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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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 26138.18093509 .00001437 00000-0 11700-3 0 9995
2 61615 97.5210 159.2708 0003953 81.8748 278.2924 15.01031029 85945Epoch: 2026-05-18T04:20Z
TLE epoch observation values (Epoch: 2026-05-18T04:20:32.791Z)
Latitude
-0.00012°
Longitude
-141.7387°
Altitude
566.382 km
Speed
7.578 km/s
True Right ascension
10h 37m 04s
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
23:45:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.455 km
Perigee altitude
557.969 km
Semi-major axis
6,938.849 km
Eccentricity
0.0004
Inclination
97.521°
RAAN
159.2708°
Arg. of periapsis
81.8748°
True anomaly
278.24757°
Mean anomaly
278.2924°
Eccentric anomaly
278.26999°
Mean motion
3.75502 °/min
Orbital period
95.87 mins
BSTAR
0.000117
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-19 01:16:18.492Z | 156.617° SSE | 2026-05-19 01:19:18.492Z | 74.738° E | 43.029° | 2026-05-19 01:22:18.492Z | 355.061° N |
| 6 mins | 2026-05-19 14:31:18.492Z | 356.407° N | 2026-05-19 14:33:18.492Z | 295.228° NW | 40.718° | 2026-05-19 14:37:18.492Z | 205.573° SW |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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