TIANPING 3A-01, 61614
Orbit data source: Space-Track
TIANPING 3A-01, 61614 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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61614 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
ZJUNI-SAT
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: 5 hours ago
TLE from 5 hours ago
0 TIANPING 3A-01
1 61614U 24189A 25342.85521677 .00007050 00000-0 55692-3 0 9991
2 61614 97.5469 3.8453 0003358 46.4998 313.6505 15.00971647 61934Epoch: 2025-12-08T20:31Z
TLE epoch observation values (Epoch: 2025-12-08T20:31:30.728Z)
Latitude
-0.00006°
Longitude
-21.88099°
Altitude
565.35 km
Speed
7.579 km/s
True Right ascension
00h 15m 22s
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
23:20:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.226 km
Perigee altitude
558.566 km
Semi-major axis
6,939.033 km
Eccentricity
0.00034
Inclination
97.5469°
RAAN
3.8453°
Arg. of periapsis
46.4998°
True anomaly
313.62265°
Mean anomaly
313.6505°
Eccentric anomaly
313.63658°
Mean motion
3.75487 °/min
Orbital period
95.88 mins
BSTAR
0.00055692
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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 3A-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 | 2025-12-09 01:26:31.470Z | 158.971° S | 2025-12-09 01:30:31.470Z | 51.357° ENE | 42.95° | 2025-12-09 01:33:31.470Z | 354.072° N |
| 5 mins | 2025-12-09 14:42:31.470Z | 354.56° N | 2025-12-09 14:44:31.470Z | 283° WNW | 40.584° | 2025-12-09 14:47:31.470Z | 208.876° 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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