TIANMU-1 16, 58701
Orbit data source: Space-Track
TIANMU-1 16, 58701 is a payload satellite owned by Hangtian Tianmu (CN) in SSO that was launched on Fri, 05 Jan 2024 UTC via a KUAIZHOU-1A launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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58701 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Hangtian Tianmu
Mission
Operational Commercial Weather
Bus & Motor
TIANMU, Unknown motor
Mass
50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
2.000 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 TIANMU-1 16
1 58701U 24004B 26291.65452422 .00005897 00000-0 22022-3 0 9991
2 58701 97.4606 117.0896 0004032 275.0974 84.9804 15.27761119154621Epoch: 2026-10-18T15:42Z
TLE epoch observation values (Epoch: 2026-10-18T15:42:30.892Z)
Latitude
-0.00012°
Longitude
-145.68283°
Altitude
485.365 km
Speed
7.623 km/s
True Right ascension
07h 48m 21s
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
19:07:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.23 km
Perigee altitude
476.7 km
Semi-major axis
6,857.602 km
Eccentricity
0.0004
Inclination
97.4606°
RAAN
117.0896°
Arg. of periapsis
275.0974°
True anomaly
85.02643°
Mean anomaly
84.9804°
Eccentric anomaly
85.00341°
Mean motion
3.82195 °/min
Orbital period
94.19 mins
BSTAR
0.00022022
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Other satellites on launch #4 in the year 2024 (2024-01-05 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.TIANMU-1 16 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-19 01:42:04.569Z | 356.009° N | 2026-10-19 01:45:04.569Z | 268.211° W | 45.839° | 2026-10-19 01:48:04.569Z | 211.955° SW |
| 5 mins | 2026-10-19 12:17:04.569Z | 145.576° SSE | 2026-10-19 12:19:04.569Z | 92.536° ESE | 51.7° | 2026-10-19 12:22:04.569Z | 1.037° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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