KINEIS-2C, 62929
Orbit data source: Space-Track
KINEIS-2C, 62929 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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62929 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: 18 hours ago
TLE from 18 hours ago
0 KINEIS-2C
1 62929U 25028B 25318.60045157 .00003111 00000-0 50015-3 0 9992
2 62929 98.0210 10.2630 0001234 28.9513 331.1762 14.72290328 41039Epoch: 2025-11-14T14:24Z
TLE epoch observation values (Epoch: 2025-11-14T14:24:39.015Z)
Latitude
-0.00009°
Longitude
100.15883°
Altitude
656.013 km
Speed
7.53 km/s
True Right ascension
00h 41m 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
05:31:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.69 km
Perigee altitude
649.955 km
Semi-major axis
7,028.96 km
Eccentricity
0.00012
Inclination
98.021°
RAAN
10.263°
Arg. of periapsis
28.9513°
True anomaly
331.16938°
Mean anomaly
331.1762°
Eccentric anomaly
331.17279°
Mean motion
3.68304 °/min
Orbital period
97.75 mins
BSTAR
0.00050015
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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-2C 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-15 15:28:30.922Z | 54.669° ENE | 2025-11-15 15:31:30.922Z | 102.468° ESE | 18.128° | 2025-11-15 15:33:30.922Z | 132.38° SE |
| 6 mins | 2025-11-15 17:05:30.922Z | 342.59° N | 2025-11-15 17:07:30.922Z | 301.458° NW | 30.695° | 2025-11-15 17:11:30.922Z | 225.046° WSW |
| 4 mins | 2025-11-16 02:28:30.922Z | 86.144° E | 2025-11-16 02:29:30.922Z | 70.164° E | 16.5° | 2025-11-16 02:32:30.922Z | 26.476° NE |
| 6 mins | 2025-11-16 04:03:30.922Z | 197.761° SSW | 2025-11-16 04:06:30.922Z | 272.823° WNW | 34.617° | 2025-11-16 04:09:30.922Z | 328.687° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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