TIANQI 30, 61196
Orbit data source: Space-Track
TIANQI 30, 61196 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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61196 intel report (Beta)
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TLE from 14 hours ago
0 TIANQI 30
1 61196U 24170B 25198.15867507 -.00000082 00000-0 31359-4 0 9997
2 61196 44.8564 190.6333 0010072 304.0201 55.9672 13.98974491 42130
TLE epoch observation values (Epoch: 2025-07-17T03:48:29.526Z)
Visualization orbit readout
Visualization observer readout
Other satellites on launch #170 in the year 2024 (2024-09-20 UTC)
TIANQI 30 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 02:16:18.110Z | 212.152° SW | 2025-07-18 02:20:18.110Z | 157.202° SSE | 36.065° | 2025-07-18 02:26:18.110Z | 73.69° E |
10 mins | 2025-07-18 04:04:18.110Z | 261.785° W | 2025-07-18 04:09:18.110Z | 9.111° NNE | 42.791° | 2025-07-18 04:14:18.110Z | 66.206° ENE |
10 mins | 2025-07-18 05:53:18.110Z | 290.672° WNW | 2025-07-18 05:57:18.110Z | 345.259° N | 38.673° | 2025-07-18 06:03:18.110Z | 80.095° E |
10 mins | 2025-07-18 07:42:18.110Z | 293.407° NW | 2025-07-18 07:46:18.110Z | 306.374° NW | 44.863° | 2025-07-18 07:52:18.110Z | 113.962° SE |
9 mins | 2025-07-18 09:30:18.110Z | 273.185° WNW | 2025-07-18 09:34:18.110Z | 222.516° SW | 26.889° | 2025-07-18 09:39:18.110Z | 162.912° 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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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