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 26270.16387144 .00002483 00000-0 11522-3 0 9998
2 64874 97.3861 333.2346 0001250 309.1395 50.9729 15.20954013 65347Epoch: 2026-09-27T03:55Z
TLE epoch observation values (Epoch: 2026-09-27T03:55:58.492Z)
Latitude
-0.00007°
Longitude
-91.72063°
Altitude
505.512 km
Speed
7.612 km/s
True Right ascension
22h 12m 56s
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
21:48:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.785 km
Perigee altitude
499.066 km
Semi-major axis
6,878.062 km
Eccentricity
0.00013
Inclination
97.3861°
RAAN
333.2346°
Arg. of periapsis
309.1395°
True anomaly
50.98403°
Mean anomaly
50.9729°
Eccentric anomaly
50.97846°
Mean motion
3.80491 °/min
Orbital period
94.61 mins
BSTAR
0.00011522
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-28 05:19:38.426Z | 227.198° WSW | 2026-09-28 05:21:38.426Z | 260.668° W | 16.231° | 2026-09-28 05:23:38.426Z | 297.826° NW |
| 5 mins | 2026-09-28 16:49:38.426Z | 34.54° NE | 2026-09-28 16:51:38.426Z | 85.369° E | 42.91° | 2026-09-28 16:54:38.426Z | 167.39° 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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