KINEIS-3A, 61223
Orbit data source: Space-Track
KINEIS-3A, 61223 is a French payload satellite in SSO that was launched on Fri, 20 Sep 2024 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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61223 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-3A
1 61223U 24172D 26171.22660288 .00001389 00000-0 22751-3 0 9992
2 61223 98.0426 261.1852 0003292 90.4883 269.6701 14.72324656 93225Epoch: 2026-06-20T05:26Z
TLE epoch observation values (Epoch: 2026-06-20T05:26:18.488Z)
Latitude
-0.0001°
Longitude
-88.83608°
Altitude
656.677 km
Speed
7.529 km/s
True Right ascension
17h 24m 44s
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
07:16:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.028 km
Perigee altitude
648.4 km
Semi-major axis
7,028.851 km
Eccentricity
0.00033
Inclination
98.0426°
RAAN
261.1852°
Arg. of periapsis
90.4883°
True anomaly
269.63238°
Mean anomaly
269.6701°
Eccentric anomaly
269.65124°
Mean motion
3.68313 °/min
Orbital period
97.74 mins
BSTAR
0.00022751
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Other satellites on launch #172 in the year 2024 (2024-09-20 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-3A 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-21 06:01:01.810Z | 166.696° S | 2026-06-21 06:05:01.810Z | 181.199° SSW | 44.801° | 2026-06-21 06:09:01.810Z | 346.777° N |
| 4 mins | 2026-06-21 17:56:01.810Z | 65.687° ENE | 2026-06-21 17:58:01.810Z | 100.289° ESE | 18.552° | 2026-06-21 18:00:01.810Z | 131.351° SE |
| 6 mins | 2026-06-21 19:32:01.810Z | 343.47° N | 2026-06-21 19:35:01.810Z | 273.939° WNW | 29.959° | 2026-06-21 19:38:01.810Z | 226.519° 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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