Showing default

MDQUBESAT-2, 58665

Orbit data source: Space-Track

MDQUBESAT-2, 58665 is a payload satellite owned by Innova Space (AR) in SSO 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.

Loading next visibility...
Identifier
58665, 2023-185P
Orbit
SSO
Country
Flag of UnknownUnknown / ARGN
Related business
Manufacturer
Innova Space
Mission
Operational Commercial Communications
Bus & Motor
POCKETQUBE 2P, Unknown motor
Mass
~0.5 kg wet, ~0.5 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 Pan, 0.1 m
Radar Cross Section
0.006 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 MDQUBESAT-2
1 58665U 23185P   25306.31309397  .00046360  00000-0  12519-2 0  9999
2 58665  97.5659  22.9553 0008669 346.8548  13.2469 15.37581027102597
Epoch: 2025-11-02T07:30Z
TLE epoch observation values (Epoch: 2025-11-02T07:30:51.319Z)
Latitude
0.00002°
Longitude
-131.58915°
Altitude
450.609 km
Speed
7.645 km/s
True Right ascension
01h 31m 49s
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
23:58:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.134 km
Perigee altitude
444.295 km
Semi-major axis
6,828.351 km
Eccentricity
0.00087
Inclination
97.5659°
RAAN
22.9553°
Arg. of periapsis
346.8548°
True anomaly
13.26969°
Mean anomaly
13.2469°
Eccentric anomaly
13.25829°
Mean motion
3.84653 °/min
Orbital period
93.59 mins
BSTAR
0.0012519
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
|