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: 5 hours ago
TLE from 5 hours ago
0 TIANPING 3B-01
1 61615U 24189B 25308.32196387 .00003345 00000-0 26611-3 0 9994
2 61615 97.5513 330.2459 0002722 84.5112 275.6423 15.01063081 56714Epoch: 2025-11-04T07:43Z
TLE epoch observation values (Epoch: 2025-11-04T07:43:37.678Z)
Latitude
-0°
Longitude
170.52825°
Altitude
566.492 km
Speed
7.578 km/s
True Right ascension
22h 00m 59s
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
08:12:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.503 km
Perigee altitude
558.726 km
Semi-major axis
6,938.751 km
Eccentricity
0.00027
Inclination
97.5513°
RAAN
330.2459°
Arg. of periapsis
84.5112°
True anomaly
275.61126°
Mean anomaly
275.6423°
Eccentric anomaly
275.62678°
Mean motion
3.7551 °/min
Orbital period
95.87 mins
BSTAR
0.00026611
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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 | 2025-11-04 14:41:40.272Z | 2.109° NNE | 2025-11-04 14:44:40.272Z | 281.208° WNW | 41.406° | 2025-11-04 14:47:40.272Z | 207.094° SW |
| 6 mins | 2025-11-05 01:27:40.272Z | 154.568° SSE | 2025-11-05 01:30:40.272Z | 46.541° ENE | 41.961° | 2025-11-05 01:33:40.272Z | 354.984° N |
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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