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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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, 0.072 m
Radar Cross Section
0.008 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 PICO-01A003
1 58326U 23174BY 26308.91008075 .00024578 00000-0 41120-3 0 9997
2 58326 97.3746 37.2773 0003970 16.1285 344.0094 15.51877012167198Epoch: 2026-11-04T21:50Z
TLE epoch observation values (Epoch: 2026-11-04T21:50:30.976Z)
Latitude
0.00005°
Longitude
25.49661°
Altitude
411.789 km
Speed
7.665 km/s
True Right ascension
02h 29m 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
09:44:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
410.862 km
Perigee altitude
405.474 km
Semi-major axis
6,786.305 km
Eccentricity
0.0004
Inclination
97.3746°
RAAN
37.2773°
Arg. of periapsis
16.1285°
True anomaly
343.99686°
Mean anomaly
344.0094°
Eccentric anomaly
344.00313°
Mean motion
3.88234 °/min
Orbital period
92.73 mins
BSTAR
0.0004112
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-05 18:30:59.666Z | 30.591° NE | 2026-11-05 18:33:59.666Z | 108.18° ESE | 35.744° | 2026-11-05 18:35:59.666Z | 161.021° S |
| 4 mins | 2026-11-06 06:28:59.666Z | 206.304° SW | 2026-11-06 06:30:59.666Z | 286.111° WNW | 35.648° | 2026-11-06 06:32:59.666Z | 328.467° NNW |
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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