USPWSA-DRAGOON, 64542
Orbit data source: Space-Track
USPWSA-DRAGOON, 64542 is an American payload satellite in SSO that was launched on Mon, 23 Jun 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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64542 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
York Space Sys
Mission
Operational Commercial Communications
Bus & Motor
YORK, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.375 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 USPWSA-DRAGOON
1 64542U 25135Q 25328.26831782 .00013025 00000-0 59484-3 0 9998
2 64542 97.4581 80.5893 0003855 156.1088 204.0327 15.20710621 23727Epoch: 2025-11-24T06:26Z
TLE epoch observation values (Epoch: 2025-11-24T06:26:22.659Z)
Latitude
-0.00003°
Longitude
-79.47583°
Altitude
509.209 km
Speed
7.608 km/s
True Right ascension
05h 22m 21s
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
14:23:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.315 km
Perigee altitude
498.011 km
Semi-major axis
6,878.8 km
Eccentricity
0.00039
Inclination
97.4581°
RAAN
80.5893°
Arg. of periapsis
156.1088°
True anomaly
204.01472°
Mean anomaly
204.0327°
Eccentric anomaly
204.02371°
Mean motion
3.80429 °/min
Orbital period
94.63 mins
BSTAR
0.00059484
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Other satellites on launch #135 in the year 2025 (2025-06-23 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.USPWSA-DRAGOON 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 | 2025-11-24 19:38:57.036Z | 49.16° ENE | 2025-11-24 19:41:57.036Z | 103.767° ESE | 17.159° | 2025-11-24 19:43:57.036Z | 137.845° SSE |
| 4 mins | 2025-11-24 21:13:57.036Z | 323.399° NNW | 2025-11-24 21:14:57.036Z | 299.399° NW | 22.939° | 2025-11-24 21:17:57.036Z | 236.372° WSW |
| 5 mins | 2025-11-25 07:50:57.036Z | 181.371° SSW | 2025-11-25 07:52:57.036Z | 264.511° W | 42.763° | 2025-11-25 07:55:57.036Z | 341.15° 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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