NUSAT 1 DEB, 43427 (Decayed)
Orbit data source: Space-Track
NUSAT 1 DEB, 43427 was space debris in LEO originally from a launch on Mon, 30 May 2016 UTC launched from the Taiyaun Space Center, China (TSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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43427 intel report (Beta)
NUSAT 1 DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 8 months ago |
Origin | |
Manufacturer | CAST |
Mission | Decayed spacecraft |
Bus & Motor | Unknown |
Mass | Unknown |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 8 months ago
0 NUSAT 1 DEB
1 43427U 16033E 24113.82383959 .10580850 26104-5 65739-2 0 9998
2 43427 97.5580 68.7815 0003275 163.3471 196.7925 16.17944899417248
Epoch: 2024-04-22T19:46Z
Definitive object data (Epoch: 2024-04-22T19:46:19.74Z)
Latitude | 0.00003° |
Longitude | -79.15791° |
Altitude | 230.426 km |
Speed | 7.767 km/s |
True Right ascension | 04h 35m 07s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
Apogee altitude | 224.143 km |
Perigee altitude | 219.819 km |
Semi-major axis | 6,600.118 km |
Eccentricity | 0.0003275 |
Inclination | 97.558° |
RAAN | 68.7815° |
Arg. of periapsis | 163.3471° |
True anomaly | 196.78166° |
Mean anomaly | 196.7925° |
Eccentric anomaly | 196.78708° |
Mean motion | 4.04777 °/min |
BSTAR | 0.0065739 |
Orbital period | 88.94 mins |
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Other satellites on launch #33 in the year 2016 (2016-05-30 UTC)
ZY 3 2, 41556 |
NUSAT 1, 41557 (Decayed) |
NUSAT 2, 41558 (Decayed) |
CZ-4B R/B, 41559 (Decayed) |
NUSAT 1 DEB, 43427 (Decayed) |
NUSAT 1 DEB Visibility forecast
Observer location: undefined°, undefined
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