PICO-02D024, 60569
Orbit data source: Space-Track
PICO-02D024, 60569 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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60569 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-02D024
1 60569U 24149DF 25297.80090653 .00115331 00000-0 33877-2 0 9996
2 60569 97.7036 23.4881 0002600 253.9078 106.1878 15.34662685 65523Epoch: 2025-10-24T19:13Z
TLE epoch observation values (Epoch: 2025-10-24T19:13:18.324Z)
Latitude
-0.00001°
Longitude
61.72115°
Altitude
465.52 km
Speed
7.633 km/s
True Right ascension
01h 33m 57s
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
20:07:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.66 km
Perigee altitude
457.104 km
Semi-major axis
6,837.019 km
Eccentricity
0.00026
Inclination
97.7036°
RAAN
23.4881°
Arg. of periapsis
253.9078°
True anomaly
106.21641°
Mean anomaly
106.1878°
Eccentric anomaly
106.20211°
Mean motion
3.83922 °/min
Orbital period
93.77 mins
BSTAR
0.0033877
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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-02D024 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 06:19:03.224Z | 207.349° SW | 2025-10-25 06:21:03.224Z | 273.475° WNW | 30.473° | 2025-10-25 06:23:03.224Z | 322.511° NNW |
| 4 mins | 2025-10-25 19:16:03.224Z | 333.468° NNW | 2025-10-25 19:18:03.224Z | 269.953° W | 26.908° | 2025-10-25 19:20:03.224Z | 228.772° WSW |
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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