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, 1.0 m
Radar Cross Section
1.244 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 PEXT
1 64874U 25154F 26317.59505293 .00004155 00000-0 18919-3 0 9999
2 64874 97.3788 19.7192 0004288 111.2147 248.9548 15.21222884 72555Epoch: 2026-11-13T14:16Z
TLE epoch observation values (Epoch: 2026-11-13T14:16:52.573Z)
Latitude
0.00007°
Longitude
112.7882°
Altitude
506.304 km
Speed
7.61 km/s
True Right ascension
01h 18m 52s
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
21:49:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.063 km
Perigee altitude
496.165 km
Semi-major axis
6,877.251 km
Eccentricity
0.00043
Inclination
97.3788°
RAAN
19.7192°
Arg. of periapsis
111.2147°
True anomaly
248.90895°
Mean anomaly
248.9548°
Eccentric anomaly
248.93187°
Mean motion
3.80558 °/min
Orbital period
94.6 mins
BSTAR
0.00018919
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-15 04:17:55.443Z | 163.75° S | 2026-11-15 04:20:55.443Z | 29.167° NE | 78.756° | 2026-11-15 04:23:55.443Z | 350.238° N |
| 6 mins | 2026-11-15 17:21:55.443Z | 1.865° NNE | 2026-11-15 17:24:55.443Z | 249.132° W | 57.71° | 2026-11-15 17:27:55.443Z | 203.917° SW |
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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