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, 0.1 m
Radar Cross Section
0.008 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 PICO-01A003
1 58326U 23174BY 26176.28783098 .00027027 00000-0 54676-3 0 9997
2 58326 97.3797 261.7794 0006817 129.1039 231.0817 15.46401483146662Epoch: 2026-06-25T06:54Z
TLE epoch observation values (Epoch: 2026-06-25T06:54:28.596Z)
Latitude
-0.0001°
Longitude
-115.27259°
Altitude
433.307 km
Speed
7.65 km/s
True Right ascension
17h 27m 07s
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
03:49:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
428.83 km
Perigee altitude
419.556 km
Semi-major axis
6,802.33 km
Eccentricity
0.00068
Inclination
97.3797°
RAAN
261.7794°
Arg. of periapsis
129.1039°
True anomaly
231.02095°
Mean anomaly
231.0817°
Eccentric anomaly
231.05132°
Mean motion
3.86863 °/min
Orbital period
93.06 mins
BSTAR
0.00054676
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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 | 2026-06-25 18:20:42.151Z | 27.964° NE | 2026-06-25 18:22:42.151Z | 79.503° E | 36.4° | 2026-06-25 18:25:42.151Z | 174.714° S |
| 4 mins | 2026-06-26 06:20:42.151Z | 218.142° SW | 2026-06-26 06:22:42.151Z | 277.328° WNW | 24° | 2026-06-26 06:24:42.151Z | 319.599° 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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