DECAYED
Showing default

INSPIRE-SAT 7, 56211 (Decayed)

Orbit data source: Space-Track

INSPIRE-SAT 7, 56211 was a payload satellite owned by LATMOS (FR) in LEO that was launched on Sat, 15 Apr 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
56211, 2023-054AK
Orbit
Decayed
Country
Flag of FRFR
Related business
Manufacturer
LATMOS/ISISBV
Mission
Decayed Civil Science
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
2023-04-15 (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
0.025 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 11 months ago

TLE from 11 months ago
0 INSPIRE-SAT 7
1 56211U 23054AK  24262.29064463  .11675157  26116-5  88932-3 0  9996
2 56211  97.3163 168.3145 0008158 207.0865 153.0010 16.40455525 80975
Epoch: 2024-09-18T06:58Z
TLE epoch observation values (Epoch: 2024-09-18T06:58:31.696Z)
Latitude
-0.00002°
Longitude
65.98937°
Altitude
172.603 km
Speed
7.8 km/s
True Right ascension
11h 13m 15s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
16:59:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
166.729 km
Perigee altitude
156.059 km
Semi-major axis
6,539.531 km
Eccentricity
0.00082
Inclination
97.3163°
RAAN
168.3145°
Arg. of periapsis
207.0865°
True anomaly
153.0434°
Mean anomaly
153.001°
Eccentric anomaly
153.0222°
Mean motion
4.10415 °/min
Orbital period
87.72 mins
BSTAR
0.00088932
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
|