PICO-02F026, 60567
Orbit data source: Space-Track
PICO-02F026, 60567 is a payload satellite owned by Apogeo Space (IT) in SSO that was launched on Fri, 16 Aug 2024 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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60567 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 PICO-02F026
1 60567U 24149DD 25297.48882227 .00117112 00000-0 34813-2 0 9994
2 60567 97.7043 23.1373 0002257 255.6634 104.4357 15.34277194 65471Epoch: 2025-10-24T11:43Z
TLE epoch observation values (Epoch: 2025-10-24T11:43:54.244Z)
Latitude
-0.00005°
Longitude
174.02829°
Altitude
466.555 km
Speed
7.633 km/s
True Right ascension
01h 32m 32s
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
19:58:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.572 km
Perigee altitude
458.485 km
Semi-major axis
6,838.165 km
Eccentricity
0.00023
Inclination
97.7043°
RAAN
23.1373°
Arg. of periapsis
255.6634°
True anomaly
104.46074°
Mean anomaly
104.4357°
Eccentric anomaly
104.44822°
Mean motion
3.83825 °/min
Orbital period
93.79 mins
BSTAR
0.0034813
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-02F026 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 | 2025-10-25 05:06:19.176Z | 107.87° ESE | 2025-10-25 05:08:19.176Z | 63.547° ENE | 19.187° | 2025-10-25 05:10:19.176Z | 24.548° NE |
| 4 mins | 2025-10-25 18:03:19.176Z | 58.711° ENE | 2025-10-25 18:05:19.176Z | 108.195° ESE | 20.671° | 2025-10-25 18:07:19.176Z | 146.605° SSE |
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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