KINEIS-3E, 61222
Orbit data source: Space-Track
KINEIS-3E, 61222 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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61222 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-3E
1 61222U 24172C 26171.24275924 .00001370 00000-0 22478-3 0 9998
2 61222 98.0427 261.1029 0001891 108.8158 251.3255 14.72256910 93806Epoch: 2026-06-20T05:49Z
TLE epoch observation values (Epoch: 2026-06-20T05:49:34.398Z)
Latitude
0.00004°
Longitude
-94.75062°
Altitude
657.305 km
Speed
7.529 km/s
True Right ascension
17h 24m 24s
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
07:17:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.259 km
Perigee altitude
649.601 km
Semi-major axis
7,029.067 km
Eccentricity
0.00019
Inclination
98.0427°
RAAN
261.1029°
Arg. of periapsis
108.8158°
True anomaly
251.30497°
Mean anomaly
251.3255°
Eccentric anomaly
251.31524°
Mean motion
3.68296 °/min
Orbital period
97.75 mins
BSTAR
0.00022478
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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-3E 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 04:49:50.147Z | 95.238° ESE | 2026-06-21 04:51:50.147Z | 65.955° ENE | 15.561° | 2026-06-21 04:53:50.147Z | 36.064° NE |
| 6 mins | 2026-06-21 06:25:50.147Z | 196.77° SSW | 2026-06-21 06:27:50.147Z | 240.443° WSW | 35.839° | 2026-06-21 06:31:50.147Z | 332.019° NNW |
| 6 mins | 2026-06-21 18:18:50.147Z | 49.388° ENE | 2026-06-21 18:20:50.147Z | 94.685° ESE | 29.618° | 2026-06-21 18:24:50.147Z | 162.564° S |
| 4 mins | 2026-06-21 19:55:50.147Z | 322.396° NNW | 2026-06-21 19:57:50.147Z | 286.144° WNW | 19.9° | 2026-06-21 19:59:50.147Z | 254.226° W |
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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