MDQUBESAT-2, 58665 (Decayed)
Orbit data source: Space-Track
MDQUBESAT-2, 58665 was a payload satellite owned by Innova Space (AR) 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.
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58665 intel report (Beta)
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Identifier
Orbit
Country
AR / ARGNRelated business
Manufacturer
Innova Space
Mission
Decayed Commercial Communications
Bus & Motor
POCKETQUBE 2P, Unknown motor
Mass
~0.5 kg wet, ~0.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.006 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 MDQUBESAT-2
1 58665U 23185P 26154.07947441 .03555560 25061-5 18993-2 0 9993
2 58665 97.5153 248.4694 0017019 272.7618 87.1722 16.19579607135726Epoch: 2026-06-03T01:54Z
TLE epoch observation values (Epoch: 2026-06-03T01:54:26.589Z)
Latitude
-0.00002°
Longitude
-31.68463°
Altitude
223.379 km
Speed
7.773 km/s
True Right ascension
16h 33m 52s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
01:10:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
228.758 km
Perigee altitude
206.308 km
Semi-major axis
6,595.67 km
Eccentricity
0.0017
Inclination
97.5153°
RAAN
248.4694°
Arg. of periapsis
272.7618°
True anomaly
87.36701°
Mean anomaly
87.1722°
Eccentric anomaly
87.2696°
Mean motion
4.05186 °/min
Orbital period
88.85 mins
BSTAR
0.0018993
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Other satellites on launch #185 in the year 2023 (2023-12-01 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.MDQUBESAT-2 Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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