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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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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 KINEIS-5B
1 62085U 24219E 25260.32258912 .00001313 00000-0 19297-3 0 9995
2 62085 97.9809 61.3900 0003089 80.2172 279.9387 14.77140088 43703Epoch: 2025-09-17T07:44Z
TLE epoch observation values (Epoch: 2025-09-17T07:44:31.699Z)
Latitude
-0.00004°
Longitude
-51.24227°
Altitude
641.008 km
Speed
7.538 km/s
True Right ascension
04h 05m 33s
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
13:25:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
637.581 km
Perigee altitude
633.248 km
Semi-major axis
7,013.551 km
Eccentricity
0.00031
Inclination
97.9809°
RAAN
61.39°
Arg. of periapsis
80.2172°
True anomaly
279.90383°
Mean anomaly
279.9387°
Eccentric anomaly
279.92127°
Mean motion
3.69519 °/min
Orbital period
97.42 mins
BSTAR
0.00019297
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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 | 2025-09-17 22:57:03.964Z | 38.722° NE | 2025-09-17 23:01:03.964Z | 106.86° ESE | 24.245° | 2025-09-17 23:04:03.964Z | 152.523° SSE |
| 5 mins | 2025-09-18 00:35:03.964Z | 329.117° NNW | 2025-09-18 00:37:03.964Z | 289.442° WNW | 23.451° | 2025-09-18 00:40:03.964Z | 240.154° WSW |
| 5 mins | 2025-09-18 09:55:03.964Z | 103.086° ESE | 2025-09-18 09:57:03.964Z | 67.062° ENE | 20.879° | 2025-09-18 10:00:03.964Z | 19.949° NNE |
| 6 mins | 2025-09-18 11:31:03.964Z | 214.711° SW | 2025-09-18 11:33:03.964Z | 255.772° W | 27.521° | 2025-09-18 11:37:03.964Z | 325.327° NNW |
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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