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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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: 8 hours ago
TLE from 8 hours ago
0 USPWSA-DRAGOON
1 64542U 25135Q 26120.03364619 .00010563 00000-0 42573-3 0 9999
2 64542 97.4645 236.2966 0002583 18.0645 342.0684 15.25017003 47589Epoch: 2026-04-30T00:48Z
TLE epoch observation values (Epoch: 2026-04-30T00:48:27.030Z)
Latitude
-0.00005°
Longitude
6.19792°
Altitude
492.141 km
Speed
7.62 km/s
True Right ascension
15h 45m 11s
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
16:39:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.469 km
Perigee altitude
485.923 km
Semi-major axis
6,865.833 km
Eccentricity
0.00026
Inclination
97.4645°
RAAN
236.2966°
Arg. of periapsis
18.0645°
True anomaly
342.05928°
Mean anomaly
342.0684°
Eccentric anomaly
342.06384°
Mean motion
3.81508 °/min
Orbital period
94.36 mins
BSTAR
0.00042573
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-30 20:15:58.806Z | 26.205° NE | 2026-04-30 20:18:58.806Z | 93.563° ESE | 35.974° | 2026-04-30 20:21:58.806Z | 171.431° S |
| 4 mins | 2026-05-01 06:52:58.806Z | 106.719° ESE | 2026-05-01 06:54:58.806Z | 69.005° E | 17.154° | 2026-05-01 06:56:58.806Z | 31.068° NE |
| 4 mins | 2026-05-01 08:26:58.806Z | 228.308° WSW | 2026-05-01 08:27:58.806Z | 252.593° W | 22.844° | 2026-05-01 08:30:58.806Z | 317.398° NNW |
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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