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: 8 hours ago
TLE from 8 hours ago
0 KINEIS-2D
1 62930U 25028C 26278.15883340 .00000952 00000-0 14575-3 0 9995
2 62930 97.9170 328.4400 0002936 184.9617 175.1564 14.75946042 88931Epoch: 2026-10-05T03:48Z
TLE epoch observation values (Epoch: 2026-10-05T03:48:43.205Z)
Latitude
-0.00005°
Longitude
-102.58175°
Altitude
647.219 km
Speed
7.533 km/s
True Right ascension
21h 53m 45s
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
05:56:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
641.257 km
Perigee altitude
637.137 km
Semi-major axis
7,017.334 km
Eccentricity
0.00029
Inclination
97.917°
RAAN
328.44°
Arg. of periapsis
184.9617°
True anomaly
175.15924°
Mean anomaly
175.1564°
Eccentric anomaly
175.15782°
Mean motion
3.6922 °/min
Orbital period
97.5 mins
BSTAR
0.00014575
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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 | 2026-10-05 15:46:33.308Z | 32.448° NE | 2026-10-05 15:50:33.308Z | 106.438° ESE | 35.77° | 2026-10-05 15:53:33.308Z | 159.765° S |
| 5 mins | 2026-10-05 17:24:33.308Z | 327.104° NNW | 2026-10-05 17:26:33.308Z | 293.641° NW | 20.323° | 2026-10-05 17:29:33.308Z | 248.478° W |
| 6 mins | 2026-10-06 02:44:33.308Z | 117.197° SE | 2026-10-06 02:46:33.308Z | 81.456° E | 28.44° | 2026-10-06 02:50:33.308Z | 12.077° NNE |
| 5 mins | 2026-10-06 04:21:33.308Z | 227.283° WSW | 2026-10-06 04:23:33.308Z | 265.04° W | 24.588° | 2026-10-06 04:26:33.308Z | 314.469° NW |
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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