TIANQI 26, 59910
Orbit data source: Space-Track
TIANQI 26, 59910 is a payload satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Wed, 29 May 2024 UTC via a GUSHENXING 1 launch vehicle from the Yellow Sea Launch Area, China (YSLA). 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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59910 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Shanghai ASES
Mission
Operational Commercial Communications
Bus & Motor
STARLIGHTB, Unknown motor
Mass
40 kg wet, ~40 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 TIANQI 26
1 59910U 24102B 26171.43483569 .00000009 00000-0 93841-4 0 9990
2 59910 44.9731 247.0884 0011460 256.1394 103.8164 13.99185892105362Epoch: 2026-06-20T10:26Z
TLE epoch observation values (Epoch: 2026-06-20T10:26:09.803Z)
Latitude
0.00001°
Longitude
-178.10195°
Altitude
898.611 km
Speed
7.403 km/s
True Right ascension
16h 28m 21s
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
00:33:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
906.477 km
Perigee altitude
889.799 km
Semi-major axis
7,276.275 km
Eccentricity
0.00115
Inclination
44.9731°
RAAN
247.0884°
Arg. of periapsis
256.1394°
True anomaly
103.94388°
Mean anomaly
103.8164°
Eccentric anomaly
103.88014°
Mean motion
3.49687 °/min
Orbital period
102.95 mins
BSTAR
0.000093841
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Other satellites on launch #102 in the year 2024 (2024-05-29 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.TIANQI 26 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 | 2026-06-22 14:22:17.689Z | 283.395° WNW | 2026-06-22 14:27:17.689Z | 227.766° WSW | 31.544° | 2026-06-22 14:32:17.689Z | 156.176° SSE |
| 10 mins | 2026-06-23 07:10:17.689Z | 213.286° SW | 2026-06-23 07:14:17.689Z | 152.786° SSE | 37.351° | 2026-06-23 07:20:17.689Z | 72.439° E |
| 10 mins | 2026-06-23 08:58:17.689Z | 263.866° W | 2026-06-23 09:02:17.689Z | 315.918° NNW | 42.216° | 2026-06-23 09:08:17.689Z | 66.211° ENE |
| 10 mins | 2026-06-23 10:47:17.689Z | 292.308° WNW | 2026-06-23 10:51:17.689Z | 352.095° N | 38.845° | 2026-06-23 10:57:17.689Z | 81.04° E |
| 11 mins | 2026-06-23 12:35:17.689Z | 293.291° NW | 2026-06-23 12:40:17.689Z | 294.168° NW | 45° | 2026-06-23 12:46:17.689Z | 115.083° SE |
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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