Showing default

PICO-01B009, 58287

Orbit data source: Space-Track

PICO-01B009, 58287 is a payload satellite owned by Apogeo Space (IT) in SSO 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.

Not visible in the next 10 days
Identifier
58287, 2023-174AH
Orbit
SSO
Country
Flag of ITIT
Related 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)
2023-11-11 (3 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, Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 PICO-01B009
1 58287U 23174AH  26171.01998630  .00159725  00000-0  73696-3 0  9993
2 58287  97.3772 268.0852 0003284 195.7672 164.3496 15.83110326146613
Epoch: 2026-06-20T00:28Z
TLE epoch observation values (Epoch: 2026-06-20T00:28:46.816Z)
Latitude
0.00004°
Longitude
-7.35048°
Altitude
326.946 km
Speed
7.711 km/s
True Right ascension
17h 52m 20s
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
21:38:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
320.731 km
Perigee altitude
316.333 km
Semi-major axis
6,696.669 km
Eccentricity
0.00033
Inclination
97.3772°
RAAN
268.0852°
Arg. of periapsis
195.7672°
True anomaly
164.35975°
Mean anomaly
164.3496°
Eccentric anomaly
164.35467°
Mean motion
3.96054 °/min
Orbital period
90.9 mins
BSTAR
0.00073696
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|