PICO-02E025, 60572
Orbit data source: Space-Track
PICO-02E025, 60572 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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60572 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: 6 hours ago
TLE from 6 hours ago
0 PICO-02E025
1 60572U 24149DJ 25297.77222676 .00159278 00000-0 37883-2 0 9997
2 60572 97.7109 24.9866 0002465 292.6625 67.4359 15.41014525 65596Epoch: 2025-10-24T18:32Z
TLE epoch observation values (Epoch: 2025-10-24T18:32:00.392Z)
Latitude
-0.00008°
Longitude
73.57264°
Altitude
445.579 km
Speed
7.645 km/s
True Right ascension
01h 39m 56s
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
20:02:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.746 km
Perigee altitude
438.384 km
Semi-major axis
6,818.202 km
Eccentricity
0.00025
Inclination
97.7109°
RAAN
24.9866°
Arg. of periapsis
292.6625°
True anomaly
67.46199°
Mean anomaly
67.4359°
Eccentric anomaly
67.44894°
Mean motion
3.85512 °/min
Orbital period
93.38 mins
BSTAR
0.0037883
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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-02E025 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 | 2025-10-25 05:35:02.911Z | 135.96° SSE | 2025-10-25 05:37:02.911Z | 83.924° E | 31.722° | 2025-10-25 05:40:02.911Z | 5.825° NNE |
| 4 mins | 2025-10-25 18:29:02.911Z | 39.202° NE | 2025-10-25 18:31:02.911Z | 107.078° ESE | 32.85° | 2025-10-25 18:33:02.911Z | 163.105° S |
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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