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 25300.42670247 .00008396 00000-0 39213-3 0 9999
2 63223 97.4141 191.9334 0002622 208.0777 152.0317 15.20057669 34475Epoch: 2025-10-27T10:14Z
TLE epoch observation values (Epoch: 2025-10-27T10:14:27.093Z)
Latitude
-0.00003°
Longitude
2.29181°
Altitude
510.351 km
Speed
7.608 km/s
True Right ascension
12h 47m 44s
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
18:50:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.437 km
Perigee altitude
500.828 km
Semi-major axis
6,880.77 km
Eccentricity
0.00026
Inclination
97.4141°
RAAN
191.9334°
Arg. of periapsis
208.0777°
True anomaly
152.04579°
Mean anomaly
152.0317°
Eccentric anomaly
152.03874°
Mean motion
3.80266 °/min
Orbital period
94.67 mins
BSTAR
0.00039213
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-28 05:45:23.206Z | 12.116° NNE | 2025-10-28 05:48:23.206Z | 14.751° NNE | 43.629° | 2025-10-28 05:52:23.206Z | 192.769° SSW |
| 5 mins | 2025-10-28 16:24:23.206Z | 125.769° SE | 2025-10-28 16:26:23.206Z | 77.788° E | 28.236° | 2025-10-28 16:29:23.206Z | 11.55° NNE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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