XR-1, 47507 (Decayed)
Orbit data source: Space-Track
XR-1, 47507 was an American payload satellite in LEO that was launched on Sun, 24 Jan 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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47507 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 XR-1
1 47507U 21006CY 25130.77731350 .32204030 24698-5 53776-3 0 9995
2 47507 97.2518 196.8209 0016573 248.3409 112.2185 16.46799156239013
Epoch: 2025-05-10T18:39Z
TLE epoch observation values (Epoch: 2025-05-10T18:39:19.886Z)
Latitude
0.60402°
Longitude
48.09739°
Altitude
155.072 km
Speed
7.811 km/s
True Right ascension
13h 06m 58s
True Declination
0° 36' 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
12:59:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
155.38 km
Perigee altitude
133.76 km
Semi-major axis
6,522.707 km
Eccentricity
0.00166
Inclination
97.2518°
RAAN
196.8209°
Arg. of periapsis
248.3409°
True anomaly
112.39417°
Mean anomaly
112.2185°
Eccentric anomaly
112.30635°
Mean motion
4.12004 °/min
Orbital period
87.38 mins
BSTAR
0.00053776
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Other satellites on launch #6 in the year 2021 (2021-01-24 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.XR-1 Visibility
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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. |
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This satellite is decayed. |
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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