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: 2 days ago
TLE from 2 days ago
0 TIANPING 3B-01
1 61615U 24189B 25259.52399245 .00001448 00000-0 11792-3 0 9995
2 61615 97.5609 282.7892 0002555 96.5897 263.5618 15.01020898 49396Epoch: 2025-09-16T12:34Z
TLE epoch observation values (Epoch: 2025-09-16T12:34:32.947Z)
Latitude
-0.00006°
Longitude
98.43887°
Altitude
567.006 km
Speed
7.577 km/s
True Right ascension
18h 51m 09s
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
16:46:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.518 km
Perigee altitude
558.972 km
Semi-major axis
6,938.882 km
Eccentricity
0.00026
Inclination
97.5609°
RAAN
282.7892°
Arg. of periapsis
96.5897°
True anomaly
263.53271°
Mean anomaly
263.5618°
Eccentric anomaly
263.54725°
Mean motion
3.75499 °/min
Orbital period
95.87 mins
BSTAR
0.00011792
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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 | 2025-09-19 01:30:06.151Z | 156.154° SSE | 2025-09-19 01:33:06.151Z | 84.853° E | 42.729° | 2025-09-19 01:37:06.151Z | 353.454° N |
| 6 mins | 2025-09-19 14:45:06.151Z | 358.102° N | 2025-09-19 14:47:06.151Z | 303.777° NW | 40.915° | 2025-09-19 14:51:06.151Z | 205.092° 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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