DROID-001, 56965
Orbit data source: Space-Track
DROID-001, 56965 is a payload satellite owned by Turion Space (US) in SSO 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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NanoAvionics
Mission
Operational 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: 7 hours ago
TLE from 7 hours ago
0 DROID-001
1 56965U 23084AK 25259.18683419 .00054946 00000-0 82109-3 0 9992
2 56965 97.5806 37.6272 0006659 171.8115 188.3248 15.54830695126239Epoch: 2025-09-16T04:29Z
TLE epoch observation values (Epoch: 2025-09-16T04:29:02.474Z)
Latitude
-0.00003°
Longitude
-25.01385°
Altitude
410.246 km
Speed
7.662 km/s
True Right ascension
02h 30m 30s
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
03:54:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
404.085 km
Perigee altitude
395.059 km
Semi-major axis
6,777.709 km
Eccentricity
0.00067
Inclination
97.5806°
RAAN
37.6272°
Arg. of periapsis
171.8115°
True anomaly
188.31376°
Mean anomaly
188.3248°
Eccentric anomaly
188.31928°
Mean motion
3.88972 °/min
Orbital period
92.55 mins
BSTAR
0.00082109
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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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-16 22:02:22.595Z | 24.345° NE | 2025-09-16 22:04:22.595Z | 89.771° E | 40.375° | 2025-09-16 22:07:22.595Z | 181.4° SSW |
| 4 mins | 2025-09-17 09:58:22.595Z | 222.025° SW | 2025-09-17 09:59:22.595Z | 247.271° WSW | 21.484° | 2025-09-17 10:02:22.595Z | 319.092° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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