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: 19 hours ago
TLE from 19 hours ago
0 INTUITION-1
1 58565U 23174CW 26022.97222936 .00153547 00000-0 11649-2 0 9996
2 58565 97.3866 116.0464 0004893 282.5047 77.5669 15.71869246123650Epoch: 2026-01-22T23:20Z
TLE epoch observation values (Epoch: 2026-01-22T23:20:00.616Z)
Latitude
-0°
Longitude
3.7261°
Altitude
356.008 km
Speed
7.696 km/s
True Right ascension
07h 44m 11s
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
19:41:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
353.743 km
Perigee altitude
347.159 km
Semi-major axis
6,728.588 km
Eccentricity
0.00049
Inclination
97.3866°
RAAN
116.0464°
Arg. of periapsis
282.5047°
True anomaly
77.62166°
Mean anomaly
77.5669°
Eccentric anomaly
77.59428°
Mean motion
3.9324 °/min
Orbital period
91.55 mins
BSTAR
0.0011649
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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 | 2026-01-24 06:02:15.447Z | 150.95° SSE | 2026-01-24 06:03:15.447Z | 115.067° SE | 40.666° | 2026-01-24 06:06:15.447Z | 354.197° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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