QUANTUTONG 1, 43158 (Decayed)
Orbit data source: Space-Track
QUANTUTONG 1, 43158 was a payload satellite owned by QuanTuTong (CN) in SSO that was launched on Fri, 19 Jan 2018 UTC via a CHANG ZHENG 11 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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43158 intel report (Beta)
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QUANTUTONG 1 radio frequencies
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changsha Tianyi
Mission
Decayed Commercial Navigation
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
8 kg wet, 8 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 QUANTUTONG 1
1 43158U 18008D 24289.57081905 .01911305 30434-2 22393-2 0 9995
2 43158 97.2486 341.2486 0006509 265.8690 94.1850 16.09457699373267Epoch: 2024-10-15T13:41Z
TLE epoch observation values (Epoch: 2024-10-15T13:41:58.765Z)
Latitude
-0.00003°
Longitude
111.17205°
Altitude
251.864 km
Speed
7.756 km/s
True Right ascension
22h 44m 59s
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
19:04:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
249.483 km
Perigee altitude
240.861 km
Semi-major axis
6,623.309 km
Eccentricity
0.00065
Inclination
97.2486°
RAAN
341.2486°
Arg. of periapsis
265.869°
True anomaly
94.25938°
Mean anomaly
94.185°
Eccentric anomaly
94.22219°
Mean motion
4.02653 °/min
Orbital period
89.41 mins
BSTAR
0.0022393
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Other satellites on launch #8 in the year 2018 (2018-01-19 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.QUANTUTONG 1 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-09-14 04:15:35.366Z | 8.213° NNE | 2025-09-14 04:23:35.366Z | 67.888° E | 43.523° | 2025-09-14 04:25:35.366Z | 344.993° N |
| 12 mins | 2025-09-14 07:57:35.366Z | 334.656° NNW | 2025-09-14 07:58:35.366Z | 265.169° W | 42.78° | 2025-09-14 08:09:35.366Z | 1.109° NNE |
| 8 mins | 2025-09-14 18:11:35.366Z | 169.638° S | 2025-09-14 18:14:35.366Z | 125.535° SE | 44.582° | 2025-09-14 18:19:35.366Z | 181.724° SSW |
| 4 mins | 2025-09-14 19:08:35.366Z | 192.371° SSW | 2025-09-14 19:10:35.366Z | 193.373° SSW | 31.923° | 2025-09-14 19:12:35.366Z | 192.896° SSW |
| 11 mins | 2025-09-14 20:00:35.366Z | 234.251° WSW | 2025-09-14 20:01:35.366Z | 335.043° NNW | 43.816° | 2025-09-14 20:11:35.366Z | 214.88° SW |
| 8 mins | 2025-09-14 20:57:35.366Z | 229.371° WSW | 2025-09-14 21:00:35.366Z | 274.208° WNW | 42.374° | 2025-09-14 21:05:35.366Z | 219.658° SW |
| 11 mins | 2025-09-14 21:51:35.366Z | 294.509° NW | 2025-09-14 21:51:35.366Z | 294.509° NW | 40.648° | 2025-09-14 22:02:35.366Z | 250.628° W |
| 4 mins | 2025-09-14 23:45:35.366Z | 276.417° WNW | 2025-09-14 23:47:35.366Z | 283.945° WNW | 26.092° | 2025-09-14 23:49:35.366Z | 272.343° WNW |
| 8 mins | 2025-09-15 01:34:35.366Z | 343.157° N | 2025-09-15 01:39:35.366Z | 28.874° NE | 37.093° | 2025-09-15 01:42:35.366Z | 317.706° NNW |
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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