PICO-02A021, 60538
Orbit data source: Space-Track
PICO-02A021, 60538 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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60538 intel report (Beta)
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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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 PICO-02A021
1 60538U 24149BY 26227.19875098 .00001973 00000-0 14829-3 0 9995
2 60538 97.6724 305.5331 0005571 155.9544 204.1942 15.03727548108609Epoch: 2026-08-15T04:46Z
TLE epoch observation values (Epoch: 2026-08-15T04:46:12.084Z)
Latitude
-0.0001°
Longitude
-89.6303°
Altitude
561.999 km
Speed
7.578 km/s
True Right ascension
20h 22m 07s
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
19:52:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
556.274 km
Perigee altitude
548.552 km
Semi-major axis
6,930.55 km
Eccentricity
0.00056
Inclination
97.6724°
RAAN
305.5331°
Arg. of periapsis
155.9544°
True anomaly
204.16805°
Mean anomaly
204.1942°
Eccentric anomaly
204.18113°
Mean motion
3.76176 °/min
Orbital period
95.7 mins
BSTAR
0.00014829
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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-02A021 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-16 18:04:29.097Z | 17.995° NNE | 2026-08-16 18:07:29.097Z | 129.453° SE | 43.648° | 2026-08-16 18:10:29.097Z | 186.35° SSW |
| 6 mins | 2026-08-17 04:49:29.097Z | 131.187° SE | 2026-08-17 04:51:29.097Z | 90.49° ESE | 30.228° | 2026-08-17 04:55:29.097Z | 5.547° NNE |
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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