KINEIS-3D, 61221
Orbit data source: Space-Track
KINEIS-3D, 61221 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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61221 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: 16 hours ago
TLE from 16 hours ago
0 KINEIS-3D
1 61221U 24172B 26171.19218565 .00001433 00000-0 23468-3 0 9999
2 61221 98.0432 261.0690 0002510 119.0884 241.0575 14.72288373 93790Epoch: 2026-06-20T04:36Z
TLE epoch observation values (Epoch: 2026-06-20T04:36:44.840Z)
Latitude
0.00001°
Longitude
-76.52817°
Altitude
657.634 km
Speed
7.528 km/s
True Right ascension
17h 24m 16s
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
07:18:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.594 km
Perigee altitude
649.066 km
Semi-major axis
7,028.967 km
Eccentricity
0.00025
Inclination
98.0432°
RAAN
261.069°
Arg. of periapsis
119.0884°
True anomaly
241.03233°
Mean anomaly
241.0575°
Eccentric anomaly
241.04492°
Mean motion
3.68304 °/min
Orbital period
97.75 mins
BSTAR
0.00023468
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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-3D 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 05:13:27.169Z | 120.301° SE | 2026-06-21 05:16:27.169Z | 68.035° E | 25.011° | 2026-06-21 05:19:27.169Z | 16.822° NNE |
| 6 mins | 2026-06-21 06:50:27.169Z | 216.977° SW | 2026-06-21 06:53:27.169Z | 271.838° WNW | 23.573° | 2026-06-21 06:56:27.169Z | 318.142° NNW |
| 7 mins | 2026-06-21 18:42:27.169Z | 21.803° NNE | 2026-06-21 18:45:27.169Z | 79.538° E | 41.983° | 2026-06-21 18:49:27.169Z | 182.495° SSW |
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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