PICO-02I029, 60568
Orbit data source: Space-Track
PICO-02I029, 60568 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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60568 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: 15 hours ago
TLE from 15 hours ago
0 PICO-02I029
1 60568U 24149DE 25287.22491600 .00085535 00000-0 27776-2 0 9990
2 60568 97.6980 12.0832 0002177 249.4708 110.6299 15.31595108 63895Epoch: 2025-10-14T05:23Z
TLE epoch observation values (Epoch: 2025-10-14T05:23:52.742Z)
Latitude
-0.00002°
Longitude
-91.90296°
Altitude
474.676 km
Speed
7.628 km/s
True Right ascension
00h 48m 19s
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
14:42:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.506 km
Perigee altitude
466.525 km
Semi-major axis
6,846.153 km
Eccentricity
0.00022
Inclination
97.698°
RAAN
12.0832°
Arg. of periapsis
249.4708°
True anomaly
110.65324°
Mean anomaly
110.6299°
Eccentric anomaly
110.64157°
Mean motion
3.83154 °/min
Orbital period
93.96 mins
BSTAR
0.0027776
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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-02I029 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 | 2025-10-15 05:03:47.439Z | 117.519° SE | 2025-10-15 05:05:47.439Z | 79.432° E | 20.126° | 2025-10-15 05:08:47.439Z | 19.145° NNE |
| 4 mins | 2025-10-15 18:02:47.439Z | 57.422° ENE | 2025-10-15 18:04:47.439Z | 110.232° ESE | 22.572° | 2025-10-15 18:06:47.439Z | 149.534° 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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