DECAYED
Showing default

ENSO, 58470 (Decayed)

Orbit data source: Space-Track

ENSO, 58470 was a payload satellite owned by Montpellier (FR) in LEO that was launched on Fri, 01 Dec 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
58470, 2023-185J
Orbit
Decayed
Country
Flag of FRFR
Related business
Manufacturer
Montpellier
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2023-12-01 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Ant, 3.0 m
Radar Cross Section
0.232 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 5 months ago

TLE from 5 months ago
0 ENSO
1 58470U 23185J   25312.86900916  .08388928  24835-5  96914-3 0  9990
2 58470  97.3304  36.0765 0010794 270.9690  89.0371 16.36702678108938
Epoch: 2025-11-08T20:51Z
TLE epoch observation values (Epoch: 2025-11-08T20:51:22.391Z)
Latitude
-0.00003°
Longitude
34.94077°
Altitude
177.726 km
Speed
7.8 km/s
True Right ascension
02h 24m 18s
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
20:11:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
178.467 km
Perigee altitude
164.328 km
Semi-major axis
6,549.534 km
Eccentricity
0.00108
Inclination
97.3304°
RAAN
36.0765°
Arg. of periapsis
270.969°
True anomaly
89.16078°
Mean anomaly
89.0371°
Eccentric anomaly
89.09894°
Mean motion
4.09475 °/min
Orbital period
87.92 mins
BSTAR
0.00096914
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
|