TIANQI 29, 61195
Orbit data source: Space-Track
TIANQI 29, 61195 is a payload satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Fri, 20 Sep 2024 UTC via a KUAIZHOU-1A launch vehicle from the Xichang Space Center, China (XSC). 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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61195 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: 12 hours ago
TLE from 12 hours ago
0 TIANQI 29
1 61195U 24170A 26171.33285618 -.00000041 00000-0 59434-4 0 9994
2 61195 44.8559 122.6916 0004511 104.0917 256.0415 13.99145226 89304Epoch: 2026-06-20T07:59Z
TLE epoch observation values (Epoch: 2026-06-20T07:59:18.773Z)
Latitude
-0.00006°
Longitude
94.31433°
Altitude
897.533 km
Speed
7.404 km/s
True Right ascension
08h 10m 45s
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
07:24:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
901.58 km
Perigee altitude
895.015 km
Semi-major axis
7,276.435 km
Eccentricity
0.00045
Inclination
44.8559°
RAAN
122.6916°
Arg. of periapsis
104.0917°
True anomaly
255.99134°
Mean anomaly
256.0415°
Eccentric anomaly
256.01642°
Mean motion
3.49676 °/min
Orbital period
102.95 mins
BSTAR
0.000059434
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Other satellites on launch #170 in the year 2024 (2024-09-20 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 29 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 | 2026-06-20 23:35:34.585Z | 211.281° SW | 2026-06-20 23:39:34.585Z | 156.747° SSE | 35.563° | 2026-06-20 23:45:34.585Z | 73.922° E |
| 10 mins | 2026-06-21 01:23:34.585Z | 261.132° W | 2026-06-21 01:28:34.585Z | 11.622° NNE | 42.823° | 2026-06-21 01:33:34.585Z | 66.25° ENE |
| 10 mins | 2026-06-21 03:12:34.585Z | 290.598° WNW | 2026-06-21 03:16:34.585Z | 347.203° N | 38.662° | 2026-06-21 03:22:34.585Z | 79.897° E |
| 10 mins | 2026-06-21 05:01:34.585Z | 293.676° NW | 2026-06-21 05:05:34.585Z | 329.967° NNW | 44.928° | 2026-06-21 05:11:34.585Z | 113.244° SE |
| 9 mins | 2026-06-21 06:49:34.585Z | 272.942° WNW | 2026-06-21 06:53:34.585Z | 220.487° SW | 27.198° | 2026-06-21 06:58:34.585Z | 161.466° S |
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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