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: 14 hours ago
TLE from 14 hours ago
0 PICO-02A021
1 60538U 24149BY 26178.48354101 .00005445 00000-0 40532-3 0 9997
2 60538 97.6769 257.2269 0004191 4.2278 355.8982 15.03351360101288Epoch: 2026-06-27T11:36Z
TLE epoch observation values (Epoch: 2026-06-27T11:36:17.943Z)
Latitude
-0.00001°
Longitude
167.55509°
Altitude
556.731 km
Speed
7.585 km/s
True Right ascension
17h 08m 54s
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
12:43:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
556.476 km
Perigee altitude
550.666 km
Semi-major axis
6,931.708 km
Eccentricity
0.00042
Inclination
97.6769°
RAAN
257.2269°
Arg. of periapsis
4.2278°
True anomaly
355.89476°
Mean anomaly
355.8982°
Eccentric anomaly
355.89648°
Mean motion
3.76082 °/min
Orbital period
95.72 mins
BSTAR
0.00040532
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-28 05:18:09.615Z | 166.8° S | 2026-06-28 05:21:09.615Z | 169.743° S | 44.806° | 2026-06-28 05:25:09.615Z | 347.731° N |
| 5 mins | 2026-06-28 18:32:09.615Z | 349.046° N | 2026-06-28 18:34:09.615Z | 289.881° WNW | 36.663° | 2026-06-28 18:37:09.615Z | 216.289° SW |
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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