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.
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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: 1 week ago
TLE from 1 week ago
0 MDQUBESAT-2
1 58665U 23185P 26153.77032476 .02780131 24937-5 17721-2 0 9994
2 58665 97.5172 248.1144 0016422 273.8674 86.0736 16.17255124135675Epoch: 2026-06-02T18:29Z
TLE epoch observation values (Epoch: 2026-06-02T18:29:16.059Z)
Latitude
0.00005°
Longitude
79.55895°
Altitude
229.507 km
Speed
7.769 km/s
True Right ascension
16h 32m 27s
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
06:15:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
234.699 km
Perigee altitude
213.016 km
Semi-major axis
6,601.994 km
Eccentricity
0.00164
Inclination
97.5172°
RAAN
248.1144°
Arg. of periapsis
273.8674°
True anomaly
86.26137°
Mean anomaly
86.0736°
Eccentric anomaly
86.16748°
Mean motion
4.04604 °/min
Orbital period
88.98 mins
BSTAR
0.0017721
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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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| MDQUBESAT-2 is likely not visible in the next few days. |
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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