DROID.002, 63223
Orbit data source: Space-Track
DROID.002, 63223 is a payload satellite owned by Turion Space (US) in SSO that was launched on Sat, 15 Mar 2025 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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63223 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Turion Space
Mission
Operational Commercial Technology
Bus & Motor
DROID, Unknown motor
Mass
90 kg wet, 90 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
0.892 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 DROID.002
1 63223U 25052P 26027.48205625 .00010878 00000-0 48847-3 0 9997
2 63223 97.4104 282.4956 0002222 276.1745 83.9238 15.21337550 48466Epoch: 2026-01-27T11:34Z
TLE epoch observation values (Epoch: 2026-01-27T11:34:09.660Z)
Latitude
-0.00002°
Longitude
-17.80747°
Altitude
504.736 km
Speed
7.612 km/s
True Right ascension
18h 49m 58s
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
18:51:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.297 km
Perigee altitude
497.241 km
Semi-major axis
6,876.906 km
Eccentricity
0.00022
Inclination
97.4104°
RAAN
282.4956°
Arg. of periapsis
276.1745°
True anomaly
83.94912°
Mean anomaly
83.9238°
Eccentric anomaly
83.93646°
Mean motion
3.80587 °/min
Orbital period
94.59 mins
BSTAR
0.00048847
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.002 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 | 2026-01-28 05:31:18.191Z | 35.443° NE | 2026-01-28 05:33:18.191Z | 128.433° SE | 37.825° | 2026-01-28 05:36:18.191Z | 178.133° S |
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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