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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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: 19 hours ago
TLE from 19 hours ago
0 TIANQI 30
1 61196U 24170B 25249.29043544 .00000226 00000-0 24311-3 0 9994
2 61196 44.8588 322.7055 0009599 199.2487 160.7982 13.98998388 49291Epoch: 2025-09-06T06:58Z
TLE epoch observation values (Epoch: 2025-09-06T06:58:13.622Z)
Latitude
-0.00001°
Longitude
-127.47765°
Altitude
903.845 km
Speed
7.398 km/s
True Right ascension
21h 30m 49s
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
18:19:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
905.791 km
Perigee altitude
891.821 km
Semi-major axis
7,276.943 km
Eccentricity
0.00096
Inclination
44.8588°
RAAN
322.7055°
Arg. of periapsis
199.2487°
True anomaly
160.83434°
Mean anomaly
160.7982°
Eccentric anomaly
160.81627°
Mean motion
3.49639 °/min
Orbital period
102.96 mins
BSTAR
0.00024311
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-09-07 07:06:35.970Z | 200.457° SSW | 2025-09-07 07:11:35.970Z | 143.683° SSE | 27.943° | 2025-09-07 07:16:35.970Z | 81.863° E |
| 10 mins | 2025-09-07 08:55:35.970Z | 248.498° W | 2025-09-07 08:59:35.970Z | 295.35° NW | 44.888° | 2025-09-07 09:05:35.970Z | 66.939° ENE |
| 10 mins | 2025-09-07 10:43:35.970Z | 282.952° WNW | 2025-09-07 10:48:35.970Z | 2.634° NNE | 39.038° | 2025-09-07 10:53:35.970Z | 72.392° E |
| 10 mins | 2025-09-07 12:32:35.970Z | 295.068° NW | 2025-09-07 12:37:35.970Z | 40.234° NE | 43.224° | 2025-09-07 12:42:35.970Z | 101.044° ESE |
| 9 mins | 2025-09-07 14:21:35.970Z | 278.292° WNW | 2025-09-07 14:25:35.970Z | 212.297° SW | 35.3° | 2025-09-07 14:30:35.970Z | 146.823° 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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Authenticating...
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