INTUITION-1, 58565
Orbit data source: Space-Track
INTUITION-1, 58565 is a payload satellite owned by KP Labs (PL) in SSO that was launched on Sat, 11 Nov 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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58565 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
PL / POLRelated business
Manufacturer
AAC ClydeSpace
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.092 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 INTUITION-1
1 58565U 23174CW 25289.20718149 .00067625 00000-0 10858-2 0 9994
2 58565 97.4014 12.9957 0005890 289.9040 70.1578 15.52797712108242Epoch: 2025-10-16T04:58Z
TLE epoch observation values (Epoch: 2025-10-16T04:58:20.480Z)
Latitude
-0.00004°
Longitude
-86.55985°
Altitude
410.342 km
Speed
7.665 km/s
True Right ascension
00h 51m 58s
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
12:43:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
409.48 km
Perigee altitude
401.488 km
Semi-major axis
6,783.621 km
Eccentricity
0.00059
Inclination
97.4014°
RAAN
12.9957°
Arg. of periapsis
289.904°
True anomaly
70.2213°
Mean anomaly
70.1578°
Eccentric anomaly
70.18955°
Mean motion
3.88464 °/min
Orbital period
92.67 mins
BSTAR
0.0010858
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Other satellites on launch #174 in the year 2023 (2023-11-11 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.INTUITION-1 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 | 2025-10-17 05:52:09.202Z | 180.906° SSW | 2025-10-17 05:53:09.202Z | 224.865° SW | 43.261° | 2025-10-17 05:56:09.202Z | 343.635° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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