DROID-001, 56965 (Decayed)
Orbit data source: Space-Track
DROID-001, 56965 was a payload satellite owned by Turion Space (US) in LEO that was launched on Mon, 12 Jun 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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56965 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NanoAvionics
Mission
Decayed Commercial Technology
Bus & Motor
CUBESAT MP42H, Unknown motor
Mass
32 kg wet, 32 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.257 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 DROID-001
1 56965U 23084AK 26059.12407982 .15531786 27588-5 16146-3 0 9995
2 56965 97.5587 217.3641 0009709 247.4524 112.5754 16.50520813152173Epoch: 2026-02-28T02:58Z
TLE epoch observation values (Epoch: 2026-02-28T02:58:40.496Z)
Latitude
0.00004°
Longitude
14.74466°
Altitude
143.659 km
Speed
7.818 km/s
True Right ascension
14h 29m 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
04:25:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
141.089 km
Perigee altitude
128.442 km
Semi-major axis
6,512.903 km
Eccentricity
0.00097
Inclination
97.5587°
RAAN
217.3641°
Arg. of periapsis
247.4524°
True anomaly
112.67808°
Mean anomaly
112.5754°
Eccentric anomaly
112.62675°
Mean motion
4.12935 °/min
Orbital period
87.18 mins
BSTAR
0.00016146
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Other satellites on launch #84 in the year 2023 (2023-06-12 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.DROID-001 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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