TIANHUI 1-03 DEB, 41024 (Decayed)
Orbit data source: Space-Track
TIANHUI 1-03 DEB, 41024 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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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown
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 TIANHUI 1-03 DEB
1 41024U 15061C 24252.43804513 .02694476 51625-2 93504-2 0 9999
2 41024 97.2796 143.7149 0015917 264.4519 95.4939 15.90507132478636Epoch: 2024-09-08T10:30Z
TLE epoch observation values (Epoch: 2024-09-08T10:30:47.099Z)
Latitude
-0.00002°
Longitude
-1.96322°
Altitude
305.087 km
Speed
7.724 km/s
True Right ascension
09h 34m 51s
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
23:29:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
308.356 km
Perigee altitude
287.104 km
Semi-major axis
6,675.867 km
Eccentricity
0.00159
Inclination
97.2796°
RAAN
143.7149°
Arg. of periapsis
264.4519°
True anomaly
95.67542°
Mean anomaly
95.4939°
Eccentric anomaly
95.58466°
Mean motion
3.97907 °/min
Orbital period
90.47 mins
BSTAR
0.0093504
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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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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