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 days ago
TLE from 5 days ago
0 TIANPING 3B-01
1 61615U 24189B 26032.85245486 .00002583 00000-0 20725-3 0 9995
2 61615 97.5382 57.1685 0003266 92.6005 267.5594 15.00930131 70149Epoch: 2026-02-01T20:27Z
TLE epoch observation values (Epoch: 2026-02-01T20:27:32.099Z)
Latitude
0.00002°
Longitude
-21.7714°
Altitude
567.185 km
Speed
7.577 km/s
True Right ascension
03h 48m 40s
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
05:44:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.29 km
Perigee altitude
558.757 km
Semi-major axis
6,939.161 km
Eccentricity
0.00033
Inclination
97.5382°
RAAN
57.1685°
Arg. of periapsis
92.6005°
True anomaly
267.52201°
Mean anomaly
267.5594°
Eccentric anomaly
267.5407°
Mean motion
3.75476 °/min
Orbital period
95.88 mins
BSTAR
0.00020725
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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 | 2026-02-07 14:36:49.145Z | 3.518° NNE | 2026-02-07 14:40:49.145Z | 262.526° W | 39.978° | 2026-02-07 14:43:49.145Z | 207.699° SW |
| 6 mins | 2026-02-08 01:23:49.145Z | 155.617° SSE | 2026-02-08 01:25:49.145Z | 124.454° SE | 41.221° | 2026-02-08 01:29:49.145Z | 353.548° 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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