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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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 TIANQI 29
1 61195U 24170A 25304.25941358 .00000107 00000-0 16130-3 0 9999
2 61195 44.8567 77.4223 0006250 97.2233 262.9308 13.99030584 56803Epoch: 2025-10-31T06:13Z
TLE epoch observation values (Epoch: 2025-10-31T06:13:33.333Z)
Latitude
-0.00004°
Longitude
-55.77304°
Altitude
897.7 km
Speed
7.404 km/s
True Right ascension
05h 09m 41s
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
10:00:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
903.243 km
Perigee altitude
894.147 km
Semi-major axis
7,276.832 km
Eccentricity
0.00063
Inclination
44.8567°
RAAN
77.4223°
Arg. of periapsis
97.2233°
True anomaly
262.85973°
Mean anomaly
262.9308°
Eccentric anomaly
262.89527°
Mean motion
3.49647 °/min
Orbital period
102.96 mins
BSTAR
0.0001613
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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 | 2025-10-31 15:07:53.349Z | 283.686° WNW | 2025-10-31 15:12:53.349Z | 0.377° NNE | 38.926° | 2025-10-31 15:17:53.349Z | 72.995° E |
| 10 mins | 2025-10-31 16:56:53.349Z | 294.844° NW | 2025-10-31 17:01:53.349Z | 39.769° NE | 43.629° | 2025-10-31 17:06:53.349Z | 102.76° ESE |
| 9 mins | 2025-10-31 18:45:53.349Z | 277.265° WNW | 2025-10-31 18:49:53.349Z | 213.384° SW | 34.035° | 2025-10-31 18:54:53.349Z | 149.08° SSE |
| 9 mins | 2025-11-01 11:32:53.349Z | 205.928° SW | 2025-11-01 11:36:53.349Z | 139.991° SSE | 34.704° | 2025-11-01 11:41:53.349Z | 76.095° E |
| 11 mins | 2025-11-01 13:19:53.349Z | 258.608° W | 2025-11-01 13:24:53.349Z | 341.413° N | 43.622° | 2025-11-01 13:30:53.349Z | 67.013° ENE |
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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