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: 3 days ago
TLE from 3 days ago
0 TIANPING 3B-01
1 61615U 24189B 25254.05757127 .00002114 00000-0 17003-3 0 9997
2 61615 97.5610 277.4692 0002609 100.0089 260.1430 15.01035353 48577Epoch: 2025-09-11T01:22Z
TLE epoch observation values (Epoch: 2025-09-11T01:22:54.157Z)
Latitude
-0.00003°
Longitude
-93.58155°
Altitude
567.073 km
Speed
7.577 km/s
True Right ascension
18h 29m 52s
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
23:29:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.511 km
Perigee altitude
558.89 km
Semi-major axis
6,938.837 km
Eccentricity
0.00026
Inclination
97.561°
RAAN
277.4692°
Arg. of periapsis
100.0089°
True anomaly
260.11355°
Mean anomaly
260.143°
Eccentric anomaly
260.12827°
Mean motion
3.75503 °/min
Orbital period
95.87 mins
BSTAR
0.00017003
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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 | 2025-09-14 14:43:45.756Z | 4.593° NNE | 2025-09-14 14:47:45.756Z | 269.684° W | 41.054° | 2025-09-14 14:50:45.756Z | 206.856° SW |
| 6 mins | 2025-09-15 01:30:45.756Z | 154.412° SSE | 2025-09-15 01:33:45.756Z | 35.721° NE | 41.356° | 2025-09-15 01:36:45.756Z | 354.449° 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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