TIANPING 3B-02, 61616
Orbit data source: Space-Track
TIANPING 3B-02, 61616 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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61616 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: 8 hours ago
TLE from 8 hours ago
0 TIANPING 3B-02
1 61616U 24189C 26171.51319230 .00001772 00000-0 14333-3 0 9999
2 61616 97.5198 191.6501 0002303 79.9155 280.2329 15.00995073 90945Epoch: 2026-06-20T12:18Z
TLE epoch observation values (Epoch: 2026-06-20T12:18:59.814Z)
Latitude
-0.00006°
Longitude
98.17414°
Altitude
566.604 km
Speed
7.578 km/s
True Right ascension
12h 46m 36s
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
07:20:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.421 km
Perigee altitude
559.225 km
Semi-major axis
6,938.96 km
Eccentricity
0.00023
Inclination
97.5198°
RAAN
191.6501°
Arg. of periapsis
79.9155°
True anomaly
280.20693°
Mean anomaly
280.2329°
Eccentric anomaly
280.21991°
Mean motion
3.75493 °/min
Orbital period
95.87 mins
BSTAR
0.00014333
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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-02 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 | 2026-06-21 01:14:04.015Z | 158.611° S | 2026-06-21 01:18:04.015Z | 44.75° NE | 42.558° | 2026-06-21 01:21:04.015Z | 354.155° N |
| 6 mins | 2026-06-21 14:29:04.015Z | 0.626° NNE | 2026-06-21 14:32:04.015Z | 276.459° WNW | 40.552° | 2026-06-21 14:35:04.015Z | 208.377° 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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