KINEIS-5B, 62085
Orbit data source: Space-Track
KINEIS-5B, 62085 is a French payload satellite in SSO that was launched on Mon, 25 Nov 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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62085 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: 20 hours ago
TLE from 20 hours ago
0 KINEIS-5B
1 62085U 24219E 26088.17462100 .00001682 00000-0 23947-3 0 9999
2 62085 97.9979 252.5177 0002726 141.9046 218.2358 14.78139670 72187Epoch: 2026-03-29T04:11Z
TLE epoch observation values (Epoch: 2026-03-29T04:11:27.254Z)
Latitude
0.00001°
Longitude
3.06985°
Altitude
639.721 km
Speed
7.537 km/s
True Right ascension
16h 50m 04s
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
06:09:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
634.161 km
Perigee altitude
630.339 km
Semi-major axis
7,010.387 km
Eccentricity
0.00027
Inclination
97.9979°
RAAN
252.5177°
Arg. of periapsis
141.9046°
True anomaly
218.21647°
Mean anomaly
218.2358°
Eccentric anomaly
218.22614°
Mean motion
3.69769 °/min
Orbital period
97.36 mins
BSTAR
0.00023947
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Other satellites on launch #219 in the year 2024 (2024-11-25 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-5B 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 | 2026-03-30 11:11:24.080Z | 185.457° SSW | 2026-03-30 11:14:24.080Z | 267.847° W | 40.15° | 2026-03-30 11:18:24.080Z | 338.519° N |
| 6 mins | 2026-03-30 23:01:24.080Z | 47.246° ENE | 2026-03-30 23:04:24.080Z | 103.686° ESE | 23.927° | 2026-03-30 23:07:24.080Z | 150.942° SSE |
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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