OBJECT M, 47424
Orbit data source: Space-Track
OBJECT M, 47424 is a payload satellite in SSO that was launched on Sun, 24 Jan 2021 UTC launched 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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47424 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 OBJECT M
1 47424U 21006M 26318.23414567 .00005220 00000-0 15692-3 0 9997
2 47424 97.2043 0.4802 0010898 33.3916 326.8013 15.34770872322603Epoch: 2026-11-14T05:37Z
TLE epoch observation values (Epoch: 2026-11-14T05:37:10.185Z)
Latitude
-0.00004°
Longitude
-137.15409°
Altitude
458.481 km
Speed
7.641 km/s
True Right ascension
00h 01m 55s
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
13:56:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.989 km
Perigee altitude
451.088 km
Semi-major axis
6,836.676 km
Eccentricity
0.00109
Inclination
97.2043°
RAAN
0.4802°
Arg. of periapsis
33.3916°
True anomaly
326.73284°
Mean anomaly
326.8013°
Eccentric anomaly
326.76708°
Mean motion
3.83951 °/min
Orbital period
93.76 mins
BSTAR
0.00015692
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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.OBJECT M 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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| OBJECT M is likely not visible in the next few days. |
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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