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, 0.072 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 26276.03543826 .00003428 00000-0 25198-3 0 9991
2 60538 97.6673 353.9526 0004935 23.5587 336.5864 15.04076259115940Epoch: 2026-10-03T00:51Z
TLE epoch observation values (Epoch: 2026-10-03T00:51:01.865Z)
Latitude
-0.00003°
Longitude
-30.55398°
Altitude
554.264 km
Speed
7.586 km/s
True Right ascension
23h 35m 48s
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
02:46:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
554.761 km
Perigee altitude
547.921 km
Semi-major axis
6,929.478 km
Eccentricity
0.00049
Inclination
97.6673°
RAAN
353.9526°
Arg. of periapsis
23.5587°
True anomaly
336.56392°
Mean anomaly
336.5864°
Eccentric anomaly
336.57516°
Mean motion
3.76264 °/min
Orbital period
95.68 mins
BSTAR
0.00025198
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-04 17:20:54.777Z | 48.558° ENE | 2026-10-04 17:23:54.777Z | 102.632° ESE | 20.927° | 2026-10-04 17:25:54.777Z | 137.567° SSE |
| 4 mins | 2026-10-04 18:56:54.777Z | 323.541° NNW | 2026-10-04 18:57:54.777Z | 300.917° NW | 26.284° | 2026-10-04 19:00:54.777Z | 239.224° WSW |
| 5 mins | 2026-10-05 05:40:54.777Z | 195.87° SSW | 2026-10-05 05:42:54.777Z | 261.949° W | 50.75° | 2026-10-05 05:45:54.777Z | 333.232° 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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