DECAYED
Showing default

PICO-01D007, 58690 (Decayed)

Orbit data source: Space-Track

PICO-01D007, 58690 was a payload satellite owned by Apogeo Space (IT) in LEO that was launched on Sat, 11 Nov 2023 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.

Loading next visibility...
Identifier
58690, 2023-174DE
Orbit
Decayed
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)
2023-11-11 (2 years 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, Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 year ago

TLE from 1 year ago
0 PICO-01D007
1 58690U 23174DE  24364.79665221  .15170440  24618-5  23558-2 0  9995
2 58690  97.3988  86.0993 0008773 292.6645  67.3723 16.33964753 64025
Epoch: 2024-12-29T19:07Z
TLE epoch observation values (Epoch: 2024-12-29T19:07:10.750Z)
Latitude
-0.00007°
Longitude
60.57667°
Altitude
182.939 km
Speed
7.798 km/s
True Right ascension
05h 44m 23s
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
14:25:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
184.474 km
Perigee altitude
172.97 km
Semi-major axis
6,556.859 km
Eccentricity
0.00088
Inclination
97.3988°
RAAN
86.0993°
Arg. of periapsis
292.6645°
True anomaly
67.46513°
Mean anomaly
67.3723°
Eccentric anomaly
67.41871°
Mean motion
4.08789 °/min
Orbital period
88.06 mins
BSTAR
0.0023558
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
|