TIANHUI 1-03 DEB, 41023 (Decayed)
Orbit data source: Space-Track
TIANHUI 1-03 DEB, 41023 was space debris in SSO originally from a launch on Mon, 26 Oct 2015 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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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41023 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 TIANHUI 1-03 DEB
1 41023U 15061B 24126.01009347 .02924571 12948-1 48679-2 0 9993
2 41023 97.2759 36.2033 0019878 209.8794 150.1355 16.05845536461587
Epoch: 2024-05-05T00:14Z
TLE epoch observation values (Epoch: 2024-05-05T00:14:32.075Z)
Latitude
-0°
Longitude
169.20115°
Altitude
272.923 km
Speed
7.737 km/s
True Right ascension
02h 24m 48s
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
23:31:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
268.297 km
Perigee altitude
241.926 km
Semi-major axis
6,633.248 km
Eccentricity
0.00199
Inclination
97.2759°
RAAN
36.2033°
Arg. of periapsis
209.8794°
True anomaly
150.24868°
Mean anomaly
150.1355°
Eccentric anomaly
150.19212°
Mean motion
4.01748 °/min
Orbital period
89.61 mins
BSTAR
0.0048679
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Other satellites on launch #61 in the year 2015 (2015-10-26 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.TIANHUI 1-03 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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