PEXT, 64874
Orbit data source: Space-Track
PEXT, 64874 is an American payload satellite in SSO that was launched on Wed, 23 Jul 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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64874 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
York Space Sys
Mission
Operational Civil Communications
Bus & Motor
S-CLASS, Unknown motor
Mass
140 kg wet, 140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 14.5 m
Radar Cross Section
1.244 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 PEXT
1 64874U 25154F 26225.16035454 .00001502 00000-0 71320-4 0 9996
2 64874 97.3924 289.0991 0004515 89.0403 271.1349 15.20745722 58502Epoch: 2026-08-13T03:50Z
TLE epoch observation values (Epoch: 2026-08-13T03:50:54.632Z)
Latitude
-0.0001°
Longitude
-90.23244°
Altitude
506.622 km
Speed
7.611 km/s
True Right ascension
19h 16m 23s
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
10:14:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.66 km
Perigee altitude
497.449 km
Semi-major axis
6,878.691 km
Eccentricity
0.00045
Inclination
97.3924°
RAAN
289.0991°
Arg. of periapsis
89.0403°
True anomaly
271.08317°
Mean anomaly
271.1349°
Eccentric anomaly
271.10904°
Mean motion
3.80438 °/min
Orbital period
94.63 mins
BSTAR
0.00007132
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Other satellites on launch #154 in the year 2025 (2025-07-23 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.PEXT 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 | 2026-08-14 03:40:34.728Z | 124.059° SE | 2026-08-14 03:43:34.728Z | 63.815° ENE | 22.623° | 2026-08-14 03:45:34.728Z | 23.055° NE |
| 4 mins | 2026-08-14 05:15:34.728Z | 234.393° WSW | 2026-08-14 05:17:34.728Z | 275.905° WNW | 17.541° | 2026-08-14 05:19:34.728Z | 310.069° NW |
| 4 mins | 2026-08-14 16:45:34.728Z | 49.557° ENE | 2026-08-14 16:47:34.728Z | 115.538° SE | 29.787° | 2026-08-14 16:49:34.728Z | 158.79° S |
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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