Showing default

PICO-02G027, 60566

Orbit data source: Space-Track

PICO-02G027, 60566 is a payload satellite owned by Apogeo Space (IT) in LEO 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.

Not visible in the next 10 days
Identifier
60566, 2024-149DC
Orbit
LEO
Country
Flag of ITIT
Related business
Manufacturer
Apogeo Space
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 0.3U, Unknown motor
Mass
0.5 kg wet, 0.5 kg dry
Launch date (UTC)
2024-08-16 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.008 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 4 days ago

TLE from 4 days ago
0 PICO-02G027
1 60566U 24149DC  26031.22751986  .13254879  26258-5  28791-2 0  9991
2 60566  97.6610 128.7595 0011638 302.3185  57.6981 16.30422006 80819
Epoch: 2026-01-31T05:27Z
TLE epoch observation values (Epoch: 2026-01-31T05:27:37.715Z)
Latitude
-0.00004°
Longitude
-83.60217°
Altitude
190.556 km
Speed
7.794 km/s
True Right ascension
08h 35m 02s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
02:55:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
195.88 km
Perigee altitude
180.596 km
Semi-major axis
6,566.375 km
Eccentricity
0.00116
Inclination
97.661°
RAAN
128.7595°
Arg. of periapsis
302.3185°
True anomaly
57.81091°
Mean anomaly
57.6981°
Eccentric anomaly
57.7545°
Mean motion
4.07901 °/min
Orbital period
88.26 mins
BSTAR
0.0028791
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|