DECAYED
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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.

Not visible in the next 10 days
Identifier
47507, 2021-006CY
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
ICEYE
Mission
Decayed Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
2021-01-24 (5 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 0.8 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 7 months ago

TLE from 7 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
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
15:05:03
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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Computing Atmospheric mass density...

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