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: 13 hours ago
TLE from 13 hours ago
0 DROID.002
1 63223U 25052P 25344.45615742 .00011649 00000-0 53382-3 0 9997
2 63223 97.4127 235.2351 0006134 79.0933 281.0993 15.20608460 41160Epoch: 2025-12-10T10:56Z
TLE epoch observation values (Epoch: 2025-12-10T10:56:52.001Z)
Latitude
0.00006°
Longitude
-8.40781°
Altitude
506.285 km
Speed
7.611 km/s
True Right ascension
15h 40m 56s
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
22:09:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.189 km
Perigee altitude
496.75 km
Semi-major axis
6,879.106 km
Eccentricity
0.00061
Inclination
97.4127°
RAAN
235.2351°
Arg. of periapsis
79.0933°
True anomaly
281.03031°
Mean anomaly
281.0993°
Eccentric anomaly
281.06481°
Mean motion
3.80404 °/min
Orbital period
94.64 mins
BSTAR
0.00053382
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-11 04:54:21.752Z | 57.182° ENE | 2025-12-11 04:56:21.752Z | 95.617° ESE | 17.57° | 2025-12-11 04:58:21.752Z | 133.08° SE |
| 4 mins | 2025-12-11 06:28:21.752Z | 330.038° NNW | 2025-12-11 06:30:21.752Z | 281.828° WNW | 23.019° | 2025-12-11 06:32:21.752Z | 240.872° WSW |
| 6 mins | 2025-12-11 17:05:21.752Z | 178.987° S | 2025-12-11 17:07:21.752Z | 217.082° SW | 41.182° | 2025-12-11 17:11:21.752Z | 342.648° N |
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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