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
Operational 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 TIANPING 3B-01
1 61615U 24189B 26318.30507854 .00002518 00000-0 20180-3 0 9995
2 61615 97.5032 333.4937 0001794 105.0561 255.0863 15.00998588112969Epoch: 2026-11-14T07:19Z
TLE epoch observation values (Epoch: 2026-11-14T07:19:18.785Z)
Latitude
0.00004°
Longitude
170.25365°
Altitude
567.198 km
Speed
7.577 km/s
True Right ascension
22h 13m 58s
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
11:21:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.056 km
Perigee altitude
559.566 km
Semi-major axis
6,938.948 km
Eccentricity
0.00018
Inclination
97.5032°
RAAN
333.4937°
Arg. of periapsis
105.0561°
True anomaly
255.06644°
Mean anomaly
255.0863°
Eccentric anomaly
255.07637°
Mean motion
3.75494 °/min
Orbital period
95.87 mins
BSTAR
0.0002018
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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 | 2026-11-15 01:02:28.408Z | 157.989° S | 2026-11-15 01:06:28.408Z | 36.251° NE | 63.385° | 2026-11-15 01:09:28.408Z | 354.244° N |
| 6 mins | 2026-11-15 14:17:28.408Z | 0.329° NNE | 2026-11-15 14:20:28.408Z | 270.495° WNW | 58.691° | 2026-11-15 14:23:28.408Z | 207.921° 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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