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: 7 hours ago
TLE from 7 hours ago
0 PICO-02A021
1 60538U 24149BY 26112.17559932 .00004598 00000-0 34902-3 0 9992
2 60538 97.6726 191.5122 0004831 199.7103 160.3935 15.02688755 91327Epoch: 2026-04-22T04:12Z
TLE epoch observation values (Epoch: 2026-04-22T04:12:51.781Z)
Latitude
-0.00011°
Longitude
-81.94434°
Altitude
564.826 km
Speed
7.577 km/s
True Right ascension
12h 46m 02s
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
17:55:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
558.96 km
Perigee altitude
552.26 km
Semi-major axis
6,933.747 km
Eccentricity
0.00048
Inclination
97.6726°
RAAN
191.5122°
Arg. of periapsis
199.7103°
True anomaly
160.41207°
Mean anomaly
160.3935°
Eccentric anomaly
160.40278°
Mean motion
3.75916 °/min
Orbital period
95.77 mins
BSTAR
0.00034902
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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 | 2026-04-22 17:34:17.361Z | 34.977° NE | 2026-04-22 17:37:17.361Z | 91.91° ESE | 28.712° | 2026-04-22 17:40:17.361Z | 157.194° SSE |
| 4 mins | 2026-04-23 04:21:17.361Z | 96.137° ESE | 2026-04-23 04:22:17.361Z | 77.899° E | 17.903° | 2026-04-23 04:25:17.361Z | 25.637° NE |
| 5 mins | 2026-04-23 05:55:17.361Z | 213.705° SW | 2026-04-23 05:57:17.361Z | 257.86° W | 26.724° | 2026-04-23 06:00:17.361Z | 319.93° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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