39.734Z)
Latitude
0.00006°
Longitude
94.12984°
Altitude
651.345 km
Speed
7.531 km/s
True Right ascension
00h 00m 35s
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
02:25:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
645.382 km
Perigee altitude
641.05 km
Semi-major axis
7,021.353 km
Eccentricity
0.00031
Inclination
97.9611°
RAAN
0.1463°
Arg. of periapsis
180.9868°
True anomaly
179.13413°
Mean anomaly
179.1336°
Eccentric anomaly
179.13387°
Mean motion
3.68903 °/min
Orbital period
97.59 mins
BSTAR
0.00033584
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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 | 2025-11-05 15:47:35.267Z | 33.445° NE | 2025-11-05 15:51:35.267Z | 99.344° ESE | 27.979° | 2025-11-05 15:54:35.267Z | 154.264° SSE |
| 5 mins | 2025-11-05 17:25:35.267Z | 332.703° NNW | 2025-11-05 17:27:35.267Z | 299.752° NW | 20.772° | 2025-11-05 17:30:35.267Z | 248.987° W |
| 6 mins | 2025-11-06 02:46:35.267Z | 112.465° ESE | 2025-11-06 02:48:35.267Z | 76.282° E | 24.065° | 2025-11-06 02:52:35.267Z | 12.173° NNE |
| 5 mins | 2025-11-06 04:23:35.267Z | 226.491° WSW | 2025-11-06 04:25:35.267Z | 267.499° W | 24.253° | 2025-11-06 04:28:35.267Z | 317.182° NNW |
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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