PRAETORIAN SDA_602, 65565
Orbit data source: Space-Track
PRAETORIAN SDA_602, 65565 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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65565 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: 15 hours ago
TLE from 15 hours ago
0 PRAETORIAN SDA_602
1 65565U 25203A 26171.27657532 .00000062 00000-0 45004-4 0 9998
2 65565 81.3029 7.9069 0005957 177.1718 182.9474 13.84277876 39124Epoch: 2026-06-20T06:38Z
TLE epoch observation values (Epoch: 2026-06-20T06:38:16.107Z)
Latitude
0.00002°
Longitude
-0.15373°
Altitude
955.978 km
Speed
7.372 km/s
True Right ascension
00h 31m 37s
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
08:32:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
950.322 km
Perigee altitude
941.596 km
Semi-major axis
7,324.096 km
Eccentricity
0.0006
Inclination
81.3029°
RAAN
7.9069°
Arg. of periapsis
177.1718°
True anomaly
182.94389°
Mean anomaly
182.9474°
Eccentric anomaly
182.94565°
Mean motion
3.46268 °/min
Orbital period
103.97 mins
BSTAR
0.000045004
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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_602 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 00:33:57.396Z | 0.549° NNE | 2026-06-21 00:38:57.396Z | 68.514° E | 40.294° | 2026-06-21 00:44:57.396Z | 156.521° SSE |
| 6 mins | 2026-06-21 02:20:57.396Z | 305.763° NW | 2026-06-21 02:23:57.396Z | 270.516° WNW | 18.095° | 2026-06-21 02:26:57.396Z | 237.84° WSW |
| 4 mins | 2026-06-21 12:17:57.396Z | 96.446° ESE | 2026-06-21 12:18:57.396Z | 86.127° E | 12.868° | 2026-06-21 12:21:57.396Z | 56.187° ENE |
| 10 mins | 2026-06-21 13:58:57.396Z | 192.601° SSW | 2026-06-21 14:03:57.396Z | 334.608° NNW | 44.003° | 2026-06-21 14:08:57.396Z | 6.845° NNE |
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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