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: 9 hours ago
TLE from 9 hours ago
0 DROID.002
1 63223U 25052P 26039.64926175 .00007842 00000-0 35084-3 0 9994
2 63223 97.4087 294.4732 0002768 203.8739 156.2369 15.21561684 50319Epoch: 2026-02-08T15:34Z
TLE epoch observation values (Epoch: 2026-02-08T15:34:56.215Z)
Latitude
-0.00001°
Longitude
-78.01643°
Altitude
505.965 km
Speed
7.61 km/s
True Right ascension
19h 37m 53s
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
02:55:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.997 km
Perigee altitude
496.19 km
Semi-major axis
6,876.23 km
Eccentricity
0.00028
Inclination
97.4087°
RAAN
294.4732°
Arg. of periapsis
203.8739°
True anomaly
156.24968°
Mean anomaly
156.2369°
Eccentric anomaly
156.24329°
Mean motion
3.80643 °/min
Orbital period
94.58 mins
BSTAR
0.00035084
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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 | 2026-02-09 04:47:39.067Z | 58.187° ENE | 2026-02-09 04:49:39.067Z | 92.977° ESE | 14.958° | 2026-02-09 04:51:39.067Z | 127.954° SE |
| 5 mins | 2026-02-09 06:21:39.067Z | 335.119° NNW | 2026-02-09 06:23:39.067Z | 282.749° WNW | 26.447° | 2026-02-09 06:26:39.067Z | 226.647° WSW |
| 5 mins | 2026-02-09 16:58:39.067Z | 170.685° S | 2026-02-09 17:00:39.067Z | 239.955° WSW | 44.835° | 2026-02-09 17:03:39.067Z | 346.236° 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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