TIANPING 3B-01, 61615
Orbit data source: Space-Track
TIANPING 3B-01, 61615 is a payload satellite owned by ZJUNI-SAT (CN) in SSO that was launched on Tue, 22 Oct 2024 UTC via a CHANG ZHENG 6 launch vehicle from the Taiyaun Space Center, China (TSC). 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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61615 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CASIC/ZJUNI
Mission
Defense Calibration
Bus & Motor
TP-3, Unknown motor
Mass
200 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.135 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 TIANPING 3B-01
1 61615U 24189B 25322.52157970 .00004553 00000-0 36083-3 0 9993
2 61615 97.5488 344.0424 0003225 86.5157 273.6436 15.01034322 58844Epoch: 2025-11-18T12:31Z
TLE epoch observation values (Epoch: 2025-11-18T12:31:04.486Z)
Latitude
-0.00002°
Longitude
98.46724°
Altitude
566.624 km
Speed
7.578 km/s
True Right ascension
22h 56m 10s
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
20:16:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.941 km
Perigee altitude
558.465 km
Semi-major axis
6,938.84 km
Eccentricity
0.00032
Inclination
97.5488°
RAAN
344.0424°
Arg. of periapsis
86.5157°
True anomaly
273.60672°
Mean anomaly
273.6436°
Eccentric anomaly
273.62516°
Mean motion
3.75503 °/min
Orbital period
95.87 mins
BSTAR
0.00036083
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Other satellites on launch #189 in the year 2024 (2024-10-22 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.TIANPING 3B-01 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-19 01:26:29.602Z | 156.835° SSE | 2025-11-19 01:29:29.602Z | 112.156° ESE | 41.621° | 2025-11-19 01:33:29.602Z | 354.059° N |
| 6 mins | 2025-11-19 14:41:29.602Z | 359.838° N | 2025-11-19 14:44:29.602Z | 248.135° W | 39.56° | 2025-11-19 14:47:29.602Z | 205.821° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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