PICO-02D024, 60569 (Decayed)
Orbit data source: Space-Track
PICO-02D024, 60569 was a payload satellite owned by Apogeo Space (IT) in LEO 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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Identifier
Orbit
Country
ITRelated business
Manufacturer
Apogeo Space
Mission
Decayed 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: 2 months ago
TLE from 2 months ago
0 PICO-02D024
1 60569U 24149DF 26033.73415338 .12918043 26154-5 28726-2 0 9992
2 60569 97.6361 132.0017 0012276 302.0457 57.9643 16.30146191 81211Epoch: 2026-02-02T17:37Z
TLE epoch observation values (Epoch: 2026-02-02T17:37:10.852Z)
Latitude
-0.00004°
Longitude
94.7813°
Altitude
191.106 km
Speed
7.794 km/s
True Right ascension
08h 48m 00s
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
09:09:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
197.04 km
Perigee altitude
180.916 km
Semi-major axis
6,567.115 km
Eccentricity
0.00123
Inclination
97.6361°
RAAN
132.0017°
Arg. of periapsis
302.0457°
True anomaly
58.08365°
Mean anomaly
57.9643°
Eccentric anomaly
58.02396°
Mean motion
4.07832 °/min
Orbital period
88.27 mins
BSTAR
0.0028726
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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
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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. |
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| This satellite is decayed. |
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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