PICO-01A003, 58326
Orbit data source: Space-Track
PICO-01A003, 58326 is a payload satellite owned by Apogeo Space (IT) 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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58326 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ITRelated business
Manufacturer
Apogeo Space
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 0.3U, Unknown motor
Mass
0.5 kg wet, 0.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.008 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 PICO-01A003
1 58326U 23174BY 26039.24589520 .00024141 00000-0 59420-3 0 9991
2 58326 97.3883 122.7788 0005417 265.7959 94.2668 15.40587134125527Epoch: 2026-02-08T05:54Z
TLE epoch observation values (Epoch: 2026-02-08T05:54:05.345Z)
Latitude
-0.00004°
Longitude
-104.10129°
Altitude
447.771 km
Speed
7.643 km/s
True Right ascension
08h 11m 06s
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
14:43:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.007 km
Perigee altitude
437.619 km
Semi-major axis
6,819.45 km
Eccentricity
0.00054
Inclination
97.3883°
RAAN
122.7788°
Arg. of periapsis
265.7959°
True anomaly
94.3287°
Mean anomaly
94.2668°
Eccentric anomaly
94.29775°
Mean motion
3.85407 °/min
Orbital period
93.41 mins
BSTAR
0.0005942
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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.PICO-01A003 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 | 2026-02-08 18:56:22.416Z | 334.725° NNW | 2026-02-08 18:58:22.416Z | 281.016° WNW | 24.443° | 2026-02-08 19:00:22.416Z | 235.503° WSW |
| 5 mins | 2026-02-09 05:25:22.416Z | 158.936° S | 2026-02-09 05:27:22.416Z | 109.32° ESE | 43.34° | 2026-02-09 05:30:22.416Z | 352.814° 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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