PRAETORIAN SDA_606, 65569
Orbit data source: Space-Track
PRAETORIAN SDA_606, 65569 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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65569 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: 4 days ago
TLE from 4 days ago
0 PRAETORIAN SDA_606
1 65569U 25203E 26168.30750804 .00000053 00000-0 37439-4 0 9991
2 65569 81.3055 10.8712 0005744 180.4388 179.6764 13.83407378 38708Epoch: 2026-06-17T07:22Z
TLE epoch observation values (Epoch: 2026-06-17T07:22:48.694Z)
Latitude
-0.00005°
Longitude
-5.39876°
Altitude
958.902 km
Speed
7.37 km/s
True Right ascension
00h 43m 29s
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
08:32:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
953.242 km
Perigee altitude
944.824 km
Semi-major axis
7,327.17 km
Eccentricity
0.00057
Inclination
81.3055°
RAAN
10.8712°
Arg. of periapsis
180.4388°
True anomaly
179.67677°
Mean anomaly
179.6764°
Eccentric anomaly
179.67659°
Mean motion
3.4605 °/min
Orbital period
104.03 mins
BSTAR
0.000037439
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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_606 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-06-21 00:28:49.310Z | 1.59° NNE | 2026-06-21 00:34:49.310Z | 92.607° ESE | 37.964° | 2026-06-21 00:39:49.310Z | 151.807° SSE |
| 7 mins | 2026-06-21 02:15:49.310Z | 311.236° NW | 2026-06-21 02:18:49.310Z | 276.092° WNW | 20.087° | 2026-06-21 02:22:49.310Z | 230.962° WSW |
| 10 mins | 2026-06-21 13:54:49.310Z | 188.294° SSW | 2026-06-21 13:58:49.310Z | 195.12° SSW | 44.541° | 2026-06-21 14:04:49.310Z | 8.898° NNE |
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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