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)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ARGNRelated business
Manufacturer
CAST
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year 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 16.17944899417248Epoch: 2024-04-22T19:46Z
TLE epoch observation values (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
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
23:07:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
224.143 km
Perigee altitude
219.819 km
Semi-major axis
6,600.118 km
Eccentricity
0.00033
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
Orbital period
88.94 mins
BSTAR
0.0065739
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Other satellites on launch #33 in the year 2016 (2016-05-30 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.NUSAT 1 DEB 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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