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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TLE from 14 hours ago
0 TIANQI 29
1 61195U 24170A 25198.14078702 -.00000073 00000-0 37915-4 0 9990
2 61195 44.8550 190.4925 0008284 298.0035 61.9957 13.98974929 42137
TLE epoch observation values (Epoch: 2025-07-17T03:22:43.998Z)
Visualization orbit readout
Visualization observer readout
Other satellites on launch #170 in the year 2024 (2024-09-20 UTC)
TIANQI 29 Visibility forecast
Observer location: undefined°, undefined°
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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10 mins | 2025-07-18 01:49:01.110Z | 201.654° SSW | 2025-07-18 01:54:01.110Z | 136.238° SSE | 29.765° | 2025-07-18 01:59:01.110Z | 78.646° E |
10 mins | 2025-07-18 03:37:01.110Z | 251.286° W | 2025-07-18 03:42:01.110Z | 16.632° NNE | 44.552° | 2025-07-18 03:47:01.110Z | 66.302° ENE |
10 mins | 2025-07-18 05:26:01.110Z | 285.79° WNW | 2025-07-18 05:31:01.110Z | 15.84° NNE | 38.528° | 2025-07-18 05:36:01.110Z | 74.69° E |
10 mins | 2025-07-18 07:15:01.110Z | 295.494° NW | 2025-07-18 07:19:01.110Z | 346.485° N | 43.602° | 2025-07-18 07:25:01.110Z | 104.201° ESE |
10 mins | 2025-07-18 09:03:01.110Z | 280.082° WNW | 2025-07-18 09:07:01.110Z | 229.122° WSW | 33.154° | 2025-07-18 09:13:01.110Z | 148.769° SSE |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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