PRAETORIAN SDA_607, 65570
Orbit data source: Space-Track
PRAETORIAN SDA_607, 65570 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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65570 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: 14 hours ago
TLE from 14 hours ago
0 PRAETORIAN SDA_607
1 65570U 25203F 26171.27890219 .00000120 00000-0 97190-4 0 9993
2 65570 81.3036 7.7808 0008896 178.9840 181.1336 13.84284906 39138Epoch: 2026-06-20T06:41Z
TLE epoch observation values (Epoch: 2026-06-20T06:41:37.149Z)
Latitude
-0.00005°
Longitude
-1.11981°
Altitude
958.112 km
Speed
7.369 km/s
True Right ascension
00h 31m 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
07:14:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
952.449 km
Perigee altitude
939.418 km
Semi-major axis
7,324.071 km
Eccentricity
0.00089
Inclination
81.3036°
RAAN
7.7808°
Arg. of periapsis
178.984°
True anomaly
181.13159°
Mean anomaly
181.1336°
Eccentric anomaly
181.13259°
Mean motion
3.4627 °/min
Orbital period
103.97 mins
BSTAR
0.00009719
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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_607 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 00:37:33.332Z | 359.558° N | 2026-06-21 00:42:33.332Z | 77.888° E | 41.652° | 2026-06-21 00:47:33.332Z | 157.287° SSE |
| 6 mins | 2026-06-21 02:24:33.332Z | 302.721° NW | 2026-06-21 02:26:33.332Z | 280.318° WNW | 16.804° | 2026-06-21 02:30:33.332Z | 237.537° WSW |
| 4 mins | 2026-06-21 12:21:33.332Z | 94.695° ESE | 2026-06-21 12:22:33.332Z | 83.854° E | 14.061° | 2026-06-21 12:25:33.332Z | 53.542° ENE |
| 10 mins | 2026-06-21 14:02:33.332Z | 196.229° SSW | 2026-06-21 14:06:33.332Z | 250.414° W | 43.859° | 2026-06-21 14:12:33.332Z | 5.599° 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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