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 25300.28373524 .00017155 00000-0 49696-3 0 9991
2 58326 97.4019 18.0048 0006034 281.0719 78.9845 15.35618914109541Epoch: 2025-10-27T06:48Z
TLE epoch observation values (Epoch: 2025-10-27T06:48:34.724Z)
Latitude
-0.00013°
Longitude
-120.02766°
Altitude
461.408 km
Speed
7.636 km/s
True Right ascension
01h 12m 01s
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
08:53:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.151 km
Perigee altitude
451.904 km
Semi-major axis
6,834.165 km
Eccentricity
0.0006
Inclination
97.4019°
RAAN
18.0048°
Arg. of periapsis
281.0719°
True anomaly
79.05238°
Mean anomaly
78.9845°
Eccentric anomaly
79.01844°
Mean motion
3.84163 °/min
Orbital period
93.71 mins
BSTAR
0.00049696
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-27 18:18:52.300Z | 5.68° NNE | 2025-10-27 18:21:52.300Z | 263.302° W | 42.773° | 2025-10-27 18:24:52.300Z | 201.018° SSW |
| 4 mins | 2025-10-28 04:51:52.300Z | 112.34° ESE | 2025-10-28 04:52:52.300Z | 81.987° E | 27.417° | 2025-10-28 04:55:52.300Z | 11.243° NNE |
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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