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: 13 hours ago
TLE from 13 hours ago
0 PEXT
1 64874U 25154F 26149.15246631 .00003725 00000-0 17449-3 0 9991
2 64874 97.3973 214.5209 0002896 26.5725 333.5658 15.20322815 46950Epoch: 2026-05-29T03:39Z
TLE epoch observation values (Epoch: 2026-05-29T03:39:33.089Z)
Latitude
-0.00003°
Longitude
-87.05391°
Altitude
506.172 km
Speed
7.612 km/s
True Right ascension
14h 18m 05s
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
01:46:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.824 km
Perigee altitude
499.839 km
Semi-major axis
6,879.968 km
Eccentricity
0.00029
Inclination
97.3973°
RAAN
214.5209°
Arg. of periapsis
26.5725°
True anomaly
333.55102°
Mean anomaly
333.5658°
Eccentric anomaly
333.55841°
Mean motion
3.80333 °/min
Orbital period
94.65 mins
BSTAR
0.00017449
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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 | 2026-05-29 16:51:13.643Z | 25.554° NE | 2026-05-29 16:54:13.643Z | 75.264° E | 33.548° | 2026-05-29 16:57:13.643Z | 166.183° S |
| 5 mins | 2026-05-30 05:04:13.643Z | 217.512° SW | 2026-05-30 05:06:13.643Z | 263.482° W | 23.944° | 2026-05-30 05:09:13.643Z | 321.342° 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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