PRAETORIAN SDA_604, 65567
Orbit data source: Space-Track
PRAETORIAN SDA_604, 65567 is a payload satellite owned by SDA (US) in LEO that was launched on Wed, 10 Sep 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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65567 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
York Space Sys
Mission
Operational Defense Communications
Bus & Motor
S-CLASS, Unknown motor
Mass
~300 kg wet, ~300 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: 21 hours ago
TLE from 21 hours ago
0 PRAETORIAN SDA_604
1 65567U 25203C 26170.96403972 .00000046 00000-0 31258-4 0 9990
2 65567 81.3052 8.5312 0005419 183.6347 176.4770 13.83047734 39060Epoch: 2026-06-19T23:08Z
TLE epoch observation values (Epoch: 2026-06-19T23:08:13.031Z)
Latitude
-0.0001°
Longitude
113.29142°
Altitude
959.927 km
Speed
7.37 km/s
True Right ascension
00h 34m 07s
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
07:13:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
954.275 km
Perigee altitude
946.333 km
Semi-major axis
7,328.441 km
Eccentricity
0.00054
Inclination
81.3052°
RAAN
8.5312°
Arg. of periapsis
183.6347°
True anomaly
176.48081°
Mean anomaly
176.477°
Eccentric anomaly
176.47891°
Mean motion
3.4596 °/min
Orbital period
104.06 mins
BSTAR
0.000031258
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Other satellites on launch #203 in the year 2025 (2025-09-10 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.PRAETORIAN SDA_604 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-06-21 00:01:27.602Z | 13.598° NNE | 2026-06-21 00:06:27.602Z | 75.379° E | 27.251° | 2026-06-21 00:11:27.602Z | 132.435° SE |
| 9 mins | 2026-06-21 01:47:27.602Z | 325.729° NNW | 2026-06-21 01:51:27.602Z | 267.9° W | 30.942° | 2026-06-21 01:56:27.602Z | 206.544° SW |
| 10 mins | 2026-06-21 13:27:27.602Z | 163.514° S | 2026-06-21 13:31:27.602Z | 98.733° ESE | 39.075° | 2026-06-21 13:37:27.602Z | 18.707° NNE |
| 7 mins | 2026-06-21 15:14:27.602Z | 259.187° W | 2026-06-21 15:17:27.602Z | 297.106° NW | 20.291° | 2026-06-21 15:21:27.602Z | 339.358° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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